CN108860638A - It is slided with efficient short distance or the platform-type jet runway of VTOL aircraft device - Google Patents

Abstract

It is slided the invention discloses a kind of efficient very-short-reach of band or the aircraft carrier of VTOL aircraft device, naval vessel, land and water platform jet runway, belongs to the technical field of aviation wisdom traffic electronic product structure；Overall structure is constituted by being provided with seven regions made of muti-piece valve body plate main body module sub-unit is combined respectively；Become a variety of gas supply gas source technologies such as gas using whirlpool spray, turbofan, axial flow blower formula, air compressor, liquid, platform jet runway device is input to by compressed air by kinds of gas sources；The beneficial effect is that：The wing type original that the jet-propelled runway solves slides landing aircraft and realizes safe landing in very-short-reach, realize various carrier-borne aircrafts and non-carrier-borne aircraft at sea 8 grades of stormy waves or more or whens bad weather circumstances be attained by 100% safe landing, VTOL Harrier and helicopter most economical can be increased to 40% mileage, can harmless recycling rocket, can reach the security control of the included moment of inertia of 100% pair of landing aircraft.

Description

It is slided with efficient short distance or the platform-type jet runway of VTOL aircraft device

Technical field

The efficient short distance of a kind of band of the present invention slides or the platform-type jet runway of VTOL aircraft device, belongs to boat The technical field of empty traffic, communication and mechano-electronic artificial intelligence product structure specifically belongs to specially for aircraft, referred to as： The technical field of the planar mechanical apparatus structure of (takeoff and landing device) take-off and landing.

Specifically type aircraft carrier deck very-short-reach landing platform wisdom traffic runway, Civil Aviation Airport very-short-reach landing platform wisdom Traffic runway, continental rise or the platform-type very short takeoff and landing runway of water surface packaged type air bag, helicopter VTOL gas injection rise Platform drops, sparrow hawk formula machine VTOL gas sprays landing platform；It is extensible that be developed to each provincial capital, county, each frontier sentry super Short take-off and landing platform runway；Area under one's jurisdiction to county, Rural Families, large, medium and small type aircraft or unmanned plane very short takeoff and landing platform wisdom are handed over Logical runway；Supermarket, logistics area very short takeoff and landing platform wisdom traffic runway；Tourist district's very short takeoff and landing platform wisdom traffic is run Road；Each desert, high mountain, mountain area very short takeoff and landing platform wisdom traffic runway；The mobile ultrashort landing platform of Concealable cavern Wisdom traffic runway or island, the water surface, cavern, marshland, jungle, extension airbag movable type very short takeoff and landing platform wisdom Traffic runway；Island very short takeoff and landing platform wisdom traffic runway；Islands and reefs very short takeoff and landing platform wisdom traffic runway；Petroleum is flat Platform very short takeoff and landing platform wisdom traffic runway；Very short takeoff and landing platform wisdom traffic runway on artificial floating island；Each frontier sentry Logistics dispenses the 5-150 ton wing type unmanned plane or unmanned helicopter, the gas that is gone out by compressed air gas injection of various goods and materials Body laminar flow safe accelerated take-off or can help support to land, and will not environment are limited by misty rain, ice and snow, frost, geographic areas be small etc. Frigid zone-low temperature of system is in subzero 60 degree, the torrid zone-high temperature in 80 degree of areas above freezing or mountain vallages, especially at sea aircraft carrier, naval vessel, water The jet-propelled very short takeoff and landing platform wisdom traffic runway of various wing unmanned planes on Lu Pingtai, Qinghai-Tibet frigid zone high-altitude aerodrome；It is right Unmanned helicopter VTOL jet platform application have safely, quickly, the important meaning of economy landing.

The present invention mainly uses：Compressed air is very-short-reach is fixed or the both the above of packaged type sprays gas laminar flow Landing platform wisdom traffic runway, the jet runway are sprayable out to gas laminar flow needed for various aircraft during take-off and landing size Kinetic forces technology, for the mechanics problem on static curved surface and plane, the particularity of the technology is to transport various high speeds Has tangible change in the application effect of dynamic aircraft entirety, main application principle is as follows：Make using by compressed air For the core drive energy of jet runway, the reverse landing aircraft of the puff prot in each region of jet runway is ejected into gas laminar flow, The gas blanket stream, which is formd, to be hanged the landing of support formula boosting to the gas of wing type aircraft, sprays gas to various sparrow hawk formula VTOL aircrafts Body laminar flow is similarly formed the outstanding support formula boosting landing of injection gas laminar flow, hangs to helicopter landing aircraft vertical injection gas laminar flow The kinetic forces technology of support formula boosting landing, it is compressed air gas injection aerodynamics, compressed air gas injection Hydrodynamics, blast injection gas laminar flow, which hang support formula landing aircraft to boosting or hover over lag formula in gas field, quickly to be accelerated To the aircraft of nature flying speed, here it is injection gas aerodynamics, the outstanding support aircraft safety of gas laminar flow boosting is sprayed, fast Speed lag, which takes off to spray the outstanding support aircraft safety of gas aerodynamics, injection gas film grade laminar flow boosting and quickly lag, blocks landing Spray gas aerodynamics, containing various ratio humidity injection gas aerodynamics, injection gas laminar flow boosting it is various fly Row device or outstanding support object aeromechanics, suspend injection gas aerodynamics, the air containing different humidity spray object viscosity Gaseous fluid mechanics is that the theoretical of the primary aerodynamic that jet runway shortens relies on, while it is also Torricelli's theorem The reproduction of every new disciplines of the hydrodynamics in aviation field.

Background technique

Since aircraft in 1903 occurs, various countries are more and more extensive in civil aviaton and military application.Constantly reinforce to the people various countries The research and discovery of the various takeoff and landing very-short-reach runways such as boat and military continental rise airport, type aircraft carrier deck.However, the existing people Boat with military continental rise airfield runway is too long, construction cost is high, airport maintenance cost is big, landing is costly；And some area because Geographical environment influences temperature in factors such as the positive and negative high lower limits of 0-60 degree, and aircraft is subjected to external environment wind direction during take-off and landing Influence.So current conventional criteria airfield runway is typically all by a plurality of north-south and a plurality of East and West direction for wing type Wind direction is selected when aircraft taxi landing, and builds up a plurality of north-south being about square and transmeridional airport landing runway.

Currently, may each be about rectangular entire area by the continental rise airport of international standard requirement, conventional formula airport runway length is 3000-4500 meters, the Medium Plane of the compatible various 0.5-300 tons of weights of landing.The large aircrafts weighed such as 400-500 tons of landing, Need to more than 6000-7000 meters of length square normal airfield runway on landing.Therefore, takeoff and landing runway overlength is asked Topic is difficult to be broken through for a long time.By international and various countries conventional criteria, airfield runway by landing wind direction because being influenced generally all Build up square.Provincial airfield runway is typically all 4500-5000 meters long, and international flight airfield runway is typically all 7000-8000 meters long not equal square airport.

Currently, each normal airfield aircraft in the world is in weather Normal Take-Off And Landing, warplane need it is sliding run at least at 400-500 meters, the people Sliding run of plane at least needs 1200-1500 meters, 0.5-1.5 used in the China General Aviation Corp of development China with communications tons of weight Sliding run of small drone at least need 200-250 meters, airfield runway, which generally requires, builds up 2000-2600 meters of length and width about 30- 40 meters are differed.Sliding run of the small drone of 5-15 tons of weight at least needs 450-650 meters, and airfield runway, which generally requires, to be built up 3000-3500 meters about 45-60 meters of length and width is differed.When there is micro ice and snow frost on runway pavement, to the various machines of required landing Type aircraft at least needs to increase skidding system of 30% wheel on former landing landing airdrome length in the sliding length for running runway of former landing Number, just separatably take off or stop is landed by face for wheel；Take off it is sliding to run long and fuel consumption big, aircraft slide during take-off and landing away from From length, wheel cannot be rapidly separated ground and take off or landing stop and the high-speed friction that causes wheel on runway, damage wheel Consumption is serious.

Currently, existing airfield runway itself all without for aircraft when taking off, to departing aeroplane on runway whole inertia force The control function safely and fast of square, the more whole moment of inertia not to departing aeroplane on runway, using flexible reverse The outstanding support gas of boosting is sprayed, Assisted Take Off aircraft is rapidly separated ground lag formula acceleration in the outstanding support gas field of boosting and climbs, quickly Realizing to hang in gas field asks lag formula to accelerate to safe take-off speed.Existing airfield runway itself is all without for decline aircraft In landing, to the safety control function of decline aircraft whole moment of inertia on runway, more without being run for decline aircraft Whole moment of inertia on road is pressed from both sides using on runway by the film grade laminar flow of contrainjection gas setting flexible, and auxiliary decline flies The lag formula in outstanding support gas field flexible of machine safety is fast and safely slowed down, is realized to the contrainjection gas for declining aircraft buffer-type Body film grade laminar flow folder asks safety barrage to land to hang.And existing airfield runway itself all lacks to landing aircraft entirety inertia force The quick control function of the intelligent and safe of square, this is always that countries in the world normal airfield runway is unable to control takeoff and landing, while The main reason for runway can not just be shortened.

The function of hanging support formula auxiliary landing aircraft due to not just being equipped with gas injection of the present invention on existing airfield runway always, so Aircraft is all very serious to the loss of aircraft damper in landing；Meanwhile because runway is too long, and cause to wheel in runway The serious abrasion of upper high speed；It is even more impossible to guarantee to decline aircraft when undercarriage is not opened, aircraft can not safe falling etc. be difficult to The serious problems of solution；Meanwhile shortening service life to aircraft entirety；The short takeoff and landing of type aircraft carrier deck runway are very uneasy Entirely, civil aviaton and military continental rise airport are at high cost in construction；In addition, when takeoff and landing, often because being influenced by extraneous wind direction, because This, airport is all built up rectangular, and occupied area is very big.Especially misty rain, ice and snow, frost weather when, airport ground it is sliding without Energy landing, this has become a great problem that can not have been overcome since World Airways transport service a century.

Since existing civil aviaton and military continental rise airport construction cost are high and take up a large area, many provincials capital to county, area under one's jurisdiction to county, It is each frontier sentry, each logistics area, each tourist district, each high mountain, mountain area, basin, each mountain vallage, island, islands and reefs, oil platform, artificial On chinampa or packaged type airfield runway all cannot achieve the aircraft of 0.5-50 tons of weight of carrying；Civil aviaton's small drone is The Main way of following each General Aviation Logistics Transportation transportation development, is the following land transportation and the province that high-speed rail is always not achieved Money, quick, safe and practical effect.Air minibus or logistics transportation machine all in the construction on landing airport always with high cost, Height, which expends, to be realized.It to select and make from the mode that civil aviaton and military continental rise airport do not have short take-off and landing runway so far It is a kind of not because of the airfield runway of the safe landing of the ultrashort type for being there is limitation to be limited by airport occupied area, the following short distance airfield runway Realize that the safe landing of aircraft is extremely urgent.

In order to further solve the more preferably safe landing of various wing type unmanned planes and play the reduction of cost declining, make aviation field circle The fast development of each navigation company's unmanned plane transportation industry, the invention use inexhaustible, the nexhaustible compression of the Nature Power source of the air as the injection gas laminar flow that auxiliary pushing landing aircraft is core 100% can be realized ultrashort In distance can safe boosting landing aircraft a kind of very-short-reach miniature jet runway, the runway by increase and decrease injection gas pressure The runway carrier of power and the various large, medium and small aircrafts of the compatible landing of flow, the length of jet runway are respectively set to 30-100 Rice, 50-100 meters, 150-200 meters, 300-500 meters, 600-800 meters, 900-1100 meters, 1200-1500 meters of each short distance From (going out high pressure gas laminar flow by blast injection, the benefit as auxiliary pushing landing aircraft safety power source is tried hard to keep again Barrier) jet-propelled runway, the runway can respectively safety by 0.5-50 tons of unmanned planes, 0.5-100 tons, 0.5-200 tons, 0.5-300 Ton, 0.5-500 ton, the various difference wing types cunnings of 0.5-1000 ton or even 0.5-3000 ton weight, large, medium and small model not etc. jump Aircraft can safely and fast boosting landing, which is the same runway of current world's original normal airfield runway landing 1/5 or 1/6 or 1/7 or 1/8 or 1/9 or 1/10 length, the width of the jetport runway and former normal airfield runway Width is constant.It can also be set as needed by the size wing overall width of various aircraft models, all size can also be set Aircraft is mutually compatible with the runway of width, its great advantage of the jet runway can exactly be scaling up injection gas pressure on small runway The flow velocity of power and gas can the various large aircrafts of boosting landing.The jet-propelled runway thoroughly solves the province being not carried out in the past City to county, area under one's jurisdiction to county, each logistics area, each high mountain, mountain area, basin, in Concealable cavern, island, islands and reefs, frontier sentry stone On oily platform, artificial floating island, large, medium and small type aircraft can support town, township, village, stockaded village, be allowed to traffic convenience, and in very-short-reach Safety problem on landing runway or packaged type landing runway.In 50-100 meters long, 150-200 meters of long very-short-reach spray , it can be achieved that a possibility that large, medium and small type aircraft Civil Aviation Airport of 0.5-300 tons of weight enables on gas runway.

With the development of science and technology, aircraft carrier has become the hot spot of countries in the world military field engineering.Because type aircraft carrier deck runway landing is short, It needs to break through there are also multinomial key core technologies.For many years, it because aircraft carrier runway is short, and can not achieve to carrier-borne aircraft during take-off and landing Runway itself does not have the control to the active safety moment of inertia of landing aircraft, this causes carrier-borne aircraft cannot safe landing One of the main reasons.Therefore, the design specialists of each aircraft carrier state have studied for many years, finally think, aircraft carrier is only forced The catapult-assisted take-off of property is only the most advanced, and each aircraft carrier state has all put into a large amount of manpower and economy thus.However, using ejection It takes off carrier-borne aircraft in fact really not so ideal, it only takes off than sliding jump formula slightly quicker.Moreover, the safety of catapult-assisted take-off Coefficient be still it is relatively low, catapult-assisted take-off once accident occurs, typically occurs within moment suddenly, and has launched every time Flying accident occurred all is the major accident that can not be saved, meanwhile, the landing mode of each aircraft carrier state carrier-borne aircraft is brought into non- Force catapult-assisted take-off and optional check cable block can not a dead end on mistaken ideas.

When carrier-borne aircraft need to launch or when ski-jump take-off, for make landing carrier-borne aircraft not by it is extraneous it is marine with the wind or the shadow of lateral wind Ring, carrier-borne aircraft need to launch or when ski-jump take-off, aircraft carrier must at sea reverse end for end it is under full steam against the wind, when aircraft carrier is at sea reversed end for end not High speed can be opened, was differed the time required to each aircraft carrier u-turn for 15-20 minutes.It will result in wartime and carrier-borne aircraft landing prolonged Accidentally, in the changeable sea area operation of marine environment stormy waves, the often ejection by Marine Weather to carrier-borne aircraft or ski-jump take-off When influence, Marine Weather can often influence ejection or the ski-jump take-off of carrier-borne aircraft, and often will cause carrier-borne aircraft cannot drop in time The problem for falling and recycling.Sometimes, for marine stormy waves only in the case where 7-8 grades or more, aircraft carrier swing angle is more than 15-20 degree angle When, also the same ejection failure of carrier-borne aircraft or ski-jump take-off, and carrier-borne aircraft can not warship landing.Especially misty rain, ice and snow, When frosty weather, it is unable to landing because of runway cunning, winter in 2015, only one land airplane field of Chicago,U.S is because of ice and snow weather Just have 8000 multi rack time can not landing, this, which undoubtedly has become, is influenced by Changes in weather and limits each frigid zone Civil Aviation Airport and aircraft carrier The key factor of (aircraft be unable to landing is general not to be reported) takeoff and landing.

Therefore, one kind is selected and made not by frigid zone weather or sea from the landing mode of Civil Aviation Airport and aircraft carrier The variation of any stormy waves influences and can improve safely again each airport of control or carrier-borne aircraft safe landing at any time, a kind of deck performance Runway, this just has to the property of deck runway from the design of the structure of each airfield runway or deck entirety and inside and outside aircraft carrier entirety It can set out in layout, to improve takeoff and landing performance and various functions to aircraft carrier, be dedicated to fundamentally thoroughly changing Continental rise airfield runway or type aircraft carrier deck run continental rise runway or type aircraft carrier deck for a long time to the irrationality of takeoff and landing track elements Road must all have and not influenced entire first by factors such as marine any stormy waves, swing angle, wetness, misty rain, ice and snow, frosts The safe takeoff and landing performance of plate runway just can fully achieve and improve the function of the all-weather safety landing carrier-borne aircraft under special sea situation Can, truly improve the operational performance of the practical safe landing of Civil Aviation Airport and aircraft carrier entirety.

Currently, the aircraft carrier of 100,000 tons of countries in the world or more rides the sea when the prominent stormy waves for meeting 7-8 grades or more, 100,000 tons it is below When the prominent stormy waves for meeting 6-7 grade or more of aircraft carrier, when the stormy waves of prominent 5-6 grades of chance of 70,000 tons of aircraft carriers below or more, 50,000 tons of boats below Mother is prominent when meeting the 4-5 grade above stormy waves, is still shaken backward the subtracting such as water tank or stabilizer or electric top using subtracting for former routine and is shaken skill Art.Due to the defect that aircraft carrier itself is up big and down small, along with aircraft carrier lacks the complete artificial intelligence of one kind, fast automatic emergency again Various subtract the safety control system shaken.Meanwhile the landing phenomenon of aircraft carrier ultralimit on the dash road of deck is caused, seriously When be likely to cause carrier-borne aircraft and be all out of action, or even cause the disaster toppled because swing angle is too big.To being at present Only, problems maximum practical difficulty together with to be still World Ship fail to break through with each aircraft carrier state.By Patent No. The a kind of of ZL201510040609.6 resists the artificial intelligence control for turning over and subtracting and shaking the flexible sash weight of self-balancing or self-balancing electromagnetism rolling stone roller Subtract and shake function, can reach the automatic control that 85% or more reduction is risen and fallen and waved by the six-freedom degree of marine stormy waves to various ships Function.

Problem of the aircraft carrier because being influenced landing difficulty by weather is each aircraft carrier state of the current world insurmountable problem always, By at present, the United States, Russia, day, English, home country of Air France aircraft Normal Take-Off And Landing when insecurity factor from the point of view of, by minimum danger at present Ratio is 0.1%-0.2%.Sometimes, when by marine weather being influenced that aircraft carrier is caused to ride the sea, degree of waving be more than positive and negative 15-20 When spending, taking off to pressure will form the risk factor that accident rate is 8-10% with the aircraft of decline, and carrier-borne aircraft at this moment can only stop Boat waits.Sometimes, 7-8 grades or more of stormy waves is at sea encountered what is worse, but it cannot safety in time when aircraft is badly in need of landing Landing, round-the-clock landing are not just known where to begin yet, and how such aircraft carrier also fights？How about guarantee that aircraft carrier is afloat Operational performance？Here it is current each aircraft carrier state, to be unable to one that front faces most realistic, most universal, and in current technology On, and be insurmountable global rigid problem.

For many years, countries in the world still are able to safe landing and fly all when how research allows aircraft carrier at sea to be dashed forward and meet violent typhoon wave Machine, and kindling aircraft can make aircraft safety on runway with damaged aircraft and breakdown plane or when undercarriage is not opened The problems such as emergency landing of quick and stable, each aircraft carrier state of the world or each civil aviaton International airport also fail to break through these core skills so far Art difficulty.Its principal element：One, the world, which only has more than ten a small number of of poweies, aircraft carrier, although aircraft carrier has last 100 years so far Development history, but as used in its army of being only, wherein being also some limited for the confidentiality in terms of its technical research Personnel, this, which also limits some places, has advanced shipbuilding technology to develop the technology of aircraft carrier on the whole；Two, due to aircraft carrier Manufacture and design more complicated, still having many positions and structure in whole design, all there is also various uncoordinated, not phases The factors such as matching；Three, designer is integrally afloat using there is no constantly tracking to aircraft carrier, and many problems are all users (soldier) is to ship structure performance because sheerly layman personnel because manipulating improper use due to often causing.

Aircraft carrier since carrier-borne type constantly improves more new change, and carries out again landing aircraft deck after having manufactured Transformation can just be created in multiple various transformation process repeatedly, this is also each aircraft carrier state in manufacture aircraft carrier overall plan On a great problem, while these defective problems also just can not be thoroughly broken through in actual use, to cause at present World's aircraft carrier all can have a kind of guarantee being mutually matched without a deck runway so far with landing carrier-borne aircraft, and control Aircraft normally can suspend and go around on runway etc. quickly, safety control it landing function, so that aircraft carrier is existed instead Usually be in the dock when landing to the safety of itself, face multiple landing it is unsuccessful when, caused accident hazard.

The accident of each aircraft carrier state carrier-borne aircraft in the world during take-off and landing happens occasionally, and the accident of a lot of fatal crass once occurred, carrier-borne In all previous disaster of machine burst accident, wherein having 90% common causes is exactly to rise on type aircraft carrier deck runway to carrier-borne aircraft Deck runway is not achieved during drop to the active safety control performance of landing carrier-borne aircraft, gives carrier-borne aircraft in the manipulation of landing instead In mode, brings one kind (to invent) pressure catapult-assisted take-off by American and Britain, meaning, moral, Deng the United Nations or check cable is forced to block drop It falls and is known as high-tech technology, uncontrollable, very unsafe mandatory catapult-assisted take-off and check cable is more caused to block landing Various dangerous hidden danger brought by manipulation.With regard to being known as go-go aircraft carrier at present, deck runway is still carrier-borne to landing Machine is unable to control.Since with the wave of wave time and the moment of inertia of itself accident repeatedly occurs for carrier-borne aircraft during take-off and landing, and When each accident occurs, personnel can not actively come to sb.'s rescue at all on warship, only passively come to sb.'s rescue very much or aircraft pours greatly soon Sea not can guarantee the life security of accident pilot at all.

Carrier-borne aircraft, due to being limited by aircraft carrier itself runway is short, can only use the required aircraft to take off at present when taking off A kind of especially single ejection type takes off, by this energy consumption greatly and effect (rate) benefit it is extremely low and also again pole cannot be guaranteed it is safe Steam ejection or electromagnetic launch mode carry out the enforceable so-called go-go catapult-assisted take-off of realization aircraft carrier.And it is true It is really not so, although ejection mode technically increases than the mode that former sliding jump formula is taken off, still no gram Clothes and exclusion are because of the various safe landings by marine environment such as marine wave, sea wind, misty rain, ice and snow, frosty weathers, to its shadow Ring and caused by ceaselessly more waves time wave on deck, maximum actual influence is exactly when marine environment influences ejection and little When, and same marine environment prevents to decline instead aircraft from landing, since aircraft carrier swing angle is very much to cause cannot achieve greatly The biggest impact of carrier-borne aircraft active safety decline, this ejection runway can only do single mandatory catapult-assisted take-off.

It is launched under marine environment and is not located at positive and negative due to by aircraft carrier in wave disturbance shake all the time to aerial aircraft Among pendulum, the positive and negative swing angle of aircraft carrier is generally no more than 15-20 degree, if swing angle is too big, aerial aircraft is in nothing Method land warship danger among, so that aircraft is hovered in the air for a long time to empty, then need to refuel again in the sky, such as It will cause the danger of air crash not in time once refueling, to cause aircraft carrier can be in passively situation in fight.Certainly due to aircraft carrier The overall structure of body is all up big and down small feature, its most lacking is exactly to resist to subtract Oscillating function, and aircraft carrier is made because swing angle is big At the uncontrollable six-freedom degree in deck.Meanwhile causing to wheel before and after decline aircraft after warship, aircraft carrier is whole to wave Angle above deck, forms spring or broadside, Zuo You Oscillating puts and slide or rise and fall up and down and make at a slant to decline aircraft At the various unstable consequences slided of bouncing, sliding for various uncontrollable centering types is formed.It will cause when serious a certain Side wing such as mutually hits at the generation of various more perils with type aircraft carrier deck.In World War II, many carrier-borne aircrafts are all because of landing After warship, because the time that aircraft carrier waves wave secondary frequencies caused by marine stormy waves cannot be below 5 seconds, waving because type aircraft carrier deck is positive and negative cannot When more than the degree angle 15-20, explodes and burning oneself to death because waving to hit due to wave secondary frequencies are fast, tilt angle is too big in type aircraft carrier deck.

In practice, aircraft carrier is under most of typicalness for mixing queuing system of the aircraft carrier under limited space conditions (by wave time takeoff condition, landing state, crossing state etc.), there are other operations in flight-deck, as the admission of carrier-borne aircraft is dropped It falls, refuel to feed and hang the comprehensive coverages such as bullet, deck trailer movement etc., this busy state is generally impossible to flight-deck It leaves the random Boulez of a large amount of carrier-borne aircrafts, and must be waited in line to as described in aircraft carrier big country, this situation is also led It has caused to be queued under the steric requirements infinitely waited, to waiting process before shipboard aircraft group catapult-assisted take-off and has mixed kinetic force not It is enough accurate.Therefore, it when building aircraft carrier, needs again to the influence of ejector quantity on flight-deck, take off to shipboard aircraft group Preceding waiting process carries out the investigation matched in design, and they are placed in a relatively true research background as far as possible and is worked as In, could thoroughly solve the problems, such as current aircraft carrier before take-off infinitely wait in line.This is catapult-assisted take-off aircraft carrier first The true practical challenges that plate runway can not overcome.

With high-tech progress, all kinds of aircraft have all obtained rapid development to varying degrees and have improved.Fly early 20th century The appearance of machine is greatly promoted aerodynamic development, while having pushed the fast development of aviation industry.It is desirable to solve The certainly gas pressure distribution situation around aircraft, and lead to the force-bearing situation and resistance of aircraft, this just promotes Popularization and development of the hydrodynamics in terms of experiment and theory analysis.

Slided at present by the present invention with efficient very-short-reach or the dedicated jet platform runway device of VTOL aircraft on, adopt Become gas etc. with whirlpool spray, turbofan, axial flow blower formula compressed air machine liquid, it is defeated as the gas supply gas source of various ways Enter into the dedicated jet-propelled each gas storage air supply system of runway of takeoff and landing of the invention, it is referred to as a kind of to be sprayed by compressed air gas Release, which is formed by gas laminar flow, outside directive can assist safely the quick landing of landing aircraft, and above these types is supplied in gas source A certain gas source is input in each storage gas supply artificial intelligent control system of the dedicated jet-propelled runway of very-short-reach of the invention, And by jet runway by artificial intelligence control, the gas ejection ports with multiple rotary sleeve valve flute profile mouth formula structures (referred to as " telescopic slot-shaped spray jet outlet "), the gas ejection ports (letter with multiple rotary sleeve valve circular hole porous mouth formula structures Claim " telescopic circular hole porous spout "), or with multiple universal globe shell types without fixed sleeves single sleeve circle hole shape structure Gas ejection ports, (referred to as " Universal-head single sleeve gas ejection ports "), with rotary sleeve in multiple universal globe shell types with The gas ejection ports (referred to as " the double telescopic gas ejection ports of Universal-head ") of fixed sleeves circle hole shape, by above four kinds of gas injections Each piece of template made of a certain template of mouth is combined afterwards just can all form a very-short-reach landing jet platform runway dress It sets.

Above four kinds of formation gases jet ports are by artificial intelligence control, by the moving sleeve valve flute profile jet port or sleeve of each row Each jet runway that valve circular hole porous jet port or Universal-head jet port are constituted, each runway jet port is sprayed Gas out adjust to, can be inversely to landing airplane complete machine body lower part, each gas ejection ports gross area ejects dry or wet upwards The gas laminar flow of formula can reach jump up sliding to wing type and drop aircraft with injection gas laminar flow, landing aircraft is quickly hanged support Safe take-off and quickly outstanding two kinds of landing effects for asking safety barrage to land will on the dedicated jet runway of artificial intelligence When to takeoff and landing track and " inclination of the yaw biasing heart, up and down sink-float ", which can constantly be ejected to required amendment The gas laminar flow of landing aircraft trace can hang support formula and stir gas Laminar Flow and landing aircraft, because each moving sleeve valve flute profile is sprayed Loophole or moving sleeve valve circular hole porous jet port are all that 180 degree rotates.The Universal-head injection of 360 degree of artificial intelligence transformation On mouth, gas laminar flow that each gas ejection ports are ejected, gas flow, gas pressure are all that a point is controllable, it is controllable System adjustment correction ensures in normal jet runway regulation footprint landing aircraft forever, can normally press landing rail safely Mark effect, accelerate to take off or block landing aircraft eject match control and amendment to landing aircraft " yaw the biasing heart incline Tiltedly, rise and fall up and down righting " the gas laminar flow that releases outward of artificial intelligence control energy it can reach 100% regulation.

In the developing history of aircraft carrier last 100 years, mode is taken off as foundation using the difference of carrier-borne aircraft, shares 3 kinds of representatives at present The stronger flight-deck master-plan mode of property, respectively：Short distance VTOL formula flight-deck, ski-jump take-off formula flight first Plate, catapult-assisted take-off formula flight-deck.Above-mentioned 3 kinds typical flight-deck modes cut both ways.Separately below to above-mentioned 3 kinds of modes Excellent, the disadvantage of flight-deck are briefly introduced.

Short distance VTOL formula flight-deck：Refer to that carrier-borne aircraft can be excellent by the VTOL ability or exception of itself Aeroperformance completes the landing operation in small range space.Since this landing mode of carrier-borne aircraft can make flight-deck not There must be the enormousness of about 300m × 70m, and favor by some powerless countries for building large-scale aircraft carrier.Currently, in-service, More representative such aircraft carrier mainly has " Jia Fuer " number and Hispanic " Ah of " brilliance " number of Britain, Italy The middle-size and small-size aircraft carrier such as prince Si Tuliyasi " number.Although Spain's short and small short distance of " Asturias prince " number aircraft carrier hangs down Straight landing formula flight-deck makes it possible that aircraft carrier minimizes, but the flight-deck of such form, to the warship with property Carrier aircraft dependence is stronger.Currently, only have in the world 3 countries such as the U.S., Russia, Britain have completely Comprehensive Designing, production, Safeguard the ability of short distance VTOL formula opportunity of combat, active service type also only has F35A, F35B of U.S.'s latest version type, Russia Refined gram 141, several series such as " sparrow hawk " formula of Britain.

Further, since short distance VTOL formula opportunity of combat inevitably have from great, landing oil consumption is big, the speed of a ship or plane is slow, load is small, The common faults such as voyage is short, Structural strength calls are high, design theory is complicated, these insoluble problems make short distance VTOL formula Opportunity of combat does not become the main force on modern battlefield, and the short distance VTOL formula flight-deck of heavy dependence opportunity of combat performance, makes yet Middle-size and small-size aircraft carrier is difficult to the powerful attack and defense ability for having large-scale aircraft carrier.

Ski-jump take-off formula flight-deck.Ski-jump take-off mode refers to that carrier-borne aircraft in required location rear stop in place, works as aircraft engine Machine power unclamps stop device when reaching maximum, carrier-borne aircraft sliding run in the section of flush deck accelerates, so along with flush deck at one The arc for determining angle upwarps deck and continues sliding race, upwarps deck and is generally set to 12-14 degree angle, carrier-borne aircraft is made to obtain enough climb Flight-path angle and nose-up rate of pitch finally realize safety lift-off.Carrier-borne aircraft will continue to increase from the angle of attack after warship and height, this to fly The form that row deck upwarps can make up the deficiency that carrier-borne aircraft ground run distance is short, the initial velocity that takes off is small, using such mode flight " Liaoning warship " aircraft carrier for mainly having China, Russian " Boris Kuznetsov " number aircraft carrier and some medium-sized aircraft carriers on deck.Russia Ross " Boris Kuznetsov " number aircraft carrier also uses the flight-deck of ski-jump take-off mode, and great advantage is using flight-deck Fore body upwarps, and realizes the ski-jump take-off of carrier-borne aircraft, and technical risk is smaller, and mechanics principle is relatively easy, the disadvantage is that only at sea At 4-5 grades of stormy waves, Bo each≤6 seconds, deck degree of waving can just be securely achieved the most no more than 8-10 degree and be taken off.

The sliding jump formula ancillary equipment taken off to carrier-borne aircraft of taking off is fairly simple.Carrier-borne aircraft regulation, stops need to only install one only Dynamic device, which need to only be arranged a shutdown device cabin on flight-deck two deck below, to the other cabins in two decks Arrangement is almost had no effect.Special equipment (braking equipment) price that ski-jump take-off mode needs is relatively cheap, weight and shared Physical space is relatively small, and economy is higher.Flight-deck is almost not necessarily to prepare before carrier-borne aircraft ski-jump take-off, substantially can be with Accomplish the carrier-borne aircraft that takes off at any time, it is higher that aircraft goes out efficiency of movement.But compared with numerous advantages that it has, ski-jump take-off formula flies There is also some unavoidable defects on row deck, for example, carrier-borne aircraft ski-jump take-off process is affected by ambient environmental factors. The conditions such as misty rain, ice and snow, frosty weather, atmospheric temperature, air humidity, concentration of saline fog, sea situation environment when especially calm are all Ship-board aircraft engine can be impacted.Sometimes carrier-borne aircraft can not take off, and may cause carrier-borne aircraft and take off unsuccessfully, cause danger Accident is more.The 12-14 degree angle of deck upturned portion occupies a large amount of flight-deck spaces (deck about 25-30% overall length).The arc Shape region deck can not arrange that carrier-borne aircraft stops or allocated and transported, turns round operation inconvenience etc., causes due to having certain hollow rate Flight-deck space utilization rate is lower.In recent years, with carrier-borne after the continuous increase of carrier-borne aircraft weight, especially carry ammunition Machine air crash due to weight increase often causes weightlessness when taking off, some 40-50 tons or more of aircraft are difficult to by 350-370 Operation of taking off is realized on the long sliding jump deck of rice, such as large-scale fixed-wing early warning plane all it is 160-200 ton heavy not, and large size early warning plane Missing will seriously affect entire aviation the union team even operational efficiency of whole branch aircraft carrier fleet, sliding jump formula flying-off deck is almost at present It is a kind of aircraft carrier that Operational Effectiveness Rat is relatively low.

Although ski-jump take-off formula flight-deck scheme haves the advantages that numerous other schemes are incomparable, with modernization opportunity of combat Weight gradually increases, and especially ski-jump take-off formula flight-deck can not rationally solve the problems, such as that large-scale early warning plane steps on warship always, Especially aircraft carrier runway it is short and cause early warning plane can not landing.In addition, marine stormy waves will result in aircraft carrier at 7-8 grades or more Upper and lower floating is swung left and right, and swing angle can be more than 15-20 degree or more, this is for sliding jump formula early warning plane takes off, just It can not slide and take off above deck.So the application prospect of sliding jump formula flying-off deck is more dull.

Catapult-assisted take-off formula flight-deck.Catapult-assisted take-off mode, refer to carrier-borne aircraft under the drive of ejector sliding block, it is carrier-borne starting While machine engine itself, the additional power provided using steam boiler assists small-sized 100 tons or less by means of ejection system Early warning plane or carrier-borne aircraft take off lift-off.When marine stormy waves is at 7-8 grades or more, will result in aircraft carrier, floating, left and right are shaken up and down Swinging is equally unable to small-sized 100 tons of safe ejection or more of early warning plane and takes off or land more than 15-20 degree or more.

Catapult-assisted take-off mode flight-deck has many good qualities, and is a kind of deck mode that current large-scale aircraft carrier generallys use.The U.S. 12 aircraft carriers of naval's active service use steam ejection device on flight-deck.What steam ejection or electromagnetic launch formula were taken off Aircraft, all cannot achieve ejection type and take off by sea 8 grades of stormy waves or more or when humidity sleet sky, especially for 100 tons of self weight with On aircraft be just at a complete loss as to what to do ejection, the aircraft arrestments decline for 100 tons of self weight or more is similarly at a complete loss as to what to do.And it is big Most aircraft carrier states externally all hold back unpleasant information, and almost refuse to say anything about to the various real drawbacks of aircraft carrier.Aircraft carrier inherently warship The platform of carrier aircraft, and carrier-borne aircraft is influenced by marine weather sometimes on aircraft carrier, and can not safe landing.It is exactly in normal sea When foreign weather landing, the accidents such as various mechanical breakdown formula manipulation commander's faults can also occur sometimes on aircraft carrier for carrier-borne aircraft, this To carrier-borne aircraft on aircraft carrier landing be not perfectly safe guarantee pressure equipment, be that each aircraft carrier national capital is hopeless.

The U.S.'s " Abraham Lincoln " number nuclear aircraft carrier is compared with ski-jump take-off formula flight-deck, catapult-assisted take-off formula flight first The advantage of plate is mainly reflected in following aspect：Catapult-assisted take-off operation be not 100% it is reliable, can only say and compare in whole efficiency Sliding jump formula is taken off mode, is improved, but be not equally also overall safety.Preceding wheel of the carrier-borne aircraft in ejection process always by It is fixed on ejection sliding block, motion profile is the linear motion carried out along ejection orbit, and the rear left and right of aircraft two Wheel but interacts on the deck of aircraft carrier with type aircraft carrier deck generation, and carrier-borne aircraft is in crosswind, harmful air currents field, marine stormy waves to deck Left and right wheel, which is directly generated, after two is no more than 15 degree to the swing angle of the lateral torque in left and right of each wave time, marine stormy waves 6 seconds floatings up and down cannot be below to each wave in deck, swing angle is no more than under the interference of the unfavorable factors such as 15 degree, ejection Time is the safety accident just seldom flown off the runway in 3-4 seconds.But it is very high to the requirement of the various weapons of carry, be not The 100% various weapons for making carrier-borne aircraft carry, are unable to guarantee the success rate in each catapult-assisted take-off.Catapult-assisted take-off side Formula can provide power by steam boiler, realize the operation of taking off of larger weight carrier-borne aircraft, make the deterrence of entire aircraft carrier fleet Power is increased dramatically with fight capability.It is still that one kind cannot be coordinated in a manner of taking off at present in the ejection type of aviation field Control, the takeoff and landing runway of single-mode, cannot achieve to reach on same runway and are safely completed two kinds of landing marks Parasexuality energy.

Wave time swing angle of the carrier-borne aircraft catapult-assisted take-off process by atmospheric temperature, air humidity, aircraft carrier with wave size, sea situation The influence of the unpredictable factor such as condition, it is sometimes by wave big small echo time swing angle that carrier-borne aircraft bullet is oblique or bullet is inclined, it will rise The case where aircraft directly enters sea, also often ejection failure can be brought to take off in the event of failure.Steam catapult can be according to difference The ejection relevant parameters such as sliding block pulling force are adjusted in marine environment, marine unexpected Changes in weather and bad gas cannot be overcome The unpredictable factors such as time, bad sea conditions cause carrier-borne aircraft round-the-clock influence in the operation process that takes off Safe take-off.All-weather safety takes off all cannot achieve in each aircraft carrier state of the world today, still more be in capricious sea On, that is with regard to less practical.Catapult-assisted take-off is affected by atmospheric temperature, air humidity, sea conditions, using steam ejection Sometimes two steam catapults front and backs work at the same time device, often will cause to by the carrier-borne aircraft of lag ejection, the ejection of sucking foreground A large amount of water vapours that device releases, cause the carrier-borne aircraft engine misses for being lagged ejection, and the carrier-borne aircraft at this moment ejected is straight Enter sea, this reason is not originally known using steam ejection state, discovery later is until remaining on and not disclosing to common people today.Afterwards The phase U.S. just has studied using powerful Electromagnetical ejector but needed to decline to aerial aircraft by normal ejection again when, but still It is so subjected to the changeable influence of marine weather, and then often will cause the consequence for the recycling that can not land, especially unmanned plane is dropped Recycling when falling should can occupy 65% probability for falling fuselage and head, thus ejector at this moment still not can solve carrier-borne aircraft and The decline safe retrieving problem of unmanned plane aircraft.Two kinds of runways that landing cannot be mutually compatible are blocked with check cable to catapult-assisted take-off, Cause the waste of the occupancy deck gross area.

Currently, since aircraft carrier takes off and lands without lifting gear that is more advanced scientific and securely and reliably controlling, for many years Also to execute catapult-assisted take-off using mechanization or semimechanized means to carrier-borne aircraft or use check cable or arresting net Etc. it is unsafe it is various force catapult-assisted take-offs, force to block the landing of the behindhand type of landing to manipulate modernization carrier-borne aircraft, And it also is being able to this pressure catapult-assisted take-off formula flight-deck to be widely used in the large and medium-sized aircraft carrier of each aircraft carrier state at present In indispensable conceptual design, the ability of design catapult-assisted take-off is also not achieved in some countries.It is set for aircraft carrier and flight-deck Present Research is counted, domestic scholars have carried out correlative study for aircraft carrier, although the states head such as the U.S., Britain, Russia, France Phase possesses design, construction, the experience using aircraft carrier, all different degrees of product in terms of aircraft carrier master-plan and research Lot of research is tired out, but has also differed greatly in terms of specific, the actual security application manipulation with current carrier-borne aircraft landing. In this field, for being known as go-go aircraft carrier now, in terms of technology and strength, remains on and lag significantly behind this hair Bright jet runway is to the actual needs at present in the various new science and technology weaponry fast development process of military aspect.

For the about estimation of ejection process acceleration：In 80m/s, suitable speed per hour is 288 kilometer (160 for ejection and speed Section), it is assumed that ejection acceleration 100m (U.S.'s C-13-2 ejector) is calculated, 80m/s=according to V=(2aS) E × P0.5 formula (2a100m)E×P0.5：Acceleration a=32m/s²(g herein represents acceleration of gravity, g=9.8m/s to=3.26g²)。

For the about estimation of sling movement time：S=0.5at², S=100m, a=32m/s², t=2.6s.

For ejection process power budget：In the case of one 30 tons of frame aircraft acceleration is 1g, 30 tons i.e. 30000 kilogram size is needed Catapult moment, every 100 meters of catapulting distance acting be 3000000 kilogram-metres.One airplane of every ejection from preparation to The time is launched about at 15-20 minutes, the actual ejection time is considered as roughly 3 seconds.Then 1000000 Kilogram-Meter Per Second=13300 of power Horsepower (9790 kilowatts).The acceleration for actually launching needs is more than 3g (according to the estimation of front 1), and corresponding power is about 3 Ten thousand kilowatts.One aircraft carrier needs to be equipped with two to four ejection runways, and 2-4 ejector, when most nervous, four ejectors will It devotes oneself to work.

For the estimation of ejection force process：Ejection acceleration a=32m/s², in the case of being 30 tons by cataplane take-off weight, Due to ejection acceleration a=32m/s, 2=3.27g, ejection force is 98 tons of 30 tons × 3.27 ≈.

U.S.'s C-13-2 ejector, track length be 324 feet (99 meters), stroke capacity be 1527 cubic feet, piston with lead 6350 pounds of lead device weight, uss ronald reagan aircraft carrier equips four sets.Steam catapult launches maximum output energy power every time can reach 95 Megajoule (95 megawatts of seconds), if a single rack time is completed in ejection in 3 seconds, the consumption power of one airplane of every ejection is 32000 Kilowatt × the total RMB=16000 yuan power consumption of 0.5 yuan/kw, in addition equal 300 U.S. dollar 24 of the daily wage of a attendant more than 400 Hour, calculated by the manipulation of physical time of 400 people, per hour per artificial 12.5 dollars, averagely launch an airplane, from hangar to Deck erects to deflector, draws sliding block, to 10 minutes ejection airplanes are added up to the time required to ejection to worrying, and 12.5 is beautiful Member was equal to 4.8 dollars/people × 1920 dollars of 400 people ≈ divided by 60 minutes, and being roughly equal to RMB is 13440 yuan, along with aircraft The loss that front and back undercarriage is impacted naturally when warship recycling landing, to front and back brake, front and back wheel tire, to front and back damper Loss, about 11000 yuan of RMB are closed to consumings such as check cable work, once direct cost is about for aircraft carrier landing at present Comprehensive RMB is 40440 yuan.Ejector most phase shorter workweek is 45 seconds, average every ejection nearly 600- consumed in one airplane 700 kg of vapor, along with the consuming of the support staff in post each on aircraft carrier estimate and not counting.

For the estimation of ejection cylinder steam pressure：If ejection force is 98 tons, ejection cylinder bore is 21 inches of (U.S. C-13-2 Ejector situation), piston diameter is 21 × 2.54=53.3 centimetres, and piston area is 2231 cm x 2, and the piston gross area is 4462 centimetres, using double cylinders, piston area is doubled, and 22 kilograms per centimeters are applied in ejection vapor pressure ejection², practised according to the past Used unit is exactly 22 atmospheric pressure engineerings.About 8000-10000 cubic metres of the gross area of air accumulator.Nuclear reaction composting per minute Produce the gas for reaching 22 technical atmospheres.

Currently, mode there are mainly five types of the lift that all kinds of aircraft obtain：

One,Fixed-wing moves along a straight line in an atmosphere obtains lift.Engine should be the energy consumption of 55-60% when taking off, until after aerial It should be the energy consumption of engine 20-25% when normal flight.Such as various military aircrafts, Boeing, Air Passenger, the raising of this kind of aircraft Rely primarily on 2000 meters or more of long range runway, can only the dealing between large-scale airport, misty rain, ice and snow, frost day or sea turn For wave more than 8 grades or more, aircraft carrier is unable to landing, directly contributes flight delay, the influence of military secret paralysis, this is world today's boat The all insurmountable hang-up of empty industry.

Two, rotorcraft rotor obtains lift in atmosphere.The energy consumption of the 78-83% of engine is all needed when landing, until after aerial It should be the energy consumption of engine 40-45% when normal flight.As various large, medium and small type helicopters or nobody go straight up to carrier Deng the pneumatic function of rotor is inferior, and fuel consumption is big, so it has, voyage is short, flying speed is slow, fuselage is small, loading capacity is small etc. lacks Point.

Three, lift is obtained by downward vector puff prot.The energy consumption of engine 75-80% is all needed when landing, until normal after aerial It should be the energy consumption of the 35-40% of engine when flight.Such as willet machine, as its name suggests, the technology of taking off vertically is exactly that aircraft is not required to Slide race, so that it may take-off and landing or the technology of warship.It is the aviation developed since phase late 1950s Technology.Britain's sparrow hawk machine, U.S. F35B, refined gram of Russian 141 some aircraft carriers use this technology.The interior U.S. in recent years A kind of new architecture F35A type is developed, which is the type a kind of type the most advanced to take off now with sparrow hawk formula, after tested Its effect is little afterwards, which equally has that fuel consumption is big, voyage is short, flying speed is slow, load-carrying is small, especially making an uproar during take-off and landing The various disadvantages such as sound is big.

Four, the lift quickly to take off is obtained using solid fuel push type.90% energy consumption of engine is needed when transmitting, after satellier injection Energy consumption is quite big.Such as satellite, airship, Shenzhou VI, ballistic missile it is various air to air, it is air to surface, to warship, warship over the ground, warship to warship, Warship obtains lift using solid fuel push type to empty or various special suicide unmanned planes and various flying missiles.

Five, using the mobile Weight balancer of gyro inertia, the lift quickly to take off is obtained.Engine 35-40% is all needed when landing Energy consumption, until normal flight is the energy consumption of engine 15-20% after aerial.Gyro inertia can be used on current various aircraft High speed rotation, can get the vertical and lateral quick movement in various aircraft.The high-speed mobile of gyro inertia is than flat Normal various aircraft are more reliable, steady, are the directions of the following various aircraft development.Its advantage：Energy conservation, flying speed be fast, Loading capacity is big, stability is high, safe landing is high-efficient.

The air maneuver of VTOL technology is flexible, has the advantages that conventional airplane is incomparable：Firstly, it has VTOL The aircraft of ability does not need special airport and runway, reduces use cost；Secondly, VTOL aircraft only needs very little Level land can take-off and landing or warship convenient for camouflage, be not easy by enemy so aircraft can be distributed in war It was found that substantially increasing the battlefield survival rate of aircraft；Even if finally, due to which VTOL aircraft is on the airfield runway being destroyed Either on the airstrip in front, can also go up to the air operation, so the rate of attendance also increases substantially, and the strike to enemy With very big emergentness.

But simultaneously using the aircraft of current VTOL technology, also there are many serious disadvantages：It is that voyage is short first, due to real Existing VTOL, the take-off weight of aircraft can only be the 75-80% of motor power, this just receives greatly the payload of aircraft To limitation, the fuel load and voyage of aircraft are affected, meanwhile, oil consumption, its landing effect of 35-40% are needed in VTOL process Rate is extremely low, and VTOL is in the case where equivalent weight, the only 18-23% that takes off of plane track.

When current aircraft vertical takes off, when engine is worked with optimum state, every kw of power can only obtain 4N lift, oil consumption Amount greatly, also limits the combat radius of aircraft.Such as the loading capacity of " sparrow hawk " formula aircraft be 1060 kilograms when, combat radius only has 92 kilometers.So in actual use, " sparrow hawk " formula aircraft uses the mode of short takeoff as far as possible, to extend flight.Cause This, VTOL aircraft is also known as V/STOL aircraft.In addition, since VTOL aircraft is in actual combat, it is often necessary to It is dispersed in field, so its maintenance is also extremely difficult, is often broken down, service life is shorter.

V/STOL aircraft is the machine of naval's favor, because the length of the flight-deck on naval vessel is limited, vertically Short range landing technology just seems particularly useful." the extra large sparrow hawk " of equipment Britain " Ark Royal " number aircraft carrier is exactly the naval of " sparrow hawk " formula Type." extra large sparrow hawk " also uses the short range landing technology of " skew surface jump flies ", by installing the oblique deck of 12-14 degree on aircraft carrier, Aircraft can be allowed to slide race jump to fly, thrust deflexion is recycled, make aircraft in the insufficient situation of thrust, remain to stable in the sky add Speed.

The former Soviet Union once had developed the vertical take off and landing fighter of the models such as Ya Ke -38, Ya Ke -141.Although VTOL technology is not A new technology, and itself there is also some great weakness, but its advantages make one not forgetting really.The U.S. is current Just developing vertical/short field aircraft F35A and F35B and (V/STOL) of new generation.There are also many countries, are studying top Spiral shell inertia moves weight to balance Convertiplane.With the development of science and technology of aviation, when VTOL technology must be by landing Oil consumption lower, just can enter a brand-new developing developing stage in this way.

The injection lift that " sparrow hawk " formula aircraft of VTOL is used now pushes gas source jet port mode, is changed to by this hair A certain kind of bright a variety of gas supply gas sources, is slided or the dedicated jet of VTOL aircraft by compressed air gas injection short distance Receive to take off, it can be achieved that various " sparrow hawk " the formula aircrafts of VTOL or the take-off weight of helicopter can only be hairs on platform runway The 16-20% of the minimum thrust oil consumption of motivation, this just makes the payload of VTOL aircraft be greatly improved, has saved Energy consumption is dropped, so that combat radius is increased to 184 kilometers from original only 92 kilometers, while realizing " sparrow hawk " formula aircraft again or going straight up to winged The development long-term with it of needs of the machine on aircraft carrier, the most outstanding is the whole battle performance for improving aircraft carrier several times or more, The operational performance of " sparrow hawk " formula aircraft itself entirety is also improved simultaneously.

There are five types of the modes of taking off that can assist various aircraft at present：

One, the lift quickly to take off is obtained using Steam ejection type.For example, at present when American Airlines mother takes off, it should be using steaming Vapour goes out aircraft from aircraft carrier runway ejection.Fixed wing aircraft landing needs 2000 meters of long runways, and is equipped with the boat of ejector Just there are 150-200 meters of long runways on female deck, and the sliding jump runway of the taper slide equipped with 12-14 degree, longest type aircraft carrier deck is 300-380 meters.Aircraft on aircraft carrier how landing？Aircraft carrier is the capital ship using ship-board aircraft as primary armament, usually Tens of framves or even 100 multi-aircrafts can be carried.The takeoff speed of day jet aircraft generally all reaches per hour 300,000 Meter or more.If runway needs 2000 meters or more, and aircraft will slide more meters of 1000-1200-1500, just in continental rise field takeoff Ground airfield runway can be detached from.

And it is typically provided the flight-deck of ejector aircraft carrier, it is less than 200 meters, then how these ship-board aircrafts take off？ The originally aircraft on aircraft carrier mostly uses greatly special ejection mode to take off.This ejection mode, using high steam as ejection The ejection energy of power, generation is very big, can have been accelerated to aircraft rapidly with several seconds in nearly hundred meters of distance Degree, even 90 tons of weight of heavy airplane, is also nothing difficult.Carrier-borne aircraft is every primary by ejection, must all undergo examining for an intensity It tests, and it is every primary by ejection, it can all shorten carrier-borne aircraft catapult-assisted take-off and check cable blocks landing, be the Normal Take-Off And Landing aircraft utilization longevity The 25-30% of life.Especially severe, nose-gear and rear tyre and brake system abrasion are very big, to nose-gear by When power is too big, it is often necessary to the economic expenditure of a large amount of great numbers such as exchange or maintenance.

The mode that Fixed Wing AirVehicle takes off from aircraft carrier can be divided to two kinds：The first is sliding jump formula landing, is for second winged Machine ejector takes off, and steam ejection uses the deck of a plane as runway.When taking off, a steam-powered bullet is leaned on Injection device drives aircraft to reach takeoff speed in two seconds.Currently, only the U.S. have this steam catapult of production at Cooking technique.Its greatest drawback is because ejection power is too big, and can not launch unmanned plane, and the unmanned plane of active service is because of weight Gently, know from experience accelerated degree on ejection opportunity to discerp, improper maneuver will cause rising on another ejector to steam catapult sometimes Fly aircraft and suck foreground, the release water vapour that ejector leaves after being launched is inhaled into engine and causes to stop working, in Liang Tai When ejector works at the same time, it is necessary to work respectively by front and back 1-2 minutes interval time.

There are two types of ejection modes for steam ejection.One is the towed ejection of front-wheel, USN tests successfully for 1964.Carrier-borne aircraft Front-wheel support load onto dragging bar, front-wheel has just directly been hung on sliding block, and when ejection is directly hauled aircraft nose wheel acceleration by sliding block It takes off, does not have to 8-10 deck hands thus and hang tow rope and pick up tow rope.Launch time shortening, the direction safety of aircraft It is good, but the intensity of the front-wheel of this carrier-borne aircraft and bracket especially then needs specially to design greatly.Originally the U.S., which has, will repeatedly launch extremely Aerial carrier-borne aircraft causes to deform since front-wheel support stress is excessive, cause carrier-borne aircraft decline when undercarriage do not open and The multiple serious consequence that can not decline safely.USN's nuclear aircraft carrier also all uses this mode of taking off.

Another kind is the ejection of tow rope formula.As its name suggests, it is exactly taken off with the acceleration of steel rope traction aircraft.This ejection mode ratio Relatively old, everyway is good not as good as the latter.Currently, " Clemenceau " grade aircraft carrier of only France uses.When tow rope formula is launched, deck Personnel first hang over aircraft on sliding block with steel tow rope, then its tail portion and ejector rear end are fixed with an index release lever Firmly.When ejection, the power of determining that the sliding block of preshoot is broken on index release lever with sudden force breaks bolt, leads aircraft and accelerates rapidly along track, Aircraft is accelerated in track end to cast deck aside until takeoff speed, tow rope falls off from aircraft, and sliding block returns to ejector starting point, Prepare next task.

Fixed-wing is in the device that aircraft carrier takes off：In working principle, steam catapult is to push piston with high steam The sliding block on ejection orbit is driven, the carrier-borne aircraft being attached thereto is launched away.It bulky, only in an ejector On the gross area that need to occupy about need to consume a large amount of steam at 15000-20000 cubic metres or more, work, power dissipation is tight Weight, one airplane of every ejection only have about 6% steam to be used effectively.To manufacture and conveying steam, it is light that aircraft carrier will have seawater Makeup sets, large-sized boiler and countless pipelines, and the personnel of outfit about hundreds of people, port of going to sea back every time all must be to steam ejection system The maintenance for accounting for about thousands of working hours is carried out, maintenance amount is very surprising.And one airplane of every ejection needs RMB 4-6 more than ten thousand Member needs practical 600-700 kilograms of water vapour (every 1/ kilogram of sea water desalination is roughly equal to RMB 12-14 member cost) to reach 22 A above technical atmosphere, and in fact, the available energy dissipation of one airplane of ejection has only used 6%-10%.All the time, own Auxiliary landing technology, maximum common fault is all that energy consumption is excessive.

Two, the lift quickly to take off is obtained using hydraulic catapult formula.The lift quickly to take off, effect are obtained using hydraulic catapult formula Fruit is good not as good as the effect of steam ejection and electromagnetic launch, the hydraulic catapult skill that only original English, beauty, meaning, moral, day develop in early stage Art.Nineteen thirty, " Ark Royal " number aircraft carrier built by Britain use fluid pressure type ejector.1936, " imperial family side Boat " number aircraft carrier also finishes the use to fluid pressure type ejector, and the hydraulic catapult technology is theoretically proved Data is sealed up for safekeeping afterwards, and final there is no outwardly promoting, aircraft carrier uses it never again so far.

Three, the lift quickly to take off is obtained using electromagnetic launch formula.Electromagnetic launch is exactly pushed using the energy of electromagnetism by bullet The object penetrated moves out.Compared with steam catapult, mainly volume reduces about 40% the advantages of Electromagnetical ejector, manipulation Number will also lack 30% or so.Electromagnetic launch is divided into：Medium voltage DC source or middle pressure exchange two kinds, the electromagnetism bullet that the U.S. now uses Emitter is middle pressure AC power source, and middle pressure AC power source is not required to power rectifier and voltage-stablizer ancillary equipment, convenient using manipulation Good reliability.Electromagnetical ejector, principle is similar to magnetic suspension train, and the ejection dynamics of Electromagnetical ejector can than steam ejection Control property will be got well, and can launch unmanned plane.The disadvantage is that power consumption is about at 100 megawatts or more, but full electric power is pushed It is not too big problem for aircraft carrier and nuclear aircraft carrier.It wants pure for economic interests, is still very big using electromagnetic launch A kind of backwardness of ground waste of energy, and extremely unsafe technical equipment.Being taken off using Electromagnetical ejector mode still can't resolve Marine stormy waves aircraft at 7-8 grades is unable to the safety problem of landing, and ship-board aircraft is equally not achieved and pacifies on a deck runway The function of full landing, be still one kind can only catapult-assisted take-off, and not can guarantee the unicity of safe falling, do not match that, one The not compatible deck runway of landing.

Four, the lift quickly to take off is obtained using ski jump formula, some aircraft carriers are equipped with one in its deck front end and " jump Platform " help is taken off.Ski jump takes off, i.e., the slope that the deck end is made into 12-14 degree is upwarped, edge after carrier-borne aircraft takes off The slope that upwarps go out deck, form inclined throw movements.This mode of taking off does not need complicated catapult-launching gear, but aircraft rises Winged runway is relatively about 270-360 meters, and maximum weight when taking off is generally no more than 30-40 tons and the efficiency taken off It can not show a candle to electromagnetism and steam ejection technology.

The patent of steam catapult and Electromagnetical ejector is former American and Britain, method, moral, meaning, the participation research invention of Deng Ji state, institute With the country such as India, Russia and China due to that can not be copied by patented technology, the protected limitation of technology is added, is led to not Develop the aircraft with transcendency that there can be the one kind for breaking through electromagnetism and steam catapult performance completely new in technology and technique Landing device, so deck still home can only be stuck up using traditional cunning on aircraft carrier.Using the aviation of sliding jump deck landing aircraft Mother ship carrier all must be carried out second-mission aircraft and be taken off in takeoff and landing with the speed griping more than 20 sections (36 kilometers/hour), but The case where departing aeroplane that happens occasionally acceleration is not achieved takeoff speed and can not fly, at this moment aircraft may fall into sea.Have When the speed normally taken off is not achieved in Shi Gaodu and speed, aircraft can be weightless.When severe weight loss, air crash will cause.Work as sea turn For wave at 7-8 grades, just it is even more impossible to realize the stable landing on the runway of deck for carrier-borne aircraft.

Five, the lift quickly to take off is obtained using solid fuel push type.For example, satellite, airship, Shenzhou VI, ballistic missile, various Air to air or air-to-ground guided missile, it is various to warship or warship over the ground or warship to warship and warship to empty flying missile, pushed away using solid fuel Dynamic formula obtains lift.

Aircraft carrier can not safe Normal Take-Off And Landing, especially can be delayed opportunity of combat in wartime, aircraft carrier is made to lose ground, be in possibility at any time Among the danger sunk by enemy, this is also that each aircraft carrier state of the current world still has and insurmountable practical challenges again. Since the defence capability of aircraft carrier itself is insufficient, nuclear submarine is only with self-contained anti-warship guided missle and torpedo, so that it may to aviation Saturation attack is unfolded in mother ship carrier, will make aircraft carrier that can not resist, the consequence for leading to heavy loss and sinking.

Currently, it is the U.S. " Forrester " grade aircraft carrier that the world is state-of-the-art, 4 steam catapults have been installed altogether, can once take off 4 Frame carrier-borne aircraft.Each steam catapult runway, it is most fast that an airplane is launched in 7-10 minutes, it can guarantee in 60 minutes By 6-8 airplane catapult-assisted take-off.Even to this day, although " Forrester " grade aircraft carrier in the U.S.'s has installed 4 steam catapults, once Can take off 4 frame carrier-borne aircrafts, can guarantee that it still dare not be emitted by 24-32 airplane catapult-assisted take-off, but regrettably in 60 minutes Danger is in 60 minutes by 24-32 airplane catapult-assisted take-off.The main reason is that after 24-32 airplane catapult-assisted take-off to sky, and It is non-every 1 single rack secondary time to be pressed by catapult-assisted take-off to the aerial aircraft in day by every 7-10 minutes, it can not in wartime 100% safety is on time homeward, landing is recycled to aircraft carrier.It actually should be that 4 steam catapults can not launch simultaneously, First is that steam is once merely able to the gas source for an ejector, the ejection failure of bleed pressure deficiency is otherwise caused, secondly steam bullet It penetrates and is merely able to launch in turn, it will be carrier-borne by lag ejection the reason is that the water vapour of the remaining release after preceding ejection cannot be sucked Engine misses are caused in machine engine, some equipments cannot only be illustrated with simple digitlization.

When marine environment influences on ejection and is little, often it is in by the aircraft of catapult-assisted take-off to sky by Marine Weather The phenomenon that being mutated and cannot normally declining warship, therefore modernizing aircraft carrier is equally to rest on theoretic 100% round-the-clock Drop.Round-the-clock landing not all exists within every day.And actually only under the conditions of Marine Weather is good, it can be just real The round-the-clock landing on border.Most people, the saying to the round-the-clock landing of aircraft carrier is not to be well aware of.The world today is each The runway of the domestic existing landing condition of aircraft carrier, it is necessary to the variation of Marine Weather, can just decide whether can it is round-the-clock or Landing after half weather or several hours or dozens of minutes, otherwise can not accomplish.

When aircraft carrier is influenced by marine 7-8 grades or more stormy waves, it can significantly be swung left and right and rise and fall up and down, will cause carrier-borne Aircraft can not safety normal warship, especially wartime can serious delay opportunity of combat, and influence the operational performance of aircraft carrier entirety, together When substantially increase aerospace plane empty occur a possibility that air crash accident, so that aircraft carrier is lost ground and is at any time Among the danger that can be sunk by enemy.After here it is current each aircraft carrier states because of ejection or ski-jump take-off, sometimes often because by sea The marine environment such as change in weather influence, and can not decline safely, this be one completely cannot mutually coordinated solution practical challenges. Therefore, in order to make carrier-borne function under conditions of 7-8 grades or more of violent typhoon is unrestrained can with 100% safe landing operation, realize The coordinative coherence of safe take-off and safe falling for the security reliability of enhancing aircraft carrier landing comprehensively, reduces accident Occurrence frequency thoroughly realizes that aircraft carrier really obtains in practice to guarantee that aircraft carrier really plays due fighting capacity To round-the-clock safe landing, the target of always each aircraft carrier state researchers' unremitting effort over 100 years.

Professional scholars many for a long time not carries out the method for solving of carrier landing offset on by means of practice Further investigation, and there are also many scholars can only all be based in the safe life period, using to USN to carrier landing Point in some theoretical new methods of distribution characteristics, is obtained to carrier-borne aircraft by emulation experiment in difference on landing runway longitudinal direction Under operating condition the regularity of distribution of the warship point on runway, convert best arrester wires layout design problem to constrained more Objective optimisation problems, and bionic optimization algorithm appropriate is utilized, to the optimal placement scheme under different arrester wires quantitative requirements point It is not solved.These only lean on emulation experiment 10000 times of theoretical side, but are applied in specific practice manipulation, still What the technical standard parameter for once not testing same numbers with 10000 times was consistent, have no saying for exaggeration, many emulation is real Testing all cannot get the blanket approval that pains test flies person itself with theoretical school, and in mother ship carrier and carrier-borne aircraft landing, two ten thousand become more The technical parameter that a standard is taken in dynamic object, there is presently no which country to accomplish, these are skimble-skamble to be ground Study carefully and consumes a large amount of man power and material.

Here it is current aircraft carriers using mandatory catapult-assisted take-off technology and using a kind of Hen Bu section of enforceable check cable landing General introduction that theory and practice can not combine and the main reason for cause, and each aircraft carrier national capital can not be ignored at present One hang-up.Landed using check cable bigger to runway area occupied, main cause be aircraft 100% after hook rope " partially The biasing heart that navigates tilts, rises and falls up and down " etc., sliding run of being swung left and right on runway.Aircraft decline problem makes current each aircraft carrier state, all It is unsubstantiated to say, when every frame declines aircraft landing, accurate standard controllable stop position and time point, It more could not explain one in the landing of the every airplane ratio controlling technology parameter for having safe and scientific guarantee.This is also each at present navigates The each military specialist guide of home country oneself is difficult make clear hang-up, even the current U.S. " Forrester " grade It is female also the same such.In the landing of every airplane will compared with it is winged when required more one times of the time or more or more times navigate, This scalar multiple is that every aircraft carrier commander and pilot both know about, and due to unscientific manipulation means, causes carrier-borne aircraft Landing can not also have an accurate and scientific technical parameter so far, and only press fuzzy algorithmic approach, including most modernize at present Aircraft carrier.

Currently, the landing modes of each aircraft carrier state normal control aircraft carrier, what is generally used is exactly directly to be bowed from landing to deck It spins and falls, prevented by check cable hardness, the torque inertia force of the sliding after aircraft landing on the runway of deck is thoroughly disappeared It removes, to realize the so-called safe falling of aircraft.Check cable is Mk7 type on U.S.'s active service aircraft carrier at present, it can be blocked Resistance weighs more than 20 tons, the continuous landing of 200,000 ms/h of speed or so of modern aircraft.Under emergency conditions, blocking power can increase It is added to about 30 tons.Check cable on U.S. aircraft carrier is started setting up from 60 meters of angled deck tail end, from flight-deck height About 10 centimetres, it is horizontally set with one every 14 meters to ship's head direction, continuous that 4-5 root is arranged, aircraft pintle is sliding after hooking to run 60-92 Rice, can safety stop get off.Aircraft hooks after check cable is turned off engine in pintle, and aircraft pintle draws check cable sometimes When disconnected or pintle breaks tail, can all it cause aircraft directly into sea, or pour safety net.

Even if being equipped with multiple tracks safety barrage rope device, modern aircraft does not close engine generally in warship.To guarantee once When airplane tail hooks incessantly safety barrage rope, aircraft can be gone around with pull-up.If pintle fails to lay down next or carrier-borne aircraft and is damaged Wound, on machine fuel oil it is again few and when can not go around, emergency safety net will just use.It is about 4.5 meters high, it is wide slightly larger than blocking The nylon or carbon fiber arresting net for hindering Suo Kuandu can carry out aircraft to force to block, and usual aircraft band net goes out four or five ten meters Afterwards, it can stop.The requiring into factory's overhaul, 40% report of the aircraft 100% of decline is blocked by nylon or carbon fiber arresting net Useless, 10% pours sea, sometimes also grain, especially hangs and plays aircraft and can explode above deck or the maximum accidents such as ignition Generation.Here it is current modernization aircraft carrier, used do not manipulated by scientific law and mandatory dangerous block landing Manipulation is true.

Modern aircraft 100% does not close engine in warship, once check cable, aircraft are not lived to guarantee that airplane tail hooks It can be gone around with pull-up.This landing modes for not closing engine bring a kind of safety to pilot and decline aircraft really Sense.But the aircraft landing mode due to not closing engine, land aircraft after stern hook hooks check cable, is hooking Closed after check cable in the moment of engine, the moment of inertia of the aircraft that at this moment lands than closing more than big several times after engine, Uncontrollable consequences such as " yaw biasing heart inclination, up and down sink-float " of the landing aircraft on runway but will be caused, here it is hook ropes Before dare not by engine stroke low-speed running, or do not close engine landing modes more increase and be unable to control on runway under The inevitable outcome of airplane inertial torque difficulty is dropped, and check cable is caused to block within the moment for closing engine using hardness pressure Resistance rope be pulled off or tail be pulled off cause pilot do not adapt to especially with after hook rope institute it is increased various man-machine dangerous hidden Suffer from.

A little quality flight-deck in short-term is set on aircraft carrier.The aircraft-carrier flight deck of early stage is all-pass formula aircraft deck, The maximum drawback on this deck is, carrier-borne aircraft can not takeoff and landing simultaneously, i.e., when taking off, landing must suspend, etc. Runway is vacateed after taking off, aerospace plane can just land.If being divided into both ends from centre to implement, aircraft landing With the runway distance taken off with regard to shorter.Until nineteen fifty-two, Englishman, which has invented tiltedly straight two-part flight-deck and just calculates, solves this A problem, later, the large and medium-sized aircraft carrier in various countries have generallyd use the flight-deck of this form.Wherein, through type flight first Plate is located at the front of warship, and runway is about 70-90 meters, uses mainly for aircraft in catapult-assisted take-off；The portion 2-4 bullet is equipped on runway Emitter respectively can launch 1 airplane simultaneously and take off.Meanwhile two " recycling angles " as goat angie type are stretched out in the front end on deck, Surrounding is equipped with nylon wire, the Tuo Suo under throwing after main recycling airplane catapult.Angled deck is located at the left side of flight-deck, with warship Head and the tail center line is in 6-13 degree angle, and landing runway is about 220-270 meters long.On the angled deck of a small number of aircraft carriers There is one to two ejector, for aircraft under emergency conditions or without using when aircraft landing.

Since the flight-deck area on aircraft carrier is much smaller compared with continental rise airport, pilot is to accurate from the air Ground settles out, and is not a nothing the matter really, warship point must be very accurate.It is too forward or skewed at an angle, aircraft May go out angled deck fall into it is marine；Too rearward, aircraft can not just land on deck, and bump against with stern.In order to reach To the landing safety of decline aircraft, therefore each aircraft carrier state all sets on aircraft carrier and has filled landing aid device.In United States aircraft carrier Upper early stage, whole day weather electronics helped drop system equipped with drop radar is helped.No matter making carrier-borne aircraft daytime, night after system installation, Or it rainy day or greasy weather, can realize round-the-clock blind landing, really give landing aircraft the practical safety effect for bringing 70-80% Fruit, the safe sex ratio to land with vision when daytime is fine not as good as pilot are big.

The safety issue of take off mode or the landing modes of aircraft carrier, it is necessary to depending on the marine weather from the Nature Variation, could determine landing carrier-borne aircraft whether safety, this be own aircraft carrier since often because of change of marine stormy waves and weather Change and carrier-borne aircraft is made to be in various most dangerous passive situations, the security performance thus provided on aircraft carrier where landing carrier-borne aircraft It is very limited, Advanced Equipment is shaken although setting to have filled high-tech gyro and subtract on aircraft carrier, sometimes when marine ultralimit stormy waves, is still It is difficult to meet current aircraft carrier safely and fast to take off at any time on runway the actual needs of operation, and war occurs and can not Determined with Changes in weather, thus fully rely on existing aircraft carrier performance protect territorial waters also be not 100%, sometimes a zero is not Know number.

Landed by current aircraft carrier using catapult-assisted take-off and check cable, the highest namely the United States, Russia of efficiency, Britain aircraft carrier Aircraft, at most in the continuous landing 20-40% of property once every hour.Prerequisite condition when landing：The normal stormy waves of weather is at 6 grades Hereinafter, mother ship carrier degree of waving is at positive and negative 15 degree of angles hereinafter, the full fuselage head and the tail of each wave of floating time only allow at positive and negative 15 degree of angles up and down Hereinafter, the shift position that each wave time or so swaying is floated partially to certain side position is no more than 160-200 millimeter, each wave secondary period Cannot have steam gas-turbine less than 5 seconds and push the quick catapult-assisted take-off of aircraft, the electromagnetic propulsion aircraft quick catapult-assisted take-off time is not Can be greater than 4 seconds, ramp type of the runway at 70-90 meter or more, ski-jump take-off runway 270-350 meters or more of cunning takeoff drop it is special Use runway.Such as change in weather, aircraft carrier starts emergency takeoff.Such as misty rain, ice and snow, frosty weather, from marine stormy waves is at 7-8 grades Drop rate highest 3-5%.It cannot all take off under normal circumstances, because risk is too big, along with emergency landing is all gone back in secure context Do not ensure.When mother ship carrier waves 20 degree of angles or more, emergency landing is actually landing of taking a risk.

Since aircraft carrier is in special weather, safety emergency landing cannot be protected, and lead to current each aircraft carrier state Aircraft carrier all cannot independently go to sea operation, and when emergency landing suddenly is fought (under the conditions of landing weather is all normal), boat 60% actual combat takeoff and landing performance is also not achieved in female aircraft.The main reason is that the airplane that often takes off is from hangar to ejector The preparation time needs 15 minutes, some to the not yet done practical operation personnel of profession, preparation just need 20-30 minutes not Deng.It such as takes off the preparation of 10 airplanes, was calculated by every frame most fast 15 minutes, 10 airplanes that take off are 150 minutes.Worst It is an airplane and aircraft carriers of some countries all do not take off within several hours, and rises and fly to aerial aircraft more than one It must land at once in hour, not so the empty of aerospace plane will nowhere land, and must then fill up in the sky at this time can be just Often make a return voyage 5% about 2 tons of fuel oils, and skyborne refueling time must need 8-10 minutes at least.It is pushed away using steam gas-turbine It is only needed really 3 seconds when the quick catapult-assisted take-off of dynamic aircraft, but such as most fast from the time to form steam ejection function is begun heat to Need 25-30 more minutes, at this moment the aircraft deck runway of steam ejection is just in semiparalysis state, and here it is rely on steam at present Cataplane landing and when flight, it is various it is whole it is uncoordinated, mismatch, not compatible landing runway and caused by it is various not Security hidden trouble.

Aircraft carrier needs the safety measure that also do not meet an urgent need equally when landing of meeting an urgent need, for required for injured or failure aircraft The aircraft of landing provides the landing guarantee of safety.Currently, aircraft carrier deck runway is badly in need of safety measure when landing, still only By check cable and arresting net, and the aircraft of some injuries or failure is inherently out of control.There are also what is worse, decline rising and falling for aircraft Frame is not opened, and injured or breakdown plane is all tilting land in falls downward, do not open undercarriage or injured inclination out of control The aircraft of landing is only that not can solve emergency safe falling problem by check cable or arresting net.It is this do not open undercarriage or The aircraft of inclination decline out of control, generally before decreasing in the sky all first bleeds off fuel oil, military aircraft is by carry ammunition after injury Jettisoning prevents fuel oil or carry after landing to be hit and set off an explosion, and after injured errant aircraft decline, can all cause to aircraft greatly Small different various damages.It is a kind of most backward means using arresting net, it equally causes more various decline aircrafts out of control Big secondary damage or the possibility scrapped, that is taken by surprise sometimes causes the consequence of fatal crass.

With regard to the go-go advanced civil aviaton of nowadays American, aircraft carrier, still used when aircraft is badly in need of emergency landing on runway Arresting net is extremely unsafe first for decline aircraft, and less scientific.The most regrettably modern aircraft, To at present still using the control mode of century-old pervious this original unscientific capture bird.For many years, arresting net has been The special disciplines that a theory must be read are defined as in aviation academia；And this subject is risen to already in states such as America and Europes The scientific research task of one high-tech technology of world's sexology number circle, this achievement of arresting net think the professional person of many countries Be it is the most safe and reliable, it is no it is other it is advanced block landing technology in the case where, also can only be using the American-European rule used Quasi- arresting net is calibrated, and the arresting net equipment of this backwardness is also defined as by each state of civil aviaton, each aircraft carrier state, emergency landing is indispensable Aircarrier aircraft field, the main high-tech equipment special that aircraft carrier blocks, for many years, no one, which can technically suspect, to be directed to The research of this international practice of arresting net, this is also the great sorrow of whole world aircraft equipment state professional researcher Yu users Sorrow.

When aircraft landing only by account for integrated airplane collect enforceable stress of 1/several one hundred or several thousand pintle of area body in It is most unscientific on check cable, because the pintle that it is a kind of pressure hardness hooks (actually root steel after check cable Cord has filled two damping balance oil cylinders), decline aircraft receives the pressure of powerful rigid pulling force in the facet plot point of pintle Property is blocked.On every aircraft carrier, it is designed with the wirerope of 4-5 root, being known as check cable this pleasing to the ear and special hazard can not rescue The so-called safety device of medicine is located at always on the private track of aircraft carrier landing.Aircraft drop in type aircraft carrier deck also It falls on runway, equipped with check cable more than 5-6 root, aircraft carrier in World War II is equipped with 9, this is actually to set to decline aircraft The most dangerous decline obstacle in several roads.Especially once decline aircraft pintle does not hook half hook of first check cable, especially pintle It breaks off relations and causes the spring up and down of aircraft floatable again afterwards, at this moment decline and cause the unbalance of decline aircraft when aircraft moves forward, And at this moment second or third root or the 4th check cable etc. are just probably suspended to aircraft nose wheel.Once hanging up front-wheel, just It will cause and roll forward or pour above deck sea to decline aircraft, the serious consequence for causing aircraft to scrap.In World War II very More decline aircrafts be all because front-wheel hangs up check cable cause rolling after pour sea, because decline aircraft in decline head to On elevation-depression angle generally in 8-12 degree, for maximum pitch angle at 15 degree of angles, declining aircraft angle will cause greatly very much wind shear (because of this When engine be low-speed running) to will cause aircraft unbalance etc. for the bad manipulation of aircraft, before institute wheel apart from deck runway very close to. This original decline mode is also being used now, can bring carrier-borne aircraft pilot every time to the fear before decline.Only lean on Daredevil spirit can't resolve fear in the minds of pilot.For pilot, whenever putting down tail in falls downward That time of hook, pilot just have a kind of fear left it to chance.So someone say in type aircraft carrier deck be equipped with 5-6 root with On check cable on the runway of aircraft landing, dance on knife dirt just as pilot like that danger, so must thoroughly give up Except the landing modes for using check cable, this is not scientific, unsafe to the man-machine security risk that can not be detached from always.

China to carrier-borne aircraft stop systematic research start late, but in recent ten years in order to meet defence science development it is urgent Demand, some scholars of Some Domestic colleges and universities have begun the correlative study for carrying out aircraft arrestment system.Wherein, continental rise is flown During machine stops, the bending wave propagation in arrester wires is studied, and is established land airplane and is hit obstruction campaign mould to the rear Type proposes the dynamic analysis formula that carrier-borne aircraft is directed at warship point, proposes the force analysis side of carrier landing point Method etc..The work of these scholars provides a large amount of with reference to basis for the research that aircraft carrier stops problem.But due to ginseng It is limited to examine data, the various reasons such as experimental condition is limited, above-mentioned work is mostly using the obstruction process of land airplane as research object.Portion The carrier-borne aircraft divided in research stops the Example Verification of process, mathematical model, and continental rise has also all generally been selected to stop the correlation of system Data, working principle still have larger difference with the warship base obstruction system that carrier-borne aircraft is obstruction object.

Retarding braking process after carrier-borne aircraft hook rope, and to carrier landing in the process always by wave feature, deck Numerous uncontrollable complicated factors such as various nondirectional airflow fields, carrier-borne aircraft aeroperformance influence on ocean, are navigating About shoulder blade=100000 time in female life cycle management in warship operation, carrier-borne aircraft is still almost without the once energy on runway Enough entirely without yaw, and arrester wires is hooked in alignment, and the analysis of sliding race process proposes new after this carrier-borne aircraft hook rope to aircraft carrier Incomparable challenge.And retarded motion feature, ground run distance after the hook ropes such as carrier-borne aircraft is eccentric, yaw, inclination, upper and lower sink-float Equal kinematicchain elements influence the design of angled deck principal dimensions huge.This is current each modernization insurmountable disaster of aircraft carrier The main reason for inscribing, and causing current type aircraft carrier deck design comparison roomy.

When 4 kinds of situations superpositions such as carrier-borne aircraft bias hook rope, yaw hook rope, inclination hook rope, upper and lower sink-float hook rope occur, to entire Sliding race process of slowing down generally is shown, runs track for the various cunnings in the design of aircraft carrier landing runway principal dimensions, it is possible to provide more true Real reference frame and design principle.Carrier-borne aircraft bias is divided with the race of sliding after yawing hook rope, tilting hook rope, up and down sink-float hook rope etc. Analysis：Carrier-borne aircraft bias and yaw hook rope, inclination hook rope, up and down sink-float hook rope etc., the length being drawn out due to both ends arrester wires is not Together, 2 arrester wires ends buffering subsystem of arresting engine will start to play a role, and run rail to the sliding of carrier-borne aircraft to a certain extent Mark is rectified a deviation, and carrier-borne aircraft slows down in pure eccentric and pure yaw state hook rope and pure inclination hook rope and pure hook rope of sink-float up and down etc. The pulled out condition etc. of arrester wires in braking process.It is pure inclined, it is inclined when the pure eccentric hook rope of carrier-borne aircraft is carrier landing hook rope Boat angle is 0, but eccentricity differs, and since the bending wave in the arrester wires of left and right generates and propagates independently of each other, this will also make left and right To split Anhui different always from the angle for stopping hook for arrester wires.In fact, this is using arrester wires tensile speed in mechanical mechanism principle On a kind of normal reaction, because the buffering subsystem 2 arrester wires ends is when by unexpected external tensile force, the buffer sublayer The performance for stretching the absolute natural adjusted value of synchronous effect is always not achieved in system, and here it is the pure eccentric point area hooks of pintle Rope, and caused by machinery itself cannot be adjusted absolute value a kind of ultralimit it is unbalance after caused by normal reaction, it is nothing The example of method mathematical model is verified rigid rule.

The movement of the pure eccentric hook rope of carrier-borne aircraft, will lead to the difference for stopping hook two sides arrester wires pulled out condition, can make carrier-borne tail Through entire sliding race process in the case that hook two sides arrester wires pulling force is uneven.Further, since pintle two sides arrester wires pulling force contracts Small pure yaw, the retarding braking after carrier-borne aircraft hook rope cross bran, the movement of the pure yaw hook rope of carrier-borne aircraft and the pure eccentric hook of carrier-borne aircraft Rope is similar, and pure yaw hook rope also results in the difference for stopping hook two sides arrester wires pulled out condition, so that in carrier-borne aircraft pintle two sides In the case that arrester wires pulling force is uneven, also extends through normally reach carrier-borne aircraft during entirely sliding race and draw equal one forever The threshold that far also can't steer clear of.

Further, since the component of pintle two sides check cable pulling force is uneven, it is easy to carrier-borne aircraft be made sideslip occur during sliding run Phenomenon, so that the sliding yaw angle of running of carrier-borne aircraft is reduced, meanwhile, it will occur eccentric sliding with the carrier-borne aircraft hook rope of yaw situation It runs.When mother ship carrier navigation is in complicated sea situation, carrier-borne aircraft warship hook rope usually exist simultaneously it is eccentric with yaw inclination, upper sinking The superposition of the various states such as floating spring, this will make carrier-borne aircraft cause very big influence during sliding run, and in each time Actual conditions after interior to the stress of carrier-borne aircraft, speed, acceleration, wash away distance, wash away angle, wash away the shapes such as direction State is all unable to get the constantly amendment on runway, causes due to mother ship carrier and landing aircraft are all in irregular two kinds of dynamics, The variation of this lightening quickly polymorphicization can not be used independent artificial intelligence control by existing runway.

And carrier-borne aircraft after warship due to three wheels all stress above deck before and after carrier-borne aircraft, the inertia force for declining complete machine All switch to three it is sliding run on wheels, during washing away above deck, deck runway itself does not have the inertia of decline aircraft Cannot achieve when elimination automatic control repair it is inclined.Aircraft carrier swing angle left and right is positive and negative spent for 5-10 when, can decline by carrier-borne aircraft When speed ratio theoretically carrier-borne aircraft hook rope after be the sliding speed prompt drop for running about 80 meters per second to zero, carrier-borne aircraft is sliding run it is inclined Heart angle reaches left and right positive and negative about 5-10 meters or aircraft carrier swing angle at positive and negative 15 degree of left and right or more, after carrier-borne aircraft hook rope Cunning run the eccentric angle in 100 meters reach left and right it is positive and negative about 15-20 meters differ.Because aircraft carrier swing angle is more than 15-20 degree When above, carrier-borne aircraft cannot safe landing.Meanwhile by check cable tensioning system be not achieved at all to eccentricity control, This is to be blocked using mechanical mode after stress point uprushes, and causing to stretch control system cannot be in wink by one kind after unexpected stress The interior control of adjustment naturally, the unbalance runaway reaction after most limiting mechanical overload, referred to as airborne full conjunction shape.It is airborne super When closing serious, hardness fractures, check cable is broken or tail is pulled off oil cylinder and is damaged after causing pintle mistake soft, leads to aircraft The appearance of the problems such as directly into arresting net or sea, this is thing common on aircraft carrier.

The carrier-borne aircraft movement technique with yaw hook rope eccentric simultaneously, be carrier-borne aircraft exist simultaneously it is eccentric with yaw inclination, up and down Rise and fall four kinds of states.After warship hook rope, there is that is, pintle two sides check cable pulls out length for carrier landing point and runway center line marking Arrester wires at left and right sides of hook starts to be drawn out, and has and must not wait.Stroke is propagated due to bending wave to split and the different, spread speed of dew Mine and difference, check cable period angular position are all each different etc., in combination with the force feedback feelings of pintle two sides check cable Condition can further result in the inclination and spring of carrier-borne aircraft above deck to carrier-borne aircraft when moving progress.It is inclined due to carrier-borne aircraft The heart and yaw, which tilt, sink-float is sliding up and down runs, and left and right arrester wires elongation is not identical, and delays due to blocking check cable end in machine The presence of punching pin system, used numerical value is not also identical.This is also carrier-borne aircraft during sliding run, and is often appeared in certain Micro correction phenomenon in degree, real effect are simultaneously little.It is blocked here it is mandatory to decline aircraft, rigid by check cable Resistance, the various hang-ups in the world that offset cannot be corrected on runway of appearance, and itself does not also set always on runway There are the eccentric more scientific Correction and Control equipment means with yaw, inclination and the various artificial intelligence to rise and fall up and down.

Race process is slided in order to most really illustrate that carrier landing slows down, and provides most reliable design for angled deck principal dimensions With reference to the sliding race process of carrier-borne aircraft with the associated iteration in the overlaying state program of " the eccentric inclination of biasing boat, up and down sink-float " Scheme is core.In the sliding program run of carrier-borne aircraft hook rope and main flow design, although some Industrial Design Software energy at present It is enough to realize arresting system modeling extremely true to nature, and carry out emulation to it and block experiment, but for being set with flight-deck principal dimensions For being calculated as that purpose carrier-borne aircraft hook rope is sliding and running, this extremely complex industrial design modeling need to expend a large amount of human and material resources, Financial resources and time, and there are many details to be difficult to determine in simulation process, and need largely to simplify practical problem, to Analogue data measures Correction and Control that is rear, can not also having the sliding race of reply carrier-borne aircraft hook rope " eccentric biasing boat tilts plus spring ".Its Chief reason is exactly after declining aircraft hook check cable, and at this moment aircraft carrier is caused mother by various mappings such as marine various wave time stormy waves Warship and landing aircraft machine rope are all to lose its a large amount of research work all to mould in the dynamic become a variety of irregular ten thousand Quasi- authenticity and carrier-borne aircraft block the practical significance of operation process.

In comparison, under the premise of guaranteeing that critical issue and data are accurate, to carrier-borne aircraft and system interaction is stopped It derives, based on the analysis of theory of practice method, is realized using self-compiling program to the simulation of the sliding race problem of carrier-borne aircraft hook rope, do not lost For a kind of more practical simulating analysis.More importantly on this basis, can arbitrarily be obtained by modification program Different carrier-borne aircraft sliding trajectory, the pintle curve of load, carrier-borne aircraft speed and acceleration curve and it is various compared with data etc., make warship Various problems during the sliding race of carrier aircraft hook rope can obtain careful analysis.This is current dependence some (including the U.S.) Solid modelling carries out the software of simulation calculation, but remains on the technical parameter for being difficult to reach more quick, more more accurate.By In stopping system using mandatory not scientific mechanical mode, in many uncertain no technology content Fuzzy Calculation parameters of inaccuracy In the case where, it also can only achieve current this digital level only for reference, but these technical parameters without content can not answer again The problems such as to the practical correction for solving carrier-borne aircraft sliding trajectory, inclination, upper and lower sink-float, spring, so a large amount of research work Only walking the various softwares without technology content that the emulation Fuzzy Calculation of ignorant goes out for many years, to be rested on some nothings accurately theoretical Technical parameter it is formal, main cause is exactly carrier-borne aircraft using sliding this less scientific behaviour for running control of check cable hook rope Control technology and cause.

To sum up, it blocks landing from carrier-borne aircraft using catapult-assisted take-off and using check cable or arresting net emergency is used to block landing and fly So far, Civil Aviation Airport runway is too long, high construction cost, some cannot be built by geographical environment frigid zone, the torrid zone, water mist, limitation for machine Large airport, in misty rain, ice and snow, frosty weather, airfield runway is sliding and is unable to landing.Landing is taken off and blocked to above situation Mode, is unable to reach safe take-off and safety barrage lands, and the landing of aircraft carrier is all for many years several big with this Critical problem was blocked always without being detached from old catapult-assisted take-off and blocking to land or use using check cable until today Net emergency blocks the mode of landing aircraft, these less scientific compulsive means modes just not can guarantee modernization at present at all and fly The safe landing of machine.It is known as the aircraft carrier lifting gear and emergency measure means of modernization now, is far from meeting current aircraft carrier What the landing safety of aircraft and stability maintenance needed, so needing new more scientific, more reliable, high intelligence, safer efficient, degree of integration Height, and a variety of high-tech contents, the quick landing mode of high safety efficiency and the safe landing quickly met an urgent need can be played again simultaneously Mode, to fill up landing low efficiency, the energy consumption of aircraft carrier, continental rise airport aircraft and various sea, land and air body panels airport aircraft Greatly, friction is big, the service life is short, and that of the differences such as dangerous not foot point again, and it is not scientific, unpractical various to change those poles The control mode and compulsive means of risk.Fundamentally to realize aircraft carrier, continental rise airport aircraft in any emergency In the case of, aircraft carrier or nothing can be completed for the artificial intelligence landing of the safety of aircraft 100% in theory and practice by reaching Man-machine actual combat needs set out, and preferably adapt to continue to develop type aircraft carrier deck general aviation aircraft landing runway platform, continental rise airport security Control aircraft needs of landing stability maintenance on runway set out

Summary of the invention

The purpose of the present invention, during take-off and landing mainly for existing various aircraft, it is possible to provide a kind of to use compressed air conduct The injection gas of the core drive energy can assist fast and safely taking off for various aircrafts 100%, with the various aircrafts 100% of control Fast and safely land, a kind of jet platform wisdom traffic runway device system by compressed air gas injection very-short-reach. Referred to as " takeoff and landing device " is equipped.Injection gas platform wisdom traffic runway device system of the invention is one kind in aircraft carrier first Plate platform wisdom traffic runway, ship deck platform wisdom traffic runway, continental rise airport platform wisdom traffic runway, each provincial capital are extremely County airport platform wisdom traffic runway, each area under one's jurisdiction to county airport platform wisdom traffic runway, each high mountain, Airport in Mountain Region platform wisdom Traffic runway, tourist district's airport platform wisdom traffic runway, airport platform wisdom traffic runway, island airport in concealed cavern Platform wisdom traffic runway, islands and reefs airport platform wisdom traffic runway, air bag support float type airport waterborne platform wisdom traffic are run Road, frigid zone-low temperature are in subzero 60 degree, the torrid zone-high temperature in 80 degree above freezing of airport platform wisdom traffic runway and ice and snow waters On Qinghai-Tibet airport platform wisdom traffic runway etc., it can set entirely and load onto very-short-reach jet platform wisdom traffic runway device system System, and can realize and surmount various function uncontrollable to landing aircraft on original all size airport platform wisdom traffic runway Can, it especially improves and very-short-reach jet can be achieved to some environment areas that large, medium and small type takeoff and landing area has limitation Platform wisdom traffic runway " takeoff and landing device " equipment.

The present invention provides a kind of efficient very-short-reach of band in view of the deficiencies of the prior art and slides or VTOL aircraft device Aircraft carrier, naval vessel, land and water platform jet runway；It include that efficient very-short-reach slides or VTOL aircraft or unmanned plane device Type aircraft carrier deck jet runway or VTOL aircraft jet stage apparatus, and the behaviour to jet runway or jet stage apparatus Vertical control system, wherein：It can second-mission aircraft landing jet runway dress in the type aircraft carrier deck, on continental rise airport or various platforms It sets, and on the preceding bow tail end position outside each jet runway and the left and right sides outside runway, is respectively equipped with symmetrical hidden sleeping Formula liftable pitches or hidden horizontal and road face horizontal 0-90 degree angle, and can erect 0-30 meters of the formula that the is laid flat high lifting big mouths of tubular type Diameter sprays gas laminar flow apparatus, and it is to prevent landing aircraft in landing safely which, which sprays gas laminar flow apparatus, When it is out of control suddenly when emergency assistance take off or meet an urgent need and block；The type aircraft carrier deck jet runway or continental rise airport and various jets Runway stage apparatus is connected with management system；

The platform jet runway be one kind can inflation/deflation sea lifting gasbag float type jet runway stage apparatus, the jet run Stage apparatus can inversely the meet an urgent need aircraft that lands in road ejects the gas laminar flow of various different angles to block aircraft, and will Aircraft inertia force of landing is eliminated on the natural coastdown jet runway stage apparatus waterborne of lifting gasbag floating body at sea, described to fill The platform-type jet runway device of deflation lifting air utricule continental rise air bag nature coastdown is connected with management system；

The platform jet runway is slided on various naval vessels by the very-short-reach that blast injection gas blanket stream is formed to be a kind of, Or it VTOL aircraft or the dedicated jet runway stage apparatus of unmanned plane or itself moves for a kind of sea-going tug drawing type or independently Dynamic jet runway platform, slided by the short distance that blast injection gas blanket stream is formed VTOL aircraft or nobody The dedicated jet runway stage apparatus of machine is a kind of and various naval vessel Contiuum types, is formed by blast injection gas blanket stream super Short distance is slided or VTOL aircraft or the dedicated jet runway stage apparatus of unmanned plane, on the various various towboats in naval vessel If the dedicated jet runway stage apparatus of dress is connected with management system；

The platform jet runway be it is a kind of naval vessel rearward end be equipped with extension type it is waterborne can independent floating gasbag platform, or it is left On certain side at right ship side two side ends position or on each position in left and right ship side two sides, extension type is equipped with by blast injection The very-short-reach that gas blanket stream is formed slides or VTOL aircraft or the dedicated jet runway device of unmanned plane, described on naval vessel Rearward end is equipped on certain side at extension type or left and right ship side two side ends position or each position in left and right ship side two sides, is equipped with ultrashort Distance slides or VTOL aircraft or the dedicated jet runway stage apparatus of unmanned plane, the device are connected with management system It connects；

The platform jet runway is a kind of fixed offshore platform, and the very-short-reach formed by blast injection gas blanket stream is sliding Capable or VTOL aircraft or the dedicated jet runway stage apparatus of unmanned plane, the dedicated jet runway of fixed platform at sea Device, it is described in island short distance airfield runway, it is islands and reefs short distance airfield runway, oil platform short distance airfield runway, artificial Short distance airfield runway on chinampa, each frontier sentry dispense various goods and materials 5-10 ton wing type unmanned plane or unmanned helicopter, Vertical boosting landing unmanned helicopter platform is sprayed by compressed air gas, and will not be by weather misty rain, ice and snow, frost Frigid zone-low temperature that the small equal environment of geographic areas are limited in subzero 60 degree, the torrid zone-high temperature in 80 degree above freezing regional or mountain vallages, especially At sea aircraft carrier, naval vessel, land and water platform, the jet-propelled short distance of the various wing type unmanned planes on the high-altitude aerodrome of Qinghai-Tibet frigid zone are run for it Road or device to unmanned helicopter VTOL platform, the device are connected with management system；

The platform jet runway is that one kind may be provided on marine or rivers and lakes floating body platform, by blast injection gas laminar flow The very-short-reach of formation slides or VTOL aircraft or the dedicated jet runway stage apparatus of unmanned plane, it is described at sea or river Lake floating body platform-specific jet runway device is in each logistics area very short takeoff and landing runway, tourist district's very short takeoff and landing runway, each Desert mountain area very short takeoff and landing runway, Concealable cavern very short takeoff and landing runway or island, the water surface, cavern or extension airbag Formula very short takeoff and landing runway device, the device are connected with management system；

The platform jet runway is a kind of land airplane field, and the very-short-reach formed by blast injection gas blanket stream is sliding Capable or VTOL aircraft or the dedicated jet runway stage apparatus of unmanned plane；Or it is flexible for a kind of continental rise Moveable foldable skeleton Charge-discharge air bag cushion jet runway stage apparatus, is slided by the very-short-reach that blast injection gas blanket stream is formed, or vertical Landing aircraft or the dedicated jet runway stage apparatus of unmanned plane, described in land airplane field, continental rise Moveable foldable skeleton is flexible Charge-discharge air bag cushion platform jet runway device is connected with management system；

The platform jet runway will be for a kind of future in town-dweller-rural-family's individual's baby plane in continental rise or continental rise sky airplane platform Frontier sentry, and may extend to the landing with international adaptability standard or store the current supermarket on family's aircraft airport, by pressing The very-short-reach that contracting air injection gas blanket stream is formed slides or VTOL aircraft or the dedicated jet runway device of unmanned plane, A kind of frigid zone-the low temperature limited by environment such as weather, geographic areas subzero 60 degree, the torrid zone-high temperature 80 degree variously Area, is slided by the very-short-reach that blast injection gas blanket stream is formed or VTOL aircraft or unmanned plane private track are put down Platform device, it is described in the personal big baby plane of town-dweller-rural-family or large, medium and small unmanned plane, continental rise or continental rise sky airplane platform, Carrier-borne fixed-wing unmanned plane landing when can 100% auxiliary recycling do not fall unmanned fuselage and head, each dedicated jet in frontier sentry Runway stage apparatus, someone or unmanned helicopter landing gas injection stage apparatus are connected with management system.

Forming the platform jet runway can be used whirlpool spray, turbofan, axial flow blower formula, air compressor, the liquid change of current maturation The gas supply gas source technology of gas various ways, the power source of the essential core as the jet runway will above several gas supply gas A certain gas source in source is input to each gas storage of the jet-propelled runway of the platform, supplies in artificial intelligent control system, can shape At the structure of the jet platform runway device of the safe landing aircraft of a very-short-reach.

Overall structure is made of seven regions；On each region, respectively by being provided with muti-piece valve body plate main body module sub-unit (73) Tangible chamber is arranged in the lower part in seven regions made of being combined, the bearing wall and frame structure of the valve body plate main body module sub-unit (73) Room；The first area of jet runway is 20 meters long (1), 20 meters of second area long (2) of jet runway, the third area of jet runway Domain is 20 meters long (3), and 20 meters of the fourth region long (4) of jet runway, the 5th region of jet runway is 20 meters long (5), jet runway The 6th region 20 meters long (6) and jet runway District 7 domain it is 20 meters long (7), respectively by each region set mounted in each airport run On road or type aircraft carrier deck is carrier-borne or each dedicated jet runway (191) in airport on, one to seven region constitutes 140 meters long of each machine , dedicated length is by setting needed for a variety of different types, or sets a kind of jet runway or aircraft carrier that size type is mutually compatible with Structure of the deck to carrier-borne aircraft or the dedicated jet runway entirety of unmanned plane landing；

The left-external side in the first area of jet runway 20 meters long (1) is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；On the left outside cliche frame longitudinal direction batten seat (16) of runway, it is respectively equipped with the left outside green warning lamp of cliche frame longitudinal direction reddish yellow of runway (24)；Cushion connecting sewing (13) and private track left fixed under-chassis (8) are installed between each region valve body plate module of runway；

The left-external side in the first area of jet runway 20 meters long (1) is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；In the left outside lower part of the left outside cliche frame longitudinal direction batten seat (16) of runway, it is equipped with the left outside 1-7 region turnbarrel valve of runway Gate slot shape puff prot or circle hole shape puff prot servo pushing motor (30)；On the right side of the first area of jet runway 20 meters long (1) Outside, it is equipped with the right outer cliche frame longitudinal direction batten seat (17) of runway；In the case where the right side of the right outer cliche frame longitudinal direction batten seat (17) of runway is outer Portion is equipped with the right outer 1-7 region rotary sleeve valve flute profile puff prot of runway or circle hole shape puff prot servo pushing motor (31)；

The laterally inboard in the first area of jet runway 20 meters long (1) is equipped with the green warning of runway rear left wheel road reddish yellow Lamp (28)；After the left-external side of the first area of jet runway 20 meters long (1) between longitudinal direction, the second area equipped with jet runway 20 meters long (2)；Preceding longitudinally outboard in the first area of jet runway 20 meters long (1) is equipped with cliche frame transverse direction press strip before runway Sealing and dustproof outer cover (14)；Before runway on cliche frame transverse direction press strip sealing and dustproof outer cover (14), it is respectively equipped with Normal Take-Off And Landing storage Deposit defeated deflation bucket connecting tube (10)；Defeated deflation bucket connecting tube (11) is stored with emergency landing；Defeated deflation bucket is stored with spare landing Connecting tube (12)；And cliche frame transverse direction press strip sealing and dustproof outer cover seat fixing bolt (18) before runway, it is whole to constitute jet runway The unblocked fixed reasonable bindiny mechanism of sealing with cliche frame transverse direction press strip in three sets of independent gas transmission sources.

Inside between the runway rear left wheel green warning lamp of road reddish yellow (28) is respectively equipped with left first region of runway and respectively sprays Mouth opens 1-2 millimeters (33)；In left first region of runway, each spout opens the Right Inboard of 1-2 millimeters (33), is equipped with runway The green warning lamp of front left wheel road reddish yellow (26) and the green warning lamp of runway front right wheel road reddish yellow (27)；It is red in runway front right wheel road Outside in the right side of yellowish green warning lamp (27) is equipped with each spout in first region in the runway right side and opens 1-2 millimeters (35)；On the runway right side In each spout in first region open the right side of 1-2 millimeter (35), equipped with the green warning lamp of right wheel road reddish yellow (29) after runway；

The right outside of the green warning lamp of right wheel road reddish yellow (29) after dedicated jet runway is equipped with right outer first area of runway Each spout in domain opens 1-2 millimeters (34)；1-2 millimeters of (34) right outsides are opened in the right outer each spout in first region of runway, are equipped with The right inside and outside multiple air curtain puff prots (61) in longitudinal direction of runway；It is right outer in the right inside and outside multiple air curtain puff prots (61) in longitudinal direction of runway Side is equipped with the right outer cliche frame longitudinal direction batten seat (17) of runway；On the right outer cliche frame longitudinal direction batten seat (17) of runway, it is respectively equipped with The runway right side green warning lamp of outer cliche frame longitudinal direction reddish yellow (25) and the fixed spiral shell of the right outer cliche frame longitudinal direction press strip sealing and dustproof outer cover of runway Bolt (21)；With the right fixed under-chassis (9) of private track；And cushion connecting sewing is installed between each region valve body plate module of runway (13)；Constitute that the consistent property of each component reasonable coordination repairs the connection of convenient for disassembly and assembly and jet protection gas source and warning rises with safety The manipulation and control of drop；

The left-external side of 20 meters of second area long (2) in jet runway is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；On the left outside cliche frame longitudinal direction batten seat (16) of runway, it is respectively equipped with the left outside green warning lamp of cliche frame longitudinal direction reddish yellow of runway (24)；Cushion connecting sewing (13) are installed between each region valve body plate module of runway；The left fixed under-chassis (8) of private track is constituted Integrally each portion position is fixedly connected with the structural compatibility with warning to jet runway；

20 meters of second area long (the horizontal left side 2), equipped with the green police of runway rear left wheel road reddish yellow in jet runway Show lamp (28)；After the left-external side of 20 meters of second area long (2) of jet runway between longitudinal direction, the third area equipped with jet runway Domain is 20 meters long (3)；Between the preceding longitudinal direction of 20 meters of second area long (2) of jet runway, the first area equipped with jet runway 20 meters long (1) constitutes the consistency of the whole cooperation control to one to three region of jet runway part runway mechanism；

The left-external side in the third region of jet runway 20 meters long (3) is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；On the left outside cliche frame longitudinal direction batten seat (16) of runway, it is respectively equipped with the left outside green warning lamp of cliche frame longitudinal direction reddish yellow of runway (24)；Cushion connecting sewing (13) and the left fixed under-chassis (8) of private track are installed between each region valve body plate module of runway；

The left side of transverse direction in the third region of jet runway 20 meters long (3) is equipped with the green warning of runway rear left wheel reddish yellow Lamp (28)；After the left-external side of the third region of jet runway 20 meters long (3) between longitudinal direction, the fourth region equipped with jet runway 20 meters long (4)；Between the preceding longitudinal direction of the third region of jet runway 20 meters long (3), the second area 20 equipped with jet runway Rice long (2) constitutes the consistency of structure connection Proper Match between each region in one to four region；

The left-external side of 20 meters of the fourth region long (4) in jet runway is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；On the left outside cliche frame longitudinal direction batten seat (16) of runway, it is respectively equipped with the left outside green warning lamp of cliche frame longitudinal direction reddish yellow of runway (24), cushion connecting sewing (13) and the left fixed under-chassis (8) of private track are installed between each region valve body plate module of runway；

The left side of transverse direction of 20 meters of the fourth region long (4) in jet runway is equipped with the green police of runway rear left wheel road reddish yellow Show lamp (28)；After the left-external side of 20 meters of the fourth region long (4) of jet runway between longitudinal direction, the 5th area equipped with jet runway Domain is 20 meters long (5)；Between the preceding longitudinal direction of 20 meters of the fourth region long (4) of jet runway, the third region equipped with jet runway 20 meters long (3) are constituted to the interconnection of each section components of jet runway and the reliability of security warning；

The left-external side in the 5th region 20 meters long (5) in jet runway is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；On the left outside cliche frame longitudinal direction batten seat (16) of runway, it is respectively equipped with the left outside green warning lamp of cliche frame longitudinal direction reddish yellow of runway (24), cushion connecting sewing (13) and the left fixed under-chassis (8) of private track are installed between each region valve body plate module of runway；

The left side of transverse direction in the 5th region 20 meters long (5) in jet runway is equipped with the green police of runway rear left wheel road reddish yellow Show lamp (28)；After the left-external side in the 5th region 20 meters long (5) of jet runway between longitudinal direction, the 6th area equipped with jet runway Domain is 20 meters long (6)；Between the preceding longitudinal direction in the 5th region 20 meters long (5) of jet runway, the fourth region equipped with jet runway 20 meters long (4)；

The left-external side in the 6th region 20 meters long (6) in jet runway is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；On the left outside cliche frame longitudinal direction batten seat (16) of runway, it is respectively equipped with the left outside green warning lamp of cliche frame longitudinal direction reddish yellow of runway (24), cushion connecting sewing (13) and the left fixed under-chassis (8) of private track are installed between each region valve body plate module of runway；

The left side of transverse direction in the 6th region 20 meters long (6) in jet runway is equipped with the green police of runway rear left wheel road reddish yellow Show lamp (28)；After the left-external side in the 6th region 20 meters long (6) of jet runway between longitudinal direction, the District 7 equipped with jet runway Domain is 20 meters long (7)；Between the preceding longitudinal direction in the 6th region 20 meters long (6) of jet runway, the 5th region equipped with jet runway 20 meters long (5), constitute each regional body and each region cooperates between each movement mechanism and fixed mechanism part in practical application It is advanced reasonable handling；

The left-external side in the District 7 domain of jet runway 20 meters long (7) is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；On the left outside cliche frame longitudinal direction batten seat (16) of runway, it is respectively equipped with the left outside green warning lamp of cliche frame longitudinal direction reddish yellow of runway (24), cushion connecting sewing (13) and the left fixed under-chassis (8) of private track are installed between each region valve body plate module of runway, Constituting each section components of jet runway can the fixed security warning of entire combination.

On the platform jet runway, it is respectively equipped with Normal Take-Off And Landing and stores defeated deflation bucket connecting tube (10), it is defeated with emergency landing storage Cliche frame transverse direction press strip seals after deflation bucket connecting tube (11) and spare landing store defeated deflation bucket connecting tube (12) and runway Dustproof encloser fixing bolt (19) is constituted to the three sets of individual secure air distribution systems sealing the most complete of whole jet runway and gas The smooth safe and practical property in source；

The left fixed under-chassis (8) of dedicated jet runway, the right fixed under-chassis (9) of private track, Normal Take-Off And Landing store defeated deflation bucket Connecting tube (10), emergency landing store defeated deflation bucket connecting tube (11), and spare landing stores defeated deflation bucket connecting tube (12), runway Cliche frame transverse direction press strip sealing and dustproof outer cover before installation cushion connecting sewing (13), runway between each region valve body plate module (14), the left outside cliche frame longitudinal direction batten seat (16) of cliche frame transverse direction press strip sealing and dustproof outer cover (15), runway, runway after runway Before right outer cliche frame longitudinal direction batten seat (17), runway after cliche frame transverse direction press strip sealing and dustproof outer cover fixing bolt (18), runway The left outside cliche frame longitudinal direction press strip sealing and dustproof outer cover of cliche frame transverse direction press strip sealing and dustproof outer cover fixing bolt (19), runway is fixed The right outer cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt (21) of bolt (20), runway；

It is described on the left outside cliche frame longitudinal direction batten seat (16) of dedicated jet runway, be respectively equipped with each region valve body plate module of runway Between installation cushion connecting sewing (13) run with the left outside cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt 20 of runway On the bottom position of the left outside cliche frame longitudinal direction batten seat (16) in road, it is equipped with the left fixed under-chassis (8) of private track；

It is described on the right outer cliche frame longitudinal direction batten seat (17) of dedicated jet runway, it is green to be equipped with the outer cliche frame longitudinal direction in runway right side reddish yellow Warning lamp (25)；On the bottom position of the right outer cliche frame longitudinal direction batten seat (17) of runway, it is equipped with the right fixed under-chassis of private track (9), with the right outer cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt (21) of runway；Cliche frame transverse direction press strip is close before runway Seal dustproof encloser 14) on, it is respectively equipped with the first green warning lamp of cliche frame transverse direction reddish yellow (22) before runway, stores defeated put with Normal Take-Off And Landing Gas bucket connecting tube (10), and emergency landing stores defeated deflation bucket connecting tube (11) and spare landing stores defeated deflation bucket connecting tube (12) and before runway cliche frame transverse direction press strip sealing and dustproof outer cover fixing bolt (18), composition consolidate jet runway entirety Fixed layout is connect and the controllability of safe Normal Take-Off And Landing with the layout closure of valve actuating mechanism；

It is described on cliche frame transverse direction press strip sealing and dustproof outer cover (15), to be respectively equipped with Normal Take-Off And Landing storage after dedicated jet runway Defeated deflation bucket connecting tube (10) stores defeated deflation bucket connecting tube (11) with emergency landing and spare landing stores defeated deflation bucket and connects The sealing of cliche frame transverse direction press strip is anti-after taking over (12) and the runway rear molding green warning lamp of cliche frame transverse direction reddish yellow (23) and runway Dirt outer cover fixing bolt (19)；

The first green warning lamp of cliche frame transverse direction reddish yellow (22), the green police of runway rear molding cliche frame transverse direction reddish yellow before the dedicated jet runway Show lamp (23), the left outside green warning lamp of cliche frame longitudinal direction reddish yellow (24) of runway, the green warning lamp of the runway right side outer cliche frame longitudinal direction reddish yellow (25), the green warning lamp of runway front left wheel road reddish yellow (26), the runway front right wheel green warning lamp of road reddish yellow (27), runway rear left machine It takes turns the green warning lamp of road reddish yellow (28), the green warning lamp of right wheel road reddish yellow (29) after runway, constitutes automatic letter whole to jet runway Number warning and the controllability of safe active.

The left outside 1-7 region rotary sleeve valve flute profile puff prot of the runway or circle hole shape puff prot servo pushing motor (30), each spout in the 7th region opens 7-8 millimeter (59) in the runway right side, if being mounted in, type aircraft carrier deck is carrier-borne or each dedicated spray in airport On gas runway (191)；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, it is longitudinal to be respectively equipped with the left outside cliche frame of runway Batten seat (16)；In the interior lower part of the left outside cliche frame longitudinal direction batten seat (16) of runway, it is equipped with the left outside 1-7 region rotary sleeve of runway Cylinder valve flute profile puff prot or circle hole shape puff prot servo pushing motor (30)；In the right outer cliche frame longitudinal direction batten seat (17) of runway Interior lower part is equipped with the right outer 1-7 region rotary sleeve valve flute profile puff prot of runway or circle hole shape puff prot servo pushing motor (31)；

It is described to open 1-2 millimeters (32) in each spout in left outside first region of jet runway, it is each in left first region of runway Spout opens 1-2 millimeters (33), 1-2 millimeters (34) is opened in the right outer each spout in first region of runway, first in the runway right side A each spout in region opens 1-2 millimeters (35)；

It is described to open 2-3 millimeters (36) in each spout of the left outside Two Areas of jet runway, it is each in the left Two Areas of runway Spout opens 2-3 millimeters (37), 2-3 millimeters (38) is opened in the right outer each spout of Two Areas of runway, second in the runway right side A each spout in region opens 2-3 millimeters (39)；

It is described to open 3-4 millimeters (40) in each spout in the left outside third region of jet runway, it is each in the left third region of runway Spout opens 3-4 millimeters (41), opens 3-4 millimeters (42) in the right outer each spout in third region of runway, the third in the runway right side A each spout in region opens 3-4 millimeters (43)；

It is described to open 4-5 millimeters (44) in each spout in left outside 4th region of jet runway, it is each in left 4th region of runway Spout opens 4-5 millimeters (45), 4-5 millimeters (46) is opened in the right outer each spout in 4th region of runway, the 4th in the runway right side A each spout in region opens 4-5 millimeters (47)；

It is described to open 5-6 millimeters (48) in each spout in left outside 5th region of jet runway, it is each in left 5th region of runway Spout opens 5-6 millimeters (49), 5-6 millimeters (50) is opened in the right outer each spout in 5th region of runway, the 5th in the runway right side A each spout in region opens 5-6 millimeters (51)；

It is described to open 6-7 millimeters (52) in each spout in left outside 6th region of jet runway, it is each in left 6th region of runway Spout opens 6-7 millimeters (53), 6-7 millimeters (54) is opened in the right outer each spout in 6th region of runway, the 6th in the runway right side A each spout in region opens 6-7 millimeters (55)；

It is described to open 7-8 millimeters (56) in each spout in left outside 7th region of jet runway, it is each in left 7th region of runway Spout opens 7-8 millimeters (57), 7-8 millimeters (58) is opened in the right outer each spout in 7th region of runway, the 7th in the runway right side Each spout in a region opens 7-8 millimeters (59), constitute first region to the 7th region on whole jet runway, to each area Domain puff prot gap opens size and meets landing aircraft in the security control of the quick landing in each region, each region jet size all with The control system of pilot and jet runway control tower mutually switches in machine, the finally completion whole in aircraft by pilot Manipulate control of the jet runway to landing aircraft.

On each region valve body plate main body module sub-unit (73) of the jet runway, it is longitudinal more to be respectively equipped with the left inside China and foreign countries of runway Outer laterally four flute profiles or circle before a air curtain puff prot (60), the multiple air curtain puff prots (61) in the inside and outside longitudinal direction in the runway right side, runway Shape puff prot is that four flute profiles of middle transverse direction or round puff prot are spare landing jet before Normal Take-Off And Landing puff prot (62), runway Laterally four flute profiles or round puff prot are to meet an urgent need landing puff prot (64) before and after mouth (63), runway；Runway longitudinally sprays 50- 400 mesh intelligence hydraulic spray nozzles (72), if mounted in type aircraft carrier deck is carrier-borne or each dedicated jet runway (191) in airport on；

It is described in the left inside China and foreign countries of jet runway longitudinally multiple air curtain puff prots (60), the right inside and outside multiple air curtain jets in longitudinal direction of runway Outer laterally four flute profiles or round puff prot are positive middle transverse direction four before normal landing puff prot (62), runway before mouthful (61), runway Flute profile or round puff prot are that laterally four flute profiles or round puff prot are to meet an urgent need for spare landing puff prot (63), runway front and back Drop puff prot (64), constitute whole runway is not influenced by external wind interference, and in runway each region be designed with it is normal, The normal work of each region main jet loophole of intelligent control of the respective independent switching system of three of emergency power landing aircraft；

The position all around of the seat under each piece of valve body plate main body module sub-unit (73) template of jet runway, all distinguishes Equipped with the longitudinal road face horizontal adjustment cushion (65) of each valve body plate main body module of installation or so；Runway installs each valve body plate main body mould Lateral road face horizontal adjustment cushion (66), runway install the self-locking fixing bolt of each valve body plate main body module dedicated buffering before and after block (67)；The various bufferings and damping after overloading to whole runway in takeoff and landing are constituted, it will not when reaching to landing aircraft Cause the vibration to runway；

In from jet runway first area to the 7th of jet runway the region, it is equipped with muti-piece valve body plate main body module sub-unit 73；On valve body plate main body module sub-unit 73, it is equipped with outer rotary shaft flute profile mouth or round hole axle outer shaft in multiple runways and connects Fork library (68) is connect, outer rotary shaft flute profile mouth or round hole axle internal axle sleeve connecting fork library (69), universal globe shell type 180- in runway 360 degree of angle rotary oscillating type puff prot amendment takeoff and landing " inclination of the yaw biasing heart, righting of rising and falling up and down " (70), inner rotary shaft Flute profile puff prot 97 is covered,；Oxygenation or manufacture anoxic puff prot (71) are manufactured, runway longitudinally sprays 50-400 mesh intelligence hydraulic spray nozzle (72)；Constitute to exterior and interior axle sleeves connecting fork library to each rotary shaft flute profile jet port or circle hole shape jet port, each jet port it is coaxial Degree and steering angle up to 100% it is accurate；

First region 20 meters long (1) on jet runway valve body plate main body module sub-unit (73) to the 7th region On 20 meters long (7), the left inside China and foreign countries of runway longitudinally multiple air curtain puff prots (60) are respectively equipped with, it is more with the right inside and outside longitudinal direction of runway Outer laterally four flute profiles or round puff prot are positive normal landing puff prot (62) before a air curtain puff prot (61) and runway, and run Before road four flute profiles of middle transverse direction or round puff prot be before and after spare landing puff prot (63) and runway laterally four flute profiles or Round puff prot is emergency landing puff prot (64), constitutes the independent switching manipulation of three sets of air curtains protection in each region of jet runway Control, and constitute interfering it for the whole various high wind of runway external environment；

The position all around of the seat under every piece of valve body plate main body module sub-unit (73) template of jet runway, all pacifies respectively Fill the longitudinal road face horizontal adjustment cushion (65) of each valve body plate main body module or so；Each valve body plate main body module front and back is installed laterally Road face horizontal adjustment cushion (66)；The self-locking fixing bolt of each valve body plate main body module dedicated buffering (67) is installed；The above, Constitute whole jet runway, the security performance during realizing integrated buffer and damping use to landing aircraft；

It is described on jet runway valve body plate main body module sub-unit 73, be respectively equipped with outer rotary shaft flute profile mouth or circle in runway Hole axle outer shaft connecting fork library (68), interior outer rotary shaft flute profile mouth or round hole axle internal axle sleeve connecting fork library (69) with runway； Constitute whole each region of jet runway laterally each interior outer rotary shaft it is in office what when being driven, each jet port angle opens size all 100% on an axis, precise angle, sealing when each puff prot switch closes prevent dirt object, rainwater or seawater from entering Each puff prot and shutoff valve shape are intracavitary；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with universal globe shell type 180- 360 degree of angle rotary oscillating type puff prot amendment takeoff and landing " inclination of the yaw biasing heart, righting of rising and falling up and down " (70)；Inner rotary shaft It covers flute profile puff prot (97), longitudinally sprays 50-400 mesh intelligent water with manufacture oxygenation or manufacture anoxic puff prot (71) and runway Atomizing nozzle (72)；Whole each region of jet runway is constituted actively to the secure safety manipulation and control of emergency landing aircraft, and It can the various large aircraft safe fallings of safety barrage.

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with outer rotary shaft in jet runway Flute profile mouth or round hole axle outer shaft connecting fork library (68)；Outer rotary shaft flute profile mouth or round hole axle internal axle sleeve connecting fork in runway Library (69)；Universal globe shell type 180-360 degree angle rotary oscillating type puff prot correct takeoff and landing " yaw the biasing heart inclination, on Lower sink-float righting " (70)；Inner rotary shaft covers flute profile puff prot (97)；With manufacture oxygenation or manufacture anoxic puff prot (71)；And race Road longitudinally injection 50-400 mesh intelligence hydraulic spray nozzle (72)；Whole each region of jet runway is constituted actively to emergency landing aircraft The constantly amendment of " eccentric biasing boat inclination, righting of rising and falling up and down ", uses water mist gas to 600 tons heavy or more aircraft landing It is with high safety to block warship control, and the reliable peace under Reasonable Protection utilization and recycling effect is constituted to jet runway gas source Full manipulation of the property to landing aircraft；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be equipped with 0-180 degree angle spray circle hole shape mouth Interior rotation solid shaft (98)；It is rotated on solid shaft (98) in 0-180 degree angle injection circle hole shape mouth, is equipped with interior rotation solid shaft Or hollow axle sleeve circle hole shape puff prot (99)；The both ends of solid shaft (98) are rotated in 0-180 degree angle injection circle hole shape mouth, if There are rotary shaft flute profile mouth or round hole axle outer shaft head end card slot (113), sets that carrier-borne mounted in type aircraft carrier deck or each airport is dedicated respectively On jet runway (191)；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be equipped with runway valve body plate main body module install Electromagnet cut off valve or gas control jet air storage chamber phase through slot room (74)；Electromagnet cut off valve or gas are installed in runway valve body plate main body module It controls under jet air storage chamber phase through slot room (74), is equipped with runway valve body plate main body module lower plate pedestal (86)；In runway valve body plate Main body module is installed in electromagnet cut off valve or gas control jet air storage chamber phase through slot room (74), and universal globe injector head or inside and outside is equipped with Rotary sleeve sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or pneumatic regulation whiff pressure graduated release valve sub-unit (137)；In universal globe injector head or inside and outside rotary sleeve sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or gas On dynamic regulation whiff pressure graduated release valve sub-unit (137), it is equipped with universal globe injector head and is oriented to jet appendix single sleeve (136)；With compressed air gas source blowing mouth or the quick plug receptacle seat (139) of hose connector, extraneous input gas source is constituted to entirety The manipulation and control of the normal safe landing of injection gas source in jet runway.

It is described on each region valve body plate main body module sub-unit (73) of jet runway, it is flexible to be equipped with Pneumatic extension and hydraulic cylinder Operating mechanism installs room maintenance blind patch (89)；Blind patch is repaired in Pneumatic extension and hydraulic cylinder flexible control mechanism installation room (89) under, oil cylinder (75) are pushed equipped with Pneumatic extension；It pushes on oil cylinder (75), is pushed equipped with Pneumatic extension hydraulic in Pneumatic extension Oil cylinder stretches interlocking lever (76)；With flexible interlocking lever and each control rotary axle valve guiding arm connecting plate (77)；With flexible gearing Fixed pin shaft and the whole jet runway of pin card dottle pin (78) composition are pneumatically mixed with the dynamic cylinder of oil up and down for bar and each guiding arm connecting plate Close the safe manoeuvring control mechanism of fast and flexible；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be equipped with rotary shaft flute profile mouth or round hole axle Outer shaft fixing seat (94)；On rotary shaft flute profile mouth or round hole axle outer shaft fixing seat (94), it is equipped with inside and outside compressed air The outer swing arm fixing groove handle seat (79) of rotary sleeve sleeve；The swing arm fixing groove handle outside rotary sleeve sleeve inside and outside the compressed air On seat (79), it is equipped with swing arm and fixing bolt (80) outside outer rotary shaft set sleeve fork library；Outside outer rotary sleeve sleeve fork library The lower end of swing arm and fixing bolt (80) is equipped with swing arm and fixing bolt (81) outside inner rotary shaft set sleeve fork library；Inside Rotary sleeve sleeve is pitched under the outer swing arm in library and fixing bolt (81), is equipped with and is oriented to active support plate swing linking arm or rotary shaft The whole jet runway of lateral pressure swivel bearing (138) composition pneumatically pushes oil cylinder Hybrid connections part and flexibly swings inside and outside set sleeve The operating-controlling mechanism reliably used of guiding freely；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, push oil cylinder (75) equipped with Pneumatic extension； It is pushed on oil cylinder (75) in Pneumatic extension, is equipped with inside and outside rotary sleeve sleeve and pushes rack gear or connection gib block (82)；Inside and outside Rotary sleeve sleeve pushes in rack gear or connection gib block (82), is equipped with flexible interlocking lever and each control rotary axle valve is oriented to arm Connecting plate (77)；With fixed pin shaft and pin card dottle pin (78) above and below flexible interlocking lever and each guiding arm connecting plate；With interior rotation Bushing sleeves pitch swing arm and fixing bolt (81) outside library；And the active support plate of guiding is swung in linking arm or rotary sleeve sleeve Outer lateral pressure swivel bearing (138)；On each 73 inside casing of region valve body plate main body module sub-unit of jet runway, it is equipped with control Cylinder is connected and fixed seat (83)；It is connected and fixed on seat (83) in master cylinder, is connected and fixed hinged shaft (84) equipped with master cylinder；With pneumatically stretch Contracting pushes the flexible realization that oil cylinder (75) constitute each control unit of whole jet runway, is swinging the sliding peace closed in precision of shaft The stability of full manipulation service life；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be equipped with runway longitudinally injection 50-400 mesh intelligence It can hydraulic spray nozzle (72)；Runway pavement panel (85)；The longitudinal multiple air curtain puff prots (60) in the left inside China and foreign countries of runway；Runway is lateral Center to bilateral symmetry is equipped with universal globe shell type 180-360 degree angle rotary oscillating type puff prot amendment takeoff and landing, and " yaw adds Bias inclination, righting of rising and falling up and down " (70) constitutes and corrects takeoff and landing " yaw biasing heart inclination, up and down on whole jet runway Rise and fall righting " puff prot to aircraft trace can adjustment constantly control；

The lower part in each region valve body plate main body module sub-unit (73) of jet runway is equipped with jet runway valve body plate main body Module lower plate pedestal (86)；On jet runway valve body plate main body module lower plate pedestal (86), it is equipped with runway valve body plate master Module installs electromagnet cut off valve or gas control jet air storage chamber phase through slot room (74)；Runway valve body plate main body module I-shaped support rib Stand (87)；Fixing threaded hole (91) above and below subject runway module air inlet air storage chamber transverse sealing end cap；Normal Take-Off And Landing storage is defeated to put Gas bucket connecting tube (10)；Landing of meeting an urgent need stores defeated deflation bucket connecting tube (11) and spare landing stores defeated deflation bucket connecting tube (12), the unimpeded control with the fixed support performance of sealing of air distribution system gas transmission of whole jet three sets of self-insurances of runway is constituted；

The lower part in each region valve body plate main body module sub-unit (73) of jet runway is equipped with jet runway valve body plate main body Module I-shaped support rib stand (87)；On jet runway valve body plate main body module I-shaped support rib stand (87), it is equipped with runway Fixing threaded hole (91) above and below main body module air inlet air storage chamber transverse sealing end cap；The flexible manipulation of hydraulic cylinder is pushed with Pneumatic extension Room (88) are installed by mechanism；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, it is flexible to be equipped with Pneumatic extension and hydraulic cylinder Operating mechanism installs room maintenance blind patch overlap joint mouth (90)；It is repaired in Pneumatic extension and hydraulic cylinder flexible control mechanism installation room Blind patch overlaps on mouth (90) left and right sides, is respectively provided with Pneumatic extension and hydraulic cylinder flexible control mechanism installation room maintenance port lid Plate (89)；Under jet runway valve body plate main body module lower plate pedestal (86), it is equipped in runway valve body plate main body module air inlet Pipe installs room transverse sealing end cap inner panel (92)；Transverse sealing end cap inner panel in room is installed in runway valve body plate main body module air inlet pipe (92) it on, is respectively equipped with Normal Take-Off And Landing and stores defeated deflation bucket connecting tube (10)；Landing of meeting an urgent need stores defeated deflation bucket connecting tube (11)； Spare landing stores defeated deflation bucket connecting tube (12)；A variety of interior main each gas transmission storages deflation bucket interface bore (140) of air supply source；Pressure Contracting air gas source blowing mouth or the quick plug receptacle seat (139) of hose connector；With subject runway module air inlet air storage chamber transverse sealing Fixing threaded hole (91), the air distribution system and Pneumatic extension for constituting whole three sets of runway of jet push hydraulic cylinder and stretch end cap up and down Installation and maintenance operating control mechanism easy to use.

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be equipped with 0-180 degree angle injection flute profile mouth in Rotate solid shaft or hollow shaft sleeve (96)；Solid shaft or hollow shaft sleeve (96) are rotated in 0-180 degree angle injection flute profile mouth On, it is equipped with inner rotary shaft set flute profile puff prot (97)；0-180 degree angle on the valve body plate main body module sub-unit (73) is set It sprays in circle hole shape mouth in rotation solid shaft (98), is equipped with interior rotation solid shaft or hollow axle sleeve circle hole shape puff prot (99), structure Each jet port air-flow of integral jet runway is adjusted with the Internal control structure of shaft and axle sleeve gap seal standard precision It is whole；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be equipped with manufacture oxygenation or manufacture anoxic jet Mouth (71)；In manufacture oxygenation or manufacture anoxic puff prot (71), it is respectively equipped with 30 degree of dead angles spray by 30-90 degree fixed angle Loophole rotates solid shaft or hollow shaft sleeve (100)；By 30-90 degree fixed angle 40 degree of dead angle jet ports rotate solid shaft or Hollow shaft sleeve (101)；Solid shaft or hollow shaft sleeve (102) are rotated by 50 degree of dead angle jet ports of 30-90 degree fixed angle； Solid shaft or hollow shaft sleeve (103) are rotated by 60 degree of dead angle jet ports of 30-90 degree fixed angle；By 30-90 degree fixed angles The 70 degree of dead angle jet ports rotation solid shaft or hollow shaft sleeve (104) of degree；It is sprayed by 80 degree of dead angles of 30-90 degree fixed angle Mouth rotation solid shaft or hollow shaft sleeve (105)；Solid shaft or sky are rotated by 90 degree of dead angle jet ports of 30-90 degree fixed angle Mandrel sleeve (106) constitutes each jet port rotary shaft axle sleeve clearance seal in one to seven region and storage inside whole jet runway The standard controllability of air chamber structure；

On each region valve body plate main body module sub-unit (73) of jet runway, it is equipped with by 0-180 degree angle injection flute profile mouth Rotate solid shaft or hollow shaft sleeve (96)；Solid shaft or hollow shaft sleeve (96) are rotated in 0-180 degree angle injection flute profile mouth On, it is equipped with rotation axis seal packing mounting groove (107)；On rotation axis seal packing mounting groove (107), it is equipped with rotation axis seal Packing (108)；It is described on each region valve body plate main body module sub-unit (73) of jet runway, be equipped with rotary shaft flute profile mouth or circle Shape hole axle internal axle sleeve fixing seat mouth (109)；On rotary shaft flute profile mouth or round hole axle internal axle sleeve fixing seat mouth (109), respectively Equipped with rotary shaft flute profile mouth or round hole axle exterior and interior axle sleeves or upper and lower gas transmission room sealing FE Tiler (110)；With rotary shaft flute profile mouth or Round hole axle exterior and interior axle sleeves or FE Tiler cage bolt hole (95) constitute whole jet runway internal spray mouth rotary shaft to gas supply Gas source sealing structure precision closes the manipulation of the reliability of gas source；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with rotary shaft flute profile mouth or circle Hole axle outer shaft fixing seat (94)；On rotary shaft flute profile mouth or round hole axle outer shaft fixing seat (94), it is respectively equipped with rotation Axial trough shape mouth or round hole axle outer shaft (93)；With rotary shaft flute profile mouth or round hole axle exterior and interior axle sleeves or FE Tiler cage bolt Hole (95)；On each region valve body plate main body module sub-unit (73) of jet runway, it is provided with manufacture oxygenation or manufacture anoxic spray Port (71)；It is manufactured in oxygenation or manufacture anoxic puff prot (71) in runway, is equipped with 0-180 degree angle and sprays circle hole shape mouth inward turning Turn solid shaft (98)；It is rotated on solid shaft (98) in 0-180 degree angle injection circle hole shape mouth, is equipped with rotary shaft flute profile mouth or circle Shape hole axle outer shaft head end card slot (113)；On rotary shaft flute profile mouth or round hole axle outer shaft head end card slot (113), it can set respectively There are rotary shaft flute profile mouth or round hole axle unofficial biography dynamic crankshaft swing angle axis (111)；Outside rotary shaft flute profile mouth or round hole axle Be driven d-axis swing angle axis (112), constitute the ensuring smooth transmission after being connected between each rotary shaft and head both ends, it is easy to assembly, Use the manipulation of safe and reliable property.

On each region valve body plate main body module sub-unit (73) of jet runway, it is equipped with universal globe shell type gas-sparging head list Sleeve or double telescopic sub-units (114)；Universal globe injector head outward flange disk seat fixing bolt (141)；If being mounted in aircraft carrier first Plate is carrier-borne or each dedicated jet runway (191) in airport on；

The universal globe shell type gas-sparging head list sleeve or double telescopic sub-units (114), in universal globe shell type gas On injector head list sleeve or double telescopic sub-units (114), fixing seat (116) are positioned outside equipped with universal globe injector head；With ten thousand To spherical sleeve type injector head flange seat (115)；Jet appendix single sleeve (136) are oriented to universal globe injector head；With ten thousand To spherical surface injector head or inside and outside rotary sleeve sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or pneumatically regulate and control jet Pressure relief valve sub-unit (137)；

It is described on the valve body plate main body module sub-unit (73) in each region of jet runway, be respectively equipped with outside universal globe injector head It positions fixing seat (116)；With universal globe injector head outward flange disk seat fixing bolt (141)；It is solid with longitudinal motor or pneumatic linear actuator Fixed rack (121)；And universal globe injector head guiding leading screw or guiding pneumatic control thick stick fixed plate (126)；

It is described to be positioned outside universal globe injector head on fixing seat (116), it is respectively equipped with universal globe injector head rotary oscillation ball Surface cover seat is fixed inner shield ring (117)；Spherical surface set fixing seat (118) is swung with universal globe jet port spinning ball；And multi-directional ball Face jet port rotary oscillation spherical surface body (119)；Constitute universal globe shell type rotary oscillation 0-360 degree can angle-adjustable, spray The connection and flexible manipulation and control of the fixation position for body sub-unit entirety of emanating；

It is described in universal globe jet port rotary oscillation spherical surface body (119), be respectively equipped with universal globe shell type injection head flange Seat (115)；Jet appendix single sleeve (136) are oriented to universal globe injector head；With universal globe injector head or interior outward turning Shaft covers sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or pneumatic regulation whiff pressure graduated release valve sub-unit (137)；Constitute universal globe shell type rotary oscillation 0-360 degree can angle-adjustable, realize that injection gas sub-unit is whole The safer manipulation and control of gas source control system；

It is described to be positioned outside universal globe injector head on fixing seat (116), it is respectively equipped with longitudinal motor or the fixed bracket of pneumatic linear actuator (121)；Motor is driven with lateral driving lever or the transmission of Pneumatic extension cylinder pushes driving lever (122)；It is controlled with longitudinal motor or pneumatic linear actuator (123)；

Described to control on (123) in longitudinal motor or pneumatic linear actuator, longitudinal dial can arbitrarily be adjusted by being respectively equipped with universal globe 0-360 degree Actuator push rod (120) are stretched in moving gear or pneumatic control；With universal globe injector head guiding leading screw worm gear pairs or guiding air valve control Processed group (127)；

It is described to be positioned outside universal globe injector head on fixing seat (116), it is respectively equipped with universal globe injection headstock gasket (124)；With universal globe injector head locknut (125)；It is fixed with universal globe injector head guiding leading screw or guiding pneumatic control thick stick Plate (126) constitutes universal globe shell type rotary oscillation 0-360 degree, can arbitrarily adjust each angle injection gas gas sub-unit entirety Fixed support and control；

It is described universal globe injector head guiding leading screw or guiding pneumatic control thick stick fixed plate (126) on, be respectively equipped with multi-directional ball Face injector head guiding leading screw worm gear pairs or guiding Air Valve Control group (127), with universal globe injector head guiding leading screw or guiding gas Valve controls flexible thick stick (128) and universal globe injector head guiding locking screw (129) and universal globe injector head guiding is lived Network support plate swings linking arm pin shaft and plum blossom latch card (134), is oriented to active support plate with universal globe injector head and swings company It connects arm (130) and universal globe injector head is oriented to active support plate and swings linking arm sliding pin (131), sprayed with universal globe It penetrates head and is oriented to active support plate swing linking arm adjustment upper arm reinforcing rib (132) and the active support of universal globe injector head guiding Plate swing linking arm pin hole (133) constitute universal globe shell type rotary oscillation 0-360 degree can angle-adjustable, and will injection The control of gas entirety, and reliable and stable control when transmission guide swinging；

It is described to be oriented on jet appendix single sleeve (136) in universal globe injector head, it is respectively equipped with universal globe injector head It is oriented to active support plate and swings linking arm driving lever support base (135), with universal globe injector head or inside and outside rotary sleeve sleeve groove Shape mouth or each region electromagnet cut off valve of circle hole shape mouth or pneumatic regulation whiff pressure graduated release valve sub-unit (137) and universal globe Injector head is oriented to active support plate and swings linking arm pin hole (133), is oriented to active support plate with universal globe injector head and swings Linking arm adjusts upper arm reinforcing rib (132) and universal globe injector head is oriented to active support plate and swings linking arm sliding pin (131) and universal globe injector head is oriented to active support plate and swings linking arm (130) and the guiding work of universal globe injector head Network support plate swings linking arm pin shaft and plum blossom latch card (134), constitutes extraneous input gas source to spraying gas source in jet runway Normal safe landing control, and the reliable manipulation of active support plate flexible swinging is oriented to universal globe injector head；

It is described that the both ends that active support plate swings linking arm (130) are oriented in universal globe injector head, it is active to be respectively equipped with guiding Support plate swings lateral pressure swivel bearing (138) inside and outside linking arm or rotary sleeve sleeve；It is swung being oriented to active support plate Inside and outside linking arm or rotary sleeve sleeve in lateral pressure swivel bearing (138), it is equipped with universal globe injector head and is oriented to active branch Fagging swings linking arm pin shaft and plum blossom latch card (134), and constituting universal globe shell type rotary oscillation 0-360 degree can arbitrarily adjust Angle, and whole the fixing of injection gas are supported and are controlled the guiding movement more flexibility of gas；

It is described on the valve body plate main body module sub-unit (73) in each region of jet runway, be respectively equipped with outside universal globe injector head It positions fixing seat (116)；It positions on fixing seat (116), is respectively equipped with outside universal globe injector head outside universal globe injector head Flange holder fixing bolt (141)；

It is described in universal globe injector head or inside and outside rotary sleeve sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or On pneumatic regulation whiff pressure graduated release valve sub-unit (137), it is respectively equipped with universal globe injector head guiding jet appendix list set Cartridge type (136), with compressed air gas source blowing mouth or the quick plug receptacle seat (139) of hose connector；Constitute extraneous input gas source pair The normal safe landing supportive control of injection gas source in jet runway；

It is described on universal globe shell type gas-sparging head list sleeve or double telescopic sub-units (114), be equipped with universal globe spray Penetrate pressure locking block set (209) of collaborating under turnbarrel in the double sleeves of head；The turnbarrel in the double sleeves of universal globe injector head Under collaborate in pressure locking block set (209), be respectively equipped with turnbarrel waterproof and dustproof in the double sleeves of universal globe injector head, anti- Turnbarrel collaborates downwards pressure buffer bearing (211) in frozen oil envelope or the double sleeves of packing (208) and universal globe injector head, Pressure locking block set (209) is collaborated outside under turnbarrel in the double sleeves of universal globe injector head, is equipped with universal globe injector head Buffing pad (210) on turnbarrel in double sleeve fixed sleeves cylinders；In the double sleeve fixed sleeves cylinder inward turnings of universal globe injector head On rotaring sleeve outside buffing pad 210, it is equipped with universal globe jet port rotary oscillation spherical surface body (119), constitutes universal globe injector head Turnbarrel flexible rotation and 360 degree of swings and dust-proof, anti-water management in double bush outer sleeve cylinders are fixed；

It is described on universal globe shell type gas-sparging head list sleeve or double telescopic sub-units (114), be respectively equipped with multi-directional ball The double sleeve fixed sleeves cylinders (212) of face injector head, with single sealing gland or the packing of collaborating on universal globe injector head inside and outside sleeve (213) slot (214) and universal globe injector head inside and outside sleeve in the defeated deflation of turnbarrel and in universal globe injector head Middle part is collaborated single sealing gland or packing (215), constitute in universal globe injector head turnbarrel flexible rotation and fixed sleeves cylinder it Between leakproofness control；

It is described on universal globe shell type gas-sparging head list sleeve or double telescopic sub-units (114), be respectively equipped with multi-directional ball Face injector head fixed sleeves cylinder gas transmission air inlet (217) open in usual；In the gas transmission open in usual of universal globe injector head fixed sleeves cylinder In air inlet (217), it is equipped with turnbarrel (225) in the double sleeves of universal globe injector head；In the double sleeves of universal globe injector head On interior turnbarrel (225), air inlet blowing mouth (216) and universal globe in turnbarrel are equipped in universal globe injector head It collaborates under injector head inside and outside sleeve double sealing glands or packing (218), constitutes the normal injection in defeated ventilation source and the normal opening of gas source With the flexible control of the normal leakproofness for closing gas source and gas source；

It is described on turnbarrel (225), to be equipped with turnbarrel in universal globe injector head in the double sleeves of universal globe injector head It collaborates compressive resistance buffering bearing (219), collaborates upwards anti-pressure locking flange with turnbarrel in universal globe injector head upwards Turnbarrel in turnbarrel locking screw tooth (221) and universal globe injector head in nut (220) and universal globe injector head Turnbarrel swing arm (223) in swing arm fixing bolt (224) and universal globe injector head, with universal globe injector head inward turning Rotaring sleeve swing arm pushes and pulls bulb (222), constitutes the flexible control of the rotation input gas source of interior turnbarrel and fixed sleeves cylinder, Swing angle it is accurate, reliable；

It is described on universal globe injector head fixed sleeves cylinder gas transmission air inlet (217) open in usual, be equipped with each valve body plate module in Soft or hard snorkel is coupled quick combination hub (169), with the defeated soft or hard coupling connecting tube of deflating of nominal gas jet port in runway (157), and can 360 degree rotation swing nominal gas jet port electromagnet cut off valve switch in connecting bend (162) and runway (151), the normal on and off of defeated ventilation source is constituted.

The interior lower part in each region valve body plate main body module sub-unit (73) of jet runway, is respectively equipped in runway and normally stores up Store gas bucket (146), with runway in emergency storage deflation bucket (147), in jet runway normal storage deflation bucket (146), with In runway in emergency storage deflation bucket (147), refrigeration, heating sensing modulator (207) being respectively provided with, acting on, which can guarantee, is run Gas source used in the enough landing aircrafts of flow that each jet port in road sprays, and guarantee that runway pavement can be made under cold, tropical environment Temperature Normal Take-Off And Landing aircraft, constituting whole jet runway, normally the safety of safe landing is grasped in misty rain, ice and snow or hot weather Vertical control；

The interior lower part in each region valve body plate main body module sub-unit (73) of jet runway is respectively equipped with multiple main gas of conveying Deflation bucket appendix (143) are stored in source Quick connector plug (142) and more runways, are put with normal storage in multiple runways Emergency storage deflation bucket check valve (145), controls the general gas of each autonomous system in gas bucket check valve (144) and multiple runways It can still Normal Take-Off And Landing, the gas supply air supply machine for constituting whole jet runway be driven when source and the switching of individual gas sources system or failure The safety guarantee of control, circuit system control；

The interior lower part in each region valve body plate main body module sub-unit (73) of jet runway, is respectively equipped in jet runway just Air pressure is regarded outside normal storage deflation bucket in often storage deflation bucket (146), with emergency storage deflation bucket (147) in runway and runway Normal injection gas pressure regulation in air gauge (149) and runway is regarded outside emergency storage deflation bucket in table (148) and runway to cut Emergency injection gas tune in only valve (150), with nominal gas jet port electromagnet cut off valve switch (151) in runway and runway In pressure cutoff valve (152) and runway in emergency gas ejection ports electromagnet cut off valve switch (153) and runway normally with emergency Gas source switching electromagnet cut off valve switch (154) in deflation bucket is stored, guarantees the normal control of each air supply source；

It is described in the interior lower part of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped in runway normally with answer Anxious storage deflation bucket current collecting tier gas supply check valve (155), deflation bucket is compressor gas supplied unidirectional with normally storing with emergency in runway Emergency gas injection in nominal gas jet port defeated deflate soft or hard coupling connecting tube (157) and runway in valve (156) and runway Normal storage deflation bucket is mutually ventilated soft or hard coupling connecting tube in mouthful defeated deflate soft or hard coupling connecting tube (158) and runway (159), it mutually ventilates soft or hard coupling connecting tube (160) with emergency storage deflation bucket in runway, composition can each gas source of safety assurance The normal gas supply of constant-pressure stable can the more selective distribution control to gas source；

The interior lower part in each region valve body plate main body module sub-unit (73) of jet runway, is respectively equipped with gas in jet runway Body pressure regulation stop valve and electromagnet cut off valve switch connection outside screw (161), and can 360 degree rotation swing connecting bend (162), with race Laterally defeated snorkel (163) and the interior emergency gas ejection ports Universal-head of runway are laterally defeated for nominal gas jet port Universal-head in road Snorkel (164) meets an urgent need gas ejection ports Universal-head laterally on defeated snorkel (164) in runway, is respectively equipped with intellectual system Fork sliding sleeve (165) is stirred in the swing of nominal gas jet port transverse pipe in cold, heating sensing modulator (207) and runway, and is run Fork sliding sleeve (166) is stirred in gas ejection ports transverse pipe of meeting an urgent need in road swing, and normally stifled with emergency transverse pipe sealing-plug in runway (167), it is ensured that the normal output and the landing of runway pavement normal temperature of each air supply system；

It is described on the low inside of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with jet runway Inside normally with meet an urgent need and storage deflation bucket electromagnet cut off valve interval freewheeling diode (168)；It is soft or hard in each valve body plate module of runway Snorkel is coupled quick combination hub (169)；Fork (170) normally are stirred with emergency transverse pipe swing in runway；In runway normally with Fork connection locking plate (171) is stirred in emergency transverse pipe swing；In runway normally with emergency transverse pipe swing stir fork locking plate with Handspike fixing bolt (172), it is ensured that the constant and transverse pipe swinging fork angle of each storage deflation bucket air pressure is controlled positive and negative In the range of 0.5 degree of angle, constituting can the more smart accurate flexible effect of safe landing using gas source and saving gas source.

It is described on the low inside of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped in runway just The mechanically automatically controlled travel switch (173) of normal jet port advance stop；Normal injection mouth retreats the mechanically automatically controlled row of stop in runway Cheng Kaiguan (174)；The emergency mechanically automatically controlled travel switch (175) of jet port advance stop in runway；Emergency jet port in runway Retreat the mechanically automatically controlled travel switch (176) of stop, it is ensured that spare and setting after angle sensor Signal-controlled switch failure A kind of stroke electric-controlled switch constitutes the artificial intelligence control of dual fail-safe circuit-mode；

It is described on the low inside of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped in runway just The normal jet port advance automatically controlled travel switch of stop artificial intelligence formula (177)；Normal injection mouth retreats stop artificial intelligence in runway The automatically controlled travel switch of formula (178)；The automatically controlled travel switch of jet port advance stop artificial intelligence formula (179) are met an urgent need in runway；Runway Interior emergency jet port retreats the automatically controlled travel switch of stop artificial intelligence formula (180), it is ensured that the accuracy of each jet port angle is constituted It controls to form mechano-electronic dual fail-safe circuit-mode and artificial intelligence manipulation and control with electronic signal sensitive switch；

It is described on the low inside of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped in runway just Normal jet port advances and retreats artificial intelligence formula angle sensor controller (181)；Emergency jet port advances and retreats people in runway The intellectual angle sensor controller (182) of work；Normal servo motor impeller-hub feed rod connection locking transition plates (183) in runway； Emergency servo motor impeller-hub feed rod connection locking transition plates (184) in runway；Normal servo motor or promotion oil cylinder in runway (185)；Emergency servo motor or promotion oil cylinder (186) in runway；In runway normally with emergency impeller-hub feed rod (187)；Runway Inside normally with emergency impeller-hub feed rod guiding axis sliding sleeve (188), optimum efficiency can normal each jet port institute of artificial intelligence control Timing, level pressure, quantitative gas needed for the various required precise angles ejected, the safety for reaching 100% to landing aircraft rise Drop；

The shape chamber in jet runway valve body plate main body module sub-unit (73) inside casing, under interior lower outer portion jet runway pavement It is respectively equipped in the melt pit on portion basis；Normally with emergency and spare three sets independent manuals intelligence and can mutual numerical control switch The non-control system of new model of air supply system, power supply system, the various safety operation control systems of flight control system and safety is run in jet In road melt pit, it is respectively equipped with runway auxiliary equipment compressor air accumulator air supply system (189)；Current collecting tier gas storage cylinder air supply system (190)；On current collecting tier gas storage cylinder air supply system (190), the refrigeration, heating sensing modulator (207) that are equipped with；Low pressure is colored Gas and the preheating main gas ejection ports of oxygen (226), act on the Normal Take-Off And Landing that can guarantee on runway.The jet runway can be used as school Fly the pneumatic dynamic of various actual measurements of examination new architecture aircraft and the static state that various actual measurements are pneumatic, this runway is that the field is optimal One detection school flies equipment line, can reach 100% accurately actual measurement and goes out；By itself can be produced in jet runway it is various can To on extraneous landing aircraft environment runway pavement, can release various one hundred point than the oxygenation processed of different proportion, anoxic processed, refrigeration, Heating, making drugs into frostlike powder, system are avenged, are made ice, rain processed, manufacture cyclone, manufacturing the functions such as various random wind, can be flown to various coming of new factory Machine model-performance and the landing Test And Checkout of technical standard and various technical parameters on jet runway；

It is described in the shape chamber of jet runway valve body plate main body module sub-unit (73) interior frame bottom, be respectively equipped with inside and outside runway The right side intellectual air control switch of air curtain normal injection gas solenoid valve (227)；And the external right side air curtain normal injection gas in runway On the intellectual air control switch of body solenoid valve (227), it is equipped with the intellectual Regulation Control of external right side air curtain normal injection gas in runway Valve (228)；It is additionally provided with external right side air curtain emergency injection gas solenoid valve air control switch (229) in runway simultaneously；And in runway In external right side air curtain emergency injection gas solenoid valve air control switch (229), it is equipped with external right side air curtain emergency injection gas in runway Intellectual Regulation Control valve (230)；In runway external right side normally with the longitudinal defeated snorkel of emergency air curtain Universal-head jet port (231)；Longitudinally fork sliding sleeve (232) is stirred in defeated snorkel swing with left and right sides air curtain Universal-head jet port inside and outside runway, maximum Actual effect prevents bad interference of the runway external right side wind to Normal Take-Off And Landing of the landing aircraft in runway when；

It is described in the shape chamber of the interior frame bottom of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with race The inside and outside left side intellectual air control switch of air curtain normal injection gas solenoid valve (233) in road；And left side air curtain is normal inside and outside runway It sprays on the intellectual air control switch of gas solenoid valve (233), is equipped with the inside and outside left side intellectual tune of air curtain normal injection gas of runway Pressure control valve (234)；And it is additionally provided with the inside and outside left side air curtain emergency injection intellectual air control switch of gas solenoid valve of runway (235)；And the left side air curtain emergency injection intellectual air control switch of gas solenoid valve (on 235) inside and outside runway, it is equipped in runway The outer left side air curtain emergency injection intellectual Regulation Control valve (236) of gas；It is normally universal with emergency air curtain with left side inside and outside runway Longitudinally defeated snorkel (237), maximum actual effect are to prevent the outer left side wind of runway to landing aircraft in runway to head jet port The bad interference of left side wind outside the road landing Shi Dui；

It is described in the shape chamber of the interior frame bottom of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with race Communication far infrared and spectrum or Beidou intelligent sensing controller (238) are normally received in road, are received and are communicated far with emergency in runway It is infrared between spectrum or Beidou intelligent sensing controller (239), the navigation of three's far and near distance can mutually switch, and various Flying object cannot any, arbitrarily, freely rise and fall on jet runway, which has intelligence software to recognize it various flyers Receive function naturally after knowing difference, and to the global navigation locating function of mobile flyer, especially to various guided missiles Commit suiside unmanned plane or have it is man-machine attack, which can lead its various unacquainted various unmanned plane or someone's aircraft The flyers such as bullet quickly exclude to blow winged, effectively protect the great advantage of the safe normal operation of jet runway；

It is described in the shape chamber of the interior frame bottom of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with race Left and right sides and the green instruction lamp driver of middle left and right sides reddish yellow input six hole power sockets (240) inside and outside road, and coupled runway is right Reddish yellow green indicator light wiring conversion terminal (242) in side in the green indicator light wiring conversion terminal (241) of outside reddish yellow and the runway right side, And the green indicator light wiring conversion terminal (243) of the left side reddish yellow of runway and the green indicator light wiring of runway left-external side reddish yellow are transferred Terminal (244), maximum efficiency be can normal supply each group indicator light power supply, and night landing it is safer to pilot wake up Mesh；

It is described in the shape chamber of the interior frame bottom of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with spray Gas runway normally inputs four hole power sockets (245) with emergency air curtain electromagnetic valve circuit with emergency main jet port and normally, with runway Interior right outside is normally with emergency main jet port and normally and in each solenoid valve control connecting terminal (259) of emergency air curtain and runway It is normally normally led with emergency with left in each solenoid valve control wiring conversion terminal (260) of emergency main jet port and runway in the right side Each solenoid valve wiring conversion terminal (261) of puff prot, in runway left-external side normally with emergency main jet port and normally with gas of meeting an urgent need Each solenoid valve wiring conversion terminal (262) of curtain；Its maximum efficiency is to guarantee that each electric-controlled parts and electronic signal can have just it The control of normal safety standard；

It is described in the lower part shape chamber of each region valve body plate main body module sub-unit (73) bearing wall and frame structure of jet runway, respectively Equipped in runway normally with emergency gas receiver solenoid valve x far-infrared spectrum x Beidou x heat tracing line input five hole power sockets (246), and In runway normally with it is normal in emergency gas receiver solenoid valve x far-infrared spectrum x Beidou x heat tracing line connecting terminal (263) and runway With emergency gas receiver solenoid valve x far-infrared spectrum x Beidou x heat tracing line connecting terminal (264), maximum efficiency is to guarantee gas source 100% there can be a good normal temperature control to runway for giving the accurate and ice and snow of navigation signal, combustion hot weather Adjustment；

It is described in the lower part shape chamber of each region valve body plate main body module sub-unit (73) bearing wall and frame structure of jet runway, respectively It normally pushes the 1-2 servo motor of main injection port to input in four hole power sockets (247) and runway equipped with runway normally to push No. 1 servo motor of main jet port front and rear angles connects on 1-2 contact wiring conversion terminal (265), to control No. 1 servo motor A closed circuit and runway in normally push No. 2 servo motors of main injection port front and rear angles to meet the 1- on 4-5 contact 2-3 connects to be laid flat on wiring conversion terminal (266) in deflector, for a closed circuit for controlling No. 2 servo motors, effect Ensure the normal power supply of each servo motor；

It is described in the lower part shape chamber of each region valve body plate main body module sub-unit (73) bearing wall and frame structure of jet runway, respectively It pushes the 3-4 servo motor of main injection port to input in four hole power sockets (248) and runway equipped with runway emergency and answers hitch Dynamic No. 3 motors of main injection port front and rear angles connect on the wiring conversion terminal (267) of 1-2 contact, to control No. 3 servo motors A closed circuit and runway in emergency push No. 4 servo motors of main injection port front and rear angles to meet 1-2 point 3-4-5 and connect to lead On the wiring conversion terminal (278) that flowing plate erects, for a closed circuit for controlling No. 4 servo motors, effect ensures respectively to watch Take the control of the normal defeated power supply of motor；

It is described in the lower part shape chamber of each region valve body plate main body module sub-unit (73) bearing wall and frame structure of jet runway, respectively No. 1 servo motor is controlled equipped with main jet port front and rear angles normal in runway to input in four hole power sockets (249) and runway normally Main jet port front and rear angles control No. 1 servo motor wiring conversion terminal (268), before and after normal main jet port in control runway Angle pushes the closed circuit of No. 1 servo motor signal transducer, and normal main jet port front and rear angles control No. 2 servos in runway Motor inputs normal main jet port front and rear angles in four hole power sockets (256) and runway and controls No. 2 servo motor wiring change-over terminals Sub (269) control No. 4 servo motors with main jet port front and rear angles of meeting an urgent need in runway and input four hole power sockets (257), in runway Main jet port front and rear angles of meeting an urgent need control No. 4 motor wiring conversion terminals (277), main jet port front and rear angles control of meeting an urgent need in runway It makes No. 3 servo motors and inputs emergency main jet port front and rear angles No. 3 servo motors of control in four hole power sockets (250) and runway Wiring conversion terminal (270), effect are guarantee input power and various electronic signal sensors normal；

It is described in the lower part shape chamber of each region valve body plate main body module sub-unit (73) bearing wall and frame structure of jet runway, respectively Six hole power sockets (251) and runway are inputted close to No. 1 servo motor sensitive switch equipped with close or retrogressing is normally advanced in runway Interior normal close or retrogressing of advancing is close to No. 1 servo motor sensitive switch wiring conversion terminal (271), before normal in runway Into it is close or retreat inputted in six hole power sockets (255) and runway close to No. 2 servo motor sensitive switches normally advance it is close or It retreats close to No. 2 servo motor sensitive switch wiring conversion terminals (272), and connects emergency in runway and advance close or retreat close No. 3 servo motor sensitive switches input emergency in six hole power sockets (252) and runway and advance close or retreat close to No. 3 servos Emergency is advanced to approach or retreat and be opened close to No. 4 servo motor sensings in motor sensitive switch wiring conversion terminal (273) and runway It closes six hole power sockets (254) of input and the interior emergency of runway is advanced close or retreated close to No. 4 servo motor sensitive switch wiring turn Connecting terminal (274), effect ensure each puff prot angle of normal control of the power supply and intelligent signal of each servo motor；

It is described in the lower part shape chamber of each region valve body plate main body module sub-unit (73) bearing wall and frame structure of jet runway, respectively Four hole power sockets (253) are inputted equipped with connecing air compressor and connecing current collecting tier, and connects compressor and connects current collecting tier gas supply electromagnetic valve Wiring conversion terminal (275) under gas control, and connect compressor and connect wiring conversion terminal on current collecting tier gas supply electromagnetic valve gas control (276), maximum efficiency can guarantee the match control of the normal gentle source stream of power supply；

It is described in the lower part shape chamber of jet runway valve body plate main body module sub-unit (73) bearing wall and frame structure, be respectively equipped with pre- Road deflector erects input and is laid flat six hole power sockets (258) of input with pre- road deflector, before emergency pushes main jet port in runway No. 4 servo motors of angle meet 1-2 point 3-4-5 and connect on the wiring conversion terminal (278) of deflector standing afterwards, are pre- road deflector A vertical automatically controlled closed circuit and pre- road deflector erect input and are laid flat six hole power sockets of input with pre- road deflector (258), No. 2 servo motors of main injection port front and rear angles are normally pushed to connect on 4-5 contact in runway, 1-2-3, which connects, to be led Flowing plate is laid flat on wiring conversion terminal (266) position, an automatically controlled closed circuit being laid flat for pre- road deflector；

It is described to be slided with efficient short distance or the dedicated jet runway of VTOL aircraft, in type aircraft carrier deck, naval vessel, the spray of land and water platform Gas runway device includes that type aircraft carrier deck is carrier-borne or first the dedicated jet runway (191) in each airport, runway region are to the 7th Region electromagnet cut off valve or pneumatic regulation whiff pressure graduated release valve (200)-(206), carrier-borne in type aircraft carrier deck or each airport is dedicated Slided on jet runway (191), equipped with carrier-borne aircraft the 60-80 rice long (197) into jet runway, on continental rise airfield runway, land On base sky body panel runway, land and water fix or mobile independent air bags platform runway on, naval vessel ship side left or right side or stern end On portion's extension type air bag platform runway, the jet runway of the multi-purpose landing aircraft of sea Lu Pingtai is constituted.

It is described to use a variety of gas supply gas sources, form that gas laminar flow short distance is slided or VTOL flies by compressed air gas injection On machine or the dedicated each region of jet runway of unmanned plane, it is equipped with that type aircraft carrier deck is carrier-borne or each dedicated jet runway (191) in airport；It is navigating Female deck is carrier-borne or each dedicated jet runway (191) in airport on, be respectively equipped with it is seven 20 meters long, 140 meters × 30 meters of overall length wide or 40 meters of wide type aircraft carrier decks are carrier-borne or each dedicated jet runway in airport, also may make up airport, the land and water platform in various environment areas Etc. the jet runway of multi-purpose landing aircraft；

It is described when carrier-borne aircraft is when taking off, when carrier-borne aircraft is slided into 20 meters long (192) of jet runway；The carrier-borne aircraft that takes off slides When into 40 meters long (193) of jet runway；When the carrier-borne aircraft that takes off is slided into 60 meters long (194) of jet runway；Take off warship When carrier aircraft is slided into 80 meters long (195) of jet runway；At this moment the carrier-borne aircraft that takes off is carrier-borne or each airport is dedicated in type aircraft carrier deck On jet runway (191), constitutes and be detached from the outstanding support of the gas of dedicated jet runway and jet runway when second-mission aircraft takes off By departing aeroplane accelerate to nature flying speed and height, realize departing aeroplane safely and fast naturally flight, constitute The lift-off of quickly taking off of jet runway paving take-off-helping aircraft；

It is described in carrier landing landing, be first when carrier-borne aircraft is slided into 20-40 rice long (196) of jet runway The film grade laminar gas at a 45 degree of angles blocks landing, warship carrier-borne aircraft when sliding into 60-80 rice long (197) of jet runway, Constituted the film grade laminar flow at second 45 degree of angle that carrier-borne aircraft blocks, at this moment warship carrier-borne aircraft continue to slide into jet runway When 100-120 meters long (198), the film grade laminar gas for having constituted third 45 degree of angles blocks landing, warship carrier-borne aircraft in aircraft carrier Deck is carrier-borne or each dedicated jet runway (191) in airport on, constituted various airport aircrafts or ship-board aircraft in warship landing It slides and enters on 140 meters long (199) on jet runway, realize the outstanding support formula of the naturally stable gas of safety and block landing, structure The outstanding support of gas when landing aircraft is helped at jet runway paving or is blocked；

It is described type aircraft carrier deck is carrier-borne or each dedicated jet runway (191) in airport on, be respectively equipped with first region electromagnetism of runway Shut-off valve or pneumatic regulation whiff pressure alleviate valve assembly (200), runway Two Areas electromagnet cut off valve or pneumatic regulation spray Atmospheric pressure alleviates valve assembly (201), runway third region electromagnet cut off valve or pneumatic regulation whiff pressure and alleviates valve assembly (202), the 4th region electromagnet cut off valve of runway or pneumatic regulation whiff pressure alleviate the 5th valve assembly (203), runway area Domain electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly (204), the 6th region electromagnet cut off valve of runway or pneumatic Regulate and control whiff pressure and alleviates valve assembly (205), the 7th region electromagnet cut off valve of runway or pneumatic regulation whiff pressure graduated release valve Assembly (206) is constituted to carrier-borne or each airport seven region electromagnet cut off valve of dedicated jet runway or pneumatic regulation and air pressure quilt The safety distribution manipulation of constant pressure after alleviation；

The aircraft is when taking off, the auto-control situation of change of each region atmospheric pressure of runway：When departing aeroplane is slided to first When a area, valve assembly (200) are alleviated by first region electromagnet cut off valve or pneumatic regulation whiff pressure, first region is whole The air pressure of body gas source is adjusted to 2-3 technical atmosphere；When departing aeroplane is slided to second area, by Two Areas electromagnetism Shut-off valve or pneumatic regulation whiff pressure alleviate valve assembly (201), and the air pressure of second region entirety gas source is adjusted to 3- 4 technical atmospheres；When departing aeroplane is slided to third area, by third region electromagnet cut off valve or pneumatic regulation jet pressure Power alleviates valve assembly (202), and the air pressure of third region entirety gas source is adjusted to 4-5 technical atmosphere；Work as departing aeroplane When sliding to the 4th area, valve assembly (203) are alleviated by the 4th region electromagnet cut off valve or pneumatic regulation whiff pressure, it will The air pressure of 4th region entirety gas source is adjusted to 5-6 technical atmosphere；When departing aeroplane is slided to the 5th area, by Five region electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly (204), by the 5th region entirety gas source Air pressure is adjusted to 6-7 technical atmosphere；When departing aeroplane is slided to the 6th area, by the 6th region electromagnet cut off valve or gas Dynamic regulation whiff pressure alleviates valve assembly (205), and the air pressure of the 6th region entirety gas source is adjusted to 7-8 engineering gas Pressure；When departing aeroplane is slided to the 7th area, the 7th region electromagnet cut off valve or pneumatic regulation whiff pressure graduated release valve are total At (206), the air pressure of the 7th region entirety gas source is adjusted to 8-10 technical atmosphere, constitutes carrier-borne aircraft in jet runway On when taking off, seven region entirety gas sources on runway alleviated after air pressure, protect the distribution pressure constancy in each region forever Regulated and controled by artificial intelligence.Used on jet runway 10-25 technical atmosphere to take off carrier-borne aircraft when operating condition various controls, It constitutes jet runway to board a plane when taking off, the air pressure in each region is incremental；

The aircraft is when warship lands, the auto-control situation of change of each region atmospheric pressure of runway：When landing aircraft taxi extremely When first region, valve assembly (200) are alleviated by first region electromagnet cut off valve or pneumatic regulation whiff pressure, by first The air pressure of region entirety gas source is adjusted to 8-10 technical atmosphere；When land aircraft taxi to Two Areas when, by second A region electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly (201), by the gas of second region entirety gas source Pressure is adjusted to 7-8 technical atmosphere；When land aircraft taxi to third region when, by third region electromagnet cut off valve or gas Dynamic regulation whiff pressure alleviates valve assembly (202), and the air pressure of third region entirety gas source is adjusted to 6-7 engineering gas Pressure；When land aircraft taxi to the 4th region when, alleviated by the 4th region electromagnet cut off valve or pneumatic regulation whiff pressure The air pressure of 4th region entirety gas source is adjusted to 5-6 technical atmosphere by valve assembly (203)；When landing aircraft taxi extremely When the 5th region, valve assembly (204) are alleviated by the 5th region electromagnet cut off valve or pneumatic regulation whiff pressure, by the 5th The air pressure of region entirety gas source is adjusted to 4-5 technical atmosphere；When land aircraft taxi to the 6th region when, by the 6th Region electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly (205), by the air pressure of the 6th region entirety gas source It is adjusted to 3-4 technical atmosphere；When land aircraft taxi to the 7th area Ge Yu when, by the 7th region electromagnet cut off valve or pneumatic Regulate and control whiff pressure and alleviate valve assembly (206), the air pressure of the 7th region entirety gas source is adjusted to 2-3 technical atmosphere, Constitute to it is carrier-borne on jet runway warship when runway on seven region entirety gas sources distribution pressure；It is adopted on jet runway Operating condition when with 10-25 technical atmosphere constitutes the air pressure in each region in landing of boarding a plane of jet runway and successively decreases.

Before and after each puff prot in each region on jet runway longitudinal direction, it is all respectively equipped with low pressure colored gas and pre- The hot main gas ejection ports of oxygen (226) are constituted to each injection gas laminar flow of adjustment each region high pressure spray loophole of jet runway The actual height of ray, with angle can vision whether reach within the scope of the various Aircraft Standards of landing.

To sum up, the technical scheme adopted by the invention is that：A kind of efficient very-short-reach of band is slided or VTOL sparrow hawk machine or is gone straight up to The various jet stage apparatus of aircraft vertical landing, aircraft carrier, naval vessel, land and water VTOL jet platform or jet very-short-reach are sliding " the takeoff and landing device " of row runway device is equipped, including type aircraft carrier deck, naval vessel, continental rise platform airport, each provincial capital to county, each area under one's jurisdiction In to county, each frontier sentry, logistics, each high mountain, mountain area, basin, tourist district, cavern, island, islands and reefs, air bag floating body waterborne, tremble with fear In band -60 degree subzero, the torrid zone -80 degree of environment above freezing, on ice and snow waters, on Qinghai-Tibet Platean, and the manipulation and control of full intelligence System.It is characterized in that：It is described on type aircraft carrier deck takeoff and landing jet platform or jet runway, each land and water high mountain, mountain area island Large, medium and small type airport takeoff and landing jet platform or jet runway on, equipped with the various gas ejection ports formulas of compressed air The jet runway that can assist the sliding outstanding support formula landing of jump formula aircraft injection gas safely of very-short-reach, can safe secondary injection gas Platform drops in outstanding support Harrier or outstanding hold up of the jet of helicopter VTOL, which sprays the outstanding support platform of gas, can Also can be used as rocket, the not damaged recycling of airship, qi of chong channel ascending adversely wave dynamic as wind (hole) for the personnel that play in park, suspend joy Find pleasure in, fire-fighting suspension lifting gasbag-type 100 meters of fire in high buildings of number are lifesaving bed or lifting gasbag lifesaving column, air bag life chute, lifting air The complete intelligent wisdom lifesaving appliance such as capsule safety ladder.

The jet runway can be used as the various aeroplane performances of the winged test in school and the school of the examination various technical parameter standards of certain aircraft flies Performance test runway up to standard, the jet runway can ban the backwardness skill of currently used original wind tunnel test for a full due Prototype of certain type after scaled, suspension type can only be carried out the quiet dynamic of small-sized micromation by art, original wind tunnel test The various performances of the test of state and various technical parameters, the accuracy rate of testing result can only be 60% effect, especially in test It is long on time, very big etc. various disadvantages of the very high workload of energy consumption cost.The jet runway is in the performance for testing various aircrafts It can be by 1 when standard：1 type directly carries out the various tests of various quiet dynamic free flight landings, can in the jet runway Gas is sprayed to produce the various strong and powerless landings to test aircraft, such as tests aircraft in landing on jet runway Various 0-360 degree angle landing counter blow, forward wind, lateral wind, yaw wind, fitful wind, whirlwind, random wind, flow-disturbing wind etc., wind-force Up to 1-20 grades of Super Typhoon.The jet runway can also produce the strong and powerless burning gases to various engines Test, such as test test of the aircraft in landing on jet runway to the strong and powerless burning gases of various engines；Hair Motivation in the various temperature difference of normal temperature 25-60 degree, the jet runway can produce it is various to engine in normal temperature anoxic Oxygen-depleted gas at 10%, at 20%, at 30%, the jet runway can produce it is various to engine in normal temperature Oxygenation is in 10-30%.For engine when subzero low temperature 25-60 is spent, engine is in subzero low temperature anoxic in 10-30% When, engine is in normal temperature oxygenation in 10-30%.For engine in the case where misty rain different moisture levels, which can 100% fly as school leading in the world, tests out and examines to the various standards of the performance of various new and old aircraft engines and complete machine type Survey standard testing that can be up to standard with the technical parameter for checking and accepting various complete machine types.The jet runway can be used as to various new and old in a word The inspection center of aeroplane performance school Darts standard and acceptance criteria station.

The jet runway school flies to check and accept the inspection center station of new older models, can the 100% current world that banned be known as international mark Runway is surveyed in quasi- various school out-of-competition testings, and the state-of-the-art school in the world is run fast at present, and not all being equipped with itself can be directly to school airplane-type system Wind speed and wind-force needed for producing various 0-360 degree any angles such as can only be at the natural wind angle and wind from daily weather Power, to school fly detection actual effect and on the time it is all too long, most fastly need 1 to two year ability school fly a kind of type, expense several thousand Ten thousand yuan to hundred million yuan are differed, and the school C919 produced such as China flies testing expense and reaches upper several hundred million yuan, and the time needs aptitude test in several years to complete, And the jet runway school flies to check and accept a kind of all test completions of various technical parameters required time most weeks of new architecture, takes With being only the 35% of original runway testing expense, test effect is the decades of times or hundred of original runway with the environment that depends on the weather Times or more.

On the device of above each takeoff and landing platform or very-short-reach jet runway, whirlpool spray, turbofan, axial flow blower are used Formula, air compressor unit etc., it is referred to as a kind of that gas source is supplied by compressed air gas type as the gas supply gas source of various ways. By a certain gas source of above these types gas supply gas source, it is input to dedicated jet runway platform or jet runway of the invention and respectively stores up In gas air supply system, if be mounted in several puff prot formulas of jet runway platform or each artificial intelligence control on jet runway In jet runway, the first is the gas ejection ports with multiple rotary sleeve valve flute profile mouth formulas, and second is with multiple The gas ejection ports of rotary sleeve valve circle hole shape mouth formula, the third is with multiple universal globe shell types without fixed sleeves list set The gas ejection ports of cylinder circle hole shape, the 4th kind is with rotary sleeve in multiple universal globe shell types and the double telescopic circles of fixed sleeves The gas ejection ports of hole shape, above four kinds of structure members are all that vertical type is set on each piece of valve body plate main body module sub-unit 's.Each jet port on (by artificial intelligence control) runway pavement of above four kinds of structures is adjusted to can be reverse, flies to landing Machine integral body lower part gross area body ejects upwards, flies to departing aeroplane and landing two kinds of gas with various pressure of aircraft and landing The gas laminar flow of the various jet angle changes used needed for machine can application solutions landing it is (necessary for departing aeroplane injection gas It is dry gas laminar flow), humidity in dry gas laminar-flow air is small, the small gas blanket of viscous drag to departing aeroplane complete machine body It is big to flow outstanding towing force, humidity of the air humidity no more than 5% in general dry gas laminar flow.

To land on miniature jet runway to the heavy airplane for blocking 1000 tons or more must be the gas laminar flow of moisture content, general Humidity in humidity gas laminar-flow air can reach sliding to wing type no more than the required gas laminar flow of 20%-30% wet type Jump decline aircraft is forming the gas laminar flow containing humidity viscosity membrane resistance with injection wet type gas with complete machine, can increase 25%-35%'s blocks power, and can save 25%-35% blocks gas source, will decline aircraft and quickly lags the outstanding safety of holding in the palm of formula The purpose for blocking landing is realized on very-short-reach runway.Because decline aircraft is not before decline wheel lands, underbelly one Directly with that can hang the strong gas field (negative pressure cushion) for holding in the palm complete machine body, when declining one landing ground of airplane wheel, at this moment strong gas field is complete Portion disappears, and loses the decline aircraft of the outstanding strong gas field negative pressure cushion of support, and moment of inertia when aircraft is declined all switches to jet In each film grade laminar flow folder that runway ejects, the various moments of inertia for declining aircraft are thoroughly disappeared.In the dedicated spray of artificial intelligence On gas runway, when the yaw of takeoff and landing track, bias, inclination are with sink-float up and down, artificial intelligence gas ejection ports are sprayable out It is various hang the gas laminar flow stirred of support landing aircraft is eccentric, yaw, inclination with sink-float up and down when, 100% can come constantly Various tracks when takeoff and landing are corrected to it in ground.Four kinds of artificial intelligence gas ejection ports can 360 degree of angles Intelligent Transformation, and it is each Gas laminar flow that a gas ejection ports are ejected, gas blanket flow, gas pressure, gas flow rate size be all that a point is controllable , it can play promotion weight, height, the speed of a ship or plane and runway each puff prot of the artificial intelligence adjustment to takeoff and landing when and rise Drop aircraft matches coordination and interaction, and the sensor that can constantly set by machine road is constantly repaired and corrected to the various rails of landing aircraft The various effects of the actual tracking of mark are 100%.

A kind of stainless steel material or special steel material, casting can be used in the road face of the very-short-reach jet runway or the material of platform Cause multiple 2.5 meters × 2.5 meters of small cube shape carry a kind of installation of the defeated air passage mechanism of gas storage, dismounting, it is easy to maintenance, The template sub-unit made of muti-piece small cube shape can mutually inlay each region assembled.Another material compares aluminium alloy Intensity is seven times larger, weight ratio aluminium alloy is 3.5 times light, resistance to 80 degree of high temperature, 60 degree of low temperature, resistance are right, frigid zone can be kept the temperature, tropical energy A kind of macromolecule new material die casting of heat-insulated rub resistance forms 2.5 meters × 2.5 meters of small cube template, in each small cube Steel skeleton or dredging feed channel are set in template.Skeleton can also be done using interior steel, aluminium or the stainless steel of setting, outer surface uses glass Steel, composite material and carbon fibre composite, manufacture are used as jet runway at 2.5 meters × 2.5 meters of muti-piece of small cube shape etc. Interior shape skeletal support body, carry in vivo defeated ventilation pipe mechanism, made of multiple 2.5 meters × 2.5 meters of small cube shapes Template is known as：The die casting of muti-piece macromolecule new material, aluminum alloy materials are cast, are stainless by runway valve body plate main body module sub-unit Steel material casting, cast steel material casting, glass fiber reinforced plastics composite material manufacture and carbon fibre composite, select a certain kind therein Optimal material manufacture mutually inlays each region assembled at multiple small cube shape template sub-units；Again by each region gas circuit system After system, electronic circuit system, mechanical connection system, transmission system and flight control system are connected with each other, then by each region combination-inlaying The very-short-reach jet runway device for connecting into a wing type, sliding takeoff and landing formula, a kind of VTOL Harrier or Helicopter sprays outstanding hold up of gas and drops stage apparatus referred to as " takeoff and landing device " equipment.It is described, very-short-reach jet runway dress It sets or vertically sprays gas landing stage apparatus and be connected with the management system of artificial intelligence.

The very-short-reach jet runway device is by whirlpool spray, turbofan, axial flow blower, compressed air gas injection as core Push the energy.It is that a kind of slide for wing type jumps aircraft during take-off and landing, and used injection gas laminar flow can play absolutely A kind of efficient, very-short-reach jet plane landing runway of the leading effect of security control.The jet runway is by multiple small sides A very-short-reach jet runway made of block shape template sub-unit combination-inlaying, and be designed in every piece of small cube template： With multiple moving sleeve valve flute profile mouth formula gas ejection ports, or multiple moving sleeve valve circle hole shape mouth formula gas ejection ports are had, or With multiple universal globe shell types without fixed sleeves valve circle hole shape gas ejection ports, with rotary sleeve in universal globe shell type with The gas ejection ports of fixed sleeves valve circle hole shape.Above four kinds of gas ejection ports are set respectively and are sprayed mounted in each very-short-reach landing On gas template runway, the design length and width of jet runway can need to set according to each airport landing type size, can also If fill a kind of standard type airfield runway can compatible large, medium and small type aircraft or unmanned plane, sparrow hawk formula machine, helicopter can rise The jet runway platform of drop.

Very-short-reach jet runway is each piece of valve body plate main body module point made of 2.5 meters × 2.5 meters of muti-piece small cube shape Assembly mutually inlays each region assembled, each region can be set as respectively it is 5 meters long, 10 meters long, 20 meters long, 30 meters It is long, 40 meters long, 50 meters long, 60 meters long, 70 meters long, 80 meters long, 90 meters long and it is 100 meters long be mutually assembled it is various by rise Each region etc. of standard setting runway width needed for dropping airframe, then by standard setting landing airdrome length needed for various landing aircrafts Each region be combined into whole runway needed for different type of machines, then again by each region be set as can independent manual's adjustment control Gas ejection ports, when taking off by the jet port in each region, be adjusted into respectively incremental angle 30 degree of first area angle, 40 degree of angles of second area, 50 degree of third region angle, 60 degree of angles of the fourth region, 70 degree of the 5th region angle, 80 degree of the 6th region angle, Seven region an angle of 90 degrees, the wing type aircraft of the reverse ski-jump take-off of the gas ejection ports in each region, from the machine of wing type departing aeroplane Body lower portion ejects the gas laminar flow of various incrementally different angles upwards, the injection gas laminar flow can auxiliary wing formula aircraft it is fast Speed climb into outstanding support gas field lag formula be rapidly accelerated to nature takeoff speed.If in the gas laminar flow that each region is ejected Pressure be respectively：The gas pressure of first area 3,4 gas pressures of second area, 5, third region gas pressure, the Four 6, region gas pressures, the 5th 7, region gas pressure, the 6th 8, region gas pressure, the 7th 9, region gas pressure Power, the board a plane jet port angle in each region and gas pressure when taking off of the jet runway is all incremental.

Above four kinds of gas ejection ports are set into the template landing spray mounted in each each region of very-short-reach takeoff and landing device respectively On gas runway, then by it is 20 meters long on each very-short-reach jet runway, 30 meters long, 40 meters long, 50 meters long, 60 meters long, 70 meters long, 80 Long, 90 meters long or 100 meters long rice is respectively a region, jet needed for can setting a plurality of different length aircraft model landings of composition Runway etc., such as 7 regions in a 20 meters long region are now connected into the small drone jet that an overall length is 140 meters and are run Road, then by each region in each 20 meters of a 7 regions long regions, be set as can independent control gas ejection ports it is reverse, downwards It drops aircraft and is adjusted to the injection gas laminar flow of film forming grade status patterns, it can be achieved that landing to the safety barrage of decline aircraft, for example now will First area jet port angle is adjusted to be adjusted to for 30 degree, second area jet port angle as 75 degree, third area spray bicker degree It is adjusted to be 25Degree, the fourth region jet port angle is adjusted to be 70Degree, the 5th area spray bicker degree is adjusted to be 25Degree, the 6th region Jet port angle is adjusted to be used as to landing aircraft for 70 degree, District 7 domain jet port adjustable angle most 20-75 degree angle various Spare area when prediction scheme.

When decline aircraft is sliding with that can hang the strong gas field (negative pressure cushion) for holding in the palm complete machine body from pre- road overhead with 8-12 degree pitch angle When to first area, first area is each gas ejection ports at 30 degree angles, ejects upwards from fuselage lower portion and outstanding holds in the palm gas blanket The flexible gas of stream blocks (torque is generally equal in decline aircraft torque), and decline aircraft receives the outstanding support in 30 degree of angles in first area Spray gas after will decline aircraft original 8-12 degree pitch angle all by shear at 30 degree of pitch angles (in aerodynamics and fluid force It is referred to as air shear in, the moment of inertia of aircraft can greatly be cut down by blocking decline aircraft using air shearing principle).And Each gas ejection ports at 75 degree of angles of second area are pressing against fuselage on decline aircraft to the lower part from back position and are ejecting flexible air Body laminar flow blocks.(stopping gas torque is entirely the 50%-60% for generally declining aircraft torque, and decline aircraft is used in this way Property torque only has the moment of inertia of 50%-40% when sliding to third region to the fourth region).From the 30-75 degree angle region Liang Ge institute The different injection gas laminar flow of the two kinds of reverse two kinds of height formed can be set to first of film grade shape for blocking landing aircraft decline Gas laminar flow is sprayed in the deceleration of stance, and referred to as first film grade laminar flow folder forms 45 degree of space gas to landing aircraft head and the tail The injection gas of the angle in flow field blocks.

At this moment, decline aircraft slides into third region with 25-28 degree pitch angle, and each gas ejection ports in third region are 25 degree of angles Jet port, eject outstanding support gas laminar flow upwards from underbelly, and the fourth region is each gas ejection ports at 70 degree of angles, from Back position is pressing against fuselage on decline aircraft to the lower part and is ejecting gas laminar flow, is formed by from the 25-70 degree angle region Liang Ge The different injection gas laminar flow of two kinds of reverse two kinds of height can be set to the second film grade status patterns for blocking landing aircraft decline Slow down injection gas laminar flow.Referred to as second film grade laminar flow folder forms 45 degree of space airflow fields to landing aircraft head and the tail The injection gas of angle blocks.

At this moment, aircraft taxi is to the 5th region, and each puff prot in the 5th region is each gas ejection ports at 20 degree of angles, under fuselage Outstanding support gas laminar flow is ejected in portion upwards, and the 6th area spray bicker degree is adjusted to as 75 degree of angles, each gas ejection ports, from fuselage Upper bit is pressing against fuselage on decline aircraft to the lower part and is ejecting gas laminar flow.It can be set to from 20-65 degree angle and block under landing aircraft Gas laminar flow is sprayed in the deceleration of the third road film grade status patterns of drop.Referred to as third film grade laminar flow folder is to landing aircraft head and the tail shape It is blocked at the injection gas of the angle of 45 degree of space airflow field.

At this moment, aircraft taxi is to District 7 domain, and each jet port should be 20-75 degree angle and inversely land aircraft.High speed is declined into aircraft It is folded to be clipped in first and each 45 degree angles of second, third road film grade status patterns are folded clips injection gas laminar flow to block decline winged Machine slows down.Decline aircraft is blocked using film grade state, can also with strong injection flexible gas in first of film grade state with being greater than The film grade injection gas of decline airplane inertial torque directly blocks in first of film grade injection gas laminar flow.Realize film grade state The injection gas laminar flow of formula blocks aircraft, and the thrust gas that each area spray goes out when blocking decline aircraft need to only be greater than decline aircraft The 10-20% of moment of inertia, otherwise spray gas can will decline aircraft be turned over, landing aircraft every one of film grade state all Can by safely, flexibly, lag formula block landing.Such as：The pressure for the gas laminar flow that each region is ejected is respectively：The One 9, region gas pressure, 8 gas pressures of second area, 7, third region gas pressure, 6 gas pressures of the fourth region Power, the 5th 5, region gas pressure, the 6th 4, region gas pressure, the 7th 3, region gas pressure.Such as：Each region The angle of the gas laminar flow sprayed is respectively that 30-75,25-70,20-65-20-75 degree angle can be set to each region puff prot angle Successively decrease with whiff pressure, it is ensured that the outstanding each film grade laminar gas of support formula of safety blocks aircraft landing, the injection gas laminar flow Can auxiliary wing formula aircraft in landing, the film grade laminar flow of the injection gas pressure in each region and jet port angle, which presss from both sides, all to successively decrease , on the jet template runway of very-short-reach can application solutions quickly block landing.

There is provided that a kind of efficient short distance of band slides or the aircraft carrier of VTOL aircraft device, naval vessel, land and water platform jet are run simultaneously Road, including：Type aircraft carrier deck, marine vessel, continental rise airport, each provincial capital to county, each area under one's jurisdiction to county, each high mountain, mountain area, basin, trip Trip area, in cavern, island, islands and reefs, on ice and snow waters etc. large, medium and small type takeoff and landing area have a limitation can not build large size The jet runway on airport, can be in 150-200 meters long, 300-500 meters, 600-1000 meters, wide 10-50 meters or 60-100 meter Very-short-reach jet strip airport device can be realized on various places or platform.The jet-propelled very-short-reach runway is only current The 10% of conventional runway total length improves several times or more than conventional runway to the landing safe effect of aircraft, economical to take Reduce several times or more with than conventional runway.It is that a kind of following in town-dweller-rural-family individual, small-sized (unmanned plane moves towards logistics, goods and materials fortune Defeated commercialization) aircraft is in continental rise or continental rise sky airplane platform (shared landing or storage man with international adaptability standard Front yard aircraft airport current supermarket), it is slided by the short distance that blast injection gas blanket stream is formed or VTOL sparrow hawk formula or straight The dedicated jet runway stage apparatus of aircraft is risen, the management system of the device mutually switches with the manipulation and control of control tower, or by The management system of pilot's artificial intelligence in drop aircraft is connected.

Wherein, a kind of efficient short distance of band slide or the type aircraft carrier deck jet runway device of VTOL aircraft device in, It is special in type aircraft carrier deck takeoff and landing equipped with by the dedicated jet runway of blast injection gas laminar-flow type type aircraft carrier deck takeoff and landing With in a certain cabin in jet runway lower part, it is equipped with and air supply system device is supplied by blast injection, dress is set in type aircraft carrier deck Have as made of the rectangular each region template combination-inlaying of muti-piece, one or more wing type slides jet-propelled super of takeoff and landing Short distance runway device is slided on the dedicated jet runway assembly of takeoff and landing in each wing type, is respectively equipped with：Jet runway It is first area 10-100 meters long, jet runway 10-100 meters of second area long, region 10-100 meters of jet runway third Long, jet runway 10-100 meters of the fourth region long, the jet runway the 5th region 10-100 meters long, jet runway the 6th area It is domain 10-100 meters long, domain 10-100 meters of jet runway District 7 long, the total length on the jet runway in seven regions, Can according to the landing needs of all size aircraft model, can respectively by each group numbers pile up in seven regions it is most short be 70 meters It is long, up to 700 meters long, each total length is not waited, by setting needed for each type standard, each aircraft carrier and continental rise airport Jet-propelled very-short-reach runway needed for different length can be installed, the beam overall on jet-propelled very-short-reach runway can basis The landings of various large, medium and small aircraft models needs, may respectively be 5-60 meter width it is not equal need standard to set and fill, can also set The compatible jet-propelled runway of a multi-model is filled, is connected with management system.

In the dedicated jet runway assembly in seven regions of the type aircraft carrier deck, it is equipped with the left fixed under-chassis of private track, dedicated race The right fixed under-chassis in road, Normal Take-Off And Landing gas transmission interface tube, landing gas transmission interface tube of meeting an urgent need, spare three kinds of independences of landing gas transmission interface tube Control again can synchronously control can the mutual switching device of artificial intelligence, be connected with management system.

In the dedicated jet runway assembly in seven regions of the type aircraft carrier deck, it is equipped with each region of private track or so valve body template die Between plate install cushion connection gap, in each region back and forth or left and right valve body template die plate surrounding, be designed with other modules it Between the transfer port that is connected.In the dedicated jet runway assembly of the type aircraft carrier deck, cliche frame is lateral before being equipped with private track Press strip sealing and dustproof outer cover, cliche frame transverse direction press strip sealing and dustproof outer cover after private track, the left outside cliche frame of private track are longitudinal Batten seat, the private track right side outer cliche frame longitudinal direction batten seat, cliche frame transverse direction press strip sealing and dustproof outer cover is fixed before private track Bolt, cliche frame transverse direction press strip sealing and dustproof outer cover fixing bolt after private track, the left outside cliche frame longitudinal direction press strip of private track The devices such as seat fixing bolt and the right outer cliche frame longitudinal direction batten seat fixing bolt of private track, manipulate with artificial intelligence and control System processed is connected.

In the dedicated jet runway assembly of the type aircraft carrier deck,Three kinds equipped with the longitudinal stealthy installation of cliche frame before private track Red, yellow, and green warning lamp, cliche frame longitudinal direction red, yellow, and green warning lamp after private track, the left outside cliche frame of private track is longitudinally red, Yellow, green warning lamp, the right outer cliche frame longitudinal direction red, yellow, and green warning lamp of private track, the warning of private track front left wheel red, yellow, and green Lamp, private track front right wheel red, yellow, and green warning lamp, private track rear left wheel red, yellow, and green warning lamp are right after private track Wheel red, yellow, and green alarm light, is connected with artificial intelligence management system.

It is arranged on the dedicated jet runway of the type aircraft carrier deck or continental rise airport, is sprayed with multiple moving sleeve valve flute profile mouth formula gases Loophole, or multiple moving sleeve valve circle hole shape mouth formula gas ejection ports are had, or with multiple universal globe shell types without fixed sleeves The gas ejection ports of cylinder valve circle hole shape, or the gas with rotary sleeve in universal globe shell type Yu fixed sleeves valve circle hole shape Jet port, the left outside 1-7 region rotary sleeve valve flute profile puff prot of runway or circle hole shape puff prot servo pushing motor, runway Right outer 1-7 region rotary sleeve valve flute profile puff prot or circle hole shape puff prot servo pushing motor.Now by jet runway If the every longitudinal every 3 row spout in 1-7 region is set as region 20-100 meters long, 3 rows of each region longitudinal direction It is divided into longitudinal front-seat (referred to as Normal Take-Off And Landing puff prot) respectively and respectively, (referred to as spare landing puff prot) is arranged in longitudinal direction, is vertical To heel row (referred to as emergency landing puff prot).FromSpray gasEach two rows of spouts point in the every lateral centre in 1-7 region of runway It is not set as：It is left with it is left outside, right in outside the right side, realize it is each region 20-100 meter of true jet runway long it is interior be equipped with, Ruo Ganpai Normally, three sets of respective autonomous intelligence control systems such as spare, emergency, and being equipped with artificial intelligence can mutual handover control system The takeoff and landing jet runway of function.

In the dedicated jet runway assembly of the type aircraft carrier deck, on the left outside longitudinal position in every piece of template area, runway it is right outer vertical To on position, it is all correspondingly provided with the air curtain puff prot of multiple protective gas laminar flows；It is set in each horizontally-arranged all correspondences of jet runway There is the air curtain puff prot of multiple protective gas laminar flows, the flute profile or round jet of outer laterally four arrangements before each region of runway Mouth is set as Normal Take-Off And Landing puff prot, and middle transverse direction four flute profiles arranged or round puff prot are set as spare before each region of runway Landing puff prot, laterally the flute profiles of four arrangements or round puff prot are set as emergency landing puff prot behind each region of runway, Artificial intelligence system for three sets of respective individual injection gas laminar flow takeoff and landing is connected.

Before the preceding outer longitudinal direction and each region of runway in each region of runway lateral out symmetrically, multiple flute profiles or circle are respectively provided with Puff prot is Normal Take-Off And Landing air curtain puff prot.The China and foreign countries in each region are longitudinal, right on each region transverse direction China and foreign countries left and right position Claim, is equipped with multiple flute profiles or round puff prot, is spare landing air curtain puff prot；Each outer cross of longitudinal heel row in each region of runway To position on bilateral symmetry, multiple flute profiles or round puff prot are respectively provided with, for landing air curtain puff prot of meeting an urgent need.Seven areas of runway Lateral air curtain puff prot is opened or contract fully entirely outside the left and right in domain.The effect of air curtain puff prot is aircraft landing on jet runway When, interference of the external wind to it is prevented, which is connected with artificial intelligence management system.

The dedicated jet runway of the type aircraft carrier deck, continental rise airport jet runway assembly outer longitudinal rear and front end position on, respectively Equipped with the strong gas-assisted puff prot of landing square amount of safety emergency in no special situation；In runway, laterally bilateral symmetry is equipped with 0- 90 degree of safety are met an urgent need strong landing square amount gas jet mouths, can boosting landing aircraft, make aircraft overshoot or emergency when manipulating fault Forced gas safety barrage；On runway laterally each jet port to longitudinal direction, it is equipped with multiple rows of longitudinal injection 50- before and after multiple runways 400 mesh intelligence hydraulic spray nozzles, jetting height can assist large-scale 800-1000 tons or more of decline aircraft short up to 8-15 meters Safety barrage lands on runway.

On the left and right sides end of each region valve body plate main body template sub-unit of jet runway, it is respectively equipped with controllable jet and runs Each puff prot in road multiple Pneumatic extensions on and off push oil cylinder, and Pneumatic extension pushes the flexible interlocking lever of hydraulic cylinder, or Servo motor stretches the main shift fork of interlocking lever, stretches interlocking lever and each control rotary axle valve is oriented to arm connecting plate, flexible interlocking lever It is swung outside with fixed pin shaft and pin card dottle pin, compressed air rotary shaft sleeve above and below each control rotary axle valve guiding arm connecting plate Arm fixing groove handle seat, compressed air outer rotary shaft cover swing arm and fixing bolt outside sleeve fork library, compressed air inner rotary shaft set Sleeve pitches swing arm and fixing bolt outside library, and rotary shaft control valve is oriented to connection strap, the rotation of 30-90 degree fixed angle jet port Solid shaft or hollow shaft sleeve, 0-180 degree can any adjusting angle jet port rotary shaft, rotate multiple telescoping valve gate-type flute profile mouths Or the multiple telescoping valve gate-type circle hole shape mouths of rotation, rotary shaft flute profile puff prot, rotary shaft circle puff prot, rotation axis seal packing Mounting groove, rotary shaft exterior and interior axle sleeves fixing seat, positioning sleeve in rotary shaft, the outer positioning sleeve of rotary shaft, rotary shaft inner-outer sleeve positioning lock The mechanism arrangements such as fixing bolt, are connected with management system.

In the dedicated jet runway of the type aircraft carrier deck or continental rise jet runway assembly, four direction 25- can be controlled forwards, backwards by being equipped with (the universal globe shell type gas-sparging head can arbitrarily adjust 25- to the universal globe shell type gas-sparging head of 180 degree angle jet port The rotary oscillating type puff prot at 180 degree angle) or universal globe shell type rotary oscillation 25-360 degree can any adjusting angle injection Mouthful, fixing seat, the fixed interior ring washer of universal globe injector head rotary oscillation spherical surface block set, multi-directional ball are positioned outside universal globe injector head Face jet port spinning ball swings spherical surface and covers fixing seat, universal globe shell type gas-sparging head list sleeve or it is double telescopic point it is total Longitudinal handsetting gear can arbitrarily be adjusted at, universal globe 0-360 degree or pneumatic control is stretched actuator push rod, servo longitudinal motor or Pneumatic linear actuator fixes bracket, and lateral driving lever transmission motor or the transmission of Pneumatic extension cylinder push driving lever, longitudinal motor or pneumatic linear actuator control, Universal globe sprays headstock gasket, universal globe injector head locknut, universal globe injector head guiding leading screw or the pneumatic control of guiding Bar fixed plate processed, universal globe injector head guiding leading screw worm gear pairs or guiding Air Valve Control group, universal globe injector head guide wire Thick stick or the flexible thick stick of guiding Air Valve Control, universal globe injector head guiding locking screw.

Universal globe injector head is oriented to active support plate and swings linking arm, and universal globe injector head, which is oriented to active support plate and swings, to be connected Arm sliding pin is connect, universal globe injector head is oriented to active support plate and swings linking arm adjustment upper arm reinforcing rib and universal globe Injector head is oriented to active support plate and swings linking arm pin hole, and universal globe injector head is oriented to active support plate and swings linking arm pin Axis and plum blossom latch card, universal globe injector head are oriented to active support plate and swing linking arm driving lever support base, universal globe injection Head guiding jet appendix single sleeve, universal globe injector head pneumatic control jet gas transmission flow stop valve sub-unit, guiding Active support plate swings lateral pressure swivel bearing inside and outside linking arm or rotary sleeve sleeve, compressed air gas source blowing mouth or soft The quick plug receptacle seat of connecting tube, interior main each gas transmission of air supply source store deflation bucket interface bore, the outer seat of Self-adjusting nozzle universal globe The mechanism arrangements such as fixing bolt are connected with management system.

In the dedicated jet runway assembly of the type aircraft carrier deck, it is connected and fixed seat equipped with master cylinder, master cylinder is connected and fixed hinged shaft, Runway pavement panel, runway valve body plate main body module lower plate pedestal, runway valve body plate main body module I-shaped support rib stand, gas The dynamic flexible hydraulic cylinder flexible control mechanism that pushes installs room, Pneumatic extension and hydraulic cylinder flexible control mechanism installation room maintenance Blind patch, Pneumatic extension and hydraulic cylinder flexible control mechanism installation room maintenance blind patch overlap mouth, runway valve body plate main body mould The fixing threaded hole up and down of block air inlet air storage chamber transverse sealing end cap, runway valve body plate main body module air inlet pipe install room transverse sealing End cap inner panel, and be connected to the management system of each injection gas ejection ports.

Band telescoping valve gate-type flute profile mouth or the gas ejection ports with telescoping valve gate-type circle hole shape mouth or band-slot mouth, or Gas ejection ports with circle hole shape mouth, or the gas injection apparatus with universal globe sleeve type valve circle hole shape includes：With multiple The dedicated landing runway of aircraft of the gas ejection ports of shaft sleeve valve gate slot shape mouth, or the spray of the gas with multiple axle sleeve valve circle hole shape mouths The dedicated landing runway of the aircraft of loophole, or dedicated, aircraft of the gas ejection ports with multiple universal globe sleeve type valve circle hole shapes Runway device drops.It is described to be equipped with blast injection gas laminar flow apparatus in the dedicated jet runway of type aircraft carrier deck takeoff and landing, It is connected with the management system of artificial intelligence.

It is sufficiently to illustrate the ability and skill of autonomous innovation using the patented invention of high quality as important support that this item, which innovates none not, Art is horizontal.The present invention, which is created, can retain one effulgent period in aviation field from now on, influence and benefit full generation The historical progress of boundary's aviation field is developed by leaps and bounds, and the scientific and technical innovation of aviation field is pushed, for economic development bring actively and Far-reaching influence.What the present invention was most of practical significance is again from practical experience to theoretically recognizing the mankind：Aviation field In there is various hidden dangers, and modernization aircraft carrier and each continental rise airport aircraft backwardness during take-off and landing at present Property, so that it is thoroughly eliminated the various security risks being all likely to occur at any time during take-off and landing, preferably reduces and caused to country Various losses.

Quickly to improve wing type aircraft on aircraft carrier or various special short distance jet runways, realize it is safe and reliable, quick, Landing naturally is slided, present invention employs whirlpool spray, turbofan, axial flow blower formula or the gas laminar flows formed by blast injection On the dedicated jet runway of short distance.Its simple working principle is：It is transformed into the gas laminar flow of blast injection to taking off Continental rise airport aircraft and carrier-borne aircraft are formed by a kind of thrust of reverse outstanding towing force square, make aircarrier aircraft and carrier-borne aircraft in jet It is realized on runway and is transformed into gas laminar flow after being released by compressed gas, sliding jump formula landing aircraft is made to form the outstanding support of gas stream Formula quickly climbs and takes off.Former national standard accumulator is the air accumulator technical atmosphere of a very High Voltage, can reach 8-20-40 atmosphere Pressure, is equipped with an air compressor distribution cabin in each airfield runway melt pit or in warship cabin, screw air compressor exists It just will form a large amount of endlessly compressed air energy sources when work, the gas source in screw air compressor be stored in In each air accumulator in each airport melt pit room or warship cabin.

After each gas ejection ports of dedicated jet runway are opened, the compressed air gas stream being stored in air accumulator quickly flows The main appendix in into each valve body plate of jet runway or each region regulates and controls valve assembly, and the size of air pressure needed for each region is conveyed Into the jet appendix of each isolated area system, then by the gas transmission manifold in each region, by the defeated gas transmission flow to each row of gas source Electromagnetism ends control valve sub-unit, by gas transmission flow electromagnetic shut-off valve sub-unit control switch, is formed to multiple puff prots The intelligent control for opening jet and closing, after gas transmission gas source electromagnet cut off valve is opened, at this moment the compressed air in air accumulator is fast Speed pours in each air flue room, and each shape for flowing to each jet port valve chamber always is intracavitary, will be each in each valve body plate of dedicated jet runway The indoor each shape chamber of air flue stores full, each main storage deflation tubular cavity in the runway with bleed pressure identical as air accumulator Room requires the landing of the various airport aircrafts of required landing or carrier-borne aircraft, and the transmitance in conjunction with spectrum is remote in 10-12Ldn Infrared band vision system, to determine that cooperative target and the corresponding maximum temperature range of spectral radiance efficiency are 152-237 DEG C.For The landing for implementing the carrier-borne aircraft and unmanned plane of view-based access control model identifies.By road machine set dress artificial intelligence interact far infrared or Photoelectric tube sensing, the puff prot angle of the whiff pressure in each region of runway and each region all switches to and landing aircraft phase Matching status, landing aircraft receives to preset the various different jet angles to match on dedicated jet runway and air pressure is big Small injection gas laminar flow, forms the landing to various aircraft safeties.Here it is the formation of dedicated jet runway, spy's invention is set It counts out：It is a kind of using whirlpool spray, turbofan, axial flow blower, aircompressor type, each injection gas blanket for directly supplying gas source Stream, forms to the landing effect of special short distance aircraft, horizontal consistent with deck level is embedded in each boat for the jet runway is hidden On female deck, various land airplane fields, marine fixed or mobile platform or the various absolutely empty body panels of height in town and country, by compressing Air reverse landing aircraft on special short distance takeoff and landing jet runway, ejects dry type or wet type gas laminar flow It is safe and efficient, rapidly realize injection gas laminar flow, various aircraft can be realized with the outstanding support formula of soft slow property injection gas laminar flow It takes off or hangs support formula and block landing.

The force techniques of blast injection gas laminar flow mechanics, for the mechanics problem on static curved surface and plane, and The application whole to the aircraft of various high-speed motions above has the change of matter, is particularly acting on wing type and slides aircraft in landing Jet-propelled very-short-reach runway, the jet-propelled air bag runway of expansion airbag type floating body very-short-reach glding type takeoff and landing waterborne, Movable air bellows very-short-reach jet runway, the vertical aircraft of extension airbag float type waterborne in the jet-propelled air bag platform of landing, OrSeaUpper very-short-reach slides or rectilinear aircraft is in the jet-propelled oil platform of landing, and the jet-propelled very-short-reach in provincial capital to county is run Road airport, the jet-propelled very-short-reach strip airport in each tourist spot, the jet-propelled very-short-reach strip airport in each logistics area, area under one's jurisdiction The very-short-reach strip airport jet-propelled to county, the jet-propelled very-short-reach strip airport in each high mountain, mountain area, basin are concealed Jet-propelled very-short-reach strip airport in cavern, the jet-propelled very-short-reach strip airport in island tremble with fear, are tropical jet-propelled ultrashort The jet-propelled very-short-reach strip airport on airfield runway, islands and reefs, or to large, medium and small type passenger plane, unmanned plane, 0.5- The various aircrafts of 2000 tons of weight can realize safe landing, can be in the short distance with Efficient Compression air injection gas stream From sliding on the jet-propelled runway of landing safe landing or VTOL sparrow hawk formula or helicopter on jet-propelled runway platform Safely and fast landing.The sliding jump of very-short-reach or the jet-propelled runway of VTOL aircraft with Efficient Compression air injection gas laminar flow Appearance, the 70-80% on the former landing airport to match by the conventional ratio of national standard, whole runway total length can be saved Length, landing efficiency improves 2-3 times or more than the landing airport runways that original matches by the conventional ratio of national standard, in entirety Landing energy consumption on can reduce 30-40%, the flyer miles of 50-60% can be improved to sparrow hawk formula or helicopter, can be extended The landing service life of aircraft 30-40% or more can integrally improve the safe manoeuvring efficiency several times of takeoff and landing or more.

It is all artificial intelligence that gas ejection ports are respectively arranged on jet runway, and swinging transformation angle forwards, backwards is 0-180 degree angle, can also By the full intelligence (360 degree rotation) of each row's compressed air universal globe shell type gas-sparging head, in universal globe shell type gas injection The angle for the actually active value that head back and forth or left and right angle of oscillation is obtained respectively is 0-180 degree angle.Realize that various landing aircrafts exist On landing jet template runway, required matched various optimal injection gas pressures all can be obtained, it is variable using above two kinds Change the gas ejection ports of a certain swing angle of gas ejection ports angle of oscillation, can auxiliary wing formula aircraft in very-short-reach On jet runway, it all can safely and fast realize and fly or hang to hold in the palm to block landing by outstanding hold up of injection gas.Spray gas laminar flow pair The intelligent shear of the various gas angles of landing aircraft all has various criterion requirement.

It, can people by each row's gas ejection ports direction in multiple rows of gas ejection ports of multiple universal globe shell type gas-sparging heads composition The underbelly position that work is intelligently adjusted to the inversely wing type aircraft of sliding drop of jumping up is upward, each to arrange Universal-head gas ejection ports or each band There are the gas ejection ports of moving sleeve valve flute profile mouth formula, or the angle of the gas ejection ports with moving sleeve valve circle hole shape mouth formula can incite somebody to action The types of various landing aircrafts, aircraft volume size, weight, slide angle, slide the speed of a ship or plane etc. all must be with each row's Universal-head gas The outstanding outstanding support of winged effective height, gas that holds up of gas pressure, the gas of body jet port blocks effective height, presses each system during take-off and landing Single standard gas flow can reach the scientific landing to match with reasonable best artificial intelligence and control.

Each row's Universal-head gas ejection ports, can the front and back transformation swing angle of artificial intelligence be 0-180 degree angle, it is each to arrange Universal-head gas Body jet port, also it is sprayable go out it is various can artificial intelligence transformation 360 degree rotation angle, it is sprayable go out different outstanding of various pressure Hold in the palm high pressure gas laminar flow, two kinds of transformation angles of oscillation it is single using a certain kind and can auxiliary wing formula aircraft, in very-short-reach On jet runway, safety, quickly outstanding hold up flies or safely and fast hangs to hold in the palm to block landing.The high-pressure injection gas is under runway Face bottom and runway pavement are equipped with multiple by compressed air gas injection nozzle, all directions that can be upward to runway face, by Artificial intelligence regulates and controls each gas injection nozzle of runway pavement, the outstanding support gas of one kind that reverse landing aircraft ejects.The compressed air Gas jetting hole, can the sliding jump formula landing aircraft of reverse wing type or rectilinear landing aircraft vertical eject it is various required for The outstanding support gas laminar flow of angle and pressure different proportion.Its reach to sliding jump formula landing aircraft very-short-reach jet runway It is interior, 100% safe take-off or a kind of wisdom traffic runway of landing can be blocked, the jet runway itself has a kind of to rising with regard to band Dropping aircraft can the outstanding function of holding in the palm control of 100% safety.

The jet track systems can greatly shorten the total length that fixed wing aircraft slides landing, or even realize on the runway Rectilinear takeoff and landing sparrow hawk formula or helicopter.Solve carrier-borne aircraft type aircraft carrier deck landing, or the safety etc. of emergency landing Various conventional difficulties realize safe landing of the various carrier-borne aircrafts at sea under the terrible weathers environmental condition such as stormy waves.The jet is run Road system can also prevent the controllability of its various aircraft self inertia torque, great advantage pre-, or directly block suicide The attack of unmanned plane or various aircraft or guided missile to the runway.These advantages of the runway, be by present invention employs whirlpools to spray, Turbofan, axial flow blower formula or by a variety of compressed airs effect such as compressed air be the core drive energy mode, the gas storage provided, Gas source is supplied, these compressed air power energies are input to each differences of the invention, in takeoff and landing jet track systems Gas chamber shape is intracavitary, and the aerodynamic principle of referred to as a kind of gas laminar flow gone out by compressed air gas injection is, it can be achieved that peace Full boosting landing aircraft.The present invention can thoroughly solve current aircraft during take-off and landing extraneous runway to aircraft self inertia torque Uncontrollability, and auxiliary needle to various aircraft during take-off and landing, on original runway in existing various uncontrollable technologies Various defects, and a kind of efficient short distance of band is provided and is slided or the type aircraft carrier deck jet runway device of VTOL aircraft device, A kind of type aircraft carrier deck, marine vessel, continental rise airport, each provincial capital to county, each area under one's jurisdiction to county, each frontier sentry, logistics, each high mountain, Mountain area, basin, tourist district, in cavern, island, islands and reefs, fever and chills band, there is large, medium and small type takeoff and landing area on ice and snow waters etc. The jet track systems of the various platforms of limitation.

The present invention uses the compressed air mode second-mission aircraft landing of technology maturation, this by compressed air energy sources jet mode section Using aerodynamic principle as the auxiliary torque of landing aircraft.Compressed air generated injection on jet runway The promotion energy of the pairs of landing aircraft of gas blanket manifold is very large, the case where compressed air gas source energy guarantees input enough Under, can by the outstanding support of the aircraft safety in dynamic in gas field can 100% positioning hover, theoretically can be in nearly 600-800 In the short distance of rice, the aircraft of 2000-3000 tons of weights is pushed into 15-20 meters of high-altitudes with 7-10 seconds.Block 3500-4000 The aircraft of ton weight, air pressure is in 25-30 atmospheric pressure, and spraying it, gas is outstanding to ask safety barrage to land.

To achieve the above object, the technical solution adopted by the present invention is that：A kind of efficient short distance of band is slided or VTOL aircraft The aircraft carrier of device, naval vessel, land and water platform jet runway device system, including：Aircraft carrier deck jet runway, inflation/deflation lifting Takeoff and landing jet platform runway, ship deck jet runway, sea-going tug drawing type or itself the independently movement of formula air sac ship The aircraft platform jet runway of formula, the aircraft platform jet runway of various naval vessel Contiuum types, aircraft carrier or naval vessel tail end be equipped with can Extension airbag lengthens formula landing runway, and the takeoff and landing scaling platform jet of scalable gasbag-type is equipped on a certain side in naval vessel Runway, marine fixed or mobile aircraft platform jet runway, at sea or on the floating body jet platform in rivers and lakes, it is empty by compression The dedicated jet platform of vertical lift sparrow hawk formula or helicopter is slided in the short distance that gas jet gas stream is formed, continental rise airport flies Machine is fixed jet runway, the aircraft jet runway of continental rise Moveable foldable gasbag-type, town and country continental rise sky airplane platform jet and is run Road.And also especially before various landing jet runways bow end rearward end outside with when runway outside the left and right sides on, respectively Equipped with symmetrical hidden horizontal liftable flexion-extension or hidden horizontal and road face horizontal 0-90 degree angle, can also erect 0-30 meters of the formula that is laid flat high The heavy caliber for going up and down cast sprays gas laminar flow, and when the purpose is to prevent 10-18 grades of strong wind weathers, external wind is to this runway aircraft Interference when landing, and to aircraft in safe landing on jet runway, high pressure gas itself is contained in runway can be better The manipulation and control of Intelligent full-closed formula can also constantly can meet an urgent need safely fast to departing aeroplane when outside sliding jump runway out of control Speed is remedied using the correction of strong gas stream and is gone around, and " the eccentric inclination of biasing boat, up and down sink-float " once out of control to decline aircraft or is gone out When outside runway, it can constantly the strong gas stream correction of safe emergency block, can also hover and accelerate in outstanding support gas field to departing aeroplane To multiple functions such as safe take-off speed.

In the jet runway, equipped with being formed by by blast injection gas stream, the sliding jump formula gas of very-short-reach is outstanding to hold in the palm layer Stream slides landing or sparrow hawk formula and helicopter VTOL it is characterized in that can realize.The dedicated very-short-reach jet track systems Inside it is equipped with：The electromechanical integration artificial intelligence control machine driving of oil cylinder mechanism is pushed with cylinder mechanism (servo motor), and On seven regions of jet runway, it is respectively equipped with multiple universal globe shell type gas-sparging heads on control jet runway.By pressing It is set in the air accumulator to runway of contracting air pressure gas source in gas storage supervisor or the jet shape chamber in each valve body plate or each valve body plate Gas receiver, until each gas transmission menifold, then each pneumatic regulation pressure valve is arrived, each air-powered electromagnetic shut-off valve is then arrived, is eventually arrived at various Gas ejection ports；And in multiple moving sleeve valve flute profile mouth formula gas ejection ports or multiple moving sleeve valve circle hole shape mouth formula gases Jet port (abbreviation casing), multiple shaft sleeve valve gate slot shape mouths or multiple axle sleeve valve circle hole shape mouths, multiple gas ejection ports institute The gas injection runway or vertical gas of composition spray landing platform.

On each branch's spout of jet runway, it is respectively equipped with for each branch's electromagnet cut off valve is controlled, jet is run to control The automatic software control with ventilation gas source is quickly opened in multiple gas ejection ports ventilation gas source on road, rapid artificial intelligence switching System is closed；The size of each piece of template gas transmission menifold throughput is by far infrared or search lighting to landing aircrafts needed for various Target and the big ting model of aircraft, the aircraft speed of a ship or plane, weight, the various angles of takeoff and landing itself, airplane complete machine volume collection Area will just be adjusted by artificial intelligence in advance by each cut-off pressure regulator valve after identification and be controlled, and reach every piece of template to gas injection The match artificial intelligence regulation of constant flow rate size and pressure size of bicker degree throughput size controls, multiple turnbarrel valves Gate slot shape mouth formula gas ejection ports or multiple rotary sleeve valve circle hole shape mouth formula gas ejection ports rotate appointing for both the above A kind of what multiple moving sleeve valve gas ejection ports, all can be changed the size in each spout gap, and then each gas spray also can be changed The various angles of loophole and the size of gas flow.

Multiple moving sleeve valve (abbreviation casing) flute profile mouth formula gas ejection ports or multiple moving sleeve valve circle hole shape mouth formula gas injections The advantages of mouth is that multiple rotary sleeve valve flute profile mouths or multiple rotary sleeve valve circle hole shape mouths can keep each puff prot Unified gap function only changes the function of the angle of each jet port, the size in each gas ejection ports gap also can be changed, in turn Also the size of the front and rear angles of gas ejection ports and the size of gas flow can be changed, until artificial intelligence signal, control switch The electromagnet cut off valve of each jet port gas source and two kinds of rotary sleeve valve the advantages of opening or closing of air source structure of control.Disadvantage It is shaft sleeve valve gate slot shape mouth or axle sleeve valve circle hole shape mouth, two kinds of gas ejection ports can only be with the rotation spray at front and back 0-180 degree angle The swing of gas virtual value, angle, changeover valve (actually carry out accurate set inside and outside two to compressed air sealing by gap The inside and outside rotary sleeve cartridge type puff prot of pipe and composition).

It is additionally provided in the jet track systems：A kind of gas ejection ports with multiple universal globe shell types, one kind is with more The gas ejection ports (referred to as universal hair style gas-sparging head) of a universal globe circle hole shape, gas size is by artificial intelligence signal The control of adjustment cut-off air pressure valve constant flow rate size and pressure size, and by adjusting the pressure size of air pressure shut-off valve, just The gas velocity of each separate gas jet port in each region and the size of flow can be changed, adjust the pressure size of air pressure shut-off valve, The size of multi-directional ball surface cover jet port air-flow can be changed；By universal globe shell type injector head it is reverse needed for slide, or vertical rise The whole lower portion of the front and back fuselage of aircraft is dropped by each gas ejection ports on jet runway, ejects various gas blankets upwards Stream is acted on the whole stress surface of the aircraft lower portion gross area of various required landings type of different sizes, is ejected Support rises or blocks gas stream, is greater than outstanding backing pressure power and stream to the best injection gas of various required landing aircraft gross weight amount ratios Amount can be only achieved and hang support formula rapid increase to the safe boosting of departing aeroplane, or blocks the outstanding support formula of injection gas stream and block safety Rapid descent realizes that universal globe shell type injector head sprays security control of the gas stream to landing aircraft on jet runway, from And reach the safety guarantee effect to landing aircraft.

In order to guarantee the security control to landing aircraft, spy is respectively equipped with artificial intelligence control in seven regions of jet runway System heating galvanic couple and refrigeration system, can protect forever constant temperature on intelligent automatic control jet runway pavement, normal to reach landing The standard runway road face of humidity and mass dryness fraction solves landing aircraft in the variation of any different weather such as the cold, torrid zone or wave, and Cause the various problems occurred on runway by various moist cunnings etc..Each Civil Aviation Airport in the world is realized in cold, the torrid zone, misty rain, frost The weather such as jelly, ice and snow influence it, and cause runway sliding, cause to be unable to landing aircraft.Artificial intelligence is equipped in the jet runway It can control Electric radiant Heating Film or heating galvanic couple and refrigerating thermal-insulation software systems regulate and control its constant temperature, the appearance of the technical functionality can be to the world Bring safer and bigger economic benefit in each Civil Aviation Airport.The former each Civil Aviation Airport runway in the world is in fever and chills, misty rain, frost, ice When snowy day gas, airport aircraft often can not landing, directly contribute each flight delay personnel be detained and airport paralysis situation, this It is the still insurmountable a great problem in current World Airways field.

Aircraft is on dedicated jet runway, and when decline is first turned on the flap of decline aircraft and the damping umbrella that slows down, to current generation 1.5-30-300 tons of logistics transportation industry of the unmanned plane effect developed required for boundary is best, and the jet runway is to unmanned plane landing Primary condition is：It is ad hoc on runway to have location navigation and tracking system to the identifying system etc. of various types：Unmanned plane is at this Must have when landing on jet runway can independent landing, corresponding matched navigation system and nothing are carried on unmanned plane Man-machine flight control system, only in this way unmanned plane can carry out to safety and precise the safe landing control on jet runway System.

Set on jet runway filled it is multiple can be according to landing aircraft, infrared radiation and video camera shoot picture on runway pavement The environment that face comprehensive assessment is landed is ejected best to the selection of landing aircraft then from main modulation posture by each gas ejection ports Landing correct posture.There is each autonomous system of artificial intelligence control at any time, each intelligence puff prot ejects the promotion of gas stream Xiu is just declining the various positive and negative bufferings of aircraft " the yaw biasing heart and inclination, upper and lower sink-float ", and adjustment landing aircraft is run by jet Road track is accurately taken off or accurate warship point.Theoretically, 100% various big, medium and small wing type aircraft safeties, quickly can be realized The artificial gyroscope Intelligent control device of landing, and can realize that sparrow hawk formula or helicopter can vertically rise on jet runway pavement Harrier is opened the strong promotion injection gas laminar flow of flexibility that low speed original place receives large area on jet runway by drop, winged by taking off After machine is quickly hanged towing force by gas, natural perpendicular positioning support is raised to 8-20,25-30 meters of high-altitudes.Gas pressure is scaled down, The perpendicular positioning landing that Harrier hangs safely support formula can be achieved, compressed air pressure is generally 10-20 safety engineering atmosphere Pressure.The manipulation and control of the various aircraft platforms (or aircraft jet runway device) and various aircraft platforms or aircraft jet runway System is connected, and after mutually switching with the manipulation of jet runway, by pilot in machine the artificial intelligence manipulation and control jet Landing of the runway to aircraft.

Its effect is best to landing unmanned plane for the jet runway, and the difference of unmanned plane and conventional airplane is that the former does not have pilot. It is just being the absence of the driving of people, so unmanned plane is difficult to flexibly select level point according to practical situation in many cases, Unmanned plane manipulation in landing is all difficult by the end of current unmanned plane slightly not noticing that, with regard to broken fuselage or head, this is international practice With satisfactory completion task.Based on current Development of UAV situation and there are problem, jet runway takeoff and landing device of the invention, By means of Beidou Navigation System INS/GPS integrated navigation system, unmanned plane can use the far infrared that runway is equipped with and obtain Associated safety landing information on jet runway, is then positioned and is identified to unmanned plane using vision system, thus by spraying The gas laminar flow that each injection port of body short distance runway of emanating is ejected, it is " eccentric when constantly being landed to landing unmanned plane Biasing boat inclination, up and down sink-float " etc. various landing attitudes can 100% artificial intelligence amendment, it is ensured that unmanned plane is in jet short distance Safe landing from best accurate 100% not broken fuselage and head on private track.

Note：The jet runway is dry type to the gas laminar flow that the aircraft contrainjection taken off goes out, and for decline aircraft in 100- The gas laminar flow that various large, medium and small type aircrafts within 500 tons inversely spray is similarly dry type.For decline aircraft in 800- It is wet type that 1000 tons or more of various heavy airplanes inversely sprayed, which blocks gas laminar flow, but decline aircraft is inversely sprayed sometimes Time when gas laminar flow out will decline according to aircraft.It, be with the vision of pilot under the weather condition in daytime or evening Condition and blind radar whether is opened to determine with dry gas laminar flow or wet type gas laminar flow.Because wet type gas laminar flow is more Mist-like is had less, pilot can be declined and be generated visual impact, and also will affect decline effect, at this moment openable blind landing thunder It reaches.When implementing injection using wet type gas laminar flow and blocking, it is necessary to pay attention to decline aircraft outer surface to environment temperature at that time, It is required that the preferably positive and negative temperature difference of hull-skin temperature of the gas laminar flow sprayed and decline aircraft itself is consistent, the wet type sprayed The gas blanket amount of flowing to end is not too low, the minimum 5-10 degree that can not be lower than the whole hull-skin temperature of decline aircraft itself.

Note：Manipulation before taking off.Front airplane wheel of airplane road when departing aeroplane needs to take off on jet runway, on jet runway Or on rear left and right wheel road, the artificial intelligence of setting prevents the safety operation control of the red, yellow, and green color of the extraneous hidden apparatus collided from holding Row takeoff and landing indicator light is that (red colored lamp light yellow indicates compressed air gas injection special short distance jet runway to red light light yellow It is upper to be first unable to landing, awaiting orders).When the operator on jet runway is connected to control tower takeoff and landing instruction, instruction person will The red light being always on is converted into flickering red light, indicates first to be unable to landing on special short distance jet runway, each one Work intelligence system is being done and is automaticly inspecting work before takeoff and landing.

Note：In landing on daytime, since the light intensity of sunlight is big, to prevent pilot wrong in photopic vision red colored lamp, On special short distance jet runway, it is necessary to equipped with the staff of the not homochromy clothing of various dresses, staff at this moment Red clothing is all worn with the instruction personnel of control tower, indicates first to be unable to landing on special short distance jet runway.It rises as in the night Drop, the visual indicia of pilot, which remains on, to be flashed by red colored lamp, work people of the dress with flashing red light label clothing The instruction personnel of member and control tower, become apparent, and the outfit label of unified visual is more eye-catching to the vision of pilot.

Preparation before taking off includes：First have to accomplish is in compressed air gas injection special short distance jet runway The unimpeded inspection work of upper appearance entirety.Remove the various particulate matters on jet runway.Check the gas storage pressure of compressed air Whether the pressure size of table is normal；Check whether the pressure size of the blow off pressure table in each region is normal on jet runway；And And check on jet runway the deflation rotary sleeve valve formula flute profile mouth in each region or rotary sleeve valve formula circle hole shape mouth, Or 0-90 degree angle or the spray of universal globe shell type of each jet port with rotary shaft slot-shaped spray jet outlet or with rotary shaft circle hole shape spout Mouthful, whether each flexibility swing position for rotating angle intelligent control is normal；Check that the snifting valve on jet runway is automatic from warship It cuts in the artificial intelligence conversion and control for going to departing aeroplane, interacts and controlled whether just with the sensing identification of the remote infrared of departing aeroplane Often；Check in compressed air gas injection, jet valve chamber on special short distance jet runway whether gas leakage, each valve road is logical Whether gas is normal；To compressed air on special short distance jet runway, it is desirable that the artificial intelligence of each each noncontinuous item system The whole normal times for checking work are that packet synchronization is completed in 10-15 seconds.

For carrier-borne aircraft on compressed air special short distance jet runway, the process before taking off is most multiple on aircraft-carrier flight deck One of miscellaneous cargo handling operation.On compressed air special short distance jet runway, in the various injection gas laminar flows of intelligently setting Under effect, running speed will be increased to rapidly 55-60 meter per second by carrier-borne aircraft in nearly 40-60 meters of distance, and leave flight Before the jet gas field runway of deck, the speed of 200 meter per second normal flights is had reached, aircraft is made to be detached from jet runway (autogenous cutting change) After gas field, the weightlessness of aircraft not will cause.Carrier-borne aircraft is in progress " receiving injection gas laminar flow " operation, operation safety warning line Within region must assure that and empty, in this way, which the gas of typically for up to nearly hundred meters of injection gas stream hangs the sliding jump row of support formula Runway and two sides safe police timberline will occupy flight-deck and take off the big quantity space in area, make rational planning for and spray gas stream Gas hangs support formula and slides, and the length of jet runway also becomes determining flight-deck and takes off the important evidence of area's main scaling factor. Carrier-borne aircraft slides the cunning race process under the effect of jet runway in the outstanding support formula of gas of injection gas stream, runs injection sliding with carrier-borne aircraft During gas stream accelerates, though there is air curtain protection, the effect of large amount of complex factor, such as deck equally also will receive sometimes The characteristics of airflow field feature, the flexible buffer air force for spraying gas stream export, carrier-borne aircraft aeroperformance etc..By certain journey The simplification of degree, carrier-borne aircraft under the basic stress condition by injection gas stream active phase, need to also in specific practice ability More accurate answer is obtained, for hanging the sliding jump runway of support formula by current jet, than in the safety of former sliding jump formula runway landing Improve several times or more.

Note：When departing aeroplane needs to take off on jet runway, on the front airplane wheel of airplane road on jet runway or rear left and right machine It is amber light light yellow, (amber light light yellow, table that the safety operation control for the artificial intelligence stealth red, yellow, and green color being arranged on wheel road, which executes instruction lamp, Show and awaiting orders on jet runway).When the operator on jet runway is connected to takeoff and landing instruction, instruction person will be always on Amber light be converted into flickering yellow light, indicate first to be unable to landing, artificial intelligence system on special short distance jet runway System is doing the preparation before takeoff and landing.

Note：In landing on daytime, since the light intensity of sunlight is big, to prevent pilot wrong in photopic vision amber light, On compressed air gas injection special short distance jet runway, it is necessary to equipped with the work people of the various not homochromy clothing of dress Member, the instruction personnel of staff and control tower at this moment wear yellow clothing, indicate that elder generation is not on special short distance jet runway It can landing.Landing as in the night, it is that amber light is flashing that the visual indicia of pilot, which remains on, and dress has blinking yellow illumination beacon light Remember the staff of clothing and the instruction personnel of control tower, become apparent, the outfit label of unified visual to the vision of pilot more It is eye-catching.

Note：When departing aeroplane needs to take off on jet runway, control staff on jet runway is carried out to required landing aircraft Type, total weight, the flight speed of a ship or plane, the total length × width × height of complete machine body, front and back wing overall length × wide × fuselage area body, fuselage it is whole By outstanding support or the damped air flows that are hit, arrestment intensity to complete machine after the anti-gas injection of maximum of body or front and back wing entirety The various technical parameters such as the best stressed effect of fuselage carry out recognition and verification calculating.These technical parameters are inputted into compressed air gas The special short distance of injection slides in the artificial intelligence controller of jet runway, is existed by sliding jet runway artificial intelligence controller It is completed in 1-2 seconds.By the jet to following several respects compressed air gas injection seven regions and each region on jet runway Pressure, the transformation of jet angle 0-90-360 degree, it is the gross area for the big small―gap suture that each gas ejection ports in each region need to open, each Jet port gas pressure flow speed, and injection gas laminar flow most preferably have the soft slow property air-flow of the departing aeroplane entirety gross area The effect support effective stress speed of rise carries out an automatic point sequence and has checked, and instructs and await orders.

Note：At this moment the artificial intelligence being arranged on the left and right wheels road of the front airplane wheel of airplane road on jet runway or rear wheel prevents the external world It is that the flickering light yellow of green light (dodge by green light one that the safety operation control for colliding the red, yellow, and green color of hidden apparatus, which executes instruction lamp, One light yellow dodged indicates awaiting orders on special short distance jet runway).Note：In landing on daytime, since the light of sunlight is strong Degree is big, to prevent pilot wrong in photopic vision, on compressed air gas injection special short distance jet runway, it is necessary to Equipped with the staff of the various not homochromy clothing of dress, the instruction personnel of staff and control tower at this moment wear green clothing Dress indicates first to be unable to landing on compressed air gas injection special short distance jet runway.Landing as in the night, the view of pilot Feeling that label remains on is green light, the instruction personnel of staff and control tower of the dress with green flashing lamp label clothing, more Obviously, the outfit label of unified visual is more eye-catching to the vision of pilot.

When control tower orders to carry out ordering to take off to the required aircraft to take off, note：At this moment all green lights on jet runway are complete Portion's light yellow, the required aircraft to take off slide on jet runway from preparation, and it is empty that speed when with 55-60 meter per second quickly slides to compression On gas gas injection special short distance runway.Meanwhile the flight scanning on compressed air gas injection special short distance runway Sensing can arbitrarily be set as 5-10 meters with the distance between runway and aircraft, and the intelligent interaction of setting and the aircraft to take off are real Synchronous manipulation is showed.To size, the flying speed of each region whiff pressure, jet angle and gaseous blast, by remote infrared or light Fulgurite sensing, synchronization interactive control, opens or closes each spray by afterflow software control procedure within the scope of the distance sensing of setting Port.

At this moment, it is first 20 meters long to slide to jet runway for the aircraft to take off, and first each puff prot in region of runway inversely takes off Aircraft is the required angle that the artificial intelligence automatic control at 25-30 degree angle adjusts.Note：At this moment carrier-borne aircraft special short distance jet runway The full intelligent controller of compressed air gas injection, can be switched on aircraft from turn by warship control, by pilot in machine directly Each district system of the whole runway of manipulation and control breaches original using ejector when taking off completely, and pilot is because being unable to automatic control Caused various senses of insecurity.Realizing each pilot can different according to itself, practical profession manipulation flight water Flat technique and skill adjusts, and completes during take-off and landing to two kinds of injection gas streams, when being formed to landing takeoff and landing Best allotment utilizing status.Can according to the piloting technique skill of each pilot itself, on special short distance jet runway, The size of fast or slow-action that can be arbitrarily safe with landing injection gas flow, then, then to slide to compressed air gas injection special With second 20 meters long, each reverse departing aeroplane 30-40 degree of puff prot of short distance jet runway it is angular on various jet angles It is synchronous to realize machine road for the optimal any angle to match needed for the artificial intelligence in region, automatic control adjustment and pilot itself Safe take-off manipulation, while realizing the most safe and reliable take-off process for being rapidly separated jet runway.

Such as fail to reach effect of taking off in Two Areas, it can be after completing Two Areas take-off process, departing aeroplane is again sliding To jet runway third 20 meters of long, each reverse departing aeroplane 40-50 degree of puff prot it is angular on jet angular zone it is artificial Match angle needed for intelligent automatic-control adjustment.Such as 50 tons of departing aeroplanes below, should be in 20 meters of long, each puff prots of third Arbitrarily match angle needed for the artificial intelligence automatic control adjustment of various jet angular zones on 40-50 degree is angular, so that it may real Now most safe and reliable take-off process.

Such as fail to reach effect of taking off in third region, then slide to jet runway the 4th 20 meters long, each puff prots it is reverse Match angle needed for the artificial intelligence automatic control adjustment of the upward various jet angular zones of departing aeroplane 50-60 degree, so that it may real Existing safe take-off.If 60 tons of departing aeroplanes below should be the jet on 50-60 degree is angular in the 4th 20 meters long, each puff prots The angle that arbitrarily matches of angle needed for the artificial intelligence automatic control of angular zone adjusts, so that it may realize that most safe and reliable rising is flown over Journey.

When the aircraft to take off slides into from first region the 5th 20 meters long, each reverse departing aeroplanes of puff prot of jet runway The required angle of the intelligent automatic-control adjustment of the upward jet angular zone of 60-70 degree, when 200-300 tons of departing aeroplanes below should be 5th 20 meters long, each puff prots are appointing for angle needed for the artificial intelligence automatic control of the upward jet angular zone of 60-70 degree adjusts Meaning matches angle, so that it may realize most safe and reliable take-off process.

It is general under normal circumstances, the aircraft taxi of various large, medium and small types is to the 5th region, before the aircraft at this moment to take off Wheel or afterwards two wheels in left and right, substantially departing from compressed air gas injection special short distance jet runway deck or continental rise Airfield runway.But when thrust of the aircraft to take off when uniformly the outstanding support of injection gas accelerates, the outstanding support reverse greater than jet runway When thrust, departing aeroplane can be rapidly separated the lift-off of jet runway.When departing aeroplane is in the outstanding support acceleration of injection gas, itself is pushed away Power, when reverse less than jet runway outstanding support thrust, departing aeroplane, which is still climbed or be left floating upwards in jet runway, to fly at a slow speed Hovering capable or in situ accelerates to takeoff speed, ejects uniform gas by compressed air gas injection special short distance jet runway Body laminar flow forms reverse soft slow property support to departing aeroplane and rises air-flow, while departing aeroplane itself engine rearwardly ejects Reverse burning gases, which are formed, more increases the thrust of Inertia in Airflow to sliding for departing aeroplane, the two reverse air-flows intersections After will, naturally outstanding support to sky quick, safe to departing aeroplane, flight lift-off speed when hanging support is two inversely by strength Flow the sum of nature rate of climb, the also referred to as reverse outstanding support gas stream of the two air-flows, the reverse outstanding support bigger landing runway of gas stream It is shorter, it is otherwise on the contrary.

The aircraft that outstanding support is taken off to sky, at this moment must accelerate at once and take off speed, at this moment aircraft can be just rapidly separated Compressed air gas injection gas field special short distance jet runway.Sometimes within moment, two reverse gas laminar flows are in equal force When square, it will cause and hover within the moment in jet runway overhead to the outstanding support of departing aeroplane, injection gas laminar flow is effectively made in aircraft In midair with height, aircraft can be made to be unable to flight forward within moment, infused：At this moment aircraft is still and is safely uniformly spraying The stop acceleration of moment pulls up winged process in gas field.In this regard, pilot just must have a set of skilled manipulation technology, it is right Landing aircraft is the desired amount of in the gas source of injection to departing aeroplane on receiving jet runway on the energy saving of gas jet source Be adjusted and switch in size, realize pilot departing aeroplane is manipulated in machine, be rapidly separated dedicated jet runway overhead with Spray the switching control of reverse gas force.Whenever the support lift-type inverted draft sprayed on dedicated jet runway to departing aeroplane overhead When, and when departing aeroplane is supported to 10-20 meters of height, fly so that departing aeroplane be made to realize the natural acceleration in atmospheric field Row.At this moment, the thrust of the injection gas of aircraft itself has been greater than effective critical height of the outstanding towing force of jet runway injection gas stream Degree, the safety for having reached departing aeroplane fly naturally when accelerating, pilot with regard to must quick lift disengaging jet runway to taking off The air damping of aircraft flight forward acts on.

When the aircraft to take off is from first region, slide into jet runway the 6th 20 meters long, each puff prots inversely take off it is winged Angle needed for the intelligent automatic-control of jet angular zone on machine 70-80 degree is angular adjusts, such as 250 tons of departing aeroplane Ying below The angle that arbitrarily matches to match needed for the intelligent automatic-control adjustment of six 20 meters long, each reverse departing aeroplane 70-80 degree of puff prot Degree, so that it may realize that most safe and reliable take-off process, the manipulation aircraft that pilot can be safe reach the normal flight of automatic control. The great advantage of the runway is exactly to increase and decrease air pressure to can be achieved with various tonnages needed for pushing various large-scale, medium-sized or baby planes Standard is to its landing.

When the aircraft to take off is from first region, slide into jet runway the 7th 20 meters long, each puff prots inversely take off it is winged Angle needed for the intelligent automatic-control of the upward jet angular zone of machine an angle of 90 degrees adjusts, as 400-600 tons of departing aeroplanes below should be The intelligent automatic-control of each jet angular zone on 7th 20 meters long, each reverse departing aeroplane 85-90 degree of puff prot are angular adjusts institute Need any angle of angle, so that it may realize most safe and reliable take-off process.At this moment, the aircraft to take off is thoroughly departing from compression Air gas sprays special short distance jet runway overhead, realizes safe take-off.Jet runway sprays each region of departing aeroplane The angle and atmospheric pressure of loophole are all incremental.

When departing aeroplane is slided from first area to the 7th region, wheel also without departing from jet runway pavement when, at this moment can will Runway outer end head on be equipped with emergent compulsive landing telescopic lifting cast heavy caliber injection gas laminar flow, realize to it is out of control with The help-fly again of failure departing aeroplane and the double layer security control function blocked again.

Note：When taking off, pressure that compressed air gas injection special short distance jet runway, each jet angular zone are sprayed Contracting air gas laminar flow should be the gas stream of dry type, exclusion, will not generate viscous drag, the dry type of no humidity to departing aeroplane Air stream can improve the lift of departing aeroplane, otherwise will affect the takeoff speed and departure time efficiency and energy consumption of aircraft, but Have no effect on the safety and stablization of aircraft.To the shape that the compressed air gas for spraying to landing aircraft flows, injection gas is inverse To landing aircraft, gas stream is rectangle bread formula.The effective height that gas is sprayed on jet runway is generally 8-10-15 meters High-altitude, a kind of band lifting hose pellet type jet blower gas injection height can be 20-25-30 as lifting disk height integrally increase Rice high-altitude discharges boosting injection gas laminar flow from inside to outside.

The fumarole of the outer two sides design of jet runway or so is air curtain puff prot, the maximum effect of the outer two sides air curtain puff prot in left and right It is：In 12 grades or more strong wind weathers, the outer two sides external world strong wind of jet runway or so can be protected normal to main jet gas source in runway It is influenced when not by landing aircraft.In 12 grades or more strong wind weathers, to prevent the outer two sides of jet runway or so a certain Crosswind influences it, the gas ejection ports of certain side of two sides in jet runway or so can be adjusted to 5-10-15-20- outward The various required angles such as 25 degree, and it is optimal reverse right to being formed from extraneous various wind direction angles with runway air curtain jet port The gas stream release for answering angle injection to match, it is ensured that jet runway or so outer two sides strong wind weather is prevented to exist its landing aircraft Various influences in jet runway when landing.In 8-16 grades of wind of ambient weather, by the outer each gas of two sides air curtain of jet runway or so Body jet port, to jet runway among adjust to the angle corresponding with extraneous wind direction angle such as 20-25-45 degree angle can spray left and right two Road air curtain, left and right air curtain jet port eject twice gas stream among runway the top, after formation twice intersect in the air Gas stream be packed to a rectangular protective gas gas field, while reducing the waste of gas source on entire runway, and It forms and the raising of whole runway injection gas laminar flow is utilized, spray gas height total gas of each of which pressure at 5-8 meters The utilization rate in source is 85% or more, to the injection gas height of the compressed air gas stream for spraying to landing aircraft at 10-15 meters Height when, the total gas source highest effective rate of utilization of each of which pressure is 65%.Temperature is general minimum in 5-10 degree above freezing, most High-temperature is 30 degree, and general normal temperature is positive and negative 15-20 degree.The compression temperature of ejection cannot be below subzero 10 degree, such as too low Deformation will cause to the overall structure of landing aircraft.General compressed air is all previously stored the gas in air accumulator, does not have Too big difference variation, each store are designed with refrigeration, thermostatic heating sensing modulator inside and outside gas bucket or storage gas tank.In frigid zone pair Aircraft before taking off, when starting is started on starting the road Qian Keyu, ad hoc on pre- road and jet runway or jet platform have can When for engine start for warm the main gas jet mouth of oxygen, each puff prot can discharge outward ensures that aircraft engine is starting The quick acceleration of front and back.

Surpass bubble technology according to torpedo, all moving objects (Media density including aircraft periphery, or when being less than aircraft, fly The density of row device integral medium), on the basis of same, speed can significantly improve aircraft.Otherwise conversely, jet of the present invention is run Periphery gas field density pressure on road then can guarantee that aircraft can obtain outstanding support formula in decline when being greater than integrated environment medium Air blast quick deceleration gas flexible blocks natural effect of the decline aircraft most preferably to injection gas stream shear to it.

Manipulation before aircraft decline prepares.Note：When aircraft decline, front airplane wheel of airplane road or rear on jet runway or so machine It takes turns on road, it is red that the artificial intelligence of setting, which prevents the safety operation control of the red, yellow, and green color of extraneous collision hidden apparatus from executing instruction lamp, In light yellow, (red colored lamp light yellow indicates first to be unable to landing on compressed air gas injection special short distance jet runway, colored lights It awaits orders).Operator on jet runway, when being connected to control tower takeoff and landing instruction, instruction person converts the red light being always on At flickering red light, indicate first to be unable to landing on special short distance jet runway, artificial intelligence system is being done winged Preparation before machine decline.

Note：In landing on daytime, since the light intensity of sunlight is big, to prevent pilot wrong in photopic vision, dedicated short On jet runway, it is necessary to equipped with the staff of the various not homochromy clothing of dress, staff and control tower at this moment Instruction personnel all wear red clothing, indicate first to be unable to landing on special short distance jet runway.Landing as in the night, flight It is that red colored lamp is flashing that the visual indicia of member, which remains on, staff and control tower of the dress with flashing red light label clothing Instruction personnel, become apparent, and the outfit label of unified visual is more eye-catching to the vision of pilot.

The preparation of aircraft before decreasing includes：Unimpeded inspection work is integrally carried out to the appearance on jet runway, first Work is emptied before doing aircraft decline, and removes various particulate matters (the various particles on jet runway on jet runway Object is generally not required to check)；Reexamine the gas storage of compressed air, whether normal (the i.e. inspection compressed air of each gage pressure size For gas injection on special short distance jet runway, whether the blow off pressure meter pressure size in each region is normal)；Check that compression is empty Gas gas injection is on special short distance jet runway, deflation rotary sleeve valve formula flute profile mouth, the turnbarrel valve in each region Gate-type circle hole shape mouth, rotary shaft flute profile jet port, rotary shaft circle hole shape spout or universal globe A seating circular hole spout 0-360 Angle is spent, whether each flexibility swing position for rotating angle intelligent control is normal.

Check whether jet electromagnet cut off valve on jet runway, carrier-borne aircraft artificial intelligence conversion and control are remote with decline aircraft Journey is infrared or photoelectric tube sensing interaction controls the normal of conversion signal；Check whether the jet valve chamber on jet runway has leakage Gas；Each jet port passes through when each Normal Take-Off And Landing, emergency landing, spare landing aircraft " eccentric biasing boat and inclination are risen and fallen up and down " Whether executing agency's gas mobile equilibrium sensor pushes regulation and each valve road ventilation of each autonomous system normal；To compressed air gas Body is injected in each project on special short distance jet runway, all checks that the normal time of work is grouping in 10-15 seconds It completes.

Note：When aircraft decline when, on compressed air gas injection special short distance jet runway front airplane wheel of airplane road or after On square left and right wheel road, the artificial intelligence being equipped with prevents the safety operation control execution of the red, yellow, and green color of extraneous collision hidden apparatus from referring to Show that lamp is amber light light yellow (amber light light yellow indicates awaiting orders on special short distance jet runway).When on jet runway Operator be connected to control tower takeoff and landing instruction when, the amber light being always on is converted into flickering yellow by control tower instruction person Light indicates first to be unable to landing on special short distance jet runway, and artificial intelligence system is doing the preparation of aircraft decline.

Note：In landing on daytime, since the light intensity of sunlight is big, to prevent pilot wrong in photopic vision amber light, On compressed air gas injection special short distance jet runway, it is necessary to equipped with the work people of the various not homochromy clothing of dress Member, the instruction personnel of staff and control tower at this moment wear yellow clothing, indicate that elder generation is not on special short distance jet runway It can landing.Landing as in the night, it is that amber flasher is flashing that the visual indicia of pilot, which remains on, and dress has blinking yellow illumination The staff of beacon light note clothing and the instruction personnel of control tower become apparent.

When aircraft decline, carry out in the operator on compressed air gas injection special short distance jet runway under required Type, total weight, the flight speed of a ship or plane, the intensity for collecting area body of the total length × width × height of complete machine body, front and back wing overall length of aircraft drop The whole anti-spray impact damping air-flow of maximum of wing blocks before and after the intensity for collecting area body of × width x thickness, fuselage are whole or each Deceleration intensity opens flap, tensile strength for collecting area body of total length × width × height of deceleration damping supporting drop umbrella etc., to landing Aircraft " eccentric biasing boat and inclination are risen and fallen up and down " gas stream pushes regulator control system and the forward and backward side of runway or so wheel road lower part The various technical parameters of jet runway (the gyro positioning adjustment set in type aircraft carrier deck jet runway) comprehensively control, will decline aircraft The input of these technical parameters slide the artificial intelligence controller of jet runway, by the artificial intelligence controller for sliding jet runway It completes to regulate and control after to its recognition and verification in 0.5-1 seconds, by each region whiff pressure to seven regions before and after jet runway, spray Air horn degree is the gross area and each spout gas pressure flow speed of each domain transformation of 0-360 degree, each big small―gap suture of spout Degree, injection gas laminar flow rise the gravity of decline to the soft slow property air-flow support of the decline aircraft entirety gross area, carry out an automatic point sequence and examine Check instructs each system synchronous after completing programming.Note：At this moment, fly on compressed air gas injection special short distance jet runway Before machine on wheel road or rear or so wheel road, the artificial intelligence of setting prevents the red, yellow, and green color of extraneous collision hidden apparatus It is the flickering light yellow of green light that safety operation control, which executes instruction lamp, indicates first to be unable to landing on special short distance jet runway, Artificial intelligence system is doing the preparation of aircraft decline.

Note：In landing on daytime, since the light intensity of sunlight is big, to prevent pilot wrong in photopic vision green light, On compressed air gas injection special short distance jet runway, it is necessary to equipped with the work people of the various not homochromy clothing of dress Member.At this moment staff wears green clothing, the work people of green clothing of the dress with flashed green signal lamp label The instruction personnel of member and control tower, indicating can be with landing on jet runway.At this moment landing light signal is issued by control tower, is red first Colored lights are glittering three times, and then yellow light is glittering three times, glittering three times followed by green, then by control tower issue can under The light signal and vision signal of drop.The control tower instruction personnel for wearing green clothing issue the instruction that can decline to decline aircraft Movement, gesture or light signal.Note：At this moment the green whole light yellow on control tower and jet runway, cannot any further lamp Flashing, so as to the completion rapid decrease for keeping observation of pilot during decline visually safer, accurate, stable.

When carrying out ordering to land to the aircraft of required landing, at this moment all control systems all switch with decline aircraft on jet runway It is controlled at networking by pilot guidance, at this moment the required aircraft to land is subtracted in the air with the speed of 200-150 km per hour from height Speed is dived and is slided, when sliding to first region of jet runway (20 meters long, the upward jet angle of 25-90 degree), and can With the decline different height of aircraft, required deceleration each region jet angle also with variation.Note：At this moment, decline plane distance Jet runway is set in an optimal arbitrary height at 5-8 meters, and each puff prot of jet runway inversely rises to before declining aircraft Falling the frame cabin gross area is 5 ㎡, and the sum of two undercarriage cabins in rear or so gross area is 10 ㎡, and decline aircraft is spraying By contrainjection gas laminar flow on gas runway, first to three undercarriage cabin gross areas before and after full underbelly position upwards its Implement the outstanding support gas of compressed air injection type for 15 ㎡, 30 ㎡ or 40 ㎡ to block, the work effective atmosphere of jet runway is 8- 10kg/ ㎡, P thrust=15 ㎡ × 8-10kg/c ㎡=120-150 Τ, can use and calculate the 1/3 of thrust is effective push 40-50 Τ, jet-propelled gas blocks can be by the outstanding support of the decline aircraft of 40-50 Τ weight in the overhead of 5-8 meters of jet runways, this is only to press The undercarriage cabin gross area of front and back three hangs support formula as the reality that damping braking gas film grade laminar flow blocks and blocks injection gas Shear damping.

After pilot opens while tail inverted draft damping deceleration safety parachute, flap and front and back wing are opened Rudder makes injection gas inversely decline aircraft, sprays large area film grade laminar flow and blocks gas.At this moment, by first of jet runway When region (20 meters long, the upward jet angle of 20-35 degree), note：(air pressure sprayed on jet runway be 8-10kg/ ㎡, 400 tons Aircraft below can not have to drag drop umbrella).The artificial intelligence automatic control set on jet runway is adjusted to phase needed for decline aircraft Compression damping gas laminar flow, is sprayed to the fuselage for declining aircraft by matched various optimal spout angles and front and back wing lower part is whole Body makes to decline aircraft when first region is 20 meters long, is a kind of flexible big strong by the injection gas laminar flow by jet runway Degree belongs to the injection gas stream of the buffer damping torque of even property；It is whole to the fuselage and front and back wing lower part of decline aircraft, by Slow support to the uniform jet-stream wind of size declines；After gaseous blast is inswept to the decline full fuselage of aircraft and wing lower portion, The air-flow of gas remaining about 80% from fuselage and wing lower part, pour tail inverted draft be punched into always landing drag umbrella or The upper flap of wing upper body, making to decline aircraft thoroughly realizes on jet runway, safer, flexible, uniformly sprayed The slow outstanding best actual effect for holding in the palm landing of body stream of emanating.

The artificial intelligent control system of the compressed air gas injection special short distance jet runway is turned to switch to by dropping by warship control The remote infrared in aircraft is fallen, to the artificial intelligence control of entire carrier-borne jet runway, pilot is realized in machine, to compression The control of air gas injection special short distance jet runway：And control the injection gas stream size of whole runway, injection gas Pressure size, injection gas flow angle size, the speed or " eccentric biasing is navigated and inclination, upper and lower sink-float " to decline aircraft are artificial Intelligent control respectively sprays gas mobile equilibrium sensor, and regulator control system is pushed to carry out to unbalance decline aircraft constantly with track Xiu Just, the various spray angles on dedicated jet runway can arbitrarily by pilot in machine manipulation and control, thoroughly solve former use Check cable mode, to pilot decline when various insecurity factors brought by fear.

The jet angle is the various natural angle of slope degree with decline aircraft, in decline, by remote infrared in aircraft and warship The sweep balance sensor for carrying jet runway, controls each jet port and sprays constant balanced gas stream, its various decline is pushed to fly The regulating effect that various inclinations angle of machine when unbalance are quickly corrected is up to 100%.By each jet port on jet runway, with Decline aircraft be formed by corresponding angles to reach 100% synchronization to match, meanwhile, each jet port all in accordance with pilot behaviour Control can be sprayed decline aircraft in evenly sized ratio and be greater than decline aircraft speed to the angular speed of decline aircraft within moment It spends, aircraft is self-possessed, the gas blanket gas field for blocking outstanding towing force square of aircraft decline moment of inertia.

To decline aircraft at the first drop zone, decline aircraft be first turned on flap and nose-gear wheel hatchcover and Rear or so undercarriage wheel hatchcover makes jet runway injection gas inversely spray large area to decline aircraft and blocks gas film grade Laminar flow, then the damping umbrella that will slow down are opened, and the speed of 50-80 km per hour are at this moment had dropped down to decline air speed, in flexibility Slow deceleration in gas stream, at this moment pilot can close engine.

It is right meanwhile to decline aircraft after the flight scanning sensing on compressed air gas injection special short distance jet runway Decline aircraft is realized to be turned to switch to by the remote infrared in decline aircraft, to carrier-borne aircraft by the warship control of artificial intelligent control system Dedicated jet runway injection gas laminar flow blocks decline aircraft, actual speed speed and the automatic control of security needs adjusts, real Showed pilot in aircraft can actively, best the warship effect of the manipulation aircraft decline of safety.

At this moment, first region is 20 meters long, and each puff prot is adjusted to inversely decline aircraft, when 30 degree of upward puff prot angles, by flying Each puff prot is inversely declined aircraft lower part by the landing height and speed of distance between aircraft and jet runway by office staff, is sprayed upwards Outstanding support gas laminar flow is projected, decline aircraft is blocked, by the decline aircraft after arrestment, it is dedicated to slide to compressed air gas injection 20 meters of Two Areas of short distance jet runway are long, and each puff prot is adjusted to inversely decline aircraft, 75 degree of upward puff prot angles When, each puff prot is inversely declined into aircraft apart from landing height, speed by between aircraft and jet runway by pilot in aircraft Gas laminar flow is sprayed to 75 degree of top angle.At this moment, each puff prot in first region is adjusted to inversely decline 30 degree of angles of aircraft, right Decline aircraft, which forms gas and hangs support formula upwards, to be ejected dry type gas and blocks；It is adjusted to inversely in each puff prot of Two Areas Decline 75 degree of angles of aircraft, the dry or humidity formula mixed gas that ejects for forming the downward pressing type of gas to decline aircraft is blocked.With On the gas that goes out in two area sprays two kinds that decline the folded angle for being clipped in 45 degree spaces of a formation of aircraft different are sprayed The gas of angle presss from both sides center, referred to as film grade laminar flow.In this way to decline aircraft in first long and Two Areas in 20 meters of region 20 meters long, the gas of two kinds of formation different spray angles blocks blocking for referred to as the 1st film grade laminated flow spray gas laminar flow At this moment folder has dropped down to 20-40 km per hour to the speed of decline aircraft, in flexible membrane grade gas laminar flow folder center.It will The various moments of inertia of decline aircraft itself fully control within the gas field of each film grade laminar flow underedge on jet runway, by gas Body is outstanding to hold in the palm the moment of inertia for being hanged locking-type disappearance decline aircraft, thoroughly eliminates until by the torque for declining airplane inertial.

When decline aircraft taxi is 20 meters long to third region, the 4th region is 20 meters long, in trizonal each jet It mouthful is adjusted to inversely decline 25 degree angles of aircraft, to aircraft formation gas is declined, outstanding support formula ejects dry type gas and blocks upwards, Each puff prot in the 4th region is adjusted to inversely decline 70 degree of angles of aircraft, and the injection of the downward pressing type of gas is formed to decline aircraft It does out or humidity formula mixed gas is blocked.Decline aircraft is folded in two kinds of gases that above three, four area sprays go out and is clipped in one The gas for forming two kinds of different angles of the angle in 45 degree of spaces presss from both sides center, the film grade laminar flow of referred to as two kinds gas.It is formed What the gas of two kinds of different spray angles blocked referred to as the 2nd film grade laminated flow spray gas laminar flow blocks folder, and at this moment, decline is winged The speed of machine has dropped down to 5-10 km speed per hour.Lock is hanged safely in flexible gas laminar flow underedge, will decline aircraft itself Various moments of inertia fully control in the outstanding support gas field on jet runway.

When decline aircraft taxi to each puff prot tune when the 5th region is 20 meters long, the 6th region is 20 meters long, in the 5th region To reverse decline 20 degree angles of aircraft, forming gas to decline aircraft, outstanding support formula ejects dry type gas and blocks upwards, the 6th Each puff prot in a region is adjusted to inversely decline 65 degree of angles of aircraft, and it is dry to form ejecting for the downward pressing type of gas to decline aircraft Or humidity formula mixed gas is blocked.Decline aircraft is folded in two kinds of gases that above five, six area sprays go out and is clipped in a formation Gas folder center, the film grade laminar flow of referred to as two kinds gas, shape are blocked in the injection of two kinds of different angles of the angle in 45 degree of spaces At two kinds of different spray angles gas block referred to as the 3rd film grade laminated flow spray gas laminar flow block folder, at this moment, under The speed of drop aircraft has dropped down to zero km per hour.In flexible gas laminar flow underedge by the outstanding lock of thoroughly safety, aircraft will be declined certainly The various moments of inertia of body fully control on jet runway.Decline aircraft after being decelerated generally all should be in the 4th to the 5th area Domain can safe falling stop, jet runway to decline each area spray mouth of aircraft angle and atmospheric pressure be all with decline After aircraft is blocked, with the abatement of decline aircraft torque, intelligence control system is decremented to aircraft original place for gas laminar flow is sprayed Land.

When decline aircraft, which is slided from first region to the 7th region, still to be slided to the 7th region to outside runway, can incite somebody to action The emergent compulsive that runway outer end is head-on equipped with, which blocks, can make the big square amount injection gas laminar flow of the heavy caliber of telescopic lifting cast, realize Control is blocked to the safe gas pressure of landing aircraft out of control.

The jet angle is the various natural angle of slope degree with decline aircraft in decline, meanwhile, compressed air gas injection The safety resistance of decline aircraft tail is quickly punched within moment to part injection gas laminar flow when blocking entire lowering aircraft Buddhist nun's fall-retarding drags in umbrella or fuselage, wing rudder, on flap and nose-gear wheel cabin in, rear or so undercarriage In wheel cabin, the deceleration that the undercarriage wheel cabin of front or rear left and right three is set as decline aircraft is damped into wind scoop, and complete To the residual air secondary recycling of injection gas laminar flow, injection gas laminar flow is realized to decline aircraft flexibility, 100% naturally Safety and steady blocks optimum utilization effect.

Film grade laminar flow is formed by using compressed air gas injection, blocks entire lowering aircraft, sprays gas film grade laminar flow pair Aircraft is naturally flexible blocks for decline, makes to decline aircraft entire area in the natural flexible gas laminar flow of safety, is formed under It is the revolution in current aviation history on the aerodynamics for the safety barrage stress pressed in drop aircraft entirety subiculum.It is most Big advantage：Injection gas has reached 100% safe, practical, scientific utilization to real control property of the landing aircraft on jet runway Rate is high, manipulation is simple, very economical, technologically advanced.It is the unmanned aircraft carrier of the following remote control or unmanned plane and continental rise airport or Small airport can landing large aircraft a kind of most safe rare equipment, and at present check cable, arresting net, steam ejection A kind of most practical high-tech takeoff and landing device that always cannot be comparable with Electromagnetical ejector is equipped.

The secondary impaired most serious consequence for causing decline aircraft 100% is blocked by check cable or arresting net hardness, especially more The damage problem again after decline can be caused to injured or breakdown plane, this is the manipulation that each uses check cable and arresting net The reason that persons know very well.

In the various naturals angle of slope that each jet righting jet port being equipped on jet runway is with decline aircraft when declining Degree, by the remote infrared in aircraft by after various signal data acquisitions, sensing to compressed air gas injection special short distance is sprayed The scanning sensing that gas runway or jet landing platform are equipped with matches interaction regulation, and by each injection on jet runway Mouthful, when interacting generated asynchronous between decline aircraft, by the righting jet port being equipped in jet runway, by it to decline Airplane-shaped is corrected its tracking to it at the constantly injection gas of corresponding angles and is synchronized, and is adjusted and is controlled by artificial intelligence；And it respectively sprays Mouth is completed to manipulate the angular speed of decline aircraft in machine, within moment, by the compressed air on jet runway all by pilot Each jet port sprays to decline aircraft and is greater than decline air speed, the moment of inertia that aircraft is self-possessed, aircraft declines, craft inclination By the size standard of injection gas flow when required righting, gas film grade laminar flow folder is blocked using flexible, completes safety Outstanding support formula blocks the warship that lands.Block landing similarly in continental rise airport.

Meanwhile declining aircraft after the flight scanning sensing on jet runway, to decline aircraft, realize by artificial intelligence control The warship control of system turns to switch to, by the remote infrared in decline aircraft, to the dedicated short distance of type aircraft carrier deck compressed air gas injection From jet runway, eject the gas laminar flow of Multistage Membranes grade laminar flow clip, block decline aircraft, slow down warship, realize flight Member in aircraft can actively, unmanned plane decline can be used full intelligence system safety manipulation aircraft decline actually block effect.

The jet-propelled flexible obstruction system is to have been able to the states such as weight, speed according to carrier-borne aircraft when homeward at present, at any time The energy absorption rank of arresting system is modified, so that rationally control carrier-borne aircraft is formed by film grade in each region on flight-deck Laminar flow, which blocks, stops distance, so that carrier-borne aircraft is blocked the prevention data of gas film grade laminar flow folder by injection, carrier-borne aircraft is blocked and is parked in finger Accuracy when positioning is set is 95% or more, and former check cable blocks warship point and is always not achieved.

At this moment, the decline aircraft after gas laminar flow arrestment is sprayed by District 7 domain, realizes safe falling.At this moment forward and backward Or the indicator light on the runway wheel of left and right is green.The staff and instruction personnel for wearing green clothing occur at the scene, will Landing aircraft is dragged in seat in the plane or hangar.Note：In fact, when the aircraft taxi to land to compressed air gas injection special short distance When the 5th (upward jet angle or upward jet angle of 20 meters of long, each jet ports for 25-90 degree) region of jet runway, At this moment three wheels in left and right, substantially fixedly land on jet runway deck in situ before or after the aircraft to land, as follows Aircraft is also small movement for drop, at this moment, pilot can natural Jian ski-running Hang Brake vehicle safely, but the aircraft to land is still empty in compression It can 100% be outstanding drop positions warship on gas gas injection special short distance jet runway, it is dedicated by compressed air gas injection Short distance jet runway slowly slides the aircraft that the reverse outstanding support formula that the aircraft of landing is formed blocks gas laminar flow and landing used Property the support lift-type air-flow that is formed, after the two reverse air-flows intersections, by the aircraft of landing quickly, safety, naturally slowly exist Short distance hangs support formula and slides landing, until by each puff prot injection gas source of jet runway injection gas source all by electromagnet cut off valve Switching control, aircraft front and back wheel could greatly improve the peace of each wheel and damper thoroughly in origin position warship stress The service life is entirely used, to save a large amount of maintenance costs.

When landing aircraft taxi to compressed air gas injection special short distance jet runway the 6th (20 meters of long, each sprays Loophole is the upward jet angle of 55-65 degree) region when, pilot can achieve the normal manipulation aircraft landing of safety after, automatic control The standard of brake, aircraft taxi after landing to jet runway the 7th (20 meters of long, each jet ports be 25-30 degree to Upper jet angle) region when, the aircraft after landing thoroughly lands on compressed air gas injection special short distance jet runway, real Safe falling is showed.It is general to take off with landing all in the 4th to the 5th region, safe falling can be normally completed.

The 5th region is slided into when declining aircraft in decline, when such as blocking incessantly, at this moment the 6th, each puff prot in District 7 domain The angle that needs are taken off to decline is automatically switched to, at this moment pilot can safely go around aircraft pull-up.

When carrier-borne aircraft " inclination of the yaw biasing heart, up and down sink-float " in the from first to the 7th arbitrary region of the aircraft of landing, by pressing Contracting air sprays gas laminar flow on dedicated jet runway, " the yaw of the lateral each injection gas laminar flow amendment decline aircraft in left and right The inclination of the biasing heart, righting of rising and falling up and down ", correction effect reaches 95% or more, this is at present using blast injection gas Preferred plan of the laminar flow to amendment decline aircraft " inclination of the yaw biasing heart, righting of rising and falling up and down ".

Note：Aircraft land in each jet angular zone of compressed air gas injection special short distance jet runway, receives and comes from The compressed air gas laminar flow that each region sprays can be to being landed such as using wet fog type, the viscous gas laminar flow of proportional moisture What aircraft can improve contrainjection humidity formula gas laminar flow blocks viscous drag.So to landing aircraft compressed air gas spray When penetrating, such as using humidity when the mixing air gas film grade laminar flow of 5-15% blocks, it will improve and blocked to landing aircraft Power, effective percentage is in 5-15%, and the general humidity of blocking of wet mixed air does not exceed 35%, the wet mixed more than 35% When air gas film grade laminar flow blocks, it will not improve again and power is blocked to landing aircraft, because of 35% wet mixed air It is the critical limit to various metal object greatest viscosity resistances.The dry-and wet-type combined air flow will not influence the landing of landing aircraft Safety less will cause to aircraft integral body or hang the damage of bullet weaponry.To the compressed air gas for spraying to landing aircraft Body laminar flow, temperature is generally minimum to cannot be below subzero 10 degree, and maximum temperature is 35 degree, and general normal temperature is positive and negative 5-10 degree. Compressed air temperature is such as too low, will cause deformation to the overall structure of landing aircraft, general compressed air is all to pass through constant temperature It is stored in air accumulator afterwards, is released after being also to be regulated and controled by thermostatic control in outside release, do not have the too big temperature difference.

On intersection connecting pin transverse direction position between seven regions of compressed air gas injection special short distance jet runway, It is all respectively equipped with line-up's work and intelligently adjusts manipulation and control, the injection of water purification humidity size misty rain adjuster jet blower. It is certain no more than 45% humidity when using injection misty rain gas, it otherwise will cause what high pressure gas was formed with hydrone thick fog Water vapor bubbles.Note：Using spray misty rain gas when, special consideration should be given to decline aircraft entirety hull-skin temperature, first using with Decline the gas stream of aircraft entirety hull-skin temperature phase matching temperature, misty rain injection that could be with high safety to decline aircraft is blocked Resistance.The gas stream for spraying humidity is too big with the whole outer surface temperature difference for declining aircraft, will cause to aircraft entirety aspect deformation and Rising-heat contracting-cold can constitute the damage etc. to internal each component.When reaching 20-25 atmospheric pressure such as compressed air gas stream, humidity No more than 45%, it otherwise will cause water vapor bubbles and spray to landing aircraft, it will form the air blast aqueous vapor formed to fuselage position Steep the hidden danger of erosion.

Note：The mixed gas stream of the high pressure humidity sprayed cannot with the naked eye perceive mist, otherwise will affect pilot's decline When visual effect and safety.As decline aircraft be 400-500 tons of weight, humidity mixed gas not less than 200- The granular hydrone gas laminar flow of 250 purposes；As decline aircraft be 600-750 tons of weight, humidity mixed gas Not less than the granular hydrone gas stream of 180-200 purpose, water spray is generally no more than 45%.Water spray is such as more than When 45% its viscosity of decline aircraft is blocked by power is remained on be 35% effect, this is the critical of water mist viscosity maximum saturation Limit.Equipped with misty rain jet blower, its biggest advantage can put out a fire in time to kindling decline aircraft, and in fire extinguishing, water spout can be with 100% It opens.

It is to continental rise airport and aircraft carrier decline aircraft on compressed air gas injection special short distance jet runway, seven above Decline process on the region a region Zhong Ge.In actual application for declining aircraft, depended mainly in decline every The practical manipulation professional standards technology of a pilot itself.Because compressed air gas injection special short distance jet runway, is Takeoff and landing at present it is most safe, most reliable, take off it is most fast, block decline it is most fast, be that current pilot's landing most has safe guarantor The flying platform of barrier takes off or complete basis of landing thus on compressed air gas injection special short distance jet runway The practical manipulation level professional technology of each pilot itself determines, to taking off or area of the aircraft on a certain jet runway of landing Optimal landing position is realized in domain.In short, the landing on special short distance jet runway, does not have unsuccessful or landing of taking off Unsuccessful various accidents occur, and third region of most of pilot on the jet runway is all answered between the 5th region Smoothly complete landing.The jet runway biggest advantage be by pilot in machine, each region puff prot angle, air pressure is big Small best match mutually manipulates, it can greatly improve the quick landing efficiency with safety, meanwhile, more obviously investigate The height of each pilot manipulation level.

In the above process, film grade laminar flow clip injection gas stops system, the film that endlessly each region can match Grade laminar flow clip blocks injection gas laminar flow, sprays to the carrier-borne aircraft of decline, makes the huge kinetic energy for declining carrier-borne aircraft, is converted into spray It emanates quickly abatement whole to decline airframe after body laminar flow, and by the way that endlessly injection gas blanket flow circulating system will It is discharged, to achieve the purpose that rapidly deplete the huge kinetic energy of carrier-borne aircraft self inertia torque to decline aircraft flexibility.From carrier-borne Machine opens front and back undercarriage hatchcover, opens that time that flap is engaged with damping umbrella, until in 3-5 seconds, in film grade layer In the outstanding support gas field that stream clip gas blocks, running speed is reduced to zero, and carrier-borne aircraft is constantly by from dedicated jet runway On, the gas film grade laminar flow folder that each gas ejection ports eject forms 1-2 grades to decline aircraft itself bring gas laminar flow The floating type of film grade laminar flow clip blocks.Gas stops the size of the braking moment of system, depends on pilot in machine Manipulation and control.

By gas ejection ports gas film grade laminar flow each on dedicated jet runway press from both sides, constantly by from continental rise airport aircraft with it is carrier-borne Machine decline when, slide with wash away during road machine the mapping for interact moment of inertia, aircraft decline when, slide and wash away process In moment of inertia and jet runway on the air-flow of both injection gas film grade laminar flows while mutually form after collision, the two After gas stream mixes within moment, the respective primary air being fused into one is the percent of a certain air blast by rapidly neutralizing It is several or be zero, it the air-flow of the two is fused into primary air acts on and decline is run in continental rise airport aircraft and carrier-borne aircraft in jet The a certain region in road realizes in rapidly moment and slows down to the safety of decline aircraft.Meanwhile dedicated jet runway continuously sprays The strong film grade laminar flow folder of gas, after quickly lagging formula deceleration to the inertia force of decline aircraft, at this moment, decline aircraft is come from once The gas laminar flow of the outstanding support formula of the safety of dedicated jet runway gas field blocks control.Support formula is hanged using compressed air gas high current Block decline aircraft, be theoretically finally attained by it is 100% safe and accurate, reliably the locking of various aircrafts blocked.

It is described to be slided or the aircraft carrier of VTOL aircraft device, naval vessel, continental rise airport land and water platform jet with efficient short distance Runway device, including：A variety of gas supply gas sources, the screw air compressor assembly, air accumulator, various air pressures of industry use at present Table, various pneumatic self-controlled valves, gas storage moisture trap, deflation moisture trap, storage gas gas cooling and gas heating sense Air supply parts or the equipments such as device, the various gas pipelines of deflation silencer, the relatively mature technology that current each industrial application can be used are fixed System.

One, it is formed using pneumatic system on the jet runway by compressed air gas supply gas source second-mission aircraft landing.Pneumatic system Also as hydraulic system, electrical system, mechanical system, including transmission system and control two parts.For the purpose of transmitting power, The system being made of a kind of dynamic Control original part such as control pressure, flow, direction and execution original part, referred to as pneumatic actuator system. By a kind of signal control original part such as sensor, logical operation original part, automatic controller and servo valve and execute original part, feedback original part The signal transmission operational loop of composition is known as pneumatic control system and discontinuous control system.

Two, it on the whole, using the pneumatic system by compressed air gas supply gas source, is made of following four part.1, gas source：It is wrapped Include air compressor, air accumulator, air cleaning facility and gas pipeline etc..It is provided for pneumatic equipment clean, dry has The compressed gas of steady pressure and enough flows, it is the energy source device of pneumatic system.The core of origin is air screw compression Machine, the mechanical energy of prime mover is converted to the pressure energy of gas by it.2, original part is executed：It is the pressure energy gas into machine Tool energy, the mechanical movement means of the practical external work done of pneumatic system.For linear motion is cylinder, makees to swing or rotary motion It is gas motor.3, original part is controlled：It includes dynamic Controls original part and the sensings such as pressure, flow, unidirectional direction valve, constant pressure self-adjusting valve Device, injection gas refrigeration and gas heating sensor, landing aircraft injection gas runway on " yaw the biasing heart inclination, on A kind of original part of the conversion of the signals such as lower sink-float righting " sensor logic original part, servo valve, logical operation and amplification.They are determined The operation law of pneumatic system.4, original part is assisted：They are to guarantee that activation system works normally indispensable original part, there is oil Day with fog, silencer, pipe fitting etc..

Three, the characteristics of pneumatic system：1, pneumatic system is adaptable.Its working media is air, inexhaustible, nexhaustible. It has fire prevention, explosion-proof, anti-tampering, resistant to pollution performance.It also can under subzero 60 degree or 80 degree of temperature condition above freezing It works by ground.2, device structure is simple, manufactures, is easy to maintenance, the service life is long.3, easily controllable, appropriately adjust compressed air Flow, pressure, direction can be achieved with to the various angular speed of landing aircraft " inclination of the yaw biasing heart, up and down sink-float ", power and position Control.4, high degree of automation.It may be constructed various automatic control systems, can also with the composition such as electronics, machinery machine, The integrated artificial intelligent control system of electricity, gas.The especially widely available and application of computer, and be the development of pneumatics Provide more wide prospect.5, self-insurance ability is strong.Air compressor is turned off, can still be made respectively by the expansion character of gas It stores blow-off system and maintains stable an injection landing flow and pressure.

Four, the whole active set area for each frame carrier-borne aircraft fuselage being equipped with by current aircraft carrier is 50 ㎡, carrier-borne aircraft from weight For 1/ frame of 30-40 ton, the operating air pressure of jet runway is 8kg/c ㎡ (10-20kg/c ㎡ can also be used) calculating：Thrust=40 P ㎡=400000 ㎡ × 8kg/c × 8=320 Τ；45.7 Τ of effective push is in desirable the 1/7 of thrust that calculates, in the jet of 40 ㎡ Puff prot needs to open total injection bore of (gross area of each jet port) 5-6 ㎡ on runway, can push 40-48 Τ, gas Flow is 21.66m³Meter per second, one airplane of landing need 6-10 seconds；By 10 seconds landing one single rack time, every landing one single rack time Aircraft needs gas consumption 217m³, along with various natural wastage 20% of the gas source on jet runway, add departing aeroplane It itself takes off and is formed by p thrust of climbing than disregarding, practical every one single rack of landing time aircraft needs gas source 260m³It can be from It is aerodynamic theoretically to complete.

Five, the overall space volume of a block matrix plate (abbreviation runway valve body plate module) is：V=2000mm × 1000mm × 100mm=200,000,000=0.2m³。

Six, runway determines 140m long, and runway beam overall is 40-60m, and spatial volume is：V=0.2m³× 140 pieces × 60 pieces= 1680m³。

Seven, air compressor motor selects JS or JR series：Select Q ﹥ 100m³/ min (Q air compressor machine discharge capacity), P ﹥

100mpa(pkg/cmg²) operating pressure：Single-machine capacity, single machine rated power are 260KW；260KW × 4=1040KW (supplying four to six runways), general power 1040KW.Air compressor machine output flow is Q ﹥ 100m³/ min (rice³/ point)；Air compressor machine output Pressure is P ﹥ 100MPa (separate unit machine).

Eight, a rotary shaft, shaft sleeve valve gate slot shape mouth, axle sleeve valve circular port, telescoping valve gate-type flute profile mouth, telescoping valve gate-type circle Hole shape mouth, universal Ball valve circular orifices, each jet port throttle hole area：1. throttle orifice open full width be 3mm, a length of 1500mm, Area is：F=1.5m × 0.003m=0.0045m²× 12=F0.054m²；2. it is 5mm that throttle orifice opens width entirely, a length of 1500mm, area are：F=1.5m × 0.005m=0.0075m²× 12=F0.09m²；It is 8mm that 3. throttle orifice opens width entirely, A length of 1500mm, area are：F=1.5m × 0.008m=0.012m²× 12=F0.144m²。

Nine, a block matrix plate throttle orifice opens the gross area entirely：Per a length of 2000mm of single block matrix plate, width 1000mm, between centers Away from for 75mm；It installs rotary shaft (shaft sleeve valve gate slot shape mouth, axle sleeve valve circular port, telescoping valve gate-type flute profile mouth, moving sleeve valve Formula circle hole shape mouth), it is 12 1/ piece；It is 1/ piece of dozens of that it, which installs multi-directional ball (universal Ball valve circular hole jet port),；1. F is total =(0.54m²)；2. F is total=(0.09m²)；3. F is total=(0.144m²)。

Ten, projected area：On jet runway, a length of 25m -30m, width are 16m -20m：1. effective area, F1=25m × 16m²=400m², F2=30m × 20m²=600m²；2. work area：F1=40m × 40m²=1600m², F2=50m × 40m²=2000m²；3. throttle hole area：F1=0.054m²× 40 (length) × 20 (width)=43.2m²；The gas vent gross area is： 43.2m²；F2=0.09m²× 40 (length) × 20 (width)=72m²The gas vent gross area is 72m²；F3=0.144m²× 40 (length) × 20 (width)=115.2m²The gas vent gross area is 115m²；4., flow is supplied to air outlet hole mouth in pipeline gas supply flow, main pipe Flow：Q1≤25~30m³/ mia (rice³/ point)；Q2≤30~40m³/ mia (rice³/ point)； Q3≧50m³/ mia (rice³/ point)； 5., appearance V (air space) air compressor machine of air feed tank carry tank：VC1=0.3Qm³(≈9—10m³)；VC2=0.2Qm³(≈8m³)； VC3=0.15Qm³(≈7.5m³)。

11, pipeline compressed air mean flow ū≤25m/s (meter per second)：Mean flow rate in critical state.

1, a joint discharge orifice opens flow entirely and is：Q1=20m/s × 0.045m²=0.9m³/ s=5.4m³/min：Q2=20m/ s×0.0075m²=0.15m³/ s=9m³/min：Q3=20m/s × 0.012m²=0.24m³/ s=14.4m³/min。

2,12 joint orifice discharge Q of block matrix plate installation are：Q1=64.8m³/min；Q2=108m³/ min, Q3= 172.8m³/min。

12, it is equipped with 4-6 jet runway in type aircraft carrier deck, is 1000- in the maximum volume of whole air supply source air accumulator 2000m³, air supply source air accumulator can also be divided into 2 to 4 tanks, the maximum volume of each tank is 500m³2 tank equal portions or 500m³ The setting of 4 tank equal portions, will can be gone here and there between each tank gas circuit or and even, also may be switched to it is independent or only to certain runway it is normal, Emergency or back-up system gas supply.

According to 1/ single-machine capacity：Single machine rated power is 260KW/h；Air compressor machine output flow is Q ﹥ 100m³/ min (rice³/ Point)；Air compressor output pressure is P ﹥ 100MPa (separate unit machine).260KW/h=air compressor machine output flow is Q ﹥ 6000m³/h；Single machine Rated power is the power consumption per hour of 260KW/h × 0.50 yuan/KW=130 yuans, can assist one frame of jet runway landing It is 7-10 seconds that 30-40 tons of aircraft, which needs the time, per second to need gas flow for 21.66m³The every landing of/s=one single rack time flies Total gas source is 217m required for machine³, along with various natural wastage of the gas source on jet runway are 20%, actually Compressed air gas source required for the aircraft of every 30-40 tons of one frame of landing weights is 260m³/, h=air compressor machine output flow is Q ﹥ 6000m³/h÷260m³=23.8 single rack time, single machine rated power are 260KW/h × 0.50 yuan/KW=130 yuans of power consumption 130 yuan of ÷ 23.8 single rack time=every one single rack of landing time aircraft institute's power consumption expense is 5.63 yuan by amount.To the above compressed air Gas is in the actual effect of this runway landing aircraft, and only simple theoretical calculation, in specific practice and need to also spray in next step The school of gas runway flies to find out more more accurate theory and technology parameters in test.

When aircraft carrier navigates by water in wave, the plane irregularity on deck is moved, will make carrier-borne aircraft usually with " eccentric biasing boat inclination, The state hook rope of sink-float up and down " blocks, and is in breakneck state；And compressed air gas blowing type is formed by gas blanket Stream, to landing aircraft can realization safely and fast hang the sliding drop of jumping up of support formula, the biggest advantage is to will decline " the bias of aircraft Or yaw and tilt, rise and fall up and down " gas laminar flow is sprayed by dedicated puff prot, it is sprayed in gas field in outstanding support formula aircraft is declined It is constantly modified, greatly improves accurately blocking off-position and set to decline aircraft warship point.Carrier-borne aircraft, can be by decline The flexibility sprayed on jet runway inversely damps strong gas laminar flow.Meanwhile carrier-borne aircraft is also by the jet runway, by Strong gas laminar flow is stirred in the flexible longitudinal damping that the swingable Universal-head longitudinal direction puff prot in each region sprays, and is constantly declined to correct " inclination of the yaw biasing heart, the up and down sink-float " of aircraft, laterally reverse gas stream can longitudinally stir gas blanket to the outstanding support of decline aircraft The constantly amendment to decline aircraft " inclination of the yaw biasing heart, up and down sink-float " is flowed, longitudinal each jet port of each swing can be used Gas laminar flow is sprayed, can quickly form the amendment of the various states of sink-float etc. up and down of positive and negative peak value to decline aircraft.Meanwhile it can put down Weigh it is outstanding hold in the palm decline aircraft, there is no " yaw the biasing heart and inclination, up and down sink-float " various hidden danger, decline aircraft can be fast Speed is hanged with injection gas like clockwork and holds in the palm and elapsed safely onto the position of warship point.Each transverse jet port of jet runway The effect that is played of positive and negative buffer gas laminar flow, same quickly amendment is to decline aircraft " the yaw biasing heart, up and down sink-float " machine The sliding track of running of the inclined aircraft of body is rectified a deviation, and efficiency can reach 95% or more.

It is that can protect in the effect played usually for the buffer gas laminar flow that the lateral symmetry air curtain jet port of runway or so sprays The intensity of main gas laminar flow needed for landing is ejected in longitudinal direction on each dedicated jet runway in region, meets landing aircraft institute as far as possible The gas source effect of the 65-80% needed.Dedicated jet runway is 65-85%, dedicated jet to the utilization rate of departing aeroplane gas source Runway is 65-80% to the utilization rate of decline aircraft gas source, and the appearance of the dedicated jet runway, breakthrough making up and thoroughly taking The various insufficient defects of landing are blocked in the catapult-assisted take-off or check cable that this current field of generation uses, and are catapult-assisted take-offs or are blocked Rope always cannot be comparable, it is that mutually compatible high-tech jet runway is blocked in a kind of takeoff and landing.Dedicated jet runway Injection gas laminar flow performance and setting are blocked to decline aircraft, to carrier-borne aircraft under the yaw state of " yaw the biasing heart " It blocks that off-position is set, acceleration peak value influences, can fully and completely eliminate, stop " inclination of the yaw biasing heart, upper sinking with blocking to amendment It is floating " decline aircraft, theoretically can reach 95% or more the controllable variations that will not overstep the limit, each region circle will not be surmounted, for Decline the deceleration feature of aircraft, has 95% or more apparent artificial intelligence automatic control adjustment effect on ground run distance jet runway.

Dedicated jet runway, blocking the allocative efficiency that outstanding support formula gas stream is theoretically set to decline aircraft injection can distinguish For；Effective braking gas in injection to decline aircraft nose landing gear cabin is 20%, is injected to having for rear left undercarriage cabin Imitating braking gas is 20%, and effective braking gas in right landing gear cabin is 20% after penetrating, sprays into flap and effectively subtracts Fast gas is 25%, and spraying into the effective braking gas of left and right wing elevator is 40%, is sprayed under decline aircraft integral body Portion or the effective braking gas of carry are 10-15%.Under normal circumstances, dedicated jet runway sprays gas blanket to decline aircraft Stream, is all greater than equal to 30%-20%-10%.It is distributed by slowing down, jet runway blocks decline aircraft with gas every time, all The gas source for subtracting natural wastage, using greater than decline aircraft self inertia torque 10-30% is the 1st film grade laminar flow folder, Realizing it quickly to decline aircraft to self inertia torque is that the gas that the 2nd film grade laminar flow presss from both sides blocks in 10-20%.

It is a kind of it is with artificial intelligence high-tech technology manipulation and control, can efficiently be able to satisfy wing type it is various by sliding jet The aircraft of runway landing, in 30-60-80-100-120-140 meters on the dedicated jet runway of very-short-reach, realization safety, Quickly slide lifting gear.Gas flight landing jet runway is sprayed in short distance, greatly optimizes current aircraft carrier ship-board aircraft Sea stand alone type, packaged type or can separate assembling airbag telescopic type landing platform, marine vessel disjunctor can Split assembled Formula airbag telescopic type landing jet runway platform, marine fixed or packaged type landing platform, the flexible dragon of marine charge-discharge air bag Band or actor playing a supporting role's formula platform, continental rise sky frame can seperated or combined console jet runway, to fly for the landing of various aircraft Safety guarantee.

Technique device science applies：Hydrodynamics and aerodynamics, the flexible uniform outstanding support of intensity injection gas stream Promotion aircraft lifting and landing technology.It is quick, safe, intelligent to various carry-on high-effect, high-tech in aviation field Landing improves decades of times or more, and breakthrough realizes to various damaged aircrafts and breakdown plane, is theoretically attained by 95% safety emergency landing, and the aircraft that do not open again to injured, failure or undercarriage, will not bring secondary damage or report It is useless, it can be achieved that safety, harmless gas shield block landing, to obtain carrier-borne aircraft on angled deck landing runway most really Deceleration be not required to long sliding race process and path lands, finally the off-position that actually blocks of carrier-borne aircraft is set and is more accurately calculated, and As guidance, the claimed range of the principal dimensions of dedicated jet runway flight-deck landing runway is set to and solves takeoff and landing Main problem.

Also, it is equipped in the jet runway：The gas of multiple universal globe sleeve type valve circle hole shapes of artificial intelligence manipulation and control The size of body jet port, gas flow adjusts control, and the gas that will change each region by the air pressure valve artificial intelligence in each region The variation of the size pressure of pressure regulator valve can be changed the integral pressure flow of the injection electromagnet cut off valve size in each region, will spray Gas laminar flow inversely to the required front and back fuselage entirety lower part for sliding landing aircraft, the entirety of each lower portion of front and back wing, By on the whole stress surface of the type aircraft gross area of all sizes, eject greater than 1: 1 ratio of landing aircraft gross weight amount Two kinds of optimal gas laminar flows of upward outstanding support lifting more than multiple, theoretically can 100% realization all size wing type aircraft peace Entirely, the artificial intelligence of quickly landing adjusts two kinds of gas laminar flow control devices, and landing Harrier or straight can be achieved in situ Rise aircraft.Required vertical-lift air-craft receives the strong injection gas blanket of flexibility of large area on jet runway in jet platform original place In flow direction.At this moment, after departing aeroplane receives the outstanding towing force of injection gas, it can vertically hold in the palm naturally and be raised to 10-25 meters of high-altitudes.Work as gas When pressure reduces therewith, the landing aircraft safety after being blocked can be realized and hang the original place vertical landing of support formula.

Using a variety of gas supply gas sources of the invention, dress is set on the dedicated jet runway of various aircraft aircrafts by compressed air, By multiple inside and outside rotary sleeve sleeve control valve flute profile mouth gaps or multiple inside and outside rotary sleeve sleeve control valve circle hole shapes Gas ejection ports gap, by multiple telescoping valve gate-type flute profile mouths or multiple telescoping valve gate-type circle hole shape mouths or multiple multi-directional balls Face sleeve type valve controls the gas ejection ports gap of circle hole shape, and the size shape gap of gas ejection ports can be changed, and is formed to institute Departing aeroplane is needed to realize safety, quickly eject the size of pressure proportional and the size of gas flow, the gas set by each region The adjustment control of body pressure regulator valve artificial intelligence.The jet-stream wind time normally in 5-8 seconds, departing aeroplane can be realized it is most safe, The outstanding high-altitude of normally taking off held up in 10-15 meters of stable rapid and natural, the available gas stream in jet runway overhead reach as high as To 25-30 meters of height, gas pressure must guarantee in 15-20 technical atmosphere, can also be according to the landing of landing aircraft It needs, is adjusted by pilot's automatic control.General landing aircraft is most completed in 3-5 seconds every fastly after entering dedicated jet runway The landing of one single rack time is most substantially finished the Normal Take-Off And Landing of each single rack time in 8-10 seconds slowly.

Aircraft is in dedicated jet runway landing, by between the inside and outside rotary sleeve sleeve control valve flute profile mouth of multiple shapes The gas ejection ports gap of gap or multiple inside and outside rotary sleeve sleeve control valve circle hole shapes, by multiple inside and outside rotary sleeve sets Cylinder valve flute profile mouth or multiple inside and outside rotary sleeve moving sleeve valve circle hole shape mouths or multiple universal globe sleeve type valve circle hole shapes Gas ejection ports gap is sensed by the far infrared set on aircraft and is sensed with the far infrared set on jet runway, by machine road The sensing control distance and position of far infrared setting is opened by each afterflow diode signal, the gas pressure electromagnet cut off valve of each spout The adjustment of switch control and whiff pressure size, foring to required decline aircraft can be with the various angle of decline aircraft Form and change intensity gas ejection ports gap flexible, realize that safety, quickly to eject ratio pressure of different sizes most Good matched injection gas stream.Each jet port it is on and off be in the far infrared and runway that are set in landing aircraft The far infrared of setting is mutually in step sensing interaction, and the use most fast time in 3-5 seconds, landing aircraft is realized most safe, flat What steady quick deceleration, outstanding support formula were slowly landed blocks function, or is sprayed by the gas of multiple universal globe sleeve type valve circle hole shapes Loophole, the size of gas pressure and the size of gas flow adjust control transformation by gas pressure regulating valve artificial intelligence, to each gas The control of the gas injection up and down balance system of jet port 25-90 degree, for decline aircraft theoretically can reach 100% safety, Balance the actual effect blocked.

It completes to each airplane during take-off and landing, each gas ejection ports can be theoretically real in each region to landing aircraft Apply 100% security control.Since the performance of various aircraft is different, required control rises on general aviation aircraft jet runway every time The various aircrafts of drop all regulate and control transformation software by artificial intelligence, to the gas of the Multi-functional changeover compressed gas jet port of angle Pressure.It is self controllable it is reverse needed for take off or the entirety for the aircraft that lands, the size of the intelligent control gas pressure ejected, The airflow balancing that jet runway sprays can be achieved, can quickly boosting be risen to from the departing aeroplane that drives in the wrong direction, to from reverse decline The moment of inertia of aircraft itself is, it can be achieved that injection gas stream declines the Fast-Balance of aircraft to it and the buffering of flexible force is blocked.

The basic performance of the compressed air gas injection special short distance runway：The jet runway can be selected according to various types Its width, the unmanned plane jet runway width of general 1.5T-5T is 10-15 meters, landing main injection oral area be divided into it is 100-150 meters long Add 50 meters of pre- road, totally 200 meters.The unmanned machine width of general 15T-20T is 20-25 meter, landing main injection oral area be divided into 150 meters add before The road Hou Yu is each 50 meters long, totally 250 meters long.It is general can be used large, medium and small aircraft mutually be compatible with jet runway width be 40-60 meters, entirely A length of 140 meters, 200 meters -250 meters, the gross area is 5600-8400 ㎡ on jet runway, and total fully open area of spout is 400- 600 ㎡, practical each jet port is the big small path for integrally collecting area according to various types, and jet runway is set remote red by machine road Rays are shown in jet runway by entire landing aircraft size fuselage in the landing path of outside line or photoelectric tube transducing signal and aircraft Diameter velocity scanning afterflow formula is opened and closed each puff prot.Total jet amount maximum pressure is that (maximum can reach 30-40 to 8-20kg/c ㎡ Kg/c ㎡), it, can be by 3-28 tons in every 1 square metre away from the gross area on dedicated flight jet runway of the gas injection lifting force When the aircraft (6-25 meters of vertical ascent) of weight slides upwards, under the action of forming two inverted drafts, it can will slide aircraft and blow Support is to 25 meters of high-altitude or more.On the jet runway of 40 ㎡, the summation of each injection open area equipped with gas flow is 18 ㎡, By in the jet port gas flow practical application to second-mission aircraft landing of 6-18 ㎡, aircraft itself occupies the jet runway gross area and is In 40 ㎡, injection gas stream can push 320-800 tons of weights to go up to the air to 16-25 meters of effective height, occupy and spray in aircraft itself The gas runway gross area is the gas source loss that 40% is subtracted in 40 ㎡, and injection gas laminar flow is actually active to be pushed as by 192-580 tons Weight goes up to the air to 16-25 meters of effective height.

Theoretically, in every 1 square metre of area (in enclosed volume), 1 atmospheric pressure can hold in the palm the object for rising 1000 kilogram weights, In 1 square metre of area, the object for rising 10000 kilogram weights can be held in the palm with 10 atmospheric pressure, gas source first will be by 10 engineerings Normal atmospheric pressure.Such as be on jet runway of the invention it is open, gas supply gas source (in the case where pressure is constant) must It must continuously flow out in the quadrature that each jet port size is added, the summation air flow rate that each jet port is sprayed, It can be by tonnage weight ramped up by support object boosting support, to be only practical quadrature.In addition it is necessary to be pushed by institute The concave-convex curved surfaces of object contour structures it is lost to the gas source other than whole effective forced area, with whole effectively forced area Be only practical the done work accurate data of aerodynamics, blast injection pneumatics technology.

Theoretically, be usually in the external environment of the Nature 0.8 standard atmospheric pressure, when aircraft is in the outer of 0.8 atmospheric pressure When taking off in boundary's environment, departing aeroplane can only by itself it is single it is sliding run movement to increase speed, then and size The lifting wing to match cooperates completion to climb with lifting wing rudder, external environment of the departing aeroplane in 0.8 standard atmospheric pressure When inside taking off, departing aeroplane quickly accelerates by wing rudder to form the atmospheric pressure in the external world 0.8 to 0.8 atmospheric pressure pressure on runway The change of power and density, portion forms an outstanding support gas field upwards to the atmospheric pressure after being changed under the wings of an airplane, with departing aeroplane Running speed is continuously increased, and the density of the strong gas field in portion also sharply increases under the wings of an airplane, and the strong gas field for being enlarged density will be fast Speed effectively form a kind of pair of departing aeroplane suspend upwards support rise torque, note：At this moment departing aeroplane must be by complete machine body tune It is whole in the 8-12 degree safe normal angled that angularly upper outstanding support gas field is most preferably taken off, departing aeroplane only have 8-12 degree it is angular on climb Optimum efficiency of the real driving cycle of torque that angle can just be such that wing lower part is risen to pop-up with the gas of certain density up to 95%, If the upward angle of departing aeroplane is too small or too big, can all directly contribute to wing lower air density be deactivated it is vertical to Overhead discharges and wastes, and also will cause resistance when ramping up to departing aeroplane and air shear.Departing aeroplane It will cause serious air drag and air shear because angle is bad, angle is improper to will result in air once departing aeroplane manipulates The various future troubles of shear.It is that optimum utilization rises gas that sliding jump formula airfoil type aircraft, which is typically all angularly upper in 8-12 degree when taking off, The virtual value of field is 95%.Decline aircraft is generally all the land angle when 12-20 degree angle is most safe falling in decline, Decline aircraft uses the landing at 12-20 degree angle that can optimise the virtual value of gas field in descent to decline aircraft as 95%. It uses with the conventional runway of the sliding jump formula landing aircraft of upper angle in landing regulation and landing condition and landing standard, all determines One of the main reason for landing runway not can be shortened.

Jet runway of the invention can also harmless, safely control aircraft expeditiously landing after why shortening.In theory On, jet runway can produce the spray of above compressed air more several ten times larger than 0.8 normal atmosphere (An) in extraneous large natural environment Gas pressure is penetrated, the atmosphere of the compressed air 0.8 standard normal to the Nature in external environment within the scope of whole jet runway Pressure will be by the change of the various different angles and pressed gas sprayed in jet runway, when departing aeroplane is in the spray of very-short-reach When taking off on gas runway, when departing aeroplane is 20 meters long from the first area that pre- road slides into jet runway, at this moment, first area Air pressure be adjusted to 3-6 technical atmosphere, the angle of each puff prot in first area be adjusted to 25-30 degree angle inversely take off it is winged Machine ejects the gas laminar flow of outstanding support formula, when departing aeroplane slides into it is 20 meters of second area long when, at this moment, the air pressure of second area It is adjusted to 4-7 technical atmosphere, the angle of each puff prot of second area is adjusted to the reverse departing aeroplane in 35-40 degree angle eject The gas laminar flow of outstanding support formula, when departing aeroplane slide into third region it is 20 meters long 20 meters long to District 7 domain when, the gas in each region Body pressure and jet port angle are incremental entirely.The received 25- of departing aeroplane is not difficult to find out in the first area of jet runway The contrainjection gas at 30 degree of angles hangs the gas laminar flow of support formula, and gas pressure is 3-6 technical atmosphere, and departing aeroplane is first The angle of complete machine body is to be 3 times of former conventional runway 8-12 degree angle, be former normal on 30 degree angular when taking off on the jet runway of region 3.6 times of atmospheric density of 0.8 air pressure of runway the Nature is advised, departing aeroplane is changed flight angle on jet runway completely With rising angular speed.At this moment, first 0.8 air pressure of region of out bound environment the Nature will be by 3.6 times of sky on jet runway The air pressure of air tightness is quickly discharged to overhead or around, and general gas flow theoretically should all be 100% in outside release Lift-off completely, the injection gas released by the upward hovering support of gas of 0.8 atmospheric pressure of jet runway overhead external environment, Until lumping into equal pressure together with 0.8 air pressure of runway overhead.

The reason of jet runway can be shortened is taken off on different runways respectively just as using two airplanes：Such as one erect fly fly Machine take off on conventional runway 0.8 atmospheric pressure fuselage 8-12 degree of external environment it is angular on, needed for taking off from ground to 100 meters of high-altitudes Landing airdrome length；If a frame departing aeroplane takes off on jet runway, the gas of the external environment injection in whole runway is 3- 25 technical atmospheres, spray angle is 25-90 degree angle, on fuselage 30-45 degree is angular, is taken off institute from ground to 100 meters of high-altitudes Need runway take-off length.To the air that do not will cause after departing aeroplane change take-off angle to institute's departing aeroplane on jet runway Shear, be because jet runway respectively sprays the 30-45 that the compressed air that port is sprayed forms safely departing aeroplane naturally A kind of gas laminar flow for spending the outstanding support of angle auxiliary, will not be always with the spray at 30-45 degree angle to departing aeroplane certainly on jet runway It penetrates the high-altitude of aircraft boosting to 100 meters, only by departing aeroplane, the phase is difficult to the running speed completed to jet runway before take-off With the change for highly accelerating to the processes such as nature flying speed, when departing aeroplane accelerates to nature flying speed on jet runway When, fuselage equally is adjusted to match with the Nature external environment by departing aeroplane when being detached from the nature flight of jet runway The natural flight attitude of the safety at 8-12 degree angle.

Using a variety of gas supply gas sources of the invention, by the excellent of blast injection gas laminar-flow type landing general aviation aircraft jet runway Gesture is mainly reflected in following aspect：The operation of taking off of the injection dedicated jet runway of gas laminar-flow type landing aircraft is relatively pacified Entirely, preparation of first airplane on jet runway is only done before taking off；When flying from the recurrence of the second airplane, flight jet is run Road is almost not necessarily to prepare, and can accomplish airport landing aircraft or carrier-borne aircraft at any time completely, and carrier-borne aircraft is whole safe landing 3-4 times or more is improved when in actual efficiency when former catapult-assisted take-off；Carrier-borne aircraft during on the dedicated jet runway of landing, Landing aircraft is controlled each spray at the 0-180 degree angle of aircraft " inclination of the yaw biasing heart, up and down sink-float " by laterally each puff prot always The gas laminar flow that loophole sprays, the center point of adjustment landing aircraft to dedicated jet runway.The maximum effect of dedicated jet runway It can be exactly that the motion profile of landing aircraft can be moved along a straight line along jet runway always, the unfailing performance of manipulation is high, rises Drop efficiency is higher than 3-4 times or more that steam or electromagnetic launch take off.When landing carrier-borne aircraft crosswind, harmful air currents field etc. it is unfavorable because Under the interference of element, will not occur skidding off the various unsafe accidents of jet runway again, carrier-borne aircraft is enabled to guarantee higher Success rate drops.

Spray the air that gas laminar flow provides the mode of required landing aircraft, the gas laminar flow that can be sprayed by compressed air Power, realize larger quality carrier-borne aircraft take off or operation of landing, surmounted every single rack when current catapult-assisted take-off time gross mass It more than decades of times, is the quality launching landing and being always not achieved.In same model carrier-borne aircraft, if being sprayed using compressed air The dedicated jet runway of gas laminar flow mode of taking off, can than launch or slide jump formula take off with landing save great amount of fuel oil, increase Add 30% combat radius.Meanwhile more, heavier weapon can be carried make entirely to navigate to enhance carrier-borne aircraft itself fighting capacity The deterrent force that mother forms into columns is increased dramatically with fight capability.Injection gas laminar flow special short distance jet runway takes off or lands Mode provides larger space so that the flight-deck outer surface portion of entire aircraft carrier is fully horizontal for other deck operations.With adopt It is compared with the flight-deck of ski-jump take-off mode, injection gas laminar flow special short distance jet runway takes off or landing modes, flies Row deck fore body can a large amount of carrier-borne aircrafts of Boulez, effectively improve the utilization rate of flight-deck area.Largely, it saves Flight-deck cabin spaces below.

Carrier-borne aircraft injection gas laminar flow jet runway on landing process by atmospheric temperature, air humidity, sea conditions etc. no Predictable factor influences smaller.Taking off or landing for injection gas laminar flow special short distance jet runway, can be according to difference The relevant parameters such as gas laminar flow that compressed air sprays are adjusted in marine environment, overcome bad climate, bad sea situation to rising Winged or landing operation process influence.It during take-off and landing because of carrier-borne aircraft, is all to be sprayed gas laminar flow and hang support formula and take off to accelerate or hang Support formula blocks warship landing.It can be said that on the dedicated jet runway of injection gas laminar flow of the invention at present, it could be really real The all-weather safety of existing carrier-borne aircraft takes off or lands, is that most reliable takeoff and landing platform and the jet runway are led in aviation In domain development in an all-round way and emerge in large numbers.

Due to the presence of numerous superiority of landing jet runway of the present invention, sprays gas laminar flow special short distance jet runway and rise Fly or landing-type flight-deck, the jet-propelled wisdom traffic runway add market carrier that can be just product market, it from now on should It can be widely used in the conceptual design of large, medium and small type (unmanned carrier) continental rise airport and aircraft carrier.China's aircraft carrier And flight-deck design studies status, domestic scholars have done correlative study for aircraft carrier.But due to the U.S., Britain, Russia The states such as Ross, France possess design, construction, the experience using aircraft carrier for a long time, in aircraft carrier master-plan and research side Face has accumulated lot of research, and in this field, which takes off or the appearance and application of landing technology, Its advanced and practicability, security reliability, economy etc. make China this research field will all have become apparent it is advanced Lead over the advantage of other countries of the world.

Since the lift of the jet runway discussed is in open endoatmosphere, in type aircraft carrier deck, the race of each continental rise airport It is arranged on road.And atmosphere therefore, is formed by lifting to injection gas laminar flow in dynamic field, now for locating airspace it Atmospheric pressure, the lift from the plate unit area of level side, between atmospheric density, atmospheric pressure and air velocity Relationship, the pressure difference above and below plate referred to as rises strong.Jet runway is sprayed into the air velocity to different height, it is referred to as different Effective critical speed of height (alternatively referred to as air velocity rises the critical altitude being saturated by force).To jet runway air velocity, pressure Power, flow etc. also need to develop domain of function, can just obtain more practical, more accurate gross data.

By swaying the preliminary description of movement to warship face, discussion is swayed the limitation range to carrier-borne aircraft landing to warship face, to be focused on The pitching of warship face is analyzed, to influence of the carrier-borne aircraft when spraying the landing of gas laminar flow on jet runway, guarantees carrier-borne aircraft peace from determining The mother ship carrier pitching of full landing, which is swung, raises sleeping draw in terms of ship moves shortest time prediction technical research, to the homeward admission of carrier-borne aircraft Mother ship carrier itself sways problem in wave in journey, carries out more complete theory analysis interpretation and inquires into more beneficial, and Preferably to the theoretical validation of jet runway overall performance.

According to ship movement characteristic, the afloat navigation process of large ship, also by means of the measurement data and bow of ship movement The Time series analysis method of preceding wave number movement, will establish the mathematical model of ship movement, and provide the predicted value of athletic posture, Finally obtain satisfied ship movement prediction as a result, can make carrier-borne aircraft injection the dedicated deck jet runway of gas laminar flow on warship Safety, obtain being substantially improved in all directions；And can significantly demonstrate a variety of can carry out large ship athletic posture The dependable algorithm of short-period forecast, and further in physical simulation system, that acquirement is satisfied with injection gas specific jet runway, Not will receive the above various unfavorable factors limitation, could more precisely to modernization jet runway, provide one it is more scientific Theoretical definition.

Injection gas laminar flow continental rise airfield runway and dedicated deck jet runway on, the gas blanket flow resistance after aircraft landing block with In terms of gas hangs the research of support formula control technology, the outstanding support control of gas is stopped to the gas of continental rise airfield runway and carrier-borne aircraft landing aircraft Technology processed carries out careful research, and solves in these work to the power output of injection gas blanket stream arresting engine；Aircraft is spraying The Simulation Model of moderating process carries out largely beneficial to discussion on the dedicated jet runway of body laminar flow of emanating；When based on aircraft decline On instant airflow and dedicated jet runway, spray after both gas laminar flow and decline aircraft are hit in moment, certainly by decline aircraft The gas energy of body institute band all effectively with the release of injection gaseous exchange, propagate to can be most on each forced area of decline aircraft Good effective trim gas intensity, after the reverse gas phase junction of inertia for spraying reverse gas and decline aircraft itself institute band, The gas inertia power that the reverse gas of the two is eliminated after hitting is one hundred point of ratio that essence effectively blocks value.The reverse gas of the two After the stronger gas inertia power of one individual event is blocked, gone out gas inertia force is one hundred point of ratio of the virtual value of remaining strong gas, The above technical parameter can by ultrathin membrane data pick-up to injection gas stream aircraft warship block aerodynamics carry out analysis with Research；And it makes in the most accurate distribution technique parameter of each stress surface, is tested more than original using pneumatic we have invented a kind of Subject to exact figures times or more a kind of ultra-thin sensing membrane of new science and technology and computer networking measuring technology, by entire airframe lower part with Each wing lower part stick be we invent a kind of ultra-thin sensing electronic film of new science and technology, by electronic chip in electron membrane and computer Network test compressed air jet gas stream joins landing aircraft injection gas stream produced by it to the various technologies of landing effect The accurate acquisition of number data.It is all had than original by various measuring and calculation results using more than pneumatic measuring technology raising several times good Good accurate precision can lay good new science and technology basis for the pneumatic test of aviation field type aircraft from now on, can be pair The consistency problem of injection gas and the ultrathin membrane sensing of " aircraft arrestment power " work compound provides accurate various reference numbers Word, and propose that transverse direction when asymmetric to ship-board aircraft, eccentric warship stirs each jet port and changes injection gas blanket flow angle, Reach to the calculation formula method for stopping power.In view of stopping umbrella warship can be established the case where blocking the dragging of gas blanket flow damping Carry aircraft warship spray gas laminar flow Aerodynamics Model, carry out ship-board aircraft warship stop emulation and analysis and research, and point The influence of warship eccentricity and asymmetry to aircraft warship is analysed, and analyze the breadth wise dimension of warship eccentricity and jet runway Analysis and research.

It is analyzed by the loading characteristic to each component in each system, establishes injection gas laminar-flow air of aircraft during blocking Kinetic model theoretically obtains：It is blocked in the course of work on the injection dedicated deck jet runway of gas laminar flow, aircraft exists Spray the relationship that speed when gas laminar flow hangs the landing of support formula decays with displacement；Meanwhile it can be outstanding in injection gas laminar flow to aircraft In the undercarriage deceleration cabin of on coasting distance and flap when support in moment and front and back three, on front or rear wing rudder with resistance Blocking the pulling force on umbrella will comprehensively be estimated that (general aircraft is not required to set use or open to stop in jet runway landing Umbrella).But decline aircraft on jet runway open stop umbrella when effect be it is best, because can be produced in jet runway respectively That plants the injection gas 85% for adapting to block umbrella angle and various pressure pours obstruction umbrella.

Above-mentioned work will be classified as the landing of aircraft with power problem is stopped to injection gas laminar flow on dedicated deck jet runway Research object, but the solution of the retarding braking process to carrier-borne aircraft on flight-deck landing jet runway, research significance is great, Because landing aircraft, which is hanged on jet runway by gas, holds in the palm landing.Landing aircraft sliding on jet runway is taken off and subtracted Speed braking descent will press each zone gas spray angle, pressure flow and required landing type speed, type entirety respectively Collect the various sequences such as area to solve, study.To the injection gas laminar flow special short distance deck jet runway that aircraft carrier is equipped with, In the relevant technology of whole design, there are also many fresh courses to study, and also only belongs to the present invention one in the world at present.Both at home and abroad Academia is to injection gas laminar flow continental rise airfield runway and dedicated deck jet runway, unmanned plane jet runway, VTOL spray Gas platform, the Discussions of The Related Issues to flight and master-plan on landing aircraft jet runway or jet platform are almost Zero.But in recent years, the domestic correlative study for aircraft carrier " catapult-assisted take-off+obstruction landing " formula flight-deck starts to present The growth trend of blowout out, the jet runway are actually what mother ship carrier was made to measure.

To carrier-borne aircraft open wing rudder, in flap and noselanding gear well room, in rear left right landing gear cabin (will before or after The three undercarriage cabins in side left and right, it will be assumed that damp wind scoop for the deceleration to the reverse angie type in decline aircraft), and complete The gross efficiency for spraying the secondary recycling of residual air of gas laminar flow realizes injection gas laminar flow to the natural flexible strong of decline aircraft Air-flow is flexible to be blocked, and realize safe, steady outstanding support formula blocks landing effect.To flap or the movement after dragging umbrella of slowing down Process is studied, and flap or damping is slowed down, the various buffering support mechanical resistances on umbrella is dragged to block, and moves past journey to stopping drawing It is mutually tied with the principle of gas field force feedback of the injection gas laminar flow on dedicated deck jet runway after suffered gas laminar flow impact It closes, inquires into and carrier-borne aircraft " eccentric biasing boat " is opened in flap and noselanding gear well room, in rear left right landing gear cabin (by before or the three undercarriage cabins in rear left and right, the reverse angie type deceleration being set as in decline aircraft damp wind scoop) deceleration cabin hinders Buddhist nun, which is slowed down, drags umbrella, be according to the basic method for solving to deceleration feature on various devices, and by the gas laminar flow on each stress point The simulation calculation that effect is included in moderating process after wherein making to open carrier-borne aircraft damping umbrella is truer.

Factorization, to carrier-borne aircraft open flap, damping deceleration buffer support umbrella, supporting plate and nose-gear cabin, after (by three undercarriage cabins of front or rear side or so, the reverse angie type being set as in decline aircraft, which slows down, to be hindered in square left and right undercarriage cabin Buddhist nun's wind scoop), or damp to slow down and drag umbrella, the various characteristic indexs in moderating process are investigated, to carrier-borne aircraft in injection gas The obstruction school of laminar flow flies test and is investigated, and verifies to the accuracy of sequential operation result.

Different typical conditions is chosen, to different weight carrier-borne aircraft or unmanned plane, opens flap, damping with different homeward speed Deceleration buffer support umbrella, supporting plate, damping, which are slowed down, drags the cunning race process that after umbrella and will be damped after the cutting of umbrella deceleration jet gas field to carry out It investigates, calculated result is depicted as respectively " ground run distance flap, the left and right sides buffering pop-up umbrella, supporting plate, or damp to slow down and drag Tail chute load after umbrella slows down is damped after umbrella " curve, " ground run distance acceleration " curve, " one speed of ground run distance " curve etc., it is Carrier-borne aircraft under various different landings and homeward status condition is opened and nose-gear cabin, rear left right landing gear cabin (the undercarriage cabin of front or rear left and right three is set as deceleration damping wind scoop in the reverse angie type in decline aircraft), carrier-borne aircraft opening Damp umbrella after moderating process provide reference, and for spray gas laminar flow take off or landing runway Design of length provide it is more accurate Foundation.When 200 tons of aircrafts below are on jet runway, left and right sides buffering pop-up umbrella and rear molding drag parachute can not generally be beaten Open or do not set this left and right sides buffering pop-up umbrella and rear molding deceleration umbrella device.

To intrinsic angled deck angle, superstructure form and position on former aircraft carrier flight-deck, aircraft lifting and landing quantity with The problem of position, carrier-borne aircraft revolution etc. 4 has a major impact flight-deck master-plan is inquired into：Weight analysis take off or The angle of the landing injection dedicated jet runway of gas laminar flow, the influence to deck master-plan and carrier-borne aircraft operation safety, upper layer The influence of principal dimensions and change in location to deck airflow field is built, aircraft elevator quantity and arrangement form, which allocate and transport carrier-borne aircraft, to be made The influence of industry safety and carrier-borne aircraft are the method for solving of flight-deck upper rotary motion path the problems such as；To injection gas blanket Stream special short distance flight-deck jet runway takes off, and is inquired into the range division principle of 2 big functional areas of landing.Base In to above analysis and research work, the principal dimensions design considerations of take off area and dropping zone is summarized, to have large-scale aircraft carrier flight The characteristic feature on deck, the body profile for the General layout Plan for spraying the dedicated deck jet runway deck of gas laminar flow are Example will carry out having the new concept of comparison to illustrate, and at every place respectively to the form of each key position and scale Design principle The critical issue being considered as on the injection dedicated deck runway of gas laminar flow in design is described in detail.

For the flight-deck design studies on the injection dedicated deck runway of gas laminar flow, and former catapult-assisted take-off mode and check cable Landing modes are blocked in the design studies of flight-deck, the deck queueing theory for having a challenge for two kinds relatively after, to spray The dedicated deck runway quantitative design research of body laminar flow of emanating.Introduction queueing theory (i.e. theory of random service system) is research injection Gas laminar flow private track is in aircraft carrier landing, the mathematics branch discipline and operational research of deck crowding phenomenon and general The important component of rate.It is each to solve by studying probability nature of various service systems during waiting in line Optimal design and optimal control problem in system.Carrier-borne aircraft on aircraft-carrier flight deck is formed into columns, in former catapult-assisted take-off first Before taking off on plate runway, frequently appears in and wait in line phenomenon with after the runway of deck；And it sprays the dedicated deck of gas laminar flow and runs Road, the increase of the speed and quantity of landing are exactly to solve the most effective method of this deck " congestion " phenomenon.Jet runway is former Catapult-assisted take-off runway take off efficiency several times or decades of times the problem of, need to be compared practice.

Therefore, if attempted from queueing theory angle, the waiting process before setting out to carrier-borne aircraft is studied, and can not only be obtained The shipboard aircraft group obtained under theoretically different wave time takeoff conditions sets out ability characteristics；More importantly can also be from carrier-borne aircraft Group goes out the angle of kinetic force, and the dedicated deck runway of gas laminar flow is sprayed on exploratory flight deck, in the speed and quantitative design of landing Problem；In the flight-deck concept phase, an efficient operating environment just is provided for shipboard aircraft group.Currently, to the present invention Injection the dedicated deck jet runway of gas laminar flow overall quantity problem, be unfolded to further investigate.To injection of the invention Reference in terms of the dedicated deck runway of gas laminar flow is almost nil, this can only in the test of multiple theory and practice, More accurate answer is found out to verify a kind of technical parameter effect that this patent jet runway is most accurate, more practical.

In the present note, temporarily have ignored it is some can be on the injection dedicated deck runway of gas laminar flow, shadow to a certain extent The complicated factor that carrier-borne aircraft goes out kinetic force is rung, as flight-deck emergency event disposition, marine environment are time-consuming to carrier-borne aircraft allocation and transportation It influences and staff's operation qualification services injection gas system layer stream time-consuming influence etc..Merely from theoretical angle Degree analysis：The correlation of sequencing problem and the flight-deck injection dedicated deck runway quantitative design problem of gas laminar flow.By right The analysis and discussion of different typical case's queue theory model scope of applications, final determine are suitable for solving flight-deck injection gas laminar flow The carrier-borne aircraft queuing model of the quantitative design problem of dedicated deck track systems, clearly injection gas laminar flow dedicated deck runway system System quantity, contacting between average waiting time-consuming before being set out with carrier-borne aircraft；And exploratory flight person is in landing on jet runway, Itself contacts the manipulation technology in machine road with time-consuming.It illustrates that flight-deck sprays gas laminar flow by example calculation, to ejection and slides Jump deck runway quantity goes out the influence of kinetic force to carrier-borne aircraft, propose flight-deck based on queueing theory with to dedicated jet deck The research that runway quantitative design method and pilot guidance technology match.

Using queuing theory, the feasibility of the injection dedicated deck jet runway quantitative design problem of gas laminar flow is studied. Since the index that countries in the world aircraft carrier designed displacement, carrier-borne aircraft are equipped with quantity, flight-deck area etc. is different, adopt With the spray on the different aircraft carriers on " injection the dedicated deck jet runway of gas laminar flow take off+stop landing " mode flight deck It emanates body laminar flow, and dedicated deck jet runway quantity is also slightly different.Spray the dedicated deck jet runway of gas laminar flow Quantitative design is to influence an important factor for carrier-borne aircraft goes out kinetic force and deck operating efficiency and flight-deck General Layout Design In important link.In the aircraft carrier concept phase, the suitable injection dedicated deck jet runway number of gas laminar flow is determined Amount, should mainly consider to start in terms of two, i.e.,：From point of theory, studies and establish " the injection dedicated deck of gas laminar flow Jet runway quantity and carrier-borne aircraft go out kinetic force " between mapping relations, so that carrier-borne aircraft is set out some keys in capability study Index directly can form mutual concord with the quantity for spraying the dedicated deck jet runway of gas laminar flow.

The great advantage for spraying the dedicated deck jet runway of gas laminar flow, in landing different size aircraft, by the gas in runway The general jet runway that the aircraft of landing model of different sizes can be mutually compatible with can be realized in pressure increase and decrease, than former catapult-assisted take-off Or check cable stops landing modes, increases the utilization efficiency to jet runway of several times or more, and improve aircraft carrier The overall performance of runway.Both from flight-deck layout angle, carrier-borne aircraft allocates and transports efficiency, cabin spaces utilization rate, using spray The dedicated deck runway of body laminar flow of emanating will carry out best injection gas laminar flow to dedicated deck from the angle of service efficiency ratio The related demonstration of runway quantitative design.Since some countries there is no any construction with using the experience of aircraft carrier, cause It may influence the injection gas laminar flow of flight-deck, complicated factor (each area of such as flight-deck of dedicated deck runway quantitative design The problems such as domain division, angled deck scale and arrangement, deck house distribution are with planning).Currently, being surveyed to the runway Examination, is investigated demonstration, so that these theories are converted to the equipment of actual effect early, it is jet runway of the invention in each boat Man of home country is approved and is used.Before designing aircraft carrier flight-deck jet runway, also need to do the research in a little theories and practices Work.Because the jet runway is there is presently no mature actual combat equipment is converted to, only a patent document, therefore, To the theory and quantitative design demonstration of various drop datas of the injection dedicated deck runway of gas laminar flow of the invention, also To in multiple practical studies.

The fixed hypothesis shipboard aircraft group of example, inlet flow and service rate, before the injection dedicated deck jet runway of gas laminar flow takes off The condition being had：Aircraft-carrier flight deck is only provided with the portion the l injection dedicated deck track systems of gas laminar flow, or due to kind Kind reason, temporarily only 1 dedicated deck runway of injection gas laminar flow can be shipboard aircraft group, and it is dedicated to provide injection gas laminar flow Deck landing jet runway service.When carrying out allocation and transportation operation, ignore other uncertain factors, carrier-borne aircraft is added by afterflow of parameter Waiting list, every frame carrier-borne aircraft receive the landing on the injection dedicated deck runway of gas laminar flow, spray gas laminar flow operation process Independently of each other, and cargo handling operation time-consuming obeys parameter as quantum condition entropy.

The landing of mode, aircraft carrier landing above deck are blocked for the above former ejection, former sliding jump, former check cable, arresting net Generated various insoluble statuses may be implemented that a variety of gas supply gas sources can be used with of the invention completely, empty by compression The data-link of gas jet gas laminar flow special short distance runway artificial intelligence control implements docking.Manual intelligent control of the invention International most mature virtual reality technology (being also augmented reality or augmented reality) at present can be used, by flying in mode processed The visualization helmet of member, can be constantly on gas injection runway of the invention, (during take-off and landing by the various Dynamically Announces of aircraft Gas field control space size, shaped position variation), visualization helmet display device on show.Utilize virtual reality (enhancing Reality) realize the control of the various postures to landing aircraft on jet runway, and AES512 bit encryption can also be used IEEE802,16E transmission control instruction and a variety of sensing data chains docking, implement dynamic data chain posture artificial intelligence Control, come the various platforms of carrier-borne aircraft or continental rise airport etc. being directed on jet runway, realizes safe landing.

For now, in the case where the offline mode of aircraft or concept change without essence, the present invention is had reached At present to the technology singular point of various aircraft takeoffs and landing modes.If any runway technology can overcome aircraft to exist not yet The control technology of self inertia torque occurs on runway, and jet runway technology of the invention just can be rated as preferred plan.The injection gas The pressure and various angles of body laminar flow runway jet are all to realize most matched whiff pressure and gas outward according to environment, type Body uninterrupted.By intelligent control, the optimum pressure and angle of aircraft incision gas field are calculated, realizes noninductive incision.This Set system can type, the various postures of complete machine body collection area, speed, height, angle according to subject and object logic, aircraft Degree, quality and the speed of a ship or plane of aircraft carrier, the landing angle of aircraft, distance, levelness, gridding variation and external overall situation wind-force, wind Speed, wind direction, the high data chain relation of wave control aircraft on the jet runway, realize in each area spray in various dynamics The transformation of gas size pressure angle, can be used Programmable Embedded single-chip microcontroller, process control mesh model to control each injection Port can execute the adjustment of artificial Intelligent Dynamic control automatically.

The landing on the jet runway of continental rise airport aircraft and carrier-borne aircraft, when landing aircraft is in acceleration and deceleration, aircraft uniform stressed. Aircraft does not have big cause as when catapult-assisted take-off and check cable block landing in landing on jet runway within moment The impact sense of life property from physiology and psychologically protects the inherently safe of pilot, makes airplane complete machine body metal structure will not It is rushed again by as the various hardness that can not be controlled carrier-borne aircraft safety and nondestructive evil after catapult-assisted take-off, with check cable hook rope are fatal Sense is hit, the time limit of Aircraft life and military service is extended, extends the service life of aircraft carrier flight-deck, reduces aircraft front and back wheel Tire is seriously worn with deck runway.Landing of the dedicated jet runway to carrier-borne aircraft is all to hang aircraft lag formula is ask to take off Or it is outstanding ask lag formula to land warship, so that the front and back tire of landing aircraft and dedicated jet runway is not generated big friction, Use catapult-assisted take-off compared with check cable blocks landing with original, at most namely 5% frictional force, or even directly land without friction Stop, this is former to block that land always cannot be comparable using catapult-assisted take-off and check cable.

Dedicated jet runway is to the great advantage of carrier-borne aircraft landing：When marine stormy waves waves maximum angular in 35- in 12 grades, aircraft carrier When 40 degree of angles, carrier-borne aircraft still can safe landing, because landing aircraft once steps on dedicated jet runway, at this moment jet runway The gas laminar flow for being directed to or having dropped just is ejected respectively, accelerates quick lag formula to take off or outstanding support in gas field outstanding hold in the palm of aircraft Quick lag formula of slowing down in gas field land warship the advantages of；Aircraft carrier is waved and is risen and fallen up and down, in dedicated jet runway The carrier-borne aircraft go up, dropped will not have much impact, and wing type can also be slided to landing aircraft in jet runway On can the gas laminar flow that sprays of each jet port as you were by jet runway, departing aeroplane is vertically pushed to 15-25 meters The above high-altitude realizes wing type and slides landing aircraft, and the great advantage of vertical, safe landing can be achieved on jet runway； When wing type aircraft realizes VTOL on jet runway, landing aircraft is opened into engine first and is kept in engine Low speed, reverse runway heavy caliber spray lifting pipe, spray lifting pipe thrust gas with it and aircraft engine machine power is opposite etc., this When, each jet port of jet runway vertically ejects the gas laminar flow pushed up towards airframe lower part upwards, at this moment to rise Drop aircraft, which is achieved that, accelerates the two kinds of effects taken off or landed in outstanding support gas field.The dedicated jet runway landing carrier-borne aircraft can To reduce the working strength Yu technical difficulty etc. of ground crew on deck.Dedicated jet runway, can be a large amount of to landing ship-board aircraft Reduction aircraft fuel oil amount, be integrally improved the combat radius of aircraft 30%, can increase by 20% carry, as aircraft carrier this conjunction The subset of collecting system has filled dedicated jet runway of the invention once setting, can be embedding more perfectly in any kind of aircraft carrier The integrated closed-loop control for entering to combine aircraft carrier system itself, finally make aircraft carrier it is qualified become marine fast and safely landing Airport platform.

Detailed description of the invention

Fig. 1 a is of the invention slided by compressed air gas injection very-short-reach or the dedicated interior outer rotary shaft of Convertiplane Cover the gas ejection ports of moving sleeve valve flute profile mouth formula, or the gas with the multiple circle hole shape mouth formulas of inside and outside rotary sleeve moving sleeve valve Jet port, or the gas ejection ports with universal globe shell type without fixed sleeves single sleeve moving sleeve valve circle hole shape, or have The gas ejection ports of rotary sleeve and the double telescopic moving sleeve valve circle hole shapes of fixed sleeves, jet runway assembly in universal globe shell type , the surface structure schematic diagram of part；

Fig. 1 b is compressed air gas injection runway of the invention, and each valve body plate main body module air inlet pipe installation room transverse sealing is left The structural schematic diagram of end cap inner panel；

Fig. 1 C is of the invention by compressed air gas injection runway, and each valve body plate main body module air inlet pipe installs room transverse sealing The structural schematic diagram of right end cap inner panel；

Fig. 2 is the various angles of the invention by multiple inside and outside rotary sleeve moving sleeve valve flute profile puff prots, and each spout is from 0-180 In the range of degree angle it is longitudinal it is suitable, while rotate counterclockwise inside and outside rotary sleeve moving sleeve valve flute profile puff prot, can be changed inside and outside Big small―gap suture and gas flow on each puff prot angle position, the figure are between the size after each area spray mouth is opened in order The surface structure schematic diagram of gap and angle；

Fig. 3 is various angles each main body module outer groove of the invention by multiple inside and outside rotary sleeve moving sleeve valve flute profile puff prots Shape puff prot is fixed puff prot, or longitudinal direction is suitable in the range of 0-180 degree, rotates counterclockwise inside and outside rotary sleeve sleeve Valve flute profile mouth (can only) change the big small―gap suture and gas flow of inside and outside each puff prot of rotary sleeve moving sleeve valve flute profile, and it is each Spout on jet outer track template road face is fixed flute profile mouth, and angular dimension is vertical 90 degree upward, with whole runway Fixed, the constant appearance flute profile mouth structure schematic diagram that template is linked together；

Fig. 4 be it is of the invention by multiple inside and outside 0-180 degree angle rotary sleeve moving sleeve valve flute profile puff prot, in each 0-180 degree The inside and outside rotary sleeve moving sleeve valve flute profile mouth of angle is suitable, rotate counterclockwise exterior and interior axle sleeves telescoping valve in the range of 0-180 degree Each puff prot, each angle and big small―gap suture can be changed in gate slot shape mouth.The figure is the size clearance angle that each region spout is opened Surface structure schematic diagram；

Fig. 5 be it is of the invention by multiple inside and outside 0-180 degree angle rotary sleeve moving sleeve valve flute profile puff prot, in each 0-180 degree It is in the range of angle, suitable, rotate counterclockwise inside and outside rotary sleeve sleeve, the big small―gap suture and gas flow of each puff prot can be changed The surface structure schematic diagram of size and each puff prot angular dimension；

Fig. 6 be it is of the invention by multiple inside and outside 0-180 degree angle rotary sleeve moving sleeve valve circle hole shape puff prot, it is each in each angle Rotary sleeve moving sleeve valve circle hole shape puff prot inside and outside main body module is to rotate clockwise interior outer shaft in the range of 0-180 degree angle The big small―gap suture of each puff prot and the surface structure schematic diagram of each puff prot angular dimension can be changed in set；

Fig. 7 be it is of the invention by multiple inside and outside 0-180 degree angle the multiple circle hole shape puff prots of rotary sleeve moving sleeve valve, in each 0- The inside and outside multiple circle hole shape mouths of bushing sleeves valve rotated of 180 degree angle are suitable, rotate counterclockwise in the range of 0-180 degree angle The inside and outside multiple circle hole shape puff prots of rotary sleeve moving sleeve valve, between angle and gas flow and size that each puff prot can be changed Gap；Each region spout from " small spout " from left to right rotationally clockwise when, each puff prot sequence become " big spout " open it is big Small―gap suture angle surface structure schematic diagram；

Fig. 8 is the inside and outside rotary sleeve moving sleeve valve flute profile mouth or inside and outside rotary sleeve moving sleeve valve of the invention by each jet The mixing puff prot of each jet port of multiple circle hole shape mouths, it is on and off after each puff prot surface structure schematic diagram；

Fig. 9 is that compressed air gas injection very-short-reach of the invention slides or the dedicated jet runway of VTOL aircraft point is total At in, inside and outside rotary sleeve moving sleeve valve flute profile mouth or the multiple circle hole shape mouths of inside and outside rotary sleeve moving sleeve valve, a certain fritters The structural schematic diagram of portion's structure and outer surface；

Figure 10 is inside and outside rotary sleeve moving sleeve valve flute profile mouth or the inside and outside multiple circle hole shapes of rotary sleeve moving sleeve valve of the invention Puff prot, the main view of the Mechanical course structural schematic diagram of outer driving crank swing angle axis；

Figure 11 is inside and outside rotary sleeve moving sleeve valve flute profile mouth or the inside and outside multiple circle hole shapes of rotary sleeve moving sleeve valve of the invention Puff prot, the left view of the Mechanical course structural schematic diagram of outer driving crank angle axis；

Figure 12 is inside and outside rotary sleeve moving sleeve valve flute profile mouth or the inside and outside multiple circle hole shapes of rotary sleeve moving sleeve valve of the invention Puff prot, outer transmission straight-shaft swing move the main view of the Mechanical course structural schematic diagram of angle axis；

Figure 13 is inside and outside rotary sleeve moving sleeve valve flute profile mouth or the inside and outside multiple circle hole shapes of rotary sleeve moving sleeve valve of the invention Puff prot, outer transmission straight-shaft swing move the left view of the Mechanical course structural schematic diagram of angle axis；

Figure 14 is the gearing smart steering regulation cylinder of the gas cap oil type of management system of the invention, multiple groups combination, can be right Each puff prot and the big small―gap suture of each angle, manipulation and control interlock the surface structure schematic diagram of cylinder sub-unit；

Figure 15 slides for compressed air gas injection short distance of the invention or the dedicated jet runway of Convertiplane, manipulation Control the structural schematic diagram of inner cylinders and oil cylinder；

Figure 16 is inner rotary shaft valve flute profile mouth of the invention, controls inner rotary shaft valve rod shape from each spout at 0-180 degree angle The structural schematic diagram of flute profile mouth；

Figure 17 is the multiple circle hole shape mouths of inner rotary shaft valve of the invention, controls inner rotary shaft valve from each spout at 0-180 degree angle The structural schematic diagram of the multiple circle hole shape mouths of bar shape；

Figure 18 is inner rotary shaft valve flute profile mouth of the invention or the multiple circle hole shape mouths of rotary shaft valve, from 0-180 degree chamfered groove shape The outline structural diagram of mouth or each spout of the oblique angle of inner rotary shaft circle hole shape mouth control inner rotary shaft valve rod；

Figure 19 is inner rotary shaft valve flute profile mouth of the invention or the multiple circle hole shape mouths of inner rotary shaft valve, is fixed for 30 degree The outline structural diagram of the valve body plate main body module inner rotary shaft of angle；

Figure 20 is inner rotary shaft valve flute profile mouth of the invention or the multiple circle hole shape mouths of inner rotary shaft valve, is fixed for 40 degree The outline structural diagram of the valve body plate main body module inner rotary shaft of angle；

Figure 21 is inner rotary shaft valve flute profile mouth of the invention or the multiple circle hole shape mouths of inner rotary shaft valve, is fixed for 50 degree The outline structural diagram of the valve body plate main body module inner rotary shaft of angle；

Figure 22 is inner rotary shaft valve flute profile mouth of the invention or the multiple circle hole shape mouths of inner rotary shaft valve, is fixed for 60 degree The outline structural diagram of the valve body plate main body module inner rotary shaft of angle；

Figure 23 is inner rotary shaft valve flute profile mouth of the invention or the multiple circle hole shape mouths of inner rotary shaft valve, is fixed for 70 degree The outline structural diagram of the valve body plate main body module inner rotary shaft of angle；

Figure 24 is inner rotary shaft valve flute profile mouth of the invention or the multiple circle hole shape mouths of inner rotary shaft valve, is fixed for 80 degree The outline structural diagram of the valve body plate main body module inner rotary shaft of angle；

Figure 25 is inner rotary shaft valve flute profile mouth of the invention or the multiple circle hole shape mouths of inner rotary shaft valve, is fixed for 90 degree The outline structural diagram of the valve body plate main body module inner rotary shaft of angle；

Outline structural diagram of the Figure 26 between inner rotary shaft circle hole shape mouth and each jet port of the invention；

Outline structural diagram of the Figure 27 between inner rotary shaft circle hole shape mouth and inner hole of the invention；

Outline structural diagram of the Figure 28 between inner rotary shaft circle hole shape mouth and shaft outside or tail end of the invention；

The outline structural diagram of Figure 29 pitch-row parameter between inner rotary shaft circle hole shape mouth and axis hole of the invention；

Figure 30 is that the multiple circle hole shape mouths of inner rotary shaft flute profile mouth or inner rotary shaft of the invention are fixed with axis valve rod appearance flute profile mouth The structural schematic diagram of installation；

Figure 31 is first or tail end on the multiple circle hole shape mouths of inner rotary shaft flute profile mouth or inner rotary shaft and shaft outer surface of the invention On, if the shape opening of dress inlays the structural schematic diagram of connection driving crank angle axis assembly flute profile mouth；

Figure 32 is on the multiple circle hole shape mouths of inner rotary shaft flute profile mouth or rotary shaft and axis valve rod head or tail end of the invention, if dress Shape opening inlay connection d-axis swing angle axis assembly handler shifting shaft flute profile mouth outer surface structure schematic diagram；

Figure 33 is rotation outer shaft sleeve flute profile mouth or rotation outer shaft sleeve circle hole shape mouth jet runway valve body plate main body mould of the invention Block is fixed the outline structural diagram of angle-style spout for 60 degree of angles；

Figure 34 is that inside and outside rotary sleeve moving sleeve valve flute profile mouth of the invention or inner rotary shaft cover the multiple circle hole shape axis of moving sleeve valve Internal axle sleeve outer end, the outline structural diagram main view of sealing support (large size) FE Tiler；

Figure 35 is that inside and outside rotary sleeve moving sleeve valve flute profile mouth of the invention or inner rotary shaft cover the multiple round hole axles of moving sleeve valve Internal axle sleeve outer end, the outline structural diagram left view of sealing support (large size) FE Tiler；

Figure 36 is that inside and outside rotary sleeve moving sleeve valve flute profile mouth of the invention or inner rotary shaft cover the multiple round hole axles of moving sleeve valve Internal axle sleeve outer end, the shape square structure schematic diagram left view of sealing support (medium size) FE Tiler；

Figure 37 is that inside and outside rotary sleeve moving sleeve valve flute profile mouth of the invention or inner rotary shaft cover the multiple round hole axles of moving sleeve valve Internal axle sleeve outer end, the shape flange-shaped structure schematic diagram main view of sealing support (medium size) FE Tiler；

Figure 38 is that inside and outside rotary sleeve moving sleeve valve flute profile mouth of the invention or inner rotary shaft cover the multiple round hole axles of moving sleeve valve Internal axle sleeve outer end, the outline structural diagram left view of sealing support (trumpet) FE Tiler；

Figure 39 is that inside and outside rotary sleeve moving sleeve valve axial trough shape mouth of the invention or inner rotary shaft cover the multiple round hole axles of moving sleeve valve Internal axle sleeve outer end, the outline structural diagram main view of sealing support (trumpet) FE Tiler；

Figure 40 is the valve body of the multiple circle hole shape mouth jet runways of inner rotary shaft housing flute profile mouth or inner rotary shaft housing of the invention Plate main body (macromolecule die casting or aluminum steel cast or welding) module (one) is fixed the shape knot of angle-style spout for 30 degree of angles Structure schematic diagram；

Figure 41 is the valve body of the multiple circle hole shape mouth jet runways of inner rotary shaft housing flute profile mouth or inner rotary shaft housing of the invention Plate main body (macromolecule die casting or aluminum steel cast or welding) module (two) is fixed the shape knot of angle-style spout for 30 degree of angles Structure schematic diagram；

Figure 42 is the valve body of the multiple circle hole shape mouth jet runways of inner rotary shaft housing flute profile mouth or inner rotary shaft housing of the invention Plate main body (macromolecule die casting or aluminum steel cast or welding) module is shown for the contour structures that 40 degree of angles are fixed angle-style spout It is intended to；

Figure 43 is the valve body of the multiple circle hole shape mouth jet runways of inner rotary shaft housing flute profile mouth or inner rotary shaft housing of the invention Plate main body (macromolecule die casting or aluminum steel cast or welding) module is shown for the contour structures that 50 degree of angles are fixed angle-style spout It is intended to；

Figure 44 is the valve body of the multiple circle hole shape mouth jet runways of inner rotary shaft housing flute profile mouth or inner rotary shaft housing of the invention Plate main body (macromolecule die casting or aluminum steel cast or welding) module is shown for the contour structures that 60 degree of angles are fixed angle-style spout It is intended to；

Figure 45 is the valve body of the multiple circle hole shape mouth jet runways of inner rotary shaft housing flute profile mouth or inner rotary shaft housing of the invention Plate main body (macromolecule die casting or aluminum steel cast or welding) module is shown for the contour structures that 70 degree of angles are fixed angle-style spout It is intended to；

Figure 46 is the valve body of the multiple circle hole shape mouth jet runways of inner rotary shaft housing flute profile mouth or inner rotary shaft housing of the invention Plate main body (macromolecule die casting or aluminum steel cast or welding) module is shown for the contour structures that 80 degree of angles are fixed angle-style spout It is intended to；

Figure 47 is the valve body of the multiple circle hole shape mouth jet runways of inner rotary shaft housing flute profile mouth or inner rotary shaft housing of the invention Plate main body (macromolecule die casting or aluminum steel cast or welding) module, the contour structures for being fixed angle-style spout for an angle of 90 degrees show It is intended to；

Figure 48 be it is of the invention by compressed air from 0-180-360 degree angle universal globe shell type without fixed sleeves single sleeve circular hole The gas ejection ports of the gas ejection ports of shape or multi-directional ball surface cover double telescopic interior rotary sleeves and fixed sleeves circle hole shape, can 360 Spend angle rotary jet；The figure is universal globe shell type circle hole shape, the dedicated jet runway assembly of gas ejection ports a small corner The outline structural diagram divided；

Figure 49 is of the invention round without fixed sleeves single sleeve from 0-180-360 degree angle, universal globe shell type by compressed air (gas ejection ports of the universal globe shell type interior rotation and fixed sleeves circle hole shape, can be 360 degree for multiple gas ejection ports of hole shape Rotary jet) outline structural diagram；

Figure 50 is of the invention round without fixed sleeves single sleeve from 0-180-360 degree angle, universal globe shell type by compressed air Multiple gas ejection ports of hole shape, the gas injection of the multi-directional ball surface cover double telescopic interior rotary sleeves and fixed sleeves circle hole shape Mouthful, it can 360 degree of angle rotary jets；The figure is the structural member of universal globe shell type, the section view shape of dedicated jet runway sub-unit Structural schematic diagram；

Figure 51 be it is of the invention by compressed air from 0-180-360 degree angle, universal globe shell type circle hole shape gas ejection ports, The outline structural diagram of outer positioning fixing seat；

Figure 52 be it is of the invention by compressed air from 0-180-360 degree angle, universal globe shell type circle hole shape gas ejection ports, The planar profile structural schematic diagram of outer positioning fixing seat；

Figure 53 be it is of the invention by compressed air from 0-360 degree angle, universal globe shell type circle hole shape gas ejection ports, swing The right view of the outline structural diagram of support guide arm rotational pressure bearing；

Figure 54 be it is of the invention by compressed air from 0-360 degree angle, universal globe shell type circle hole shape gas ejection ports, swing The main view of the outline structural diagram of support guide arm rotational pressure bearing；

Figure 55 be it is of the invention by compressed air from 0-360 degree angle, universal globe shell type circle hole shape gas ejection ports it is dedicated The main view of the outline structural diagram of multi-directional ball surface cover inner shield ring circlip；

Figure 56 be compressed air of the invention from 0-360 degree angle, the gas ejection ports of universal globe shell type circle hole shape dedicated ten thousand To the left view of the outline structural diagram of spherical surface set inner shield ring circlip；

Figure 57 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the main view of the outline structural diagram of multi-directional ball injector head and jet gas transmission connecting pipe；

Figure 58 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the top view of the outline structural diagram of multi-directional ball injector head and the injection of jet appendix nozzle；

Figure 59 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the main view of the outline structural diagram of the wear-resisting cover for seat of multi-directional ball injector head location at spherical surface；

Figure 60 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the top view of the outline structural diagram of the wear-resisting cover for seat of multi-directional ball injector head location at spherical surface；

Figure 61 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the main view of the outline structural diagram of multi-directional ball injector head spheric seating set locknut；

Figure 62 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the top view of the outline structural diagram of multi-directional ball injector head spheric seating set locknut；

Figure 63 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the outline structural diagram that multi-directional ball injector head is oriented to active support plate, swings linking arm, driving lever support base Main view；

Figure 64 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the outline structural diagram that multi-directional ball injector head is oriented to active support plate, swings linking arm, driving lever support base Left view；

Figure 65 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the main view that multi-directional ball injector head is oriented to active support plate, the outline structural diagram for swinging linking arm；

Figure 66 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the top view that multi-directional ball injector head is oriented to active support plate, the outline structural diagram for swinging linking arm；

Figure 67 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the main view of the outline structural diagram of multi-directional ball injector head guiding locking screw；

Figure 68 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the left view of the outline structural diagram of multi-directional ball injector head guiding locking screw；

Figure 69 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the main view that multi-directional ball injector head is oriented to active support plate, the outline structural diagram for swinging linking arm；

Figure 70 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the top view that multi-directional ball injector head is oriented to active support plate, the outline structural diagram for swinging linking arm.

Figure 71 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the outline structural diagram that multi-directional ball injector head is oriented to active support plate, swings linking arm, sliding pin Main view；

Figure 72 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the outline structural diagram that multi-directional ball injector head is oriented to active support plate, swings linking arm, sliding pin Left view；

Figure 73 be it is of the invention by compressed air from 0-360 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the contour structures signal that multi-directional ball injector head is oriented to active support plate, swings linking arm, sliding pin double-end plug The main view of figure；

Figure 74 be it is of the invention by compressed air from 0-180 degree angle, the dedicated spray of gas ejection ports of universal globe shell type circle hole shape Gas runway；The figure is the contour structures signal that multi-directional ball injector head is oriented to active support plate, swings linking arm, sliding pin double-end plug The left view of figure；

Figure 75 is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft Frame bottom shape chamber in one region, valve body plate main body module sub-unit 73, each mechano-electronic communication being equipped with and manoeuvre portion The bindiny mechanism of part can constitute the outline structural diagram of a complete autonomous system；

Figure 76 is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft Frame bottom shape chamber in one region, valve body plate main body module sub-unit 73, each mechano-electronic communication being equipped with and manoeuvre portion The bindiny mechanism of part, transmission mechanism being capable of structures with the artificial intelligence control of each air supply system, avionics system and electromechanical integration At the outline structural diagram of a complete autonomous system；

Figure 77 is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway gas of VTOL aircraft In a certain region of curtain, frame bottom shape chamber in valve body plate main body module sub-unit 73, each mechano-electronic communication being equipped with and behaviour It indulges in bindiny mechanism, transmission mechanism and each air supply system, far infrared BEI-DOU position system and electromechanical integration and the runway of component The outline structural diagram that can constitute a complete autonomous system of the artificial intelligence control of red, yellow, and green color indicator light；

Figure 78 is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft Frame bottom shape chamber in one region, valve body plate main body module sub-unit 73, each telecommunications being equipped with and each operating circuit With the connection of each system of signal circuit control unit in runway, a complete autonomous system can be constituted with artificial intelligence control Outline structural diagram；

Figure 79 is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft In in one region, valve body plate main body module sub-unit 73 distribution input each system and outside with circuit and each telecommunications of signal and The connection of each system of operating circuit control unit circuit can constitute the outer of a complete system with artificial intelligence control cabinet Shape structural schematic diagram；

Figure 80 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, For on the dedicated jet runway 191 of type aircraft carrier deck ship-board aircraft or each airport, if the outline structural diagram of the jet runway of dress；

Figure 81 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, For the contour structures signal on the dedicated jet runway 191 of type aircraft carrier deck ship-board aircraft or each airport, taken off at 20 meters long 192 Figure；

Figure 82 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, For the contour structures signal on the dedicated jet runway 191 of type aircraft carrier deck ship-board aircraft or each airport, taken off at 40 meters long 193 Figure；

Figure 83 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, For the contour structures signal on the dedicated jet runway 191 of type aircraft carrier deck ship-board aircraft or each airport, taken off at 60 meters long 194 Figure；

Figure 84 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, For on the dedicated jet runway 191 of type aircraft carrier deck ship-board aircraft or each airport, the shape knot for continuous action of taking off at 80 meters long 195 Structure schematic diagram；

Figure 85 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, When taking off at 20 meters long 192 to 80 meters long 195, to connect on the dedicated jet runway 191 of type aircraft carrier deck ship-board aircraft or each airport The outline structural diagram of continuous four sequentially-operatings；

Figure 86 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, For on the dedicated jet runway 191 of type aircraft carrier deck ship-board aircraft or each airport, the film grade laminar flow at 20-40 meters long 196 lands The outline structural diagram of warship；

Figure 87 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, For on the dedicated jet runway 191 of type aircraft carrier deck ship-board aircraft or each airport, the film grade laminar flow at 60-80 meters long 197 lands The outline structural diagram of warship；

Figure 88 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, For the film grade laminar flow landing on the dedicated jet runway 191 of type aircraft carrier deck ship-board aircraft or each airport, at 100-120 meters long 198 The outline structural diagram of warship；

Figure 89 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, For on the dedicated jet runway 191 of type aircraft carrier deck ship-board aircraft or each airport, in the shape of the spare warship that lands of 140 meters long of film grades Structural schematic diagram；

Figure 90 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, For on the dedicated jet runway 191 of type aircraft carrier deck ship-board aircraft or each airport, in the 20-40 rice long 196 to 60- of film grade laminar flow zone Land at 80 meters long 197 to 100-120 meters long 198 to 140 meters long 199 of film grade prediction scheme spare area warship when, continuous four are suitable The outline structural diagram of sequence movement；

Figure 91 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, The puff prot sub-unit of inside and outside rotary sleeve moving sleeve valve flute profile mouth or the multiple circle hole shape mouth formulas of inside and outside rotary sleeve moving sleeve valve Outline structural diagram；

Figure 92 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, Outer rotary shaft covers the puff prot left end screw plug of moving sleeve valve flute profile mouth or the multiple circle hole shape mouth formulas of inside and outside rotary sleeve moving sleeve valve The outline structural diagram of set；

Figure 93 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, Outer rotary shaft covers the contour structures of moving sleeve valve flute profile puff prot or the multiple circle hole shape jet ports of inside and outside rotary sleeve moving sleeve valve Schematic diagram；

Figure 94 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, Outer rotary shaft covers the outline structural diagram of sleeve right end screw plug set；

Figure 95 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, Inner rotary shaft covers the outline structural diagram of moving sleeve valve flute profile mouth or circle hole shape mouth left end screw plug set；

Figure 96 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, Inner rotary shaft covers the contour structures signal of moving sleeve valve flute profile mouth or the multiple circle hole shape jet ports of inside and outside rotary sleeve moving sleeve valve Figure；

Figure 97 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, Inner rotary shaft covers the outline structural diagram of moving sleeve valve right end screw plug set；

Figure 98 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, Inside and outside rotary sleeve moving sleeve valve flute profile puff prot or the multiple circle hole shape jet ports of inside and outside rotary sleeve moving sleeve valve and rotation are curved The input and output gas of hair style connection type can under the action of interior outer rotary shaft set sleeve pushes rack gear or connection gib block Convert the outline structural diagram of puff prot angle；

Figure 99 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, Inside and outside rotary sleeve moving sleeve valve flute profile puff prot or the multiple circle hole shape jet ports of inside and outside rotary sleeve moving sleeve valve with upper and lower watt The input and output gas of lid hermetic rotary connection type pushes rack gear in interior outer rotary shaft set sleeve or connects the work of gib block Under, the outline structural diagram of convertible puff prot angle；

Figure 100 be it is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet runway of VTOL aircraft, Inside and outside rotary sleeve moving sleeve valve flute profile puff prot or the multiple circle hole shape jet ports of inside and outside rotary sleeve moving sleeve valve, using gas Push up the outline structural diagram of each circuit system of hydraulic cylinder machine driving and artificial intelligence program's manipulation and control；

Figure 101 be in the double sleeves of jet runway universal globe injector head of the invention rotary sleeve air inlet input hole and fixed sleeves into Gas inputs hole location, the 100% corresponding full outline structural diagram for opening air-suction state；

Figure 102 be in the double sleeves of jet runway universal globe injector head of the invention rotary sleeve air inlet input hole and fixed sleeves into Gas inputs hole location, the outline structural diagram of 100% full closing state.

Figure 103 is of the invention slided by compressed air gas injection very-short-reach or the dedicated jet wisdom of VTOL aircraft Runway, inside and outside rotary sleeve moving sleeve valve flute profile puff prot or the multiple circle hole shape jet ports of inside and outside rotary sleeve moving sleeve valve, are adopted With pneumatic jack hydraulic cylinder machine driving and artificial intelligence program, manipulates inside and outside rotary sleeve sleeve and be separated by interior between on coaxial line Outer rotary shaft covers the outline structural diagram that sleeve is connected with each other the control system in fork library.

Specific embodiment

Below in conjunction with the drawings and specific embodiments, slided with efficient very-short-reach or VTOL aircraft device to of the invention Aircraft carrier, naval vessel, each continental rise airport, land and water platform jet runway are referred to as：The structure of " takeoff and landing device " is described in further detail.

Technical solution of the present invention by a variety of gas supply gas sources, using 8-20-40kg/c ㎡ technical atmosphere, sprayed by compressed air The air power source penetrating generated gas laminar flow and being formed, is introduced in dedicated jet runway, landing aircraft can be assisted quick Safe take-off and fast and safely land, and be subject to technically with design improvement comprehensive in overall structure.In addition, in the present invention Above-mentioned compressed air gas injection dedicated jet runway device on, if a variety of gas supply gas sources of the invention have been filled, by compressing Transformation of the gas laminar flow that air injection generates to each area spray gas flow structure, has carried out the overall technology at hundreds of Theoretically, to the design and research of shape and structure inside and outside each jet port, through designing improved blast injection gas blanket Each puff prot that dress is set on jet runway is divided into the injection port configurations of five kinds of modes by the optimum efficiency of stream, spy：The first is 0-90-180 degree angle arbitrarily adjustment type can spray gas laminar flow, be inside and outside rotary sleeve telescoping valve gate-type flute profile mouth or interior outward turning The jet mouth structure for the dedicated jet runway pavement that the gas ejection ports of shaft set telescoping valve gate-type circle hole shape mouth are composed；The Two kinds are the outer shaft template body at 30-90 degree angle to be fixed into dead angle formula injection gas laminar flow, and inner shaft is rotary shaft flute profile Mouth or outer shaft template body are fixed injection gas laminar flow, the gas injection that inner shaft lever is rotary solid shaft circle hole shape mouth The jet mouth structure in dedicated each region of jet runway pavement that mouth is composed is fixed.

The third is for 0-90-180-360 degree angle rotary type, by multiple universal globe shell types without fixed sleeves list casing circle hole shape Gas ejection ports, the dedicated jet runway pavement being composed single casing universal globe shell type jet mouth structure；4th kind For 0-90-180-360 degree angle rotary type gas ejection ports, by rotary sleeve and fixed sleeves circular hole in multiple universal globe shell types The gas ejection ports of shape, the vertical interior turnbarrel of the double sleeves for the dedicated jet runway pavement being composed and outer fixed ten thousand To spherical sleeve type jet mouth structure；5th kind of jet mode structure is two ends or runway pavement before and after the outside in runway face Outside at left and right sides of symmetrical hidden horizontal liftable pitch or it is hidden it is horizontal with road face horizontal can 0-90 degree angle arbitrarily adjust, and It is that 50-300 mm in size can that the formula of being laid flat or 0-30 meters of extension type high heavy caliber gas injection tubes, internal orifice dimension puff prot, which can be erected, The gas laminar flow jet port for the multiple big square amounts adjusted, the size of gas pressure flow is by the artificial intelligence of air pressure graduated release valve that sets in runway It can adjust and control.Above five kinds of jet mouth structures can apply the gas set mounted in there is blast injection of the invention to generate On the various runways of laminar flow constructional device, sea can itself mobile, sea can itself fixed platform, land airplane field, land Base sky frame airport, marine air sac ship platform, continental rise packaged type air bag jet runway, principle are complete pneumatically injections The thrust torque of the strong gas field of the strong gas field stream pressure of the flexibility of generation and gas flow, the landing effect of application solutions aircraft Fruit.

According to characteristic of the dedicated super-short distance of blast injection gas laminar flow from jet runway, in conjunction with achievable wing of the invention Formula slides or the characteristics of VTOL device jet runway with the needs of various aircraft, generates to its blast injection The needs of gas blanket flow structure jet runway and various different type of machines devices use technical standard requirement by various types, to special It is subject to the design of whole multinomial technology and contour structures with jet runway, by the dedicated jet of blast injection gas laminar flow After runway is subject to whole design, the first is set as the adjustable inside and outside rotary sleeve moving sleeve valve flute profile mouth of 0-90-180 degree, or The gas ejection ports of the inside and outside multiple circle hole shapes of rotary sleeve moving sleeve valve.It is for second 30-90 axle sleeve template body of being outside one's consideration is fixed The puff prot of formula dead angle degree, interior solid shaft are rotary solid shaft flute profile mouth or interior rotation solid shaft circle hole shape puff prot.Third Kind is the universal globe shell type at 0-180-360 degree angle without the circle hole shape gas ejection ports of fixed sleeves list bushing type.4th kind is A kind of universal globe shell type of double sleeve vertical structure inner sleeve cartridge types at 0-180-360 degree angle, interior rotary sleeve and fixed sleeves formula Circle hole shape gas ejection ports.5th kind of jet structure is two ends or the outside of runway or so before and after the outside of jet runway The symmetrical hidden horizontal liftable in two sides pitch or with road face it is horizontal it is hidden it is horizontal can 0-90 degree angle arbitrarily adjust, and the formula of being laid flat can be erected 0-30 meters of high lifting pipes, the injection gas that bigbore internal diameter is adjustable, the big square amount artificial intelligence control of 50-300 mm in size Body stream spout (0-360 degree oscillating type spray angle).

Five kinds of jet modes of the invention belong to new structure heterogenous, the special of gas laminar flow is sprayed in multi-functional, high efficiency landing With the jet runway device of wisdom traffic.The various technical parameters of the runway, basic principle and technical performance are essentially identical, only It is different in the structure of each jet port.The dedicated jet runway of gas laminar flow is sprayed in the landing, has surmounted current modernization completely The various technical requirements such as the speed of a ship or plane that matches of aircraft landing have reached the several times of standard or more, breach any in the world at present The manipulation and control and command system of one modernization landing technology, and thoroughly banned world continental rise airport and aircraft carrier With various cumbersome, the unsafe landing control devices of unmanned plane.

It is described to be slided or the aircraft carrier of VTOL aircraft device, naval vessel, land and water platform jet runway device with efficient short distance Artificial intelligence high-tech technology manipulation and control is used completely, can be efficiently able to satisfy the various of wing type and be relied on plane track landing Aircraft, can be in 60-80-100-120-140 meters on short-range dedicated jet runway, by blast injection gas The outstanding support gas that laminar flow is formed, realizes the safely and fast landing to large-scale unmanned plane and carrier-borne aircraft controllability；It is empty by compression The outstanding support gas that gas jet gas blanket stream is formed, realizes the landing of sliding jump formula aircraft safety reliability, in favor of greatly improving Large-scale unmanned plane, aircraft carrier ship-board aircraft, continental rise airport aircraft, the continental rise sky frame that General Aviation is badly in need of Development of Logistics transport at present fly Row platform, continental rise packaged type air bag landing stretch jet runway, marine stand alone type, packaged type, can separate assembling, air bag Telescopic landing platform, marine vessel disjunctor can separate assembling airbag telescopic type landing jet runway platforms, marine fixed Or the landing jet runway platform of packaged type, it is provided with the various ways gas supply gas of at least one aircraft carrier landing use Source, by the dedicated very-short-reach jet runway of blast injection gas laminar flow, the aircraft carrier landing blast injection In the management system of the dedicated very-short-reach jet runway device of gas laminar flow, with the manipulation and control of aircraft carrier, landing aircraft Manipulation and control or the control tower management system of each airfield runway mutually switch.

It is of the invention to be slided with efficient short distance or the aircraft carrier of VTOL aircraft device, naval vessel, land and water platform jet runway, packet It has included：A kind of type aircraft carrier deck jet runway device；A kind of injection of the lifting gasbag runway of inflation/deflation, reverse emergency landing aircraft Gas laminar flow blocks aircraft, and the afloat independent-lifting floating gasbag runway of aircraft inertia force elimination that will land, On natural coastdown support ship jet runway device；A kind of dedicated jet runway device on various naval vessels；A kind of sea is dragged The dedicated jet runway device of ship drawing type, itself freestanding mobile；A kind of dedicated jet runway with various naval vessel Contiuum types Device；A kind of marine or rivers and lakes fixed platform dedicated jet runway device；It is a kind of at sea or rivers and lakes floating body platform it is special With jet runway device；A kind of dedicated jet runway device in land airplane field；It is a kind of continental rise Moveable foldable skeleton, flexible The dedicated jet runway device of charge-discharge air bag cushion；It is a kind of future town-dweller-rural-family personal baby plane in continental rise or continental rise sky frame On aircraft platform (in future development artificial intelligence nobody it is passenger-cargo with military aircraft on, landing with international adaptability standard or Store aircraft supermarket), the dedicated very-short-reach that at least one aircraft carrier landing blast injection gas laminar flow is arranged is sliding Line runway, the dedicated very-short-reach runway device of the fluent line of the aircraft carrier landing blast injection gas blanket should The control tower of the manipulation and control of the management system of device and aircraft carrier, the manipulation and control in landing aircraft or each airfield runway is grasped Vertical control system mutually switches.

On the type aircraft carrier deck runway, the dedicated jet-propelled race for covering the multiple tracks carrier-borne aircraft landing of whole deck jet runway is added Road, and it is divided into seven fixed jet angles to be respectively on whole deck jet runway；0-30,40,50,60,70,80,90 degree Each runway zone that seven different angles at angle or seven 0-180 degree angles are connected, and along before and after seven runway zones or each It is connected with each other between region and is integrated the various gas ejection ports devices added.In the considerable view of appearance exposed position of jet runway Into jet runway, injection gas laminar flow or 0- equipped with front and back injection gas laminar flow 30-90 degree angle, multiple angle variable An angle of 90 degrees, multiple rotary sleeve moving sleeve valve flute profile gas jet ports, multiple multiple circle hole shapes of rotary sleeve moving sleeve valve The gas injection of multiple Universal-head angle of oscillation spherical sleeve type circle hole shapes at the gas ejection ports 0-180 degree angle (0-360 degree angle) of mouth Mouthful, or the high lifting tubular type of 0-30 meters of the formula that is laid flat, the adjustable gas ejection ports of bore 50-300 mm in size can be erected, non- In special circumstances, standing can be laid flat or telescopic lifting tubular gas jet port, can securely achieves and takes off or block down by force by force Drop.The air curtain puff prot that position is equipped at left and right sides of runway is that amendment landing aircraft " eccentric biasing boat inclination, help up and down by sink-float Interference from outer lateral wind to landing aircraft can be controlled just " and efficiently, the air curtain puff prot being equipped with inside runway is protection Gas device, the management system with manipulation and control or each approach tower in aircraft carrier mutually switch.

Wherein, in the type aircraft carrier deck jet runway, the gas ejection ports equipped with inside and outside rotary sleeve moving sleeve valve flute profile mouth It can be changed in every set idol type component of interior outer rotary shaft set sleeve in left-right rotation with the gas ejection ports of circle hole shape mouth The size in jet port gap can change the gas flow size of gas ejection ports.Universal globe shell type single sleeve circle hole shape Jet port changes gas pressure and the size of flow is unable to self-regulated, and can only lean on pressure regulator valve and flow valve artificial intelligence control tune It is whole.And the gas ejection ports of the double sleeve circle hole shapes of universal globe shell type, screw surface cover inner rotary shaft housing when covering sleeve Fixed i.e. controllable air inlet, the size of choke and adjustment angle and the size in changeable spout gap, and changeable gas spray The size of the size of loophole flow, gas pressure adjusts control by the total gas pressure valve artificial intelligence in each region, by size pressure It is slided needed for gas stream is reverse or each lower part of the front and back fuselage entirety lower part of VTOL aircraft, front left and right or rear left starboard wing The entirety at position on the whole stress surface by the aircraft lower portion gross area of type of all sizes, ejects upwards Support rises or blocks the self inertia torque that gas laminar flow is greater than various required landing aircrafts, the supports more than several times of total weight ratio It rises or blocks gas laminar flow, be just able to achieve on blast injection gas specific very-short-reach jet runway, safely, match Injection gas source fast and safely assist control takeoff and landing main peak value.It is described to be run in the dedicated jet of type aircraft carrier deck takeoff and landing On road, connected equipped with blast injection gas laminar flow apparatus and the management system of artificial intelligence.

To blast injection gas laminar-flow type, the dedicated jet runway of type aircraft carrier deck takeoff and landing is provided at least one, institute The dedicated jet runway device of each airport takeoff and landing of blast injection gas laminar-flow type, type aircraft carrier deck aircraft is stated, is manipulated Control system mutually switches with the pilot guidance control in the manipulation and control or landing aircraft of control tower.

There are also one kind in type aircraft carrier deck, second-mission aircraft landing or continental rise airport or various platforms, before landing jet runway At left and right sides of the outside of head end and tail end it is symmetrical it is hidden it is horizontal be equipped with liftable pitch or with the horizontal hidden horizontal 0-90 degree angle in road face, and And can erect or be laid flat 0-30 meters of formula high lifting tubular types, heavy caliber injection gas laminar flow apparatus include：Blast injection gas The aircraft jet runway of body laminar-flow type type aircraft carrier deck, the aircraft jet runway of continental rise airport blast injection gas laminar-flow type, It sprays gas safety to it to landing errant aircraft air blast flexible to block, it is than former arresting net the safety is improved number Times or more, to the aircraft fanout free region under blocking, and to the management system of each injection gas laminar flow aircraft jet runway It is connected.

Wherein, it is sprayed in the blast injection gas laminar-flow type type aircraft carrier deck aircraft jet runway, continental rise airport compressed air It emanates on body laminar-flow type aircraft jet runway, is additionally arranged the various platforms of second-mission aircraft landing continental rise；Outside landing jet runway On the left and right sides antimere on side, be equipped with liftable pitch or with the horizontal hidden horizontal 0-90 degree angle in road face, and can erect or put 0-30 meters of flat high lifting tubular types, heavy caliber spray gas laminar flow apparatus；Jet runway aircraft in Normal Take-Off And Landing loses suddenly When control can Emergency use, which should all be equipped on most of jet runway.Fly on each airport of type aircraft carrier deck aircraft On the dedicated jet runway of machine landing, it is connected equipped with blast injection gas laminar flow apparatus with the management system of artificial intelligence It connects.

In type aircraft carrier deck, on continental rise airport or various platforms, it is provided at least one landing jet runway, is run in landing jet Preceding head end outside road and the left and right sides outside rearward end position and jet runway are symmetrical hidden horizontal, be equipped with liftable pitch or with The horizontal hidden horizontal 0-90 degree angle in road face, and 0-30 meters of formula high lifting tubular types can be erected or be laid flat, 50-300 mm in size can The bore of tune sprays gas laminar flow.In no special situation, to landing aircraft " eccentric biasing boat inclination, righting of rising and falling up and down " etc. Correcting action, can safe second-mission aircraft quickly meet an urgent need lifting gear, continental rise sky frame flying platform, the dedicated flight landing of gas injection The takeoff and landing device of jet runway.Second-mission aircraft landing or continental rise or various platform landing jet runways in the type aircraft carrier deck Rear and front end position on, be equipped with symmetrical hidden horizontal liftable pitch or with the horizontal hidden horizontal 0-90 degree angle in road face, and can Erect or be laid flat 0-30 meters of formula high lifting tubular types, heavy caliber injection gas laminar flow apparatus management system and empty frame control tower Manipulation and control or landing aircraft in the manipulation and control of pilot mutually switch.

There are also it is a kind of can be with landing aircraft height, the naval vessel of front and back quick sliding, on the water or on continental rise before inflation/deflation After automatically move, oscilaltion gasbag-type field jet runway device can in a kind of no special situation (undercarriage is not opened) Breakdown plane inversely is blocked to emergency landing aircraft injection gas laminar flow to slow down, and the inertia force for the aircraft that lands is eliminated at sea On air bag jet platform or continental rise jetport runway, and can be with the synchronous original place of decline aircraft quick sliding formula backward automatically Air bag moves takeoff and landing original place acceleration and deceleration idler pulley wheel shaft type jet platform, can be to the jet of upper and lower lifting gasbag formula safety barrage Runway stage apparatus, or the jet runway device of natural coastdown support boat equipment, at sea can folding and unfolding manipulation and control.This is one It is kind not only independent, but also after capable of being connected to each other with aircraft carrier, will block landing again with decline aircraft synchronize automatically move gasbag-type slow down it is special With on takeoff and landing support ship jet runway, and the aircraft to slow down on support ship jet runway will be dropped to and be recovered to aircraft carrier again, After the air bag aircraft support ship is deflated again, withdraws aircraft carrier automatic rescue and equip cabin.And it can also be achieved VTOL Aircraft receives in situ the flexible injection gas laminar flow by force of large area on runway, holds in the palm gas force to needing departing aeroplane to be hanged by strong injection Afterwards, Harrier can vertically be held in the palm naturally is raised to 15-20 meters of high-altitudes.When spray gas pressure reduce when, it can be achieved that being blocked after Aircraft safety hangs the vertical origin landing of support formula, and to inflation/deflation lifting gasbag platform waterborne inversely to emergency landing aircraft Gas laminar flow is sprayed, blocks emergency landing aircraft quick deceleration, and the inertia force for the aircraft that lands is eliminated into afloat various air bags On formula jet runway stage apparatus, formation blocks management system with the emergency of each injection gas laminar flow aircraft and is connected.

Wherein, in the inflation/deflation lifting air bellows field packaged type jet runway, gas inversely is sprayed to emergency landing aircraft Body laminar flow blocks emergency aircraft quick deceleration, and the inertia force for the aircraft that lands is eliminated afloat air bag jet runway platform On, the natural coastdown on support ship jet runway device.Especially on air bag jet runway platform to landing aircraft from On right coastdown support ship, be additionally arranged can pitch or with the horizontal hidden horizontal 0-90 degree angle in road face, and can erect or be laid flat formula 0- 30 meters high of lifting tubular type, heavy caliber spray gas stream jet port, block aircraft decline, inversely meet an urgent need in inflation/deflation lifting gasbag Landing aircraft injection gas laminar flow blocks aircraft, and the inertia force for the aircraft that lands is eliminated afloat gasbag-type jet and is run On road platform, the jet runway device of various coastdown landing aircrafts is connected with the management system of artificial intelligence.

It is provided with the field jet runway of at least one inflation/deflation lifting air bellows, inversely sprays gas blanket to emergency landing aircraft Stream blocks aircraft, and the inertia force for the aircraft that lands is eliminated on afloat air bag jet runway platform, dedicated in support ship It slides, slow down naturally on takeoff and landing jet runway device, the behaviour of management system and fixable type or movable control tower Management system in vertical control or landing aircraft mutually switches.

On continental rise or continental rise sky airplane platform, it is provided with the personal baby plane or unmanned plane of at least one town-dweller-rural-family. Using a variety of gas supply gas sources, slided by the short distance that blast injection gas blanket stream is formed or VTOL aircraft it is dedicated Jet runway device.The personal baby plane or unmanned plane of the town-dweller-rural-family are used in continental rise or continental rise sky airplane platform A variety of gas supply gas sources, are slided or the dedicated jet of Convertiplane by the short distance that blast injection gas blanket stream is formed Runway device mutually switches with the management system in manipulation and control or landing aircraft.

There are also a kind of by the frigid zone-low temperature that environment are limited such as weather, geographic areas be small in subzero 60 degree, the torrid zone-high temperature zero Upper 80 degree of various areas, are slided or VTOL aircraft using the very-short-reach formed by blast injection gas blanket stream Private track device, frigid zone includes the areas such as Xinjiang, Qinghai, Tibet, Russia and south poles, the torrid zone include Chongqing, force The areas such as the Chinese, Nanjing, Shanghai, Pearl River Delta, Vietnam, South Africa.

The jet runway can set dress, apply in variety carrier, and great advantage is exactly that internal structure is just the same, make in design When making each piece of block insert type template, the material of each modular construction is selected, to the precision for processing each component, each component gasproof Pressure, each component anti-gas-leak and service life will be rigid in checking up.It is on naval vessel and offshore platform the selection of material：A kind of necessary resistance So, light-weight, intensity is big, a kind of corrosion resistant macromolecule, mature various technical standards can have jet runway institute usability A kind of new material of energy.The jet runway of continental rise Moveable foldable skeleton, flexible charge-discharge air bag cushion, in order to mitigate whole jet Weight, the proof strength of runway, can be used carbon fibre composite as runway pavement.In order to ensure to whole jet runway The needs of intensity and safe life must to the various safety loading coefficients of the receiving air pressure of each pneumatic original part inside whole runway It must doubly ensure that first-class quality is manufactured with standard required by accurate size.

It is of the invention to be slided with efficient short distance or the aircraft carrier of VTOL aircraft device, naval vessel, land and water platform jet runway packet It includes：A kind of efficient short distance of band slides or the type aircraft carrier deck jet runway device of VTOL aircraft device；One kind is in aircraft carrier first On plate, can second-mission aircraft landing on continental rise airport or various platforms.It can left and right sides outside second-mission aircraft landing jet runway On, be equipped with symmetrical hidden horizontal liftable pitch or with the horizontal hidden horizontal 0-90 degree angle in road face, and 0-30 meters of the formula that is laid flat can be erected High lifting tubular type, heavy caliber spray gas laminar flow apparatus；A kind of inflation/deflation lifting gasbag is platform-type inversely to fly to emergency landing Machine sprays gas laminar flow, helps support to block aircraft, and the inertia force for the aircraft that lands is eliminated afloat lifting gasbag platform On jet runway device；It is a kind of to be slided on various naval vessels by the very-short-reach that blast injection gas blanket stream is formed or vertically The dedicated jet runway device of landing aircraft；It is a kind of to assist the marine with mother ship carrier towboat drawing type itself of aircraft carrier landing carrier-borne aircraft Can freestanding mobile, slided by the short distance that blast injection gas blanket stream is formed or the dedicated jet of VTOL aircraft is run Road device；It is a kind of with various naval vessel Contiuum types, slided by the very-short-reach that blast injection gas blanket stream is formed or be vertical The dedicated jet runway device of aircraft drops；One kind being equipped with extension type in naval vessel rearward end, on independent floating gasbag platform waterborne On certain side at left and right ship side two side ends position or on each position in left and right ship side two sides, sprayed equipped with extension type by compressed air The very-short-reach that body laminar flow of emanating is formed slides or the dedicated jet runway device of VTOL aircraft；It is a kind of marine fixed flat Platform, is slided or the dedicated jet runway device of VTOL aircraft by the very-short-reach that blast injection gas blanket stream is formed； A kind of at sea or in rivers and lakes gasbag-type stretches on floating body platform, and the very-short-reach formed by blast injection gas blanket stream is sliding Capable or VTOL aircraft dedicated jet runway device；A kind of land airplane field is formed by blast injection gas blanket stream Very-short-reach slide or the dedicated jet runway device of VTOL aircraft；A kind of continental rise Moveable foldable skeleton flexible fills The jet runway device of deflation capsule cushion is slided by the very-short-reach that blast injection gas blanket stream is formed or VTOL flies The dedicated jet runway device of machine；A kind of following personal baby plane in town-dweller-rural-family is in continental rise or continental rise sky airplane platform In (landing or storage supermarket with international adaptability standard), the very-short-reach formed by blast injection gas blanket stream is sliding Capable or VTOL aircraft dedicated jet runway device；It is a kind of that by weather, geographic areas be small etc., frigid zone-that environment are limited is low Temperature is at subzero 60 degree, and the torrid zone-high temperature is in 80 degree above freezing of various areas, the short distance formed by blast injection gas blanket stream From sliding or the private track device of VTOL aircraft.

It is described to be slided or the aircraft carrier of VTOL aircraft device, naval vessel, continental rise airport, land and water platform jet with efficient short distance Runway device function is realized in.

A variety of gas supply gas sources of the use, the gas laminar flow short distance formed by the gas injection of compressed air are slided or vertically Each regional device of the dedicated jet runway of landing aircraft includes：It is described slided with efficient short distance or VTOL aircraft it is special With jet runway on type aircraft carrier deck, naval vessel, land and water platform jet runway, a jet runway is divided into seven regions modules Section, such as fixing tentatively module for each region is 20 meters long, seven regions of jet runway be combined into amount to it is 140 meters long, if fill Type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, on the jet runway of continental rise airport, continental rise sky body panel jet is run On road, on each mountain area, mountain vallage jet runway, land and water fix or mobile independent air bags platform jet runway on, naval vessel ship side On each position of jet runway of left and right sides or stern end position extension type air bag platform.

A variety of gas supply gas sources of the use, the gas laminar flow formed by the gas injection of compressed air are slided in very-short-reach Or the structure in dedicated each region of jet wisdom traffic runway of VTOL aircraft includes：The first area of jet runway is 20 meters long 1, if on each airport head end position or on the position of aircraft carrier tail end.On 20 meters long 1 of the first area of jet runway, Seven regions made of muti-piece valve body plate main body module sub-unit 73 is combined are respectively equipped with, are the firstth area of jet runway respectively 20 meters long 1 of domain, 20 meters long 2 of second area, 20 meters long 3 of third region, 20 meters of the fourth region, 20 meters long 5 of the long 4, the 5th region, Six 20 meters of regions long 6 and the District 7 domain of jet runway are 20 meters long by 7, each region are set dedicated jet-propelled mounted in carrier-borne or each airport 191 type aircraft carrier deck rearward ends of runway with before in position on.The above constitutes each airport or type aircraft carrier deck to carrier-borne The construction profile of the dedicated jet runway entirety of machine landing.

The left-external side 20 meters long 1 of the first area of jet runway, is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway, On the left outside cliche frame longitudinal direction batten seat 16 of runway, it is respectively equipped with the green warning lamp 24 of the left outside cliche frame longitudinal direction reddish yellow of runway；Runway is each Cushion connecting sewing 13 is installed between the valve body plate module of region；And the left fixed under-chassis 8 of private track.The above constitutes jet The sealing fixation of runway entirety and caution structure.

The left-external side 20 meters long 1 of the first area of jet runway, is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；? The left outside lower part of the left outside cliche frame longitudinal direction batten seat 16 of runway is equipped with the left outside 1-7 region rotary sleeve valve flute profile spray of runway Port or circle hole shape puff prot servo pushing motor 30；It is outer on 20 meters long 1 of the right side in the first area of runway, it is equipped with the right outer edge of runway Bezel longitudinal direction batten seat 17；In the outer lower part in the right side of the right outer cliche frame longitudinal direction batten seat 17 of runway, it is equipped with the right outer 1-7 region of runway Rotary sleeve valve flute profile puff prot or circle hole shape puff prot servo pushing motor 31.The above constitutes jet runway each Region whole fixation all around and mechanical linkage and gas transmission source are unblocked, connect flexible operating control mechanism.

The laterally inboard 20 meters long 1 of the first area of jet runway, is equipped with the green warning lamp of runway rear left wheel road reddish yellow 28；It is 20 meters of second area long by 2 equipped with runway after the left-external side of 20 meters long 1 of the first area of runway between longitudinal direction；In runway 20 meters long 1 of first area preceding longitudinally outboard, be equipped with cliche frame transverse direction press strip sealing and dustproof outer cover 14 before runway；Before runway On cliche frame transverse direction press strip sealing and dustproof outer cover 14, it is respectively equipped with Normal Take-Off And Landing and stores defeated deflation bucket connecting tube 10；Emergency landing Store defeated deflation bucket connecting tube 11；Spare landing stores defeated deflation bucket connecting tube 12；And cliche frame transverse direction press strip is close before runway Seal dustproof encloser fixing bolt 18.The above, the gas transmission source of composition jet runway entirety is unblocked laterally to press with cliche frame The fixed bindiny mechanism of item sealing.

The inside between the green warning lamp 28 of dedicated jet runway rear left wheel road reddish yellow, is respectively equipped with runway left first A each spout in region opens 1-2 millimeter 33；In left first region of runway, each spout opens the Right Inboard of 1-2 millimeter 33, if There is the green warning lamp 26 of runway front left wheel road reddish yellow；With the green warning lamp 27 of runway front right wheel road reddish yellow；In runway front right wheel Outside in the right side of the green warning lamp 27 of road reddish yellow is equipped with each spout in first region in the runway right side and opens 1-2 millimeter 35；On the runway right side In each spout in first region open the right side of 1-2 millimeter 35, equipped with reddish yellow green warning lamp 29 in right wheel road after runway.The above institute It states, constitutes the warning of safe manoeuvring and the artificial intelligence manipulation and control of jet mechanism.

The right outside of the green warning lamp 29 of right wheel road reddish yellow after dedicated jet runway is equipped with right outer first region of runway Each spout opens 1-2 millimeter 34；The right outside of 1-2 millimeter 34 is opened in the right outer each spout in first region of runway, it is right to be equipped with runway The inside and outside multiple air curtain puff prots 61 in longitudinal direction；In the right outside of the right inside and outside multiple air curtain puff prots 61 in longitudinal direction of runway, it is equipped with runway Right outer cliche frame longitudinal direction batten seat 17；On the right outer cliche frame longitudinal direction batten seat 17 of runway, it is respectively equipped with the right outer cliche frame of runway Longitudinal green warning lamp 25 of reddish yellow；The right outer cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt 21 of runway；The private track right side is solid Determine under-chassis 9；And cushion connecting sewing 13 is installed between each region valve body plate module of runway.The above constitutes each component and closes Manage, coordinate the connection and warning control for facilitating maintenance dismounting and jet to protect main landing gas source of consistent property.

20 meters long 2 of second area of the left-external side in jet runway is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；? On the left outside cliche frame longitudinal direction batten seat 16 of runway, it is respectively equipped with the green warning lamp 24 of the left outside cliche frame longitudinal direction reddish yellow of runway；Runway is each Cushion connecting sewing 13 is installed between the valve body plate module of region；And the left fixed under-chassis 8 of private track.The above constitutes spray Integrally each site location is fixedly connected with the structural compatibility with warning to gas runway.

20 meters long 2 of second area of the left side of transverse direction in jet runway is equipped with the green warning of runway rear left wheel road reddish yellow Lamp 28；Between longitudinal direction, the third region equipped with runway is 20 meters long by 3 after 20 meters long 2 of runway second area of left-external side；In runway 20 meters long 2 of second area of preceding longitudinal direction between, be equipped with runway first area it is 20 meters long by 1.The above is constituted whole to jet Runway cooperation, the consistency of control.

The left-external side 20 meters long 3 of the third region of jet runway, is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；? On the left outside cliche frame longitudinal direction batten seat 16 of runway, it is respectively equipped with the green warning lamp 24 of the left outside cliche frame longitudinal direction reddish yellow of runway；Runway is each Cushion connecting sewing 13 is installed between the valve body plate module of region；With the left fixed under-chassis 8 of private track.The above constitutes jet Runway is integrally fixedly connected with the associativity with warning.

The left side of transverse direction 20 meters long 3 of the third region of jet runway, is equipped with the green warning lamp of runway rear left wheel reddish yellow 28；It between longitudinal direction, is being equipped with 20 meters of runway the fourth region long by 4 after the left-external side in 20 meters long 3 of runway third region；In runway third It is 20 meters of second area long by 2 equipped with runway between the preceding longitudinal direction that 20 meters long 3 of region.The above constitutes the knot between each region Structure connects Proper Match consistency.

20 meters long 4 of the fourth region of the left-external side in jet runway is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；? On the left outside cliche frame longitudinal direction batten seat 16 of runway, it is respectively equipped with the green warning lamp 24 of the left outside cliche frame longitudinal direction reddish yellow of runway；Runway is each Cushion connecting sewing 13 is installed between the valve body plate module of region；And the left fixed under-chassis 8 of private track.The above constitutes spray The fixed associativity of gas runway integrated connection.

20 meters long 4 of the fourth region of the left side of transverse direction in jet runway is equipped with the green warning of runway rear left wheel road reddish yellow Lamp 28；Between longitudinal direction, it is 20 meters long by 5 to be equipped with the 5th region of runway after 20 meters long 4 of the fourth region of runway of left-external side；In runway Between the preceding longitudinal direction that 20 meters long 4 of the fourth region, the third region equipped with runway is 20 meters long by 3.The above constitutes each region to spray The connection of gas runway and the reliability of security warning.

The left-external side 20 meters long 5 of the 5th region of jet runway, is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；? On the left outside cliche frame longitudinal direction batten seat 16 of runway, it is respectively equipped with the green warning lamp 24 of the left outside cliche frame longitudinal direction reddish yellow of runway；Runway is each Cushion connecting sewing 13 is installed between the valve body plate module of region；And the left fixed under-chassis 8 of private track.The above constitutes spray The fixed security warning of the combination of gas runway entirety.

The left side of transverse direction 20 meters long 5 of the 5th region of jet runway, is equipped with the green warning of runway rear left wheel road reddish yellow Lamp 28；Between longitudinal direction, the 6th region equipped with runway is 20 meters long by 6 after the left-external side in 20 meters long 5 of the 5th region of runway；In runway 20 meters long 5 of the 5th region preceding longitudinal direction between, be equipped with 20 meters of runway the fourth region long by 4.The above is constituted between each region To the modular subregionization installation of jet runway entirety, dismounting, repair and in debugging, advance in practical use.

The left-external side 20 meters long 6 of the 6th region of jet runway, is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；? On the left outside cliche frame longitudinal direction batten seat 16 of runway, it is respectively equipped with the green warning lamp 24 of the left outside cliche frame longitudinal direction reddish yellow of runway；Runway is each Cushion connecting sewing 13 is installed between the valve body plate module of region；And the left fixed under-chassis 8 of private track.The above constitutes spray Combination, the fixation, safety, warning of gas runway entirety.

The left side of transverse direction 20 meters long 6 of the 6th region of jet runway, is equipped with the green warning lamp of runway rear left wheel reddish yellow 28；Between longitudinal direction, the District 7 domain equipped with runway is 20 meters long by 7 after the left-external side in 20 meters long 6 of the 6th region of runway；In runway Between the preceding longitudinal direction in six 20 meters of regions long 6, it is 20 meters long by 5 to be equipped with the 5th region of runway.The above constitutes each regional body and each Region cooperation, it is advanced, reasonable, reliable handling in practical application between each movement mechanism and fixed mechanism part.

The left-external side 20 meters long 7 of the District 7 domain of jet runway, is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；? On the left outside cliche frame longitudinal direction batten seat 16 of runway, it is respectively equipped with the green warning lamp 24 of the left outside cliche frame longitudinal direction reddish yellow of runway；Runway is each Cushion connecting sewing 13 is installed between the valve body plate module of region；And the left fixed under-chassis 8 of private track.The above constitutes spray Combination, the fixation, safety, warning of gas runway entirety.

The left side of transverse direction 20 meters long 7 of the District 7 domain of jet runway, is equipped with the green warning of runway rear left wheel road reddish yellow Lamp 28；In 20 meters long 7 of the rear longitudinally outboard in the District 7 domain of runway, it is equipped with cliche frame transverse direction press strip sealing and dustproof outer cover after runway 15；After runway on cliche frame transverse direction press strip sealing and dustproof outer cover 15, it is respectively equipped with Normal Take-Off And Landing and stores defeated deflation bucket connecting tube 10；Landing of meeting an urgent need stores defeated deflation bucket connecting tube 11；Spare landing stores defeated deflation bucket connecting tube 12；And cliche frame after runway Lateral press strip sealing and dustproof outer cover fixing bolt 19.The above is constituted to whole jet runway security warning the most complete Air distribution system sealing and the smooth practicability of gas source.

It is described to be slided with efficient short distance or the dedicated jet runway of VTOL aircraft, it is flat in type aircraft carrier deck, naval vessel, land and water The jet runway device of platform, including the left fixed under-chassis 8 of the private track and the right outer cliche frame longitudinal direction press strip sealing and dustproof of runway Outer cover fixing bolt 21, if mounted in type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, continental rise airport jet runway On upper, continental rise sky body panel jet runway, land and water fix or mobile independent air bags platform jet runway on and naval vessel ship side On left and right sides or the extension type air bag platform jet runway at stern end position.

It is described using slided by the gas laminar flow short distance that is formed of gas injection of compressed air or VTOL aircraft it is dedicated The fixed structure in each region of jet runway includes：The left fixed under-chassis 8 of private track, the right fixed under-chassis 9 of private track, Normal Take-Off And Landing Store defeated deflation bucket connecting tube 10, emergency landing stores defeated deflation bucket connecting tube 11, spare landing stores defeated deflation bucket connecting tube 12, cushion connecting sewing 13 is installed, before runway outside cliche frame transverse direction press strip sealing and dustproof between each region valve body plate module of runway The right outer edge of cliche frame transverse direction press strip sealing and dustproof outer cover 15, the left outside cliche frame longitudinal direction batten seat 16 of runway, runway after cover 14, runway Cliche frame is lateral after cliche frame transverse direction press strip sealing and dustproof outer cover fixing bolt 18, runway before bezel longitudinal direction batten seat 17, runway Press strip sealing and dustproof outer cover fixing bolt 19, the left outside cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt 20 of runway, and The right outer cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt 21 of runway, is constituted reliable to the connection of jet runway total system Property.

It is described on the left outside cliche frame longitudinal direction batten seat 16 of dedicated jet runway, be respectively equipped with each region valve body plate module of runway it Between install cushion connecting sewing 13, with the left outside cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt 20 of runway；On a runway left side On the bottom position of outer cliche frame longitudinal direction batten seat 16, it is equipped with the left fixed under-chassis 8 of private track.The above is constituted to jet The stationarity of runway entirety.

It is described on the right outer cliche frame longitudinal direction batten seat 17 of dedicated jet runway, be equipped with the green police of the runway right side outer cliche frame longitudinal direction reddish yellow Show lamp 25；On the bottom position of the right outer cliche frame longitudinal direction batten seat 17 of runway, it is equipped with the right fixed under-chassis 9 of private track；With race The right outer cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt 21 in road；The cliche frame transverse direction press strip sealing and dustproof outer cover before runway On 14, it is respectively equipped with the green warning lamp 22 of first cliche frame transverse direction reddish yellow before runway；Normal Take-Off And Landing stores the connecting tube 10 of defeated deflation bucket； Emergency landing stores the connecting tube 11 of defeated deflation bucket；Spare landing stores the connecting tube 12 of defeated deflation bucket；And it is inlayed before runway Frame transverse direction press strip sealing and dustproof outer cover fixing bolt 18.The above constitutes the fixed layout and distribution whole to jet runway The layout of mechanism closes connection.

It is described that on cliche frame transverse direction press strip sealing and dustproof outer cover 15, it is defeated to be respectively equipped with Normal Take-Off And Landing storage after dedicated jet runway The connecting tube 10 of deflation bucket；Emergency landing stores the connecting tube 11 of defeated deflation bucket；Spare landing stores the connecting tube of defeated deflation bucket 12；The green warning lamp 23 of runway rear molding cliche frame transverse direction reddish yellow；And cliche frame transverse direction press strip sealing and dustproof outer cover is fixed after runway Bolt 19.Constitute to jet runway globality valve train system and closing connection warning can manipulation and control.

It is described to be slided with efficient short distance or the dedicated jet runway of VTOL aircraft is flat in type aircraft carrier deck, naval vessel, land and water Right wheel after the green warning lamp 22 of head cliche frame transverse direction reddish yellow, runway before platform jet runway device, including the dedicated jet runway The green warning lamp 29 of road reddish yellow, set respectively mounted in type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, continental rise airport jet On runway, on continental rise sky body panel jet runway, land and water fix or mobile, independent air bags platform jet runway on, naval vessel ship On side of a ship left and right sides or stern end position extension type air bag platform jet runway.

A variety of gas supply gas sources of the use, the gas laminar flow short distance formed by the gas injection of compressed air are slided, or are hung down Directly the various colors control instruction modulated structure in dedicated each region of jet runway of landing aircraft includes：First cliche frame is lateral before runway The green warning lamp 22 of reddish yellow, the green warning lamp 23 of runway rear molding cliche frame transverse direction reddish yellow, the left outside green warning of cliche frame longitudinal direction reddish yellow of runway The green warning lamp 25 of the right outer cliche frame longitudinal direction reddish yellow of lamp 24, runway, the green warning lamp 26 of runway front left wheel road reddish yellow, runway front right machine Take turns the rear right wheel road of the green warning lamp 27 of road reddish yellow, the green warning lamp 28 of runway rear left wheel road reddish yellow and dedicated jet runway The green warning lamp 29 of reddish yellow.Constitute the controllability of the automatic warning safety active to jet runway entirety.

It is described on the preceding cliche frame transverse direction press strip sealing and dustproof outer cover 14 of dedicated jet runway, first cliche frame is horizontal before being equipped with runway To the green warning lamp 22 of reddish yellow；After runway on cliche frame transverse direction press strip sealing and dustproof outer cover 15, it is horizontal to be equipped with runway rear molding cliche frame To the green warning lamp 23 of reddish yellow.The above is constituted and is controlled the security warning of jet runway entirety.

It is described on the left outside cliche frame longitudinal direction batten seat 16 of dedicated jet runway, be equipped with the left outside cliche frame longitudinal direction reddish yellow of runway it is green Warning lamp 24；On the right outer cliche frame longitudinal direction batten seat 17 of runway, it is respectively equipped with the green warning of the right outer cliche frame longitudinal direction reddish yellow of runway Lamp 25；The green warning lamp 26 of runway front left wheel road reddish yellow；The green warning lamp 27 of runway front right wheel road reddish yellow；Runway rear left wheel road The green warning lamp 28 of reddish yellow；And the rear green warning lamp 29 of right wheel road reddish yellow of runway.The above is constituted whole to jet runway The handling of operation safety active that give warning in advance.

It is described to be slided with efficient short distance or the dedicated jet runway of VTOL aircraft, in type aircraft carrier deck, naval vessel, land and water platform Jet runway device, including the left outside 1-7 region rotary sleeve valve flute profile puff prot of runway or circle hole shape puff prot servo push away Each spout in the 7th region opens 7-8 millimeter 59 in dynamic motor 30, the runway right side, if being mounted in, type aircraft carrier deck is carrier-borne or each airport is dedicated On jet runway 191, on the jet runway of continental rise airport, on continental rise sky body panel jet runway, land and water fix, mobile independent gas On capsule platform jet runway, on naval vessel ship side left and right sides or stern end position extension type air bag platform jet runway.

A variety of gas supply gas sources of the use, the gas laminar flow short distance formed by the gas injection of compressed air are slided or vertically The dedicated jet runway of landing aircraft is respectively equipped with that runway is left outside to be inlayed on each region valve body plate main body module sub-unit 73 Frame longitudinal direction batten seat 16；In the interior lower part of the left outside cliche frame longitudinal direction batten seat 16 of runway, it is equipped with the left outside 1-7 region rotation of runway Moving sleeve valve flute profile puff prot or circle hole shape puff prot servo pushing motor 30；In the right outer cliche frame longitudinal direction batten seat 17 of runway Lower part is equipped with the right outer 1-7 region moving sleeve valve flute profile puff prot of runway or circle hole shape puff prot servo pushing motor 31.More than It is described, it constitutes and the gas source of the flexible safety of the fixed closed of jet runway entirety is quickly ended and quick smooth manipulation and control.

It is described to open 1-2 millimeter 32 in each spout in left outside first region of jet runway, it is respectively sprayed in left first region of runway Mouth opens 1-2 millimeter 33, opens 1-2 millimeter 34 in the right outer each spout in first region of runway, first region in runway is right Each spout opens 1-2 millimeter 35, the connection in whole first region and lower continuous region is constituted, to each puff prot on jet runway The consistency of the adjustment control and mixing ratio of pressure, flow and puff prot gap size.

It is described to open 2-3 millimeter 36 in each spout of the left outside Two Areas of jet runway, it is respectively sprayed in the left Two Areas of runway Mouth opens 2-3 millimeter 37, opens 2-3 millimeter 38 in the right outer each spout of Two Areas of runway, the Two Areas in runway is right Each spout opens 2-3 millimeter 39, the connection of whole Two Areas and lower continuous region is constituted, to each puff prot on jet runway The consistency of the adjustment control and mixing ratio of pressure, flow and puff prot gap size.

It is described to open 3-4 millimeter 40 in the left outside trizonal each spout of jet runway, in the left third region of runway Each spout opens 3-4 millimeter 41, opens 3-4 millimeter 42 in the right outer each spout in third region of runway, the third in the runway right side Each spout in region opens 3-4 millimeter 43, constitutes the coordination up and down between whole third region and lower continuous region, cooperates to jet Each puff prot pressure, flow on runway, the consistency with the adjustment control and mixing ratio of puff prot gap size.

Each spout in left outside 4th region of jet runway opens 4-5 millimeter 44, each in left 4th region of runway Spout opens 4-5 millimeter 45,4-5 millimeter 46 is opened in the right outer each spout in 4th region of runway, the 4th in the jet runway right side A each spout in region opens 4-5 millimeter 47, constitutes puff prot pressure between whole 4th region, being mutually matched up and down The adjustment of flow and each puff prot gap size, to the controllable mechanism of standard air-flow needed for landing aircraft.

Each spout in left outside 5th region in jet runway opens 5-6 millimeter 48, in left 5th region of runway Each spout opens 5-6 millimeter 49,5-6 millimeter 50 is opened in the right outer each spout in 5th region of runway, the 5th in the runway right side Each spout in region opens 5-6 millimeter 51, constitutes whole 5th region to the injection gas on jet runway, needed by landing aircraft Body flow manipulates the airflow clearance size of each area spray mouth with the artificial intelligence automatic control standard increased or reduced.

Each spout in left outside 6th region in jet runway opens 6-7 millimeter 52, in left 6th region of runway Each spout opens 6-7 millimeter 53,6-7 millimeter 54 is opened in the right outer each spout in 6th region of runway, the 6th in the runway right side Each spout in region opens 6-7 millimeter 55, constitute integrally the 6th region on jet runway, by the stabilization of landing aircraft, safety, Normal manipulation, each jet port airflow clearance size meet the security control of the quick landing of landing aircraft.

Each spout in left outside 7th region in jet runway opens 7-8 millimeter 56, in left 7th region of runway Each spout opens 7-8 millimeter 57,7-8 millimeter 58 is opened in the right outer each spout in 7th region of runway, the 7th in the runway right side Each spout in region opens 7-8 millimeter 59, constitutes whole 7th region on jet runway, size is opened in each puff prot gap Control, all manipulation with pilot in aircraft and jet runway control tower mutually switch.Finally, whole in aircraft by pilot Body completes control of the manipulation to landing aircraft on jet runway.

It is described to be slided with efficient short distance or the dedicated jet runway of VTOL aircraft, it is flat in type aircraft carrier deck, naval vessel, land and water Platform jet runway device, including longitudinally multiple air curtain puff prots 60, runway longitudinally spray 50-400 mesh to the left inside China and foreign countries of the runway Intelligent hydraulic spray nozzle 72, set respectively mounted in type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, continental rise airport jet is run On road, on continental rise sky body panel jet runway, land and water is fixed, on mobile independent air bags platform jet runway, and naval vessel ship side is left On the extension type air bag platform jet runway at right side or stern end position.

The gas laminar flow short distance of the use formed by the gas injection of compressed air slide or VTOL aircraft it is special Include with each region air curtain protective gas laminar flow structure of jet runway：The left inside China and foreign countries of runway longitudinally multiple air curtain puff prots 60, Outer laterally four flute profiles or round puff prot are positive normal landing spray before the multiple air curtain puff prots 61 in the right inside and outside longitudinal direction of runway, runway Four flute profiles of middle transverse direction or round puff prot are lateral four slots before and after spare landing puff prot 63, runway before port 62, runway Shape or round puff prot are emergency landing puff prot 64；The above, constitute whole runway is not influenced by external wind interference, And to be designed with normal, emergency, the intelligent control of three independent switching systems of spare landing aircraft each in each region in runway The normal work of region main jet loophole.All of above jet port is designed with the dedicated liquid of cleaning in the runway, in each jet or spray Mist mouth is designed with self-cleaning function.

The position all around of the seat under every piece of 73 template of valve body plate main body module sub-unit of jet runway, is all respectively equipped with Runway installs each valve body plate main body module or so longitudinal road face horizontal adjustment cushion 65；Runway installs each valve body plate main body module Front and back transverse direction road face horizontal adjustment cushion 66；Runway installs each self-locking fixing bolt 67 of valve body plate main body module dedicated buffering. The various bufferings and damping after overloading to whole runway in takeoff and landing are constituted, not will cause shake when reaching to landing aircraft It is dynamic.

Each puff prot effect on from first region of jet runway to the 7th region is identical；Outer rotary shaft flute profile mouth in runway Or round hole axle outer shaft connecting fork library 68；Outer rotary shaft flute profile mouth or round hole axle internal axle sleeve connecting fork library 69 in runway；Ten thousand To spherical sleeve type 180-360 degree angle rotary oscillating type puff prot amendment takeoff and landing, " inclination of the yaw biasing heart, sink-float is helped up and down Just " 70；Inner rotary shaft covers flute profile puff prot 97；Manufacture oxygenation or manufacture anoxic puff prot 71；Longitudinal injection 50-400 mesh intelligence Hydraulic spray nozzle 72.The above constitutes whole each region of jet runway and controls the handling safety of landing aircraft, and increases Can initiatively be met an urgent need each jet port of landing aircraft and spare landing aircraft, rapidly used exterior and interior axle sleeves connecting fork library and passed When moving with interacting, the manipulation to the full intelligent standard of automatic control of each jet port angular speed.

The outer rotary shaft flute profile mouth in jet runway or round hole axle outer shaft connecting fork library 68, with outer rotary shaft in runway It is laterally using fork library that its is each inside and outside to constitute whole each region of jet runway for flute profile mouth or round hole axle internal axle sleeve connecting fork library 69 Rotary shaft, which connects, pitches the connection of library formula, while can be in any transmission, each inside and outside rotary sleeve moving sleeve valve flute profile mouth or interior outward turning Shaft cover the multiple circle hole shape mouths of moving sleeve valve each jet port angle, open size all 100% on an axis, in each spray Precise angle and sealing when port is on and off prevent dirt object, rainwater or seawater from entering each puff prot and shutoff valve shape chamber It is interior.

It is described on jet runway valve body plate main body module sub-unit 73, be respectively equipped with universal globe shell type 180-360 degree angle rotation Switch dynamic jet mouth corrects takeoff and landing " inclination of the yaw biasing heart, righting of rising and falling up and down " 70；Inner rotary shaft covers flute profile jet Mouth 97；Manufacture oxygenation or manufacture anoxic puff prot 71；And longitudinal injection 50-400 mesh intelligence hydraulic spray nozzle 72, constitute whole spray Each region of gas runway actively can meet an urgent need the secure safety manipulation and control of landing to failure or errant aircraft.

Each region 20 meters long 7 of 20 meters long 1 of the first area of jet runway to runway District 7 domain, is respectively equipped with left inside The longitudinal multiple air curtain puff prots 60 in China and foreign countries；The right inside and outside multiple air curtain puff prots 61 in longitudinal direction of runway；Outer laterally four slots before runway Shape or round puff prot are positive normal landing puff prot 62；Four flute profiles of middle transverse direction or round puff prot are spare landing spray before runway Port 63；Laterally four flute profiles or round puff prot are emergency landing puff prot 64 before and after runway；Runway installs each valve body plate master Module or so longitudinal direction road face horizontal adjustment cushion 65；Runway installs lateral road face level tune before and after each valve body plate main body module Whole cushion 66；Runway installs each self-locking fixing bolt 67 of valve body plate main body module dedicated buffering.The above is constituted whole Jet runway realizes the interference for preventing extraneous various wind directions to landing aircraft, it is ensured that jet runway each normal, emergency, spare three The intelligent control of a independent switching system, and to the security reliability during integrated buffer and damping use.

It is described to be slided with efficient short distance or the dedicated jet runway of VTOL aircraft is in type aircraft carrier deck, naval vessel, land and water platform The device of jet runway, including the jet runway valve body plate main body module sub-unit 73, rotary shaft flute profile mouth or round hole axle Outer shaft head end card slot 113, if mounted in type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, continental rise airport jet runway On upper, continental rise sky body panel jet runway, land and water fix, on mobile independent air bags platform jet runway, naval vessel ship side or so Dress can be set on the extension type air bag platform jet runway of side or after run.

A variety of gas supply gas sources of the use, the gas laminar flow short distance formed by the gas injection of compressed air are slided, or are hung down Directly each region valve body plate main body module structure of dedicated jet runway of landing aircraft includes：Runway valve body plate main body module sub-unit 73, on valve body plate main body module sub-unit 73, runway valve body plate main body module installation electromagnet cut off valve or gas control jet are equipped with Air storage chamber phase through slot room 74；Electromagnet cut off valve or gas control jet air storage chamber phase through slot room 74 are installed in runway valve body plate main body module Outside, it is respectively equipped with runway valve body plate main body module air inlet pipe installation room transverse sealing end cap inner panel 92；Runway pavement panel 85；? Under runway valve body plate main body module sub-unit 73, it is equipped with runway valve body plate main body module lower plate pedestal 86；In runway valve body plate On main body module lower plate pedestal 86, it is equipped with runway valve body plate main body module I-shaped support rib stand 87；In runway valve body plate master Module slot room is installed in electromagnet cut off valve or gas control jet air storage chamber phase through slot room 74, and universal globe injector head or inside and outside is equipped with Rotary sleeve sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or pneumatic regulation whiff pressure graduated release valve sub-unit 137；In universal globe injector head or inside and outside rotary sleeve sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or pneumatically Regulate and control on whiff pressure graduated release valve sub-unit 137, is equipped with universal globe injector head guiding jet appendix single sleeve 136 and pressure Main each gas transmission storage of air supply source in contracting air gas source blowing mouth or the quick plug receptacle seat 139 of hose connector and each valve body plate module Deflation bucket interface bore 140.The above, constitute extraneous input gas source to sprayed in whole jet runway gas source it is normal with it is right The control of safe landing gas source.

It is described on runway valve body plate main body module sub-unit 73, be equipped with Pneumatic extension and hydraulic cylinder flexible control mechanism and install Repair blind patch 89 in room；Under Pneumatic extension and hydraulic cylinder flexible control mechanism installation room maintenance blind patch 89, it is equipped with pneumatic It is flexible to push oil cylinder 75；It is pushed on oil cylinder 75 in Pneumatic extension, pushes the flexible interlocking lever 76 of hydraulic cylinder equipped with Pneumatic extension；It stretches Contracting interlocking lever and each control rotary axle valve are oriented to arm connecting plate 77；It is solid up and down with flexible interlocking lever and each guiding arm connecting plate Rationed marketing axis and pin card dottle pin 78.The above constitutes whole jet runway and pneumatically mixes with the dynamic cylinder of oil and rapidly, flexibly brakes Security control mechanism.

It is described outside rotary sleeve sleeve on swing arm fixing groove handle seat 79, to be equipped with outside outer rotary shaft set sleeve fork library inside and outside runway Swing arm and fixing bolt 80；The lower end of swing arm and fixing bolt 80 outside runway outer rotary shaft set sleeve fork library, is equipped with interior Rotary sleeve sleeve pitches swing arm and fixing bolt 81 outside library；Swing arm and fixing bolt 81 outside interior rotary sleeve sleeve fork library Under, it is equipped with and is oriented to lateral pressure swivel bearing 138 inside and outside active support plate swing linking arm or rotary sleeve sleeve.The above institute It states, constitute whole jet runway pneumatically pushes oil cylinder Hybrid connections part, more can neatly be put according to the dynamic that oil cylinder stretches Dynamic, guiding freely to it is each need to reliable position brake.

It is described to be pushed on rack gear or connection gib block 82 in interior outer rotary shaft set sleeve, it is equipped with flexible interlocking lever and each control rotates Axis valve is oriented to arm connecting plate 77；Fixed pin shaft and pin card dottle pin 78 above and below flexible interlocking lever and each guiding arm connecting plate；It is interior Rotary sleeve sleeve pitches swing arm and fixing bolt 81 outside library；And the active support plate of guiding swings linking arm or rotary sleeve set Lateral pressure swivel bearing 138 inside and outside cylinder；It is connected and fixed on seat 83 in master cylinder, is connected and fixed hinged shaft 84 and gas equipped with master cylinder Dynamic stretch pushes oil cylinder 75.The above, constitute the flexible gearing of whole each control unit of jet runway, swing shaft it is sliding close and Each component is assembling the safe manoeuvring in precision, and realizes and improve the stability of service life.

It is described on jet runway valve body plate main body module sub-unit 73, be equipped with runway longitudinally injection 50-400 mesh intelligence water mist Nozzle 72；With runway pavement panel 85.Each region is respectively equipped with the left inside China and foreign countries of runway longitudinally multiple air curtain puff prots 60；With it is universal Spherical sleeve type 180-360 degree angle rotary oscillating type puff prot corrects takeoff and landing " inclination of the yaw biasing heart, righting of rising and falling up and down " 70.The above constitutes on whole jet runway to landing aircraft at abnormal track, constantly obtains amendment and control with adjustment System.

It is described on jet runway valve body plate main body module lower plate pedestal 86, be equipped with runway valve body plate main body module install electromagnetism Shut-off valve or gas control jet air storage chamber phase through slot room 74；Runway valve body plate main body module I-shaped support rib stand 87；Runway valve body Fixing threaded hole 91 above and below plate main body module air inlet air storage chamber transverse sealing end cap；It is installed in runway valve body plate main body module air inlet pipe On room transverse sealing end cap inner panel 92, it is equipped with Normal Take-Off And Landing and stores defeated deflation bucket connecting tube 10；Landing of meeting an urgent need stores defeated deflation bucket Connecting tube 11；Spare landing stores defeated deflation bucket connecting tube 12；And interior each gas transmission of main air supply source stores deflation bucket interface bore 140, constitute the unimpeded control with the fixed support performance of sealing of air distribution system gas transmission of whole jet runway.

It is described on jet runway valve body plate main body module I-shaped support rib stand 87, be equipped with the main body module air inlet of runway valve body plate Pipe installs room transverse sealing end cap inner panel 92；With fixing threaded hole above and below subject runway module air inlet air storage chamber transverse sealing end cap 91；Hydraulic cylinder flexible control mechanism installation room 88 is pushed with Pneumatic extension；In Pneumatic extension and the flexible manipulation machine of hydraulic cylinder Structure is installed in room maintenance blind patch 89, pushes oil cylinder 75 equipped with Pneumatic extension.The above constitutes the pneumatic of whole jet runway It is flexible to push the more stable control effect of hydraulic cylinder flexible control mechanism.

It is described on runway valve body plate main body module sub-unit 73, be equipped with Pneumatic extension and hydraulic cylinder flexible control mechanism and install It repairs blind patch and overlaps mouth 90 in room；On runway valve body plate main body module air inlet pipe installation room transverse sealing end cap inner panel 92, point It She You not the defeated deflation bucket connecting tube 10 of Normal Take-Off And Landing storage；Landing of meeting an urgent need stores defeated deflation bucket connecting tube 11；Spare landing storage Defeated deflation bucket connecting tube 12；Interior each gas transmission of main air supply source stores deflation bucket interface bore 140；Compressed air gas source blowing mouth is soft The quick plug receptacle seat 139 of connecting tube；And fixing threaded hole 91 above and below subject runway module air inlet air storage chamber transverse sealing end cap.With Upper described, the air distribution system and Pneumatic extension for constituting whole jet runway push the flexible installation, maintenance of hydraulic cylinder, user Just operating control mechanism.

It is described to be rotated on solid shaft or hollow shaft sleeve 96 in 0-180 degree angle injection flute profile mouth, it is equipped with inner rotary shaft and covers flute profile Puff prot 97；It is rotated in solid shaft 98 in 0-180 degree angle injection circle hole shape mouth, is equipped with interior rotation solid shaft or hollow axle sleeve Circle hole shape puff prot 99.The above constitutes each jet port air-flow of whole jet runway, by shaft and axle sleeve clearance seal mark The Internal control structure of quasi- precision cooperates adjustment.

30 degree of dead angle jet ports in 30-90 degree fixed angle rotate on solid shaft or hollow shaft sleeve 100, in 30-90 It spends in the 40 degree of dead angle jet ports rotation solid shaft or hollow shaft sleeve 101 of fixed angle, at 50 degree of 30-90 degree fixed angle Dead angle jet port rotates on solid shaft or hollow shaft sleeve 102, in 60 degree of dead angle jet ports rotation of 30-90 degree fixed angles In solid shaft or hollow shaft sleeve 103, in 70 degree of dead angle jet ports rotation solid shaft of 30-90 degree fixed angle or air-cored axis It is rotated on solid shaft or hollow shaft sleeve 105 on sleeve 104, in 80 degree of dead angle jet ports of 30-90 degree fixed angle, Yi Ji In the 90 degree of dead angle jet ports rotation solid shaft or hollow shaft sleeve 106 of 30-90 degree fixed angle, whole jet runway is constituted Internal spray mouth rotary shaft axle sleeve gap sealing and gas storage cell structure another kind mode standard controllability.

It is described to be rotated on solid shaft or hollow shaft sleeve 96 in 0-180 degree angle injection flute profile mouth, it is equipped with rotation axis seal packing Mounting groove 107；On rotation axis seal packing mounting groove 107, it is equipped with rotation axis seal packing 108；In rotary shaft flute profile mouth or On round hole axle internal axle sleeve fixing seat mouth 109, it is respectively equipped with rotary shaft flute profile mouth or round hole axle internal axle sleeve or upper and lower gas transmission room Seal FE Tiler 110；With rotary shaft flute profile mouth or round hole axle exterior and interior axle sleeves or FE Tiler cage bolt hole 95.The above, structure Reliability of the internal spray mouth rotary shaft of integral jet runway to the accurate closing gas source of gas supply gas source sealing structure.

It is described on rotary shaft flute profile mouth or round hole axle outer shaft fixing seat 94, be respectively equipped with rotary shaft flute profile mouth or round hole Axis outer shaft 93；With rotary shaft flute profile mouth or round hole axle exterior and interior axle sleeves or FE Tiler cage bolt hole 95；In rotary shaft flute profile On mouth or round hole axle outer shaft head end card slot 113, rotary shaft flute profile mouth can be respectively equipped with or round hole axle unofficial biography dynamic crankshaft is swung Angle axis 111；D-axis swing angle axis 112 is moved with rotary shaft flute profile mouth or round hole axle unofficial biography.The above, composition are connected Ensuring smooth transmission, it is easy to assembly and use safe reliability.

The dedicated jet runway includes in type aircraft carrier deck, naval vessel, land and water platform jet runway device：In the jet runway valve On 73 on body plate main body module, it is equipped with universal globe shell type gas-sparging head list sleeve or double telescopic sub-units 114；With it is universal Spherical surface injector head outward flange disk seat fixing bolt 141；If mounted in type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, Or on continental rise airfield runway, on continental rise sky body panel runway, land and water fix, on mobile independent air bags platform runway, Yi Jijian On the extension type air bag platform runway of ship ship side left and right sides or after run.

On dedicated each region of jet runway, it is equipped with universal globe shell type gas-sparging head list sleeve or double telescopic sub-units 114；On universal globe shell type gas-sparging head list sleeve or double telescopic sub-units 114, it is equipped with outside universal globe injector head Position fixing seat 116；Universal globe shell type injector head flange seat 115；Universal globe injector head is oriented to jet appendix list sleeve Formula 136；And universal globe injector head or inside and outside rotary sleeve sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or Pneumatic regulation whiff pressure graduated release valve sub-unit 137.It is flexible with driving jet angle to constitute being oriented to for universal globe injector head Change the flexible controlling with the supportive and each jet port rotary oscillating type puff prot that position fixed various point locations.

It is described on jet runway valve body plate main body module sub-unit 73, be respectively equipped with outside universal globe injector head and position fixing seat 116；Universal globe injector head outward flange disk seat fixing bolt 141；Longitudinal motor or the fixed bracket 121 of pneumatic linear actuator；And it is universal Spherical surface injector head guiding leading screw or guiding pneumatic control thick stick fixed plate 126.The guiding and driving for constituting universal globe injector head are sprayed The flexible supportive for changing and positioning fixed various point locations of air horn degree.

It is described to be positioned in fixing seat 116 outside universal globe injector head, it is respectively equipped with universal globe injector head rotary oscillation spherical surface Block set fixes inner shield ring 117；Universal globe jet port spinning ball swings spherical surface and covers fixing seat 118；And universal globe injection Mouth rotary oscillation spherical surface body 119.Constitute universal globe shell type rotary oscillation 0-360 degree can angle-adjustable, realize to injection The connection of the fixation position of gas sub-unit entirety controls.

It is described in universal globe jet port rotary oscillation spherical surface body 119, be respectively equipped with universal globe shell type injector head flange seat 115；Universal globe injector head is oriented to jet appendix single sleeve 136；And universal globe injector head or inside and outside rotary sleeve Sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or pneumatic regulation whiff pressure graduated release valve sub-unit 137.Constitute ten thousand To spherical sleeve type rotary oscillation 0-360 degree can angle-adjustable, realize to injection gas sub-unit entirety gas source control system Security control.

It is described to be positioned in fixing seat 116 outside universal globe injector head, it is respectively equipped with longitudinal motor or the fixed bracket of pneumatic linear actuator 121；Lateral driving lever transmission motor or the transmission of Pneumatic extension cylinder push driving lever 122；And longitudinal motor or pneumatic linear actuator control 123. Constitute universal globe shell type rotary oscillation 0-360 degree can angle-adjustable, realize to injection gas swinging transmission mechanism Control lateral angles are more flexibly stirred and oscillatory.

Described to control on 123 in longitudinal motor or pneumatic linear actuator, longitudinal stir can arbitrarily be adjusted by being respectively equipped with universal globe 0-360 degree Gear or the flexible actuator push rod 120 of pneumatic control；With universal globe injector head guiding leading screw worm gear pairs or guiding Air Valve Control group 127.Constitute universal globe shell type rotary oscillation 0-360 degree can angle-adjustable, and it is whole in injection gas sub-unit Accurate, the flexibility of artificial intelligence switching, manipulation steering spray angle are realized in swinging transmission mechanism control.

It is described to be positioned in fixing seat 116 outside universal globe injector head, it is respectively equipped with universal globe injection headstock gasket 124； Universal globe injector head locknut 125；And universal globe injector head guiding leading screw or guiding pneumatic control thick stick fixed plate 126.Structure At universal globe shell type rotary oscillation 0-360 degree, the fixation that can arbitrarily adjust each angle to injection gas sub-unit entirety is realized Support and control.

It is described universal globe injector head guiding leading screw or guiding pneumatic control thick stick fixed plate 126 on, be respectively equipped with universal globe Injector head guiding leading screw worm gear pairs or guiding Air Valve Control group 127；Universal globe injector head guiding leading screw or guiding Air Valve Control Flexible thick stick 128；Universal globe injector head guiding locking screw 129；Universal globe injector head is oriented to active support plate and swings connection Arm pin shaft and plum blossom latch card 134；Universal globe injector head is oriented to active support plate and swings linking arm 130；Universal globe injection Head is oriented to active support plate and swings linking arm sliding pin 131；Universal globe injector head is oriented to active support plate and swings linking arm Adjust upper arm reinforcing rib 132；And universal globe injector head is oriented to active support plate and swings linking arm pin hole 133.Constitute ten thousand To spherical sleeve type rotary oscillation 0-360 degree can angle-adjustable, realize to the injection fixation of gas sub-unit entirety, support, Control, and the weave control of transmission guiding.

It is described to be oriented in jet appendix single sleeve 136 in universal globe injector head, it is respectively equipped with universal globe injector head and leads Linking arm driving lever support base 135 is swung to active support plate；Universal globe injector head or inside and outside rotary sleeve sleeve flute profile mouth or Each region electromagnet cut off valve of circle hole shape mouth or pneumatic regulation whiff pressure graduated release valve sub-unit 137；Universal globe injector head guiding Active support plate swings linking arm pin hole 133；Universal globe injector head is oriented to active support plate and swings linking arm adjustment upper arm Reinforcing rib 132；Universal globe injector head is oriented to active support plate and swings linking arm sliding pin 131；Universal globe injector head is led Linking arm 130 is swung to active support plate；And universal globe injector head is oriented to active support plate and swings linking arm pin shaft and plum Flower latch card 134.It constitutes extraneous input gas source to control normal, the safe landing for spraying gas source in jet runway, and realizes The connectivity of the active support plate flexible swinging of guiding of universal globe injector head.

It is described that the both ends that active support plate swings linking arm 130 are oriented in universal globe injector head, it is respectively equipped with the active branch of guiding Fagging swings lateral pressure swivel bearing 138 inside and outside linking arm or rotary sleeve sleeve；Connection is swung being oriented to active support plate Inside and outside arm or rotary sleeve sleeve in lateral pressure swivel bearing 138, it is equipped with universal globe injector head and is oriented to active support plate pendulum Dynamic linking arm pin shaft and plum blossom latch card 134.The above constitutes universal globe shell type rotary oscillation 0-360 degree and can arbitrarily adjust Angle realizes the fixed support and the flexibility of guiding movement control whole to injection gas sub-unit.

It is described on jet runway valve body plate main body module sub-unit 73, equipped with positioning fixing seat outside universal globe injector head 116；It is positioned in fixing seat 116 outside universal globe injector head, is equipped with universal globe injector head outward flange disk seat fixing bolt 141.Constitute universal globe shell type rotary oscillation 0-360 degree can angle-adjustable, realize that spray it gas sub-unit whole The maintenance dismounting and the control of fixed supportive of body.

It is described in universal globe injector head or inside and outside rotary sleeve sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or On pneumatic regulation whiff pressure graduated release valve sub-unit 137, it is respectively equipped with universal globe injector head guiding jet appendix list sleeve Formula 136；Compressed air gas source blowing mouth or the quick plug receptacle seat 139 of hose connector；And main each gas transmission storage of air supply source in runway Store gas bucket interface bore 140.Constitute support of the extraneous input gas source to normal, the safe landing for spraying gas source in jet runway Property control.

It is described on universal globe shell type gas-sparging head list sleeve or double telescopic sub-units 114, be equipped with universal globe spray It collaborates under turnbarrel in the double sleeves of head pressure locking block set 209；It is gone here and there under turnbarrel in the double sleeves of universal globe injector head In atmospheric pressure locking block set 209, be respectively equipped with rotary sleeve waterproof and dustproof in the double sleeves of universal globe injector head, antifreeze oil sealing or Packing 208；It collaborates downwards pressure buffer bearing 211 with turnbarrel in the double sleeves of universal globe injector head；It is sprayed in universal globe It penetrates in the double sleeves of head and collaborates outside pressure locking block set 209 under turnbarrel, be equipped with the double sleeve fixed sleeves of universal globe injector head Buffing pad 210 on turnbarrel in cylinder；The buffing pad 210 on turnbarrel in the double sleeve fixed sleeves cylinders of universal globe injector head Outside, it is equipped with universal globe jet port rotary oscillation spherical surface body 119.Constitute the fixed interior rotation of the double bush outer sleeves of universal globe injector head Sleeve rotating is flexibly swung with 360 degree and dust-proof, anti-water management；

It is described on universal globe shell type gas-sparging head list sleeve or double telescopic sub-units 114, be respectively equipped with universal globe The double sleeve fixed sleeves cylinders 212 of injector head；With single sealing gland or the packing of collaborating on the double sleeve inside and outside sleeves of universal globe injector head 213；With slot 214 in the defeated deflation of turnbarrel in the double sleeves of universal globe injector head；And the double sleeves of universal globe injector head It collaborates in the middle part of inside and outside sleeve single sealing gland or packing 215.Constitute turnbarrel flexible rotation and outer fixation in universal globe injector head Leakproofness control between set；

It is described on universal globe shell type gas-sparging head list sleeve or double telescopic sub-units 114, be respectively equipped with universal globe The double sleeve fixed sleeves cylinders of injector head gas transmission air inlet 217 open in usual；It is normal in the double sleeve fixed sleeves cylinders of universal globe injector head In open type gas transmission air inlet 217, it is equipped with turnbarrel 225 in the double sleeves of universal globe injector head；It is double in universal globe injector head In sleeve on turnbarrel 225, air inlet blowing mouth 216 in turnbarrel is equipped in the double sleeves of universal globe injector head；And ten thousand It collaborates under to the double sleeve inside and outside sleeves of spherical surface injector head double sealing glands or packing 218.Constitute the normal injection and gas source in defeated ventilation source The normal flexible effective control opened with the normal leakproofness for closing gas source and gas source；

It is described on turnbarrel 225, to be equipped with rotation in the double sleeves of universal globe injector head in the double sleeves of universal globe injector head Sleeve collaborate upwards compressive resistance buffering bearing 219；It collaborates upwards anti-pressure with turnbarrel in the double sleeves of universal globe injector head Lock flange nut 220；With turnbarrel locking screw tooth 221 in the double sleeves of universal globe injector head；And universal globe injector head Turnbarrel swing arm fixing bolt 224 in double sleeves；With turnbarrel swing arm 223 in the double sleeves of universal globe injector head；With Turnbarrel swing arm pushes and pulls bulb 222 in the double sleeves of universal globe injector head.Rotary sleeve and fixed sleeves rotation spirit in constituting Swing angle living is accurate, reliable；

It is described on the double sleeve fixed sleeves cylinders of universal globe injector head gas transmission air inlet 217 open in usual, be equipped with each valve body template die Soft or hard snorkel is coupled quick combination hub 169 in block；With the defeated soft or hard coupling connecting tube of deflating of nominal gas jet port in runway 157；With in runway can 360 degree rotation swing connecting bend 162；And nominal gas jet port electromagnet cut off valve switchs in runway 151.It constitutes the normal opening input in defeated ventilation source and closes.

In the normal storage deflation bucket 146 in jet runway, with emergency storage deflation bucket 147 in runway and runway Refrigeration, heating sensing modulator 207.Its act on can guarantee it is cold, can ensure that Normal Take-Off And Landing to runway temperature under tropical environment Aircraft.

The conveying gas source Quick connector plug 142 in jet runway stores deflation bucket appendix 143, runway in runway Emergency storage deflation bucket check valve 145 in interior normal storage deflation bucket check valve 144 and multiple runways.Control each general gas The normal gas supply in source and the intelligence switching of each individual gas sources system.Even if encountering failure, still can artificial intelligence switching control just Normal landing.

It is described in jet runway, be equipped with multiple normal storage deflation buckets 146；Emergency storage deflation bucket 147 in runway；In runway Air gauge 148 is regarded outside normal storage deflation bucket；Air gauge 149 is regarded outside emergency storage deflation bucket in runway；Normal injection in runway Gas pressure regulation stop valve 150；Nominal gas jet port electromagnet cut off valve switch 151 in runway；Emergency injection implication in runway Body pressure regulation stop valve 152；Emergency gas ejection ports electromagnet cut off valve switch 153 in runway；And it is normally stored up with emergency in runway It stores gas source in gas bucket and switches electromagnet cut off valve switch 154.To guarantee the normal control of each gas supply gas source.

It is described in jet runway, be equipped with it is multiple normally with emergency storage deflation bucket current collecting tier supply check valve 155；In runway just Often the compressor gas supplied check valve 156 of deflation bucket is stored with emergency；The defeated soft or hard coupling connection of deflating of nominal gas jet port in runway Pipe 157；The defeated soft or hard coupling connecting tube 158 of deflating of emergency gas ejection ports in runway；Normal storage deflation bucket is mutually ventilated in runway Soft or hard coupling connecting tube 159；And emergency storage deflation bucket is mutually ventilated soft or hard coupling connecting tube 160 in runway.It can safety assurance The normal gas supply of each gas source system controls.

It is described in jet runway, be equipped with multiple gas pressure regulation shut-off valves and electromagnet cut off valve and switch connection outside screw 161；It can 360 Spend rotary oscillation connecting bend 162；And the lateral defeated snorkel 163 of nominal gas jet port Universal-head in runway；In runway Emergency gas ejection ports Universal-head laterally on defeated snorkel 164, adjust by refrigeration, the heating sensing being respectively equipped in each valve body plate module Control device 207；Fork sliding sleeve 165 is stirred in the swing of nominal gas jet port transverse pipe in runway；Emergency gas ejection ports are lateral in runway Fork sliding sleeve 166 is stirred in pipe swing；And 167 normally are blocked up with emergency transverse pipe sealing-plug in runway.The above can guarantee each gas The normal output and the landing of runway face normal temperature of source system.

In jet runway normally with meet an urgent need and storage deflation bucket electromagnet cut off valve interval freewheeling diode 168, each valve body plate module Interior soft or hard snorkel is coupled quick combination hub 169, normally stirs fork 170 in runway with emergency transverse pipe swing, is normal in runway It is stirred with emergency transverse pipe swing and normally stirs fork lock in fork connection locking plate 171 and runway with emergency transverse pipe and swing Only plate and handspike fixing bolt 172.It can guarantee the constant and transverse pipe swinging fork angle and electromagnetism of each storage deflation bucket air pressure The intermittent time of valve freewheeling diode can be controlled between 0.001-2.5 seconds positive and negative, so that it may each puff prot is on and off, angle Degree error can be controlled in 0.15-0.2 quickly with the swing for spraying gas flow layer in the range of swing angle needed for landing aircraft.

The mechanically automatically controlled travel switch 173 of normal injection mouth advance stop in jet runway, the retrogressing of normal injection mouth stops in runway The mechanically automatically controlled travel switch 175 of emergency jet port advance stop and race in dynamic mechanical automatically controlled travel switch 174, runway Jet port of meeting an urgent need in road retreats the mechanically automatically controlled travel switch 176 of stop.Ensure artificial intelligence angle sensor signal in runway Still the auto-changeover control function of normal controllable standby line electric-controlled switch after malfunctioning switch and failure.

It is described in the lower part shape chamber of 73 inner frame structure of jet runway valve body plate main body module sub-unit, be respectively equipped in runway Normal injection mouth retreats stop artificial intelligence in the automatically controlled travel switch 177 of normal injection mouth advance stop artificial intelligence formula, runway The automatically controlled travel switch 179 of emergency jet port advance stop artificial intelligence formula and runway in the automatically controlled travel switch 178 of formula, runway Interior emergency jet port retreats the automatically controlled travel switch 180 of stop artificial intelligence formula.It can ensure that pendulum needed for each jet port 10-360 degree angle The accuracy angle of dynamic position and stop position.

Normal injection mouth advances in jet runway sprays with emergency in retrogressing artificial intelligence formula angle sensor controller 181, runway Mouth, which advances, connect locking with servo motor impeller-hub feed rod normal in retrogressing artificial intelligence formula angle sensor controller 182, runway Emergency servo motor impeller-hub feed rod connection locking transition plates 184 in transition plates 183, runway, in runway normal servo motor or Push oil cylinder 185, in runway emergency servo motor or push oil cylinder 186, in runway normally with emergency impeller-hub feed rod 187, run In road normally with emergency impeller-hub feed rod guiding axis sliding sleeve 188.Its optimum efficiency can normal each jet port institute of artificial intelligence control Timing, level pressure, quantitative gas needed for the various required precise angles ejected, the safety for reaching 100% to landing aircraft rise Drop.

The shape chamber in 73 inside casing of jet runway valve body plate main body module sub-unit, interior lower outer portion jet runway pavement lower part In the melt pit on basis, be respectively equipped with normally with emergency and spare three sets independent manuals intelligence, and can mutual numerical control switch The non-control system of new model of air supply system, power supply system, the various safety operation control systems of flight control system and safety is run in jet In road melt pit, it is respectively equipped with runway auxiliary equipment compressor air accumulator air supply system 189；Current collecting tier spare gas storage cylinder gas supply system System 190；On the spare gas storage cylinder air supply system 190 of current collecting tier, it is equipped with refrigeration, heating sensing modulator 207；Low pressure colour gas Body and the preheating main gas ejection ports 226 of oxygen, act on the Normal Take-Off And Landing that can guarantee on runway.The jet runway, which can be used as, flies school The pneumatic dynamic of various actual measurements of various new architecture aircrafts and the static state that various actual measurements are pneumatic are checked and accepted, this runway is that the field is best A detection school fly equipment line, can reach 100% accurately actual measurement and go out；It is a variety of by that itself can be produced in jet runway Can on extraneous landing aircraft environment runway pavement, can release various one hundred point than different proportion manufacture oxygenation, manufacture anoxic, Refrigeration, heating, making drugs into frostlike powder, system are avenged, are made ice, rain processed, manufacturing the functions such as flow-disturbing wind of all sizes, cyclone, various random wind, It can fly test and inspection to the school of landing of the aircraft model performance technologies standard parameter that various coming of new are dispatched from the factory on jet runway It tests.

In the shape chamber of the frame bottom in jet runway valve body plate main body module sub-unit 73, it is respectively equipped with inside and outside runway right The intellectual air control switch 227 of side air curtain normal injection gas solenoid valve；And the external right side air curtain normal injection gas electricity in runway On the intellectual air control switch 227 of magnet valve, it is equipped with the intellectual Regulation Control valve 228 of external right side air curtain normal injection gas in runway； It is additionally provided with external right side air curtain emergency injection gas solenoid valve air control switch 229 in runway simultaneously；And the external right side air curtain in runway On emergency injection gas solenoid valve air control switch 229, it is equipped with the external right side air curtain emergency injection intellectual pressure regulation control of gas in runway Valve 230 processed；In runway external right side normally with the longitudinal defeated snorkel 231 of emergency air curtain Universal-head jet port；With left and right inside and outside runway Longitudinally fork sliding sleeve 232 is stirred in defeated snorkel swing to side air curtain Universal-head jet port.Its maximum actual effect prevents runway external right side Bad interference when wind is to Normal Take-Off And Landing of the landing aircraft in runway.

In the shape chamber of the frame bottom in jet runway valve body plate main body module sub-unit 73, it is respectively equipped with inside and outside runway left The intellectual air control switch 233 of side air curtain normal injection gas solenoid valve；And the left side air curtain normal injection gas electricity inside and outside runway On the intellectual air control switch 233 of magnet valve, it is equipped with the inside and outside left side intellectual Regulation Control valve 234 of air curtain normal injection gas of runway； And it is additionally provided with the inside and outside left side air curtain emergency injection intellectual air control switch 235 of gas solenoid valve of runway；And it is left inside and outside runway On the side air curtain emergency injection intellectual air control switch 235 of gas solenoid valve, it is equipped with the inside and outside left side air curtain emergency injection gas of runway Intellectual Regulation Control valve 236；With left side inside and outside runway normally with the longitudinal defeated snorkel 237 of emergency air curtain Universal-head jet port. Its maximum actual effect is the bad interference for preventing the outer left side wind of runway to the landing in runway of landing aircraft.

In the shape chamber of the frame bottom in each piece of valve body plate main body module sub-unit 73 of jet runway, it is respectively equipped with runway Communication far infrared and spectrum or Beidou intelligent sensing controller 238 are inside normally received, is received with emergency in runway and communicates far infrared Between spectrum or Beidou intelligent sensing controller 239, the navigation of three's far and near distance can mutually switch, and scope of heading is complete Ball and domestic various airports, and various flying objects cannot any, arbitrarily, freely rise and fall on jet runway, and the runway is to each Kind of flyer there is intelligence software to recognize it difference after receive function, and the worldwide navigation to mobile flyer naturally Positioning function, especially to various guided missiles or commit suiside unmanned plane or have it is man-machine attack, which various can not recognize its The various unmanned planes or the flyers such as someone's airborne missile known quickly exclude to blow winged, are effectively protecting jet runway safely just The great advantage often runed.

In the heart-shaped chamber of the frame bottom in jet runway valve body plate main body module sub-unit 73, it is respectively equipped in runway Outer left and right sides and the green instruction lamp driver of middle left and right sides reddish yellow input six hole power sockets 240；The right outside of coupled runway is red Yellowish green indicator light wiring conversion terminal 241；With reddish yellow green indicator light wiring conversion terminal 242 in side in the runway right side；And runway is left The green indicator light wiring conversion terminal 243 of side reddish yellow；And the green indicator light wiring conversion terminal 244 of runway left-external side reddish yellow.It is most Big effect be can normal supply each group indicator light power supply, and it is safer to pilot eye-catching in night landing.

In the shape chamber of the frame bottom in jet runway valve body plate main body module sub-unit 73, it is being respectively equipped with jet runway just Often four hole power sockets 245 are inputted with emergency air curtain electromagnetic valve circuit with emergency main jet port and normally；Just with outside right in runway Often with emergency main jet port and normally with meet an urgent need each solenoid valve control connecting terminal 259 of air curtain；With in runway in the right side normally with answer Anxious each solenoid valve control wiring conversion terminal 260 of main jet port；And in runway it is left normally with emergency each solenoid valve of main jet port Wiring conversion terminal 261；Left-external side normally turns with emergency main jet port and normally with emergency each solenoid valve wiring of air curtain in runway Connecting terminal 262.Its maximum efficiency is to guarantee that each electric-controlled parts and electronic signal can have the control of normal safety standard to it.

It is described in the heart-shaped chamber of 73 bearing wall and frame structure lower part of jet runway valve body plate main body module sub-unit, be respectively equipped with Five hole power sockets 246 normally are inputted with emergency gas receiver solenoid valve x far-infrared spectrum x Beidou x heat tracing line in runway；In runway Normally with emergency gas receiver solenoid valve x far-infrared spectrum x Beidou x heat tracing line connecting terminal 263；With in runway normally with emergency Gas receiver solenoid valve x far-infrared spectrum x Beidou x heat tracing line connecting terminal 264.Its maximum efficiency is to guarantee gas source for giving navigation The accurate and ice and snow of signal, hot weather 100% can have a good normal temperature control adjustment to runway.

It is described in the lower part shape chamber of 73 bearing wall and frame structure of jet runway valve body plate main body module sub-unit, be respectively equipped with runway The normal 1-2 servo motor for pushing main injection port inputs four hole power sockets 247；Before normally pushing main jet port in runway No. 1 servo motor of angle connects on 1-2 contact wiring conversion terminal 265 afterwards；For the closure electricity for controlling No. 1 servo motor It normally pushes No. 2 servo motors of main injection port front and rear angles to meet the 1-2-3 on 4-5 contact in road and runway to connect in deflector It is laid flat on wiring conversion terminal 266；For a closed circuit for controlling No. 2 servo motors, effect ensures each servo motor Normal defeated power supply.

It is described in the lower part shape chamber of 73 bearing wall and frame structure of jet runway valve body plate main body module sub-unit, be respectively equipped with runway Emergency pushes the 3-4 servo motor of main injection port to input four hole power sockets 248；Main jet is pushed to emanate with emergency in runway Mouth No. 3 motors of front and rear angles connect on the wiring conversion terminal 267 of 1-2 contact；For a closure for controlling No. 3 servo motors Emergency pushes No. 4 servo motors of main injection port front and rear angles to meet 1-2 point 3-4-5 and connects deflector standing in circuit and runway On wiring conversion terminal 278；Emergency pushes main injection port in a closed circuit and runway to control No. 4 servo motors No. 4 servo motors of front and rear angles meet 1-2 point 3-4-5 and connect on the wiring conversion terminal 278 of deflector standing, to control No. 4 servos One closed circuit of motor, effect ensure the control of the normal defeated power supply of each servo motor.

It is described in the lower part shape chamber of 73 bearing wall and frame structure of jet runway valve body plate main body module sub-unit, be respectively equipped with runway Interior normal main jet port front and rear angles control No. 1 servo motor and input four hole power sockets 249；Before main jet port normal in runway Angle controls No. 1 servo motor wiring conversion terminal 268 afterwards；No. 1 is pushed for normal main jet port front and rear angles in control runway The closed circuit of servo motor signal transducer, normal main jet port front and rear angles control No. 2 servo motors inputs four in runway Hole power socket 256；No. 2 servo motor wiring conversion terminals 269 are controlled with main jet port front and rear angles normal in runway；With runway Interior emergency main jet port front and rear angles control No. 4 servo motors and input four hole power sockets 257；In runway before and after emergency main jet port Angle controls No. 4 motor wiring conversion terminals 277；Emergency main jet port front and rear angles control No. 3 servo motor inputs in runway Four hole power sockets 250；No. 3 servo motor wiring conversion terminals 270 are controlled with main jet port front and rear angles of meeting an urgent need in runway, are made With being guarantee input power and various signal transducers normal.

It is described in the lower part shape chamber of 73 bearing wall and frame structure of jet runway valve body plate main body module sub-unit, be respectively equipped with runway Interior normal close or retrogressing of advancing inputs six hole power sockets 251 close to No. 1 servo motor sensitive switch；With normally advance in runway It approaches or retreats close to No. 1 servo motor sensitive switch wiring conversion terminal 271；Close or retrogressing connects with normally advancing in runway Nearly No. 2 servo motor sensitive switches input six hole power sockets 255；It approaches or is retreated close to No. 2 servos with normally advancing in runway Motor sensitive switch wiring conversion terminal 272；And it connects to meet an urgent need to advance to approach or retreat in runway and be opened close to No. 3 servo motor sensings Close six hole power sockets 252 of input；Advance close with emergency in runway or retreats close to No. 3 servo motor sensitive switch wiring switchings Terminal 273；Advance close with emergency in runway or retreats close to No. 4 servo motor sensitive switches six hole power sockets 254 of input； Advance close with emergency in runway or retreat close to No. 4 servo motor sensitive switch wiring conversion terminals 274, effect ensures each The power supply of servo motor and each puff prot angle of the normal control of intelligent signal.

It is described in the lower part shape chamber of 73 bearing wall and frame structure of jet runway valve body plate main body module sub-unit, be respectively equipped with and connect sky Air compressor inputs four hole power sockets 253 with current collecting tier is connect；And it connects compressor and connects wiring under current collecting tier gas supply electromagnetic valve gas control Conversion terminal 275；And it connects compressor and connects wiring conversion terminal 276 on current collecting tier gas supply electromagnetic valve gas control, maximum efficiency energy Guarantee the match control of the normal gentle source stream of power supply.

It is described in the lower part shape chamber of 73 bearing wall and frame structure of jet runway valve body plate main body module sub-unit, be respectively equipped with pre- road Deflector erects input and is laid flat six hole power sockets 258 of input with pre- road deflector；Emergency pushes main jet port front-and-back angle in runway Spend No. 4 servo motors connect 1-2 point 3-4-5 connect deflector standing wiring conversion terminal 278 on, for pre- road deflector stand one A automatically controlled closed circuit；And pre- road deflector erects input and is laid flat six hole power sockets 258 of input with pre- road deflector；In runway It is normal that No. 2 servo motors of main injection port front and rear angles is pushed to connect on 4-5 contact；1-2-3, which connects, is laid flat wiring in deflector It is input and the output circuit of the automatically controlled closure that pre- road deflector is laid flat on 266 position of conversion terminal.

It is described to be slided with efficient short distance or the dedicated jet runway of VTOL aircraft, in type aircraft carrier deck, naval vessel, land and water platform Jet runway device includes：It is described type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, be equipped with runway District 7 domain Electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly 206；Type aircraft carrier deck is carrier-borne or each dedicated jet runway in airport On 191, slided equipped with various airport aircrafts or ship-board aircraft when warship lands on 140 meters long 199 into jet runway；Land Base airfield runway, continental rise sky body panel runway, land and water is fixed or mobile independent air bags platform runway and naval vessel ship side or so On side or after run extension type air bag platform runway, safe landing can be all realized.

A variety of gas supply gas sources of the use, the gas laminar flow short distance formed by the gas injection of compressed air are slided, or are hung down On dedicated each region of jet runway of straight landing aircraft, it is equipped with that type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport；It is navigating Female deck is carrier-borne or each dedicated jet runway 191 in airport on, be respectively equipped with seven 20 meters long (140 meters of overall length) × 30 or 40 meters wide The takeoff and landing runway that type aircraft carrier deck is carrier-borne or each dedicated jet in airport is mutually compatible with.

Each airport aircraft or carrier-borne aircraft are when taking off, when carrier-borne aircraft has just been slided into 20 meter long 192 of jet runway；It takes off carrier-borne When machine is slided into 40 meter long 193 of jet runway；When the carrier-borne aircraft that takes off is slided into 60 meter long 194 of jet runway；It takes off When carrier-borne aircraft is slided into 80 meter long 195 of jet runway；Carrier-borne aircraft take off type aircraft carrier deck is carrier-borne or each airport jet runway On 191, the outstanding support nature flying speed of gas and the height being detached from when the second-mission aircraft of dedicated jet runway takes off are constituted, has been taken off Aircraft can take off safely, quickly, naturally generally in the fourth region, when nature flying speed is not achieved such as departing aeroplane, can incite somebody to action Symmetrical hidden horizontal liftable pitches or hidden horizontal with road face on left and right sides outside jet runway or on the outer rear and front end position of runway Horizontal 0-90 degree angle, and 0-30 meters of the formula that is laid flat high lifting tubular type can be erected, heavy caliber sprays the emergency landing of gas laminar flow Device automatically switch open, can Assisted Take Off aircraft quickly accelerate to take off.

Each airport aircraft or carrier-borne aircraft are when warship lands, when just to have slided the 20-40 rice into jet runway long by 196 for carrier-borne aircraft When, landing is blocked for the film grade laminar flow gas enclosure body at first 45 degree of angle；The 60- into jet runway is slided in the presence of warship carrier-borne aircraft At 80 meter long 197, the film grade laminar flow folder at second 45 degree of angle that carrier-borne aircraft blocks has been constituted；At this moment warship carrier-borne aircraft continue to slide Into jet runway 100-120 rice long 198 when, the film grade laminar flow gas enclosure body for having constituted third 45 degree of angles blocks landing；This When, when aircraft is slided when warship lands into 140 meter long 199 of jet runway, it is outstanding to realize the naturally stable gas of safety Support formula blocks landing.It, can will be before on the left and right sides outside jet runway or outside runway as when film grade laminar flow folder, which blocks, incessantly declines aircraft Afterwards on two-end part, symmetrical hidden horizontal liftable pitches or hidden horizontal and road face horizontal 0-90 degree angle, and can erect and be laid flat The emergency lifting gear of the high lifting tubular type heavy calibers injection gas laminar flows of 0-30 meters of formula automatically switches to open, and 100% can reach Landing is quickly blocked to the various aircrafts of auxiliary landing.

Each airport aircraft type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, be respectively equipped with：First region of runway Electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly 200；Runway Two Areas electromagnet cut off valve or pneumatic regulation Whiff pressure alleviates valve assembly 201；Runway third region electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly 202；The 4th region electromagnet cut off valve of runway or pneumatic regulation whiff pressure alleviate valve assembly 203；The 5th region electricity of runway Magnetic shut-off valve or pneumatic regulation whiff pressure alleviate valve assembly 204；The 6th region electromagnet cut off valve of runway or pneumatic regulation spray Atmospheric pressure alleviates valve assembly 205；The 7th region electromagnet cut off valve of runway or pneumatic regulation whiff pressure alleviate valve assembly 206, It constitutes and carrier-borne seven region electromagnet cut off valve of dedicated jet runway or pneumatic regulation is reached with to the gas source of all size air pressure The safety distribution of the artificial intelligence of 100% uniform constant pressure.

When carrier-borne aircraft or each airport aircraft take off on jet runway, the pressure of first region entirety gas source of runway, Alleviate 200 intelligent control of valve assembly by first region electromagnet cut off valve or pneumatic regulation whiff pressure to complete, by first area The air pressure of domain entirety gas source is adjusted to 2-3 technical atmosphere；The air pressure of second region entirety gas source is adjusted to 3-4 A technical atmosphere；Alleviate 201 intelligent control of valve assembly by Two Areas electromagnet cut off valve or pneumatic regulation whiff pressure to complete, The air pressure of third region entirety gas source is adjusted to 4-5 technical atmosphere；By third region electromagnet cut off valve or pneumatically Regulate and control whiff pressure and alleviate the completion of 202 intelligent control of valve assembly, the air pressure of the 4th region entirety gas source is adjusted to 5-6 Technical atmosphere；Alleviate 203 intelligent control of valve assembly by the 4th region electromagnet cut off valve or pneumatic regulation whiff pressure to complete, it will The air pressure of 5th region entirety gas source is adjusted to 6-7 technical atmosphere；By the 5th region electromagnet cut off valve or pneumatic tune It controls whiff pressure and alleviates the completion of 204 intelligent control of valve assembly, the air pressure of the 6th region entirety gas source is adjusted to 7-8 work Journey air pressure；Alleviate 205 intelligent control of valve assembly by the 6th region electromagnet cut off valve or pneumatic regulation whiff pressure to complete, by the The air pressure of seven region entirety gas sources is adjusted to 8-10 technical atmosphere；By the 7th region electromagnet cut off valve or pneumatic regulation Whiff pressure alleviates the completion of 206 intelligent control of valve assembly.The above constitutes seven of carrier-borne aircraft when taking off on jet runway The pressure allocation proportion parameter of region entirety gas source, and regulated and controled by the artificial intelligence in each region.Note：On jet runway, adopt Operating condition when with 10-25 technical atmosphere to landing carrier-borne aircraft.

When each airport aircraft or carrier-borne aircraft are in jet runway landing warship, the pressure of first region entirety gas source of runway Power is alleviated 200 intelligent control of valve assembly by first region electromagnet cut off valve or pneumatic regulation whiff pressure and is completed, by first The air pressure of region entirety gas source is adjusted to 8-10 technical atmosphere；By Two Areas electromagnet cut off valve or pneumatic regulation spray Atmospheric pressure alleviates the completion of 201 intelligent control of valve assembly, and the air pressure of second region entirety gas source is adjusted to 7-8 engineering gas Pressure；Alleviate 202 intelligent control of valve assembly by third region electromagnet cut off valve or pneumatic regulation whiff pressure to complete, by third The air pressure of a region entirety gas source is adjusted to 6-7 technical atmosphere；By the 4th region electromagnet cut off valve or pneumatic regulation spray Atmospheric pressure alleviates the completion of 203 intelligent control of valve assembly, and the air pressure of the 4th region entirety gas source is adjusted to 5-6 engineering gas Pressure；Alleviate 204 intelligent control of valve assembly by the 5th region electromagnet cut off valve or pneumatic regulation whiff pressure to complete, by the 5th The air pressure of region entirety gas source is adjusted to 4-5 technical atmosphere；By the 6th region electromagnet cut off valve or pneumatically regulate and control jet 205 intelligent control of stress reduction valve assembly is completed, and the air pressure of the 6th region entirety gas source is adjusted to 3-4 engineering gas Pressure；Alleviate 206 intelligent control of valve assembly by the 7th region electromagnet cut off valve or pneumatic regulation whiff pressure to complete, by the 7th The air pressure of region entirety gas source is adjusted to 2-3 technical atmosphere.The above constitute to carrier-borne aircraft on jet runway warship When, can the uniform constant-pressure pressure of gas source to seven region entireties distribution, and regulated and controled by the artificial intelligence in each region.Note： Operating condition on jet runway, when using 10-25 technical atmosphere.

It is of the invention to be slided with efficient short distance or the continental rise airport of VTOL aircraft device, aircraft carrier, naval vessel, water in conjunction with attached drawing What the function of Lu Pingtai jet runway was realized in：

A variety of gas supply gas sources of the use, the gas laminar flow short distance formed by the gas of blast injection are slided, or are hung down The dedicated jet runway of straight landing aircraft is respectively equipped on continental rise airport, type aircraft carrier deck, naval vessel, land and water platform jet runway Runway first area is 20 meters long 1 20 meters long by 7 to runway District 7 domain, and totally seven region total lengths are 140 meters.From first area to The front and back of each region puff prot in District 7 domain is all respectively equipped with low pressure colored gas and the preheating main gas ejection ports 226 of oxygen, makees With the height and angle that be each region high pressure spray port of adjustment spray each jet port to the more intuitive vision of color ray.Such as figure Shown in 1a, Fig. 2, Fig. 4, Fig. 6, Fig. 7 and Fig. 8.

It is described to be slided with efficient short distance or the dedicated jet runway of VTOL aircraft, including continental rise airport, type aircraft carrier deck, warship Ship and land and water platform jet runway.The 20 meters long area 7, Gong Qige in 20 meters long 1 of the runway first area and the District 7 domain of runway Domain, if mounted in type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, on the jet runway of continental rise airport, continental rise sky frame is flat On platform jet runway, land and water fix or mobile independent air bags platform jet runway on, naval vessel ship side left and right sides or stern end On each position of the extension type air bag platform jet runway in portion.As Fig. 2, Fig. 4, Fig. 6, Fig. 7, Fig. 8, Figure 80, Figure 81, Figure 82, Shown in Figure 83, Figure 84, Figure 85, Figure 86, Figure 87, Figure 88, Figure 89 and Figure 90.

A variety of gas supply gas sources of the use, the gas laminar flow very-short-reach formed by compressed air gas injection slide or vertically The dedicated jet runway of landing aircraft, the structure in each region include：Runway first area is 20 meters long by 1,20 meters of runway first area Long 1, it is provided with muti-piece valve body plate main body module sub-unit 73, header bits are in and on each position of rearward end before runway, respectively 20 meters long 1 of runway first area, runway second area 20 made of being combined equipped with muti-piece valve body plate main body module sub-unit 73 Rice is long 2,20 meters long 3 of runway third region, 20 meters long 4 of runway the fourth region, 20 meters long 5 of the 5th region of runway, the 6th area of runway 20 meters long 6 of domain and runway District 7 domain are 20 meters long by 7, each region being composed of muti-piece valve body plate main body module sub-unit 73, If mounted in type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on.The above structure realizes an airport or type aircraft carrier deck The whole control to landing aircraft of carrier-borne or each dedicated jet runway in airport.Such as Fig. 1 a, Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7, figure 8, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Figure 80, Figure 81, Figure 82, Shown in Figure 83, Figure 84, Figure 85, Figure 86, Figure 87, Figure 88, Figure 89 and Figure 90.

The left-external side 20 meters long 1 of jet runway first area, is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；It is running On the left outside cliche frame longitudinal direction batten seat 16 in road, it is respectively equipped with the green warning lamp 24 of the left outside cliche frame longitudinal direction reddish yellow of runway；Each area of runway Cushion connecting sewing 13 is installed between the valve body plate module of domain；And the left fixed under-chassis 8 of private track.The above constitutes jet The whole sealing fixation and safety warning structure of runway.As shown in Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7 and Fig. 8.

The left-external side 20 meters long 1 of jet runway first area, is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；It is running The left outside lower part of the left outside cliche frame longitudinal direction batten seat 16 in road is equipped with the left outside 1-7 region rotary sleeve valve flute profile jet of runway Mouth or circle hole shape puff prot servo pushing motor 30；It is outer on 20 meters long 1 of the right side in runway first area, it is equipped with the right outer cliche frame of runway Longitudinal batten seat 17；In the outer lower part in the right side of the right outer cliche frame longitudinal direction batten seat 17 of runway, it is equipped with the right outer 1-7 region rotation of runway Moving sleeve valve flute profile puff prot or circle hole shape puff prot servo pushing motor 31.The above constitutes jet runway in each region The unblocked flexible operating control mechanism of connection of whole fixation and mechanical linkage all around and gas transmission source.As Fig. 2, Fig. 3, Shown in Fig. 4, Fig. 5, Fig. 6, Fig. 7 and Fig. 8.

The laterally inboard 20 meters long 1 of jet runway first area, is equipped with the green warning lamp 28 of runway rear left wheel road reddish yellow； It is 20 meters of second area long by 2 equipped with runway after the left-external side of 20 meters long 1 of runway first area between longitudinal direction；The of runway The preceding longitudinally outboard in one 20 meters of region long 1 is equipped with cliche frame transverse direction press strip sealing and dustproof outer cover 14 before runway；It is inlayed before runway On frame transverse direction press strip sealing and dustproof outer cover 14, it is respectively equipped with Normal Take-Off And Landing and stores defeated deflation bucket connecting tube 10；Landing of meeting an urgent need stores Defeated deflation bucket connecting tube 11；Spare landing stores defeated deflation bucket connecting tube 12；And the sealing of cliche frame transverse direction press strip is anti-before runway Dirt outer cover fixing bolt 18.The above, the gas transmission source for constituting jet runway entirety are unblocked close with cliche frame transverse direction press strip The fixed bindiny mechanism of sealing.As shown in Fig. 1 b, Fig. 1 c, Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7 and Fig. 8.

The inside between the green warning lamp 28 of dedicated jet runway rear left wheel road reddish yellow, is respectively equipped with runway left first A each spout in region opens 1-2 millimeter 33；In left first region of runway, each spout opens the Right Inboard of 1-2 millimeter 33, if There are the green warning lamp 26 of runway front left wheel road reddish yellow and the green warning lamp 27 of runway front right wheel road reddish yellow；In runway front right wheel Outside in the right side of the green warning lamp 27 of road reddish yellow is equipped with each spout in first region in the runway right side and opens 1-2 millimeter 35；On the runway right side In each spout in first region open the right side of 1-2 millimeter 35, equipped with reddish yellow green warning lamp 29 in right wheel road after runway.The above institute It states, the composition warning of safe manoeuvring and the good artificial intelligence manipulation and control of jet mechanism in landing on runway to pilot. As shown in Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6 and Fig. 7.

The right outside of the green warning lamp 29 of right wheel road reddish yellow after dedicated jet runway is equipped with right outer first region of runway Each spout opens 1-2 millimeter 34；The right outside of 1-2 millimeter 34 is opened in the right outer each spout in first region of runway, it is right to be equipped with runway The inside and outside multiple air curtain puff prots 61 in longitudinal direction；In the right outside of the right inside and outside multiple air curtain puff prots 61 in longitudinal direction of runway, it is equipped with runway Right outer cliche frame longitudinal direction batten seat 17；On the right outer cliche frame longitudinal direction batten seat 17 of runway, it can be respectively equipped with outside the runway right side and inlay The right outer cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt 21 of the green warning lamp 25 of frame longitudinal direction reddish yellow, runway, dedicated jet are run Cushion connecting sewing 13 is installed between the right fixed under-chassis 9 in road and each region valve body plate module of runway.The above is constituted each Parts for maintenance, the reasonability of dismounting, harmony, consistent property and convenience form air curtain and protect each puff prot, the total gas of protection Source makes the Normal Take-Off And Landing of aircraft safety, and the connection with each component and warning control.Such as Fig. 1 a, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6, figure 7, shown in Fig. 8 and Fig. 9.

20 meters long 2 of second area of the left-external side in jet runway is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；? On the left outside cliche frame longitudinal direction batten seat 16 of runway, it is respectively equipped with the green warning lamp 24 of the left outside cliche frame longitudinal direction reddish yellow of runway；Runway is each Cushion connecting sewing 13 and private track left fixed under-chassis 8 are installed between the valve body plate module of region.The above constitutes spray Gas runway integrally each site location be fixedly connected with warning structural compatibility.Such as Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7 and Fig. 8 institute Show.

20 meters long 2 of second area of the left side of transverse direction in jet runway is equipped with the green warning of runway rear left wheel road reddish yellow Lamp 28；Between longitudinal direction, it is 20 meters long by 3 to be equipped with runway third region after 20 meters long 2 of runway second area of left-external side；In runway Between the preceding longitudinal direction in two 20 meters of regions long 2, it is 20 meters long by 1 to be equipped with runway first area.The above is constituted whole to jet runway The consistent matching of cooperation control.As shown in Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7 and Fig. 8.

The left-external side 20 meters long 3 of the third region of jet runway, is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；? On the left outside cliche frame longitudinal direction batten seat 16 of runway, it is respectively equipped with the green warning lamp 24 of the left outside cliche frame longitudinal direction reddish yellow of runway；Runway is each Cushion connecting sewing 13 and private track left fixed under-chassis 8 are installed between the valve body plate module of region.The above constitutes spray The entirety of gas runway is fixedly connected with the associativity with warning.As shown in Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7 and Fig. 8.

The left side of transverse direction 20 meters long 3 of the third region of jet runway, is equipped with the green warning lamp of runway rear left wheel reddish yellow 28；It between longitudinal direction, is being equipped with 20 meters of runway the fourth region long by 4 after the left-external side in 20 meters long 3 of runway third region；In runway third Between the preceding longitudinal direction that 20 meters long 3 of region, it is equipped with 20 meters of runway second area long by 2.The above constitutes the structure between each region Connect Proper Match and consistency.As shown in Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7 and Fig. 8.

20 meters long 4 of the fourth region of the left-external side in jet runway is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；? On the left outside cliche frame longitudinal direction batten seat 16 of runway, it is respectively equipped with the green warning lamp 24 of the left outside cliche frame longitudinal direction reddish yellow of runway；Runway is each Cushion connecting sewing 13 and private track left fixed under-chassis 8 are installed between the valve body plate module of region.The above constitutes spray The fixed associativity of gas runway integrated connection.As shown in Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7 and Fig. 8.

20 meters long 4 of the fourth region of the left side of transverse direction in jet runway is equipped with the green warning of runway rear left wheel road reddish yellow Lamp 28；Between longitudinal direction, it is 20 meters long by 5 to be equipped with the 5th region of runway after 20 meters long 4 of the fourth region of runway of left-external side；In runway Between the preceding longitudinal direction that 20 meters long 4 of the fourth region, it is 20 meters long by 3 to be equipped with runway third region.The above constitutes each region to jet The connection of runway and the reliability of security warning.As shown in Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7 and Fig. 8.

The left-external side 20 meters long 5 of the 5th region of jet runway, is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；? On the left outside cliche frame longitudinal direction batten seat 16 of runway, it is respectively equipped with the green warning lamp 24 of the left outside cliche frame longitudinal direction reddish yellow of runway；Runway is each Cushion connecting sewing 13 and private track left fixed under-chassis 8 are installed between the valve body plate module of region.The above constitutes spray The fixed security warning of the whole combination of gas runway.As shown in Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7 and Fig. 8.

The left side of transverse direction 20 meters long 5 of the 5th region of jet runway, is equipped with the green warning of runway rear left wheel road reddish yellow Lamp 28；Between longitudinal direction, it is 20 meters long by 6 to be equipped with the 6th region of runway after the left-external side in 20 meters long 5 of the 5th region of runway；In runway Between the preceding longitudinal direction in five 20 meters of regions long 5, it is equipped with 20 meters of runway the fourth region long by 4.The above is constituted between each region to spray The installation of modular subregionization, dismounting, maintenance, the practicability of debugging and the reliability of gas runway entirety.As Fig. 2, Fig. 3, Fig. 4, Shown in Fig. 6, Fig. 7 and Fig. 8.

The left-external side 20 meters long 6 of the 6th region of jet runway, is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；? On the left outside cliche frame longitudinal direction batten seat 16 of runway, it is respectively equipped with the green warning lamp 24 of the left outside cliche frame longitudinal direction reddish yellow of runway；Runway is each Cushion connecting sewing 13 and private track left fixed under-chassis 8 are installed between the valve body plate module of region.The above constitutes spray The structure combination of gas runway entirety, fixed security warning.As shown in Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7 and Fig. 8.

The left side of transverse direction 20 meters long 6 of the 6th region of jet runway, is equipped with the green warning lamp of runway rear left wheel reddish yellow 28；Between longitudinal direction, it is 20 meters long by 7 to be equipped with runway District 7 domain after the left-external side in 20 meters long 6 of the 6th region of runway；In runway the 6th Between the preceding longitudinal direction that 20 meters long 6 of region, it is 20 meters long by 5 to be equipped with the 5th region of runway.The above constitutes each regional body and each area The cooperation in domain, between each movement mechanism and fixed mechanism part, the reasonable manipulation of advance and artificial intelligence in practical application Property.As shown in Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7 and Fig. 8.

The left-external side 20 meters long 7 of the District 7 domain of jet runway, is equipped with the left outside cliche frame longitudinal direction batten seat 16 of runway；? On the left outside cliche frame longitudinal direction batten seat 16 of runway, it is respectively equipped with the green warning lamp 24 of the left outside cliche frame longitudinal direction reddish yellow of runway；Runway is each Cushion connecting sewing 13 and private track left fixed under-chassis 8 are installed between the valve body plate module of region.The above constitutes spray The security warning of combination, the fixation of gas runway entirety.As shown in Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7 and Fig. 8.

The left side of transverse direction 20 meters long 7 of the District 7 domain of jet runway, is equipped with the green warning of runway rear left wheel road reddish yellow Lamp 28；In 20 meters long 7 of the rear longitudinally outboard in the District 7 domain of runway, it is equipped with cliche frame transverse direction press strip sealing and dustproof outer cover after runway 15；After runway on cliche frame transverse direction press strip sealing and dustproof outer cover 15, it is respectively equipped with Normal Take-Off And Landing and stores defeated deflation bucket connecting tube 10；Landing of meeting an urgent need stores defeated deflation bucket connecting tube 11；Spare landing stores defeated deflation bucket connecting tube 12；And cliche frame after runway Lateral press strip sealing and dustproof outer cover fixing bolt 19.The above is constituted to whole jet runway air distribution system the most complete Seal security warning and the smooth practicability of gas source.As shown in Fig. 1 b, Fig. 1 c, Fig. 2, Fig. 3, Fig. 4, Fig. 6, Fig. 7 and Fig. 8.

It is described to be slided with efficient short distance or the dedicated jet runway of VTOL aircraft, in continental rise airport, type aircraft carrier deck, warship Device on ship, land and water platform jet runway includes：The longitudinal pressure of the right outer cliche frame of the left fixed under-chassis 8 of the private track, runway Sealing and dustproof outer cover fixing bolt 21, if mounted in type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, continental rise airport On jet runway, on continental rise sky body panel jet runway, land and water fix or mobile independent air bags platform jet runway on, and On naval vessel ship side left and right sides or the extension type air bag platform jet runway at stern end position.Such as Fig. 2, Fig. 3, Fig. 8, Figure 80, figure 81, shown in Figure 82, Figure 83, Figure 84, Figure 85, Figure 86, Figure 87, Figure 88, Figure 89 and Figure 90.

A variety of gas supply gas sources of the use, the gas laminar flow short distance formed by compressed air gas injection slide or vertically The dedicated jet runway of aircraft drops, and the fixed structure in each region includes：The left fixed under-chassis 8 of private track, the right fixed machine of private track Foot 9, Normal Take-Off And Landing store defeated deflation bucket connecting tube 10, emergency landing stores defeated deflation bucket connecting tube 11, spare landing storage is defeated Cliche frame is laterally pressed before installing cushion connecting sewing 13, runway between each region valve body plate module of deflation bucket connecting tube 12, runway Cliche frame transverse direction press strip sealing and dustproof outer cover 15, the left outside cliche frame longitudinal direction batten seat of runway after sealing and dustproof outer cover 14, runway 16, cliche frame transverse direction press strip sealing and dustproof outer cover fixing bolt 18, runway before the right outer cliche frame longitudinal direction batten seat 17 of runway, runway The left outside cliche frame longitudinal direction press strip sealing and dustproof outer cover of cliche frame transverse direction press strip sealing and dustproof outer cover fixing bolt 19, runway is fixed afterwards Bolt 20 and the right outer cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt 21 of runway.The above is constituted and is run to jet The air-channel systems such as whole defeated, the storage deflation in road are connected and fixed with each component.Such as Fig. 1 b, Fig. 1 c, Fig. 2, Fig. 3, Fig. 4 and Fig. 8 It is shown.

It is described on the left outside cliche frame longitudinal direction batten seat 16 of dedicated jet runway, be respectively equipped with each region valve body plate module of runway it Between install cushion connecting sewing 13；The left outside cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt 20 of runway；It is left outside in runway On the bottom position of cliche frame longitudinal direction batten seat 16, it is equipped with the left fixed under-chassis 8 of private track.The above is constituted and is run to jet Road it is whole inlay after being locked property.As shown in Fig. 2, Fig. 3 and Fig. 8.

It is described on the right outer cliche frame longitudinal direction batten seat 17 of dedicated jet runway, it is green to be equipped with the outer cliche frame longitudinal direction in runway right side reddish yellow Warning lamp 25；On the bottom position of the right outer cliche frame longitudinal direction batten seat 17 of runway, it is equipped with the right fixed under-chassis 9 of private track；With The right outer cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt 21 of runway；Before runway outside cliche frame transverse direction press strip sealing and dustproof On cover 14, it is respectively equipped with the green warning lamp 22 of first cliche frame transverse direction reddish yellow before runway；Normal Take-Off And Landing stores defeated deflation bucket connecting tube 10； Landing of meeting an urgent need stores defeated deflation bucket connecting tube 11；Cliche frame is horizontal before spare landing stores defeated deflation bucket connecting tube 12 and runway To press strip sealing and dustproof outer cover fixing bolt 18.The above constitutes the fixed layout and valve actuating mechanism whole to jet runway Layout close connection.As shown in Fig. 1 b, Fig. 1 c, Fig. 2, Fig. 3, Fig. 4 and Fig. 8.

It is described on the rear cliche frame transverse direction press strip sealing and dustproof outer cover 15 of dedicated jet runway, be respectively equipped with Normal Take-Off And Landing storage Defeated deflation bucket connecting tube 10；Landing of meeting an urgent need stores defeated deflation bucket connecting tube 11；Spare landing stores defeated deflation bucket connecting tube 12；It runs The green warning lamp 23 of road rear molding cliche frame transverse direction reddish yellow；And cliche frame transverse direction press strip sealing and dustproof outer cover fixing bolt after runway 19, constitute to jet runway globality valve train system and closing connection warning can manipulation and control.Such as Fig. 1 b, Fig. 1 c, figure 2, shown in Fig. 3 and Fig. 4.

It is described to be slided with efficient short distance or the dedicated jet runway of VTOL aircraft is flat in type aircraft carrier deck, naval vessel and land and water Device on platform jet runway, including the green warning lamp 22 of first cliche frame transverse direction reddish yellow before runway, with wheel right after runway road reddish yellow Green warning lamp 29, set respectively mounted in type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, continental rise airport jet runway On upper, continental rise sky body panel jet runway, land and water fix or mobile, independent air bags platform jet runway on and naval vessel ship On side of a ship left and right sides or the extension type air bag platform jet runway at stern end position.Such as Fig. 2, Fig. 3, Figure 80, Figure 81, Figure 82, figure 83, shown in Figure 84, Figure 85, Figure 86, Figure 87, Figure 88, Figure 89 and Figure 90.

A variety of gas supply gas sources of the use, the gas laminar flow short distance formed by the gas injection of compressed air slide landing or On the dedicated jet runway of VTOL aircraft, the green control instruction modulated structure of the reddish yellow in each region includes：First cliche frame before runway The lateral green warning lamp 22 of reddish yellow, the green warning lamp 23 of runway rear molding cliche frame transverse direction reddish yellow, the left outside cliche frame longitudinal direction reddish yellow of runway are green Warning lamp 24, the green warning lamp 25 of the runway right side outer cliche frame longitudinal direction reddish yellow, the green warning lamp 26 of runway front left wheel road reddish yellow, runway The green warning lamp 27 of front right wheel road reddish yellow, right wheel road reddish yellow after the green warning lamp 28 of runway rear left wheel road reddish yellow and runway Green warning lamp 29.The above is constituted to the automatic warning of jet runway entirety, safety, the controllability of active.Such as Fig. 2 and Shown in Fig. 3.

It is described on the preceding cliche frame transverse direction press strip sealing and dustproof outer cover 14 of dedicated jet runway, first cliche frame is horizontal before being equipped with runway To the green warning lamp 22 of reddish yellow；On runway rear molding cliche frame transverse direction press strip sealing and dustproof outer cover 15, it is equipped with runway rear molding cliche frame The lateral green warning lamp 23 of reddish yellow.The above is constituted and is controlled the security warning of jet runway entirety.As shown in Figures 2 and 3.

It is described on the left outside cliche frame longitudinal direction batten seat 16 of dedicated jet runway, be equipped with the left outside cliche frame longitudinal direction reddish yellow of runway it is green Warning lamp 24；On the right outer cliche frame longitudinal direction batten seat 17 of runway, it is respectively equipped with the green warning of the right outer cliche frame longitudinal direction reddish yellow of runway Lamp 25；The green warning lamp 26 of runway front left wheel road reddish yellow；The green warning lamp 27 of runway front right wheel road reddish yellow；Runway rear left wheel road The green warning lamp 28 of reddish yellow；And reddish yellow green warning lamp 29 in right wheel road after runway.The above is constituted to jet runway entirety Give warning in advance operation safety, active it is handling.As shown in Figures 2 and 3.

It is described to be slided with efficient short distance or the dedicated jet runway of VTOL aircraft, in type aircraft carrier deck, naval vessel, land and water platform Device on jet runway, including the left outside 1-7 region rotary sleeve valve flute profile puff prot of runway or circle hole shape puff prot are watched It takes pushing motor 30, open 7-8 millimeter 59 with each spout in the 7th region in the runway right side, type aircraft carrier deck is carrier-borne or each machine if being mounted in On dedicated jet runway 191, on the jet runway of continental rise airport, on continental rise sky body panel jet runway, land and water fixes or moves The extension type air bag platform jet on formula independent air bags platform jet runway and naval vessel ship side left and right sides or stern end position On runway.Apparatus above constitutes the artificial intelligence control to each region puff prot size and flow.As Fig. 4, Fig. 5, Fig. 6, Fig. 7, Shown in Figure 80, Figure 81, Figure 82, Figure 83, Figure 84, Figure 85, Figure 86, Figure 87, Figure 88, Figure 89 and Figure 90.

A variety of gas supply gas sources of the use, the gas laminar flow short distance formed by the gas injection of compressed air are slided or vertically The dedicated jet runway of landing aircraft.On each region of runway valve body plate main body module sub-unit 73, it is left outside to be respectively equipped with runway Cliche frame longitudinal direction batten seat 16；In the interior lower part of the left outside cliche frame longitudinal direction batten seat 16 of runway, it is equipped with the left outside 1-7 region of runway Rotary sleeve valve flute profile puff prot or circle hole shape puff prot servo pushing motor 30；In the right outer cliche frame longitudinal direction batten seat of runway Lower part in 17, is equipped with the right outer 1-7 region rotary sleeve valve flute profile puff prot of runway or circle hole shape puff prot servo pushes electricity Machine 31.The above, constitute to the fixed closed of jet runway entirety and flexibly safe gas source quickly end with it is quick unimpeded Manipulation and control.Such as Fig. 1 a, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, figure 46, shown in Figure 47, Figure 48 and Figure 49.

Each spout in left outside first region in jet runway opens 1-2 millimeter 32, each in left first region of runway Spout opens 1-2 millimeter 33, opens 1-2 millimeter 34 in the right outer each spout in first region of runway, first area in the runway right side Each spout in domain opens 1-2 millimeter 35, the connection in whole first region and lower continuous region is constituted, to each puff prot on jet runway Pressure, flow and puff prot gap size adjustment control and the consistency of cooperation jet ratio.Such as Fig. 4, Fig. 5, Fig. 6 With shown in Fig. 7.

Each spout of the left outside Two Areas in jet runway opens 2-3 millimeter 36, each in the left Two Areas of runway Spout opens 2-3 millimeter 37, opens 2-3 millimeter 38 in the right outer each spout of Two Areas of runway, second area in the runway right side Each spout in domain opens 2-3 millimeter 39, the connection of whole Two Areas and lower continuous region is constituted, to each puff prot on jet runway Pressure, flow and puff prot gap size adjustment control and the consistency of cooperation jet ratio.Such as Fig. 4, Fig. 5, Fig. 6 and Shown in Fig. 7.

Each spout in the left outside third region in jet runway opens 3-4 millimeter 40, each in the left third region of runway Spout opens 3-4 millimeter 41, opens 3-4 millimeter 42 in the right outer each spout in third region of runway, the third area in the runway right side Each spout in domain opens 3-4 millimeter 43, constitutes the cooperation up and down between whole third region and lower continuous region, runs to jet The adjustment control and the consistency of cooperation jet ratio of the pressure of each puff prot, flow and puff prot gap size on road.Such as Shown in Fig. 4, Fig. 5, Fig. 6 and Fig. 7.

Each spout in left outside 4th region in jet runway opens 4-5 millimeter 44, each in left 4th region of runway Spout opens 4-5 millimeter 45,4-5 millimeter 46 is opened in the right outer each spout in 4th region of runway, in the right area Zhong Sige of runway Each spout in domain opens 4-5 millimeter 47, constitute the upper and lower puff prot pressure flow being mutually matched between integrally the 4th region, with And the adjustment of each puff prot gap size, constitute the controllable mechanism to standard air-flow required for landing aircraft.Such as Fig. 4, figure 5, shown in Fig. 6 and Fig. 7.

Each spout in left outside 5th region in jet runway opens 5-6 millimeter 48, each in left 5th region of runway Spout opens 5-6 millimeter 49,5-6 millimeter 50 is opened in the right outer each spout in 5th region of runway, in the right area Zhong Wuge of runway Each spout in domain opens 5-6 millimeter 51, constitutes whole 5th region to the injection gas on jet runway, needed by landing aircraft Flow manipulate the airflow clearance size of each area spray mouth can with the artificial intelligence automatic control standard increasedd or decreased.Such as Shown in Fig. 4, Fig. 5, Fig. 6 and Fig. 7.

Each spout in left outside 6th region in jet runway opens 6-7 millimeter 52, each in left 6th region of runway Spout opens 6-7 millimeter 53,6-7 millimeter 54 is opened in the right outer each spout in 6th region of runway, in the right area Zhong Liuge of runway Each spout in domain opens 6-7 millimeter 55, and it is stable, safe, normal to landing aircraft on jet runway, is made to constitute whole 6th region Each jet port airflow clearance size of manipulation, meet the security control of the quick landing of landing aircraft.Such as Fig. 4, Fig. 5, Fig. 6 and Fig. 7 It is shown.

Each spout in left outside 7th region in jet runway opens 7-8 millimeter 56, each in left 7th region of runway Spout opens 7-8 millimeter 57,7-8 millimeter 58 is opened in the right outer each spout in 7th region of runway, in the right area Zhong Qige of runway Each spout in domain opens 7-8 millimeter 59, constitutes seven whole regions on jet runway, opens size to each puff prot gap Control mutually switches with the control system of pilot in machine and runway control tower.Finally, whole in aircraft by pilot Complete control of the manipulation jet runway to landing aircraft.As shown in Figure 4, Figure 5, Figure 6 and Figure 7.

It is described to be slided with efficient short distance or the dedicated jet runway of VTOL aircraft, it is flat in type aircraft carrier deck, naval vessel, land and water Device on platform jet runway includes：The longitudinal multiple air curtain puff prots 60 in the left inside China and foreign countries of runway, with the longitudinal injection 50-400 of runway Mesh intelligence hydraulic spray nozzle 72, set respectively mounted in type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, continental rise airport jet On runway, on continental rise sky body panel jet runway, land and water fix or mobile independent air bags platform jet runway on, naval vessel ship side On left and right sides or the extension type air bag platform jet runway at stern end position.Such as Fig. 1 a, Fig. 4, Fig. 5, Fig. 6, Fig. 7, Fig. 8, figure 9, shown in Figure 80, Figure 81, Figure 82, Figure 83, Figure 84, Figure 85, Figure 86, Figure 87, Figure 88, Figure 89 and Figure 90.

The gas laminar flow short distance of the use formed by the gas injection of compressed air slide or VTOL aircraft it is special Include with each region air curtain protective gas laminar flow structure of jet runway：The left inside China and foreign countries of runway longitudinally multiple air curtain puff prots 60, run Outer laterally four flute profiles or round puff prot are positive normal landing spray before the multiple air curtain puff prots 61 in the right inside and outside longitudinal direction in road, runway Four flute profiles of middle transverse direction or round puff prot are spare landing puff prot 63, lateral four slots before and after runway before port 62, runway Shape or round puff prot are emergency landing puff prot 64；The above, constitutes whole runway not by the interference effect of external wind, And each region main injection of intelligent control of normal emergency, spare three independent switching systems of landing aircraft is designed in runway The normal work of mouth.All of above jet port is designed with the dedicated liquid of cleaning in the runway, all can oneself in each jet or atomizing nozzle Clean function.As shown in Fig. 1 a, Fig. 4, Fig. 5, Fig. 6, Fig. 7, Fig. 8 and Fig. 9

The position all around of the seat under every piece of 73 template of valve body plate main body module sub-unit of jet runway, is all installed respectively Each valve body plate main body module or so longitudinal direction road face horizontal adjustment cushion 65；Each valve body plate main body module front and back lateral road face is installed Horizontal adjustment cushion 66；Each self-locking fixing bolt 67 of valve body plate main body module dedicated buffering is installed.Composition exists to entire runway Various bufferings when landing not will cause vibration when reaching to landing aircraft.As Fig. 1 a, Fig. 2, Fig. 3, Fig. 8, Fig. 9, Figure 33, Shown in Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48 and Figure 49

Each puff prot effect on from first region of jet runway to the 7th region is identical：Outer rotary shaft flute profile mouth in runway Or round hole axle outer shaft connecting fork library 68；Outer rotary shaft flute profile mouth or round hole axle internal axle sleeve connecting fork library 69 in runway；Ten thousand To spherical sleeve type 180-360 degree angle rotary oscillating type puff prot amendment takeoff and landing, " inclination of the yaw biasing heart, sink-float is helped up and down Just " 70；Inner rotary shaft covers flute profile puff prot 97；Manufacture oxygenation or manufacture anoxic puff prot 71；Runway longitudinally sprays 50-400 mesh Intelligent hydraulic spray nozzle 72.The above constitutes whole each region of jet runway and controls the handling safety of landing aircraft, Yi Jizeng The function of having added can actively meet an urgent need landing aircraft and spare landing aircraft, eliminates various external winds and does to landing aircraft It disturbs, each jet port is rapidly switched to full smart steering.Such as Fig. 1 a, Fig. 9, Figure 16, Figure 49, Figure 50, Figure 75, Figure 76, Figure 91, figure 93, shown in Figure 96, Figure 98, Figure 99, Figure 100, Figure 101, Figure 102 and Figure 103.

20 meters long 1 of first region to jet runway is respectively equipped with a runway left side on 20 meters long 7 of runway District 7 domain Outer laterally four before the multiple air curtain puff prots 61 in the right inside and outside longitudinal direction of the multiple air curtain puff prots 60 in inside and outside longitudinal direction, runway, runway Be positive four flute profiles of middle transverse direction or round puff prot before normal landing puff prot 62, runway of flute profile or round puff prot is spare landing Laterally four flute profiles or round puff prot are emergency landing puff prot 64 before and after puff prot 63 and runway.Constitute jet runway Each region can respectively independence be normal, meets an urgent need, three sets of spare switching management systems.As Fig. 1 a, Fig. 2, Fig. 4, Fig. 5, Fig. 6, Shown in Fig. 7, Fig. 8 and Fig. 9.

The outer rotary shaft flute profile mouth in jet runway or round hole axle outer shaft connecting fork library 68, with outward turning in jet runway Shaft flute profile mouth or round hole axle internal axle sleeve connecting fork library 69 constitute whole each region inner rotary shaft of jet runway and cover moving sleeve valve Each inside and outside rotary shaft sleeve of flute profile mouth and inside and outside rotary sleeve moving sleeve valve circle hole shape mouth, which connects, to be pitched library formula and connect, while inside and outside Rotary sleeve pitch library connection with rotation when, can each puff prot is on and off, sealing, prevent dirt object, rainwater or seawater into Enter each puff prot and shutoff valve shape is intracavitary.As shown in Figure 103.

It is described on the valve body plate main body module sub-unit 73 of jet runway, be respectively equipped with universal globe shell type 180-360 degree angle Rotary oscillating type puff prot corrects takeoff and landing " inclination of the yaw biasing heart, righting of rising and falling up and down " 70；Inner rotary shaft covers flute profile spray Port 97；Manufacture oxygenation or manufacture anoxic puff prot 71 and runway longitudinally injection 50-400 mesh intelligence hydraulic spray nozzle 72.It constitutes Whole each region of jet runway is actively to the secure safety manipulation and control of emergency landing aircraft.As Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 16, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Figure 50, Figure 75, Figure 76, figure 91, shown in Figure 93, Figure 96, Figure 98, Figure 99, Figure 100, Figure 101, Figure 102 and Figure 103.

Each region 20 meters long 7 of 20 meters long 1 of the first area of jet runway and runway District 7 domain, is respectively equipped with runway The longitudinal multiple air curtain puff prots 60 in left inside China and foreign countries；With the right inside and outside multiple air curtain puff prots 61 in longitudinal direction of runway；It is outer lateral before runway Four flute profiles or round puff prot are positive normal landing puff prot 62；Four flute profiles of middle transverse direction or round puff prot are spare before runway Landing puff prot 63；And laterally four flute profiles or round puff prot are emergency landing puff prot 64 before and after runway.The above, Whole runway is constituted not by the interference of extraneous various wind directions, and each region is designed with normal, emergency, spare in runway The normal work of each region main jet loophole of the intelligent control of three independent switching systems of landing aircraft.As Fig. 1 a, Fig. 2, Fig. 4, Shown in Fig. 5, Fig. 6, Fig. 7, Fig. 8 and Fig. 9.

] seat under every piece of 73 module of valve body plate main body module sub-unit of jet runway position all around, all set respectively There is runway that each valve body plate main body module or so longitudinal road face horizontal adjustment cushion 65 is installed；Runway installs each valve body plate main body mould Lateral road face horizontal adjustment cushion 66 before and after block；Runway installs the self-locking fixing bolt of each valve body plate main body module dedicated buffering 67.The various bufferings and damping to runway after overloading to whole runway in takeoff and landing are constituted, are reached to landing aircraft When 100% not will cause resonance, and the reliability that uses.Such as Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, figure 42, shown in Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48 and Figure 49.

It is described on the valve body plate main body module sub-unit 73 of jet runway, be respectively equipped with outer rotary shaft flute profile mouth or circle in runway Shape hole axle outer shaft connecting fork library 68；With outer rotary shaft flute profile mouth in runway or round hole axle internal axle sleeve connecting fork library 69；It is universal Spherical sleeve type 180-360 degree angle rotary oscillating type puff prot corrects takeoff and landing " eccentric biasing boat inclination, righting of rising and falling up and down " 70；Inner rotary shaft covers flute profile puff prot 97；Manufacture oxygenation or manufacture anoxic puff prot 71 and runway longitudinally injection 50-400 mesh Intelligent hydraulic spray nozzle 72.The above constitutes rotary sleeve moving sleeve valve jet port rotation inside and outside each region of whole jet runway The consistency of angle, while the actively constantly amendment to " the eccentric biasing boat inclination, righting of rising and falling up and down " of emergency landing aircraft, Water mist gas injection is used to 400 tons heavy or more aircraft landing, it is with high safety to block warship control, and to jet runway Gas source constitutes reliable, safety manipulation under reasonable protection, utilization and recycling effect.Such as Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, figure 16, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Figure 50, Figure 75, Figure 76, figure 91, shown in Figure 93, Figure 96, Figure 98, Figure 99, Figure 100, Figure 101, Figure 102 and Figure 103.

It is described to be slided with efficient short distance or the dedicated jet runway of VTOL aircraft is in type aircraft carrier deck, naval vessel, land and water platform Device on jet runway includes：The jet runway valve body plate main body module sub-unit 73, with rotary shaft flute profile mouth or circle Hole axle outer shaft head end card slot 113, if mounted in type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, continental rise airport jet On runway, on continental rise sky body panel jet runway, land and water fix or mobile independent air bags platform jet runway on and naval vessel On ship side left and right sides or stern end position extension type air bag platform jet runway, one may make up by rotary shaft flute profile mouth or circle The structure jet runway of two kinds of shape hole jet port formula.As Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 16, Figure 17, Figure 18, Figure 26, Figure 31, Figure 32, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Figure 80, Figure 81, Figure 82, Shown in Figure 83, Figure 84, Figure 85, Figure 86, Figure 87, Figure 88, Figure 89, Figure 90 and Figure 103.

A variety of gas supply gas sources of the use, the gas laminar flow short distance formed by the gas injection of compressed air are slided or vertically The structure of the dedicated jet runway of landing aircraft, each region valve body plate main body module includes：Runway valve body plate main body module point is total At 73, in the shape chamber heart of 73 lower portion inside casing of runway valve body plate main body module sub-unit, it is equipped with runway valve body plate main body Module installs electromagnet cut off valve or gas control jet air storage chamber phase through slot room 74；In the installation electromagnetism cut-off of runway valve body plate main body module Outside valve or gas control jet air storage chamber phase through slot room 74, it is respectively equipped with runway valve body plate main body module air inlet pipe installation room transverse sealing End cap inner panel 92；Runway pavement panel 85；Under runway valve body plate main body module sub-unit 73, it is equipped with runway valve body plate main body mould Block lower plate pedestal 86；On runway valve body plate main body module lower plate pedestal 86, it is equipped with runway valve body plate main body module I-shaped Support rib stand 87；It is installed in electromagnet cut off valve or gas control jet air storage chamber phase through slot room 74 in runway valve body plate main body module, Equipped with universal globe injector head or inside and outside rotary sleeve sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or pneumatic tune Control whiff pressure graduated release valve sub-unit 137；In universal globe injector head or inside and outside rotary sleeve sleeve flute profile mouth or circle hole shape mouth On each region electromagnet cut off valve or pneumatic regulation whiff pressure graduated release valve sub-unit 137, it is equipped with the guiding spray of universal globe injector head Gas appendix single sleeve 136；With compressed air gas source blowing mouth or the quick plug receptacle seat 139 of hose connector and interior main confession Each gas transmission of gas source stores deflation bucket interface bore 140.The above constitutes extraneous input gas source to spraying in whole jet runway The gas supply of gas source needed for the normal and safe landing aircraft of gas source controls.As Fig. 1 a, Fig. 1 b, Fig. 1 c, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6, Fig. 7, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Figure 57, Figure 75, Shown in Figure 76, Figure 77, Figure 99, Figure 101 and Figure 102.

It is described Pneumatic extension and hydraulic cylinder flexible control mechanism installation room maintenance blind patch 89 under, pushed equipped with Pneumatic extension Oil cylinder 75；It is pushed on oil cylinder 75 in Pneumatic extension, pushes the flexible interlocking lever 76 of hydraulic cylinder equipped with Pneumatic extension；Flexible interlocking lever Arm connecting plate 77 is oriented to each control rotary axle valve；And fixed pin shaft above and below flexible interlocking lever and each guiding arm connecting plate And pin card dottle pin 78.The above constitutes the safety control that entirety jet runway is pneumatically mixed with the dynamic cylinder of oil, quickly, flexibly braked Mechanism processed.As shown in Fig. 1 a, Fig. 4, Fig. 5, Figure 14, Figure 15 and Figure 100.

It is described outside rotary shaft sleeve on swing arm fixing groove handle seat 79, to be equipped with outer rotary shaft set sleeve inside and outside compressed air and pitch library Outer swing arm and fixing bolt 80；The lower end of swing arm and fixing bolt 80 outside outer rotary sleeve sleeve fork library, is equipped with inward turning Turn swing arm and fixing bolt 81 outside bushing sleeves fork library；Swing arm and fixing bolt 81 outside interior rotary sleeve sleeve fork library Under, it is equipped with and is oriented to lateral pressure swivel bearing 138 inside and outside active support plate swing linking arm or rotary sleeve sleeve.The above institute It states, the whole jet runway of composition pneumatically pushes oil cylinder Hybrid connections part can be according to the flexible more flexible swing of dynamic of oil cylinder, guiding It need to reliably be braked at position to each freely.As Fig. 1 a, Fig. 1, Fig. 4, Fig. 5, Figure 14, Figure 49, Figure 53, Figure 54, Figure 91, Figure 95, Shown in Figure 97, Figure 98, Figure 99 and Figure 103.

It is described to be pushed on rack gear or connection gib block 82 in interior outer rotary shaft set sleeve, it is equipped with flexible interlocking lever and each control shaft valve It is oriented to arm connecting plate 77；Fixed pin shaft and pin card dottle pin 78 above and below flexible interlocking lever and each guiding arm connecting plate；Interior rotation Bushing sleeves pitch swing arm and fixing bolt 81 outside library；And the active support plate of guiding is swung in linking arm or rotary sleeve sleeve Outer lateral pressure swivel bearing 138；It is connected and fixed on seat 83 in master cylinder, is connected and fixed hinged shaft 84 equipped with master cylinder and pneumatically stretches Contracting pushes oil cylinder 75.The above constitutes the flexible connection swing of each control unit of whole jet runway, sliding close of shaft is realized In high precision, the stability of safe manoeuvring and service life.Such as Fig. 1 a, Fig. 1, Fig. 4, Fig. 5, Figure 14, Figure 15, Figure 49, Figure 53, figure 54, shown in Figure 91, Figure 95, Figure 97, Figure 98, Figure 99, Figure 100 and Figure 103.

It is described on valve body plate main body module sub-unit 73, be equipped with runway pavement panel 85；Runway longitudinally sprays 50-400 mesh intelligence It can hydraulic spray nozzle 72；It is formed by each region after multiple valve body plate main body module sub-units 73 are connected, is respectively equipped with race The longitudinal multiple air curtain puff prots 60 in the left inside China and foreign countries in road；It is corrected with universal globe shell type 180-360 degree angle rotary oscillating type puff prot Takeoff and landing " inclination of the yaw biasing heart, righting of rising and falling up and down " 70.Constituting amendment takeoff and landing on whole jet runway, " yaw adds Bias inclination, righting of rising and falling up and down " puff prot can control the amendment that obtains of aircraft trace constantly with adjustment.As Fig. 1 a, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6, Fig. 7, Fig. 8, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, figure 48, shown in Figure 49, Figure 50, Figure 75, Figure 76, Figure 101 and Figure 102.

It is described on valve body plate main body module sub-unit 73, be respectively equipped with Pneumatic extension and hydraulic cylinder flexible control mechanism and install It repairs blind patch and overlaps mouth 90 in room；Runway valve body plate main body module lower plate pedestal 86；It goes to the bottom in runway valve body plate main body module On board bottom seat 86, it is equipped with runway valve body plate main body module installation electromagnet cut off valve or gas control jet air storage chamber phase through slot room 74；It runs Road valve body plate main body module I-shaped support rib stand 87；Subject runway module air inlet air storage chamber transverse sealing end cap fixes spiral shell up and down Hole 91；On subject runway module air inlet pipe installation room transverse sealing end cap inner panel 92, it is respectively equipped with Normal Take-Off And Landing and stores defeated put Gas bucket connecting tube 10；Landing of meeting an urgent need stores defeated deflation bucket connecting tube 11；Spare landing stores defeated deflation bucket connecting tube 12；Interior main confession Each gas transmission of gas source stores deflation bucket interface bore 140.The air distribution system gas transmission for constituting whole jet runway is unimpeded, sealing is fixed and The control of support performance.Such as Fig. 1 a, Fig. 1 b, Fig. 1 c, Fig. 2, Fig. 3, Fig. 4, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, figure 44, shown in Figure 45, Figure 46, Figure 47, Figure 48 and Figure 49.

It is described on jet runway valve body plate main body module I-shaped support rib stand 87, be equipped with subject runway module air inlet pipe install Room transverse sealing end cap inner panel 92；Fixing threaded hole 91 above and below subject runway module air inlet air storage chamber transverse sealing end cap；With it is pneumatic It is flexible to push hydraulic cylinder flexible control mechanism installation room 88.It is tieed up in Pneumatic extension and hydraulic cylinder flexible control mechanism installation room It repairs in blind patch 89, pushes oil cylinder 75 equipped with Pneumatic extension, the Pneumatic extension for constituting whole jet runway quickly pushes hydraulic oil The more stable control effect of cylinder flexible control mechanism.As Fig. 1 a, Fig. 1 b, Fig. 1 c, Fig. 4, Figure 14, Figure 15, Figure 40, Figure 41, Figure 42, Shown in Figure 43, Figure 44, Figure 45, Figure 46, Figure 47 and Figure 100.

It is described on Pneumatic extension and hydraulic cylinder flexible control mechanism installation room maintenance blind patch overlap joint mouth 90, equipped with pneumatically stretching Contracting repairs blind patch 89 with hydraulic cylinder flexible control mechanism installation room；It is horizontal in runway valve body plate main body module air inlet pipe installation room To on end cover inner panel 92, it is respectively equipped with Normal Take-Off And Landing and stores defeated deflation bucket connecting tube 10；Landing of meeting an urgent need stores defeated deflation bucket Connecting tube 11；Spare landing stores defeated deflation bucket connecting tube 12；Interior each gas transmission of main air supply source stores deflation bucket interface bore 140； Compressed air gas source blowing mouth or the quick plug receptacle seat 139 of hose connector；And subject runway module air inlet air storage chamber is laterally close Sealing end covers lower fixing threaded hole 91, and so that the air distribution system of whole jet runway is pushed flexible become of hydraulic cylinder with Pneumatic extension makes With convenient installation and maintenance operating control mechanism.Such as Fig. 1 a, Fig. 1 b, Fig. 1 c, Fig. 2, Fig. 3, Fig. 4, Figure 33, Figure 40, Figure 41, figure 42, shown in Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 49, Figure 75, Figure 76, Figure 77, Figure 99, Figure 101 and Figure 102.

It is described to be rotated on solid shaft or hollow shaft sleeve 96 in 0-180 degree angle injection flute profile mouth, it is equipped with inner rotary shaft and covers flute profile Puff prot 97；It is rotated in solid shaft 98 in 0-180 degree angle injection circle hole shape mouth, is equipped with interior rotation solid shaft or hollow axle sleeve Circle hole shape puff prot 99.The above constitutes each jet port air-flow of whole jet runway, by shaft and axle sleeve clearance seal The Internal control structure of algnment accuracy cooperates adjustment.As Fig. 9, Figure 16, Figure 17, Figure 18, Figure 26, Figure 27, Figure 28, Figure 29, Figure 30, Shown in Figure 31, Figure 91, Figure 93, Figure 96, Figure 98, Figure 99, Figure 100 and Figure 103.

30 degree of dead angle jet ports in 30-90 degree fixed angle rotate on solid shaft or hollow shaft sleeve 100, in 30-90 It spends in the 40 degree of dead angle jet ports rotation solid shaft or hollow shaft sleeve 101 of fixed angle, at 50 degree of 30-90 degree fixed angle Dead angle jet port rotates on solid shaft or hollow shaft sleeve 102, in 60 degree of dead angle jet ports rotation reality of 30-90 degree fixed angle On mandrel or hollow shaft sleeve 103, in the 70 degree of dead angle jet ports rotation solid shaft or hollow axle sleeve of 30-90 degree fixed angle Cylinder 104 on, 30-90 degree fixed angle 80 degree dead angle jet ports rotation solid shaft or hollow shaft sleeve 105 on, Yi Ji In the 90 degree of dead angle jet ports rotation solid shaft or hollow shaft sleeve 106 of 30-90 degree fixed angle, whole jet runway is constituted Internal spray mouth, the standard controllability of rotary shaft axle sleeve clearance seal and gas storage cell structure.As Figure 19, Figure 20, Figure 21, Figure 22, Shown in Figure 23, Figure 24 and Figure 25.

It is described to be rotated on solid shaft or hollow shaft sleeve 96 in 0-180 degree angle injection flute profile mouth, it is equipped with rotation axis seal packing Mounting groove 107；On rotation axis seal packing mounting groove 107, it is equipped with rotation axis seal packing 108；In rotary shaft flute profile mouth or On round hole axle internal axle sleeve fixing seat mouth 109, it is respectively equipped with rotary shaft flute profile mouth or round hole axle internal axle sleeve or upper and lower gas transmission room Seal FE Tiler 110；With rotary shaft flute profile mouth or round hole axle exterior and interior axle sleeves or FE Tiler cage bolt hole 95.Constitute whole jet Jet port rotary shaft inside runway, to the reliability of gas supply gas source sealing structure and accurate closing gas source.Such as Fig. 1 a, Fig. 4, figure 5, Fig. 9, Figure 14, Figure 16, Figure 30, Figure 31, Figure 33, Figure 34, Figure 35, Figure 36, Figure 37, Figure 38, Figure 39, Figure 40, Figure 41, Figure 42, Shown in Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 91, Figure 93, Figure 96, Figure 98, Figure 99, Figure 100 and Figure 103.

It is described on rotary shaft flute profile mouth or round hole axle exterior and interior axle sleeves fixing seat 94, be respectively equipped with rotary shaft flute profile mouth or circle Hole axle outer shaft sleeve 93；With rotary shaft flute profile mouth or round hole axle exterior and interior axle sleeves or FE Tiler cage bolt hole 95；It is rotating On axial trough shape mouth or round hole axle outer shaft head end card slot 113, it is respectively equipped with rotary shaft flute profile mouth or round hole axle unofficial biography dynamic crankshaft Swing angle axis 111；D-axis swing angle axis 112 is moved with rotary shaft flute profile mouth or round hole axle unofficial biography.Composition is connected transmission Flexibly, easy to assembly, use safe and reliable rotary sleeve flute profile mouth or outstanding shaft set circle hole shape mouth structure jet runway. Such as Fig. 1 a, Fig. 4, Fig. 5, Fig. 9, Figure 10, Figure 11, Figure 12, Figure 13, Figure 14, Figure 16, Figure 17, Figure 18, Figure 26, Figure 31, Figure 32, figure 33, Figure 34, Figure 35, Figure 36, Figure 37, Figure 38, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 91, Figure 93, figure 96, shown in Figure 98, Figure 99, Figure 100 and Figure 103.

The efficient short distance of band slides or the dedicated jet runway of VTOL aircraft, continental rise airport, type aircraft carrier deck, naval vessel, On land and water platform jet runway valve body plate main body module sub-unit 73, it is respectively equipped with universal globe shell type gas-sparging head list sleeve Or double telescopic sub-units 114；With universal globe injector head outward flange disk seat fixing bolt 141, if mounted in type aircraft carrier deck it is carrier-borne Or on each dedicated jet runway 191 in airport, on continental rise airfield runway, on continental rise sky body panel runway, land and water fixes or mobile On independent air bags platform runway and on naval vessel ship side left and right sides or after run extension type air bag platform runway, one is constituted Universal globe shell type sprays gas runway.As Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Figure 50, Figure 52, Figure 75, Figure 76, Figure 80, Figure 81, Figure 82, Figure 83, Figure 84, Figure 85, figure 86, shown in Figure 87, Figure 88, Figure 89, Figure 90, Figure 101 and Figure 102.

A variety of gas supply gas sources of the use, the gas laminar flow short distance formed by compressed air gas injection are slided, or vertical On the dedicated jet runway valve body plate main body module sub-unit 73 of landing aircraft, it is respectively equipped with universal globe shell type gas-sparging head Single sleeve or double telescopic sub-units 114；In universal globe shell type gas-sparging head list sleeve or double telescopic sub-units 114 On, it is equipped with outside universal globe injector head and positions fixing seat 116；Universal globe shell type injector head flange seat 115；Universal globe injection Head guiding jet appendix single sleeve 136；And universal globe injector head or inside and outside rotary sleeve sleeve flute profile mouth or circular hole Each region electromagnet cut off valve of shape mouth or pneumatic regulation whiff pressure graduated release valve sub-unit 137.Constitute universal globe injector head guiding Flexible variation and positioning with driving jet angle are fixed, the supportive of various point locations and each jet port rotary oscillating type are sprayed The flexible controlling of port.As Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Shown in Figure 47, Figure 48, Figure 49, Figure 50, Figure 51, Figure 52, Figure 57, Figure 75, Figure 76, Figure 101 and Figure 102.

It is described on jet runway valve body plate main body module sub-unit 73, it is solid to be respectively equipped with universal globe injector head outward flange disk seat Determine bolt 141；Longitudinal motor or the fixed bracket 121 of pneumatic linear actuator；And universal globe injector head guiding leading screw or guiding pneumatically control Thick stick fixed plate 126 processed.Universal globe injector head guiding and driving are constituted, the flexible variation of jet angle and positioning can be made fixed each The supportive of point position.Such as Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, figure 47, shown in Figure 48, Figure 49, Figure 50, Figure 75, Figure 76, Figure 101 and Figure 102.

It is described to be positioned in fixing seat 116 outside universal globe injector head, it is respectively equipped with universal globe injector head rotary oscillation spherical surface Block set fixes inner shield ring 117；Universal globe jet port spinning ball swings spherical surface and covers fixing seat 118；And universal globe injection Mouth rotary oscillation spherical surface body 119.Constitute universal globe shell type rotary oscillation 0-180 degree or 360 degree can intellectual any adjustment Angle constitutes the connection control of the fixation position of injection gas sub-unit entirety.Such as Figure 49, Figure 51, Figure 55, Figure 56, Figure 57, figure 58, shown in Figure 59, Figure 60, Figure 75, Figure 76, Figure 101 and Figure 102.

It is described in universal globe jet port rotary oscillation spherical surface body 119, be respectively equipped with universal globe shell type injector head flange seat 115；Universal globe injector head is oriented to jet appendix single sleeve 136；And universal globe injector head or inside and outside rotary sleeve Sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or pneumatic regulation whiff pressure graduated release valve sub-unit 137.Constitute ten thousand To spherical sleeve type rotary oscillation 0-180 degree or 360 degree can intellectual angle-adjustable, realize injection gas sub-unit integrally gas The security control of source control system.Such as Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, figure 49, shown in Figure 50, Figure 51, Figure 52, Figure 57, Figure 58, Figure 75, Figure 76, Figure 101 and Figure 102.

It is described to be positioned in fixing seat 116 outside universal globe injector head, it is respectively equipped with longitudinal motor or the fixed bracket of pneumatic linear actuator 121；Lateral driving lever transmission motor or the transmission of Pneumatic extension cylinder push driving lever 122；And longitudinal motor or pneumatic linear actuator control 123； Constitute universal globe shell type rotary oscillation 0-180 degree or 360 degree can intellectual angle-adjustable, with the pendulum for spraying gas Dynamic and transmission mechanism, the controllable lateral angles of composition are more flexibly stirred and oscillatory.As Figure 48, Figure 49, Figure 50, Figure 51, Shown in Figure 75, Figure 76, Figure 101 and Figure 102.

Described to control on 123 in longitudinal motor or pneumatic linear actuator, longitudinal stir can arbitrarily be adjusted by being respectively equipped with universal globe 0-360 degree Gear or the flexible transmission handspike 120 of pneumatic control；With universal globe injector head guiding leading screw worm gear pairs or guiding Air Valve Control group 127.Constitute universal globe shell type rotary oscillation 0-180 degree or 360 degree can intellectual angle-adjustable, and spraying gas In the swinging transmission mechanism control of sub-unit entirety, realize that artificial intelligence switching manipulation turns to accurate, the flexibility of spray angle. As shown in Figure 48, Figure 49 and Figure 50.

It is described to be positioned in fixing seat 116 outside universal globe injector head, it is respectively equipped with universal globe injection headstock gasket 124； Universal globe injector head locknut 125；And universal globe injector head guiding leading screw or guiding pneumatic control thick stick fixed plate 126.Structure At each angle that intellectual can arbitrarily adjust of universal globe shell type rotary oscillation 0-180 degree or 360 degree, injection gas point is constituted Total integral fixation support and control.As shown in Figure 49, Figure 51, Figure 61, Figure 62, Figure 75, Figure 76, Figure 101 and Figure 102.

It is described universal globe injector head guiding leading screw or guiding pneumatic control thick stick fixed plate 126 on, be respectively equipped with universal globe Injector head guiding leading screw worm gear pairs or guiding Air Valve Control group 127；Universal globe injector head guiding leading screw or guiding Air Valve Control Flexible thick stick 128；Universal globe injector head guiding locking screw 129；Universal globe injector head is oriented to active support plate and swings connection Arm pin shaft and plum blossom latch card 134；Universal globe injector head is oriented to active support plate and swings linking arm 130；Universal globe injection Head is oriented to active support plate and swings linking arm sliding pin 131；Universal globe injector head is oriented to active support plate and swings linking arm Adjust upper arm reinforcing rib 132；And universal globe injector head is oriented to active support plate and swings linking arm pin hole 133.Constitute ten thousand To spherical sleeve type rotary oscillation 0-180 degree or 360 degree can intellectual angle-adjustable, it is whole to form injection gas sub-unit Fixation, support and control, and transmission, guiding and weave control.As Figure 48, Figure 49, Figure 50, Figure 65, Figure 66, Figure 67, Figure 68, Shown in Figure 69, Figure 70, Figure 71, Figure 72, Figure 73 and Figure 74.

It is described to be oriented in jet appendix single sleeve 136 in universal globe injector head, it is respectively equipped with universal globe injector head and leads Linking arm driving lever support base 135 is swung to active support plate；Universal globe injector head or inside and outside rotary sleeve sleeve flute profile mouth or Each region electromagnet cut off valve of circle hole shape mouth or pneumatic regulation whiff pressure graduated release valve sub-unit 137；Universal globe injector head guiding Active support plate swings linking arm pin hole 133；Universal globe injector head is oriented to active support plate and swings linking arm adjustment upper arm Reinforcing rib 132；Universal globe injector head is oriented to active support plate and swings linking arm sliding pin 131；Universal globe injector head is led Linking arm 130 is swung to active support plate；And universal globe injector head is oriented to active support plate and swings linking arm pin shaft and plum Flower latch card 134.The extraneous input gas source of composition controls the normal safe landing that gas source is sprayed in jet runway, and formation pair Universal globe injector head is oriented to the connectivity of active support plate flexible swinging.As Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 49, Figure 56, Figure 57, Figure 63, Figure 64, Figure 65, Figure 66, Figure 69, Figure 70, Figure 71, Figure 72, Tu73He Shown in Figure 74.

It is described that the both ends that active support plate swings linking arm 130 are oriented in universal globe injector head, it is respectively equipped with the active branch of guiding Fagging swings lateral pressure swivel bearing 138 inside and outside linking arm or rotary sleeve sleeve；Connection is swung being oriented to active support plate Inside and outside arm or rotary sleeve sleeve in lateral pressure swivel bearing 138, it is equipped with universal globe injector head and is oriented to active support plate pendulum Dynamic linking arm pin shaft and plum blossom latch card 134.The above constitutes universal globe shell type rotary oscillation 0-180 degree or 360 degree Can intellectual angle-adjustable, form the whole fixed support of injection gas sub-unit and the flexibility of guiding movement control. As shown in Figure 49, Figure 53, Figure 54, Figure 65, Figure 66, Figure 69, Figure 70, Figure 91, Figure 95, Figure 97, Figure 98, Figure 99 and Figure 103.

It is described on jet runway valve body plate main body module sub-unit 73, be equipped with universal globe injector head outside position fixing seat 116； It is positioned in fixing seat 116 outside universal globe injector head, is equipped with universal globe injector head outward flange disk seat fixing bolt 141.Structure At universal globe shell type rotary oscillation 0-180 degree or 360 degree can intellectual angle-adjustable, composition sprays gas to it The maintenance dismounting of sub-unit entirety and fixed supportive control.As Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Figure 50, Figure 51, Figure 75, Figure 76, shown in Figure 101 Figure 102.

It is described in universal globe injector head or inside and outside rotary sleeve sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or On pneumatic regulation whiff pressure graduated release valve sub-unit 137, it is respectively equipped with universal globe injector head guiding jet appendix list sleeve Formula 136；Compressed air gas source blowing mouth or the quick plug receptacle seat 139 of hose connector；And main each gas transmission storage of air supply source in runway Store gas bucket interface bore 140.Constitute support of the extraneous input gas source to the normal safe landing for spraying gas source in jet runway Property control.Such as Fig. 1 b, Fig. 4, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 49, Figure 57, figure 75, shown in Figure 76, Figure 77, Figure 99, Figure 101 and Figure 102.

It is described that multiple conveying gas source Quick connector plugs 142, storage deflation bucket appendix in more are equipped in jet runway 143, multiple interior normal storage deflation bucket check valves 144 and multiple interior emergency store deflation bucket check valve 145.Constitute control The switching of the system of each general gas source and individual gas sources.It, still can Normal Take-Off And Landing even if break down.Such as Figure 75, Figure 76 and figure Shown in 77.

It is described on universal globe shell type gas-sparging head list sleeve or double telescopic sub-units 114, be equipped with universal globe spray It collaborates under turnbarrel in the double sleeves of head pressure locking block set 209；It is gone here and there under turnbarrel in the double sleeves of universal globe injector head In atmospheric pressure locking block set 209, it is respectively equipped with turnbarrel waterproof and dustproof, antifreeze oil sealing in the double sleeves of universal globe injector head Or packing 208；It collaborates downwards pressure buffer bearing 211 with turnbarrel in the double sleeves of universal globe injector head；In universal globe It collaborates outside pressure locking block set 209, is equipped with fixed outside the double sleeves of universal globe injector head under turnbarrel in the double sleeves of injector head Buffing pad 210 on turnbarrel in sleeve；The buffing pad on turnbarrel in the double sleeve fixed sleeves cylinders of universal globe injector head Outside 210, it is equipped with universal globe jet port rotary oscillation spherical surface body 119；In universal globe jet port rotary oscillation spherical surface body 119 Outside, it is equipped with outside universal globe injector head and positions fixing seat 116.Constitute the fixed interior rotary sleeve of the double bush outer sleeves of universal globe injector head Cylinder flexible rotation and 360 degree of swings and dust-proof, anti-water management；Such as Figure 48, Figure 49, Figure 50, Figure 51, Figure 52, Figure 57, Figure 58, figure 75, shown in Figure 76, Figure 101 and Figure 102.

It is described on universal globe shell type gas-sparging head list sleeve or double telescopic sub-units 114, be respectively equipped with universal globe The double sleeve fixed sleeves cylinders 212 of injector head；With single sealing gland or the packing of collaborating on the double sleeve inside and outside sleeves of universal globe injector head 213；With slot 214 in the defeated deflation of turnbarrel in universal globe injector head；And the double sleeve inner-outer sleeves of universal globe injector head It collaborates single sealing gland or packing 215 at cylinder middle part.Constitute in universal globe injector head turnbarrel flexible rotation and fixed sleeves cylinder it Between leakproofness control；As shown in Figure 48, Figure 49, Figure 50, Figure 52, Figure 75, Figure 76, Figure 101 and Figure 102.

It is described on universal globe shell type gas-sparging head list sleeve or double telescopic sub-units 114, be respectively equipped with universal globe The double sleeve fixed sleeves cylinders of injector head gas transmission air inlet 217 open in usual；Again in the double sleeve fixed sleeves cylinders of universal globe injector head In gas transmission air inlet 217 open in usual, it is equipped with turnbarrel 225 in the double sleeves of universal globe injector head；In universal globe injector head In double sleeves on turnbarrel 225, air inlet blowing mouth 216 in turnbarrel is equipped in the double sleeves of universal globe injector head；And It collaborates under the double sleeve inside and outside sleeve cylinders of universal globe injector head double sealing glands or packing 218.Constitute the normal injection in defeated ventilation source with The normal flexible effective control opened with the normal leakproofness for closing gas source and gas source of gas source；As Figure 48, Figure 49, Figure 50, Shown in Figure 52, Figure 75, Figure 76, Figure 101 and Figure 102.

It is described on turnbarrel 225, to be equipped with rotation in the double sleeves of universal globe injector head in the double sleeves of universal globe injector head Sleeve collaborate upwards compressive resistance buffering bearing 219；It collaborates upwards anti-pressure with turnbarrel in the double sleeves of universal globe injector head Lock flange mother 220；With turnbarrel locking screw tooth 221 in the double sleeves of universal globe injector head；And universal globe injector head is double Turnbarrel swing arm fixing bolt 224 in sleeve；With turnbarrel swing arm 223 in the double sleeves of universal globe injector head；With ten thousand Into spherical surface injector head double sleeves, turnbarrel swing arm pushes and pulls bulb 222.Turnbarrel and fixed sleeves cylinder rotate in constituting Flexible swing angle is accurate, reliable；As shown in Figure 101 and Figure 102.

It is described on the double sleeve fixed sleeves cylinders of universal globe injector head gas transmission air inlet 217 open in usual, be equipped with each valve body template die Soft or hard snorkel is coupled quick combination hub 169 in block；The defeated soft or hard coupling connecting tube 157 of deflating of nominal gas jet port in runway； With can 360 degree rotation swing connecting bend 162；And nominal gas jet port electromagnet cut off valve switch 151 in runway.It constitutes defeated The input of normal opening and closing in ventilation source.As shown in Figure 75, Figure 76, Figure 98, Figure 99, Figure 101 and Figure 102.

It is described multiple normal storage deflation buckets 146 are equipped in jet runway, multiple emergency store deflation bucket 147, in runway Freeze, regard the interior emergency storage deflation bucket of air gauge 148, runway in heating sensing modulator 207, runway outside normal storage deflation bucket Normal injection gas pressure regulation stop valve 150 in outer view air gauge 149, runway, nominal gas jet port electromagnetism cut-off in runway The interior emergency gas ejection ports electromagnet cut off valve of emergency jet port gas pressure regulation shut-off valve 152, runway is opened in threshold switch 151, runway It closes in 153 and runway and normally switches electromagnet cut off valve switch 154 with gas source in emergency storage deflation bucket, to guarantee each gas supply The normal control of gas source.As shown in Figure 75, Figure 76, Figure 77, Figure 98, Figure 99, Figure 101 and Figure 102.

It is described be equipped in jet runway multiple groups normally with emergency storage deflation bucket current collecting tier gas supply check valve 155, in runway just Often connected with the defeated soft or hard coupling of deflating of nominal gas jet port in the compressor gas supplied check valve 156 of emergency storage deflation bucket, runway Normal storage deflation bucket is mutually ventilated in the defeated soft or hard coupling connecting tube 158 of deflating of gas ejection ports of meeting an urgent need in pipe 157, runway, runway Emergency storage deflation bucket is mutually ventilated soft or hard coupling connecting tube 160 in soft or hard coupling connecting tube 159 and runway, and composition can be safe Guarantee the normal gas supply control of gas source.As shown in Figure 75, Figure 76, Figure 98, Figure 99, Figure 101 and Figure 102.

It is described that multiple gas pressure regulation shut-off valves and electromagnet cut off valve switch connection outside screw 161 are equipped in jet runway；It can be 360 degree Rotary oscillation connecting bend 162；And the lateral defeated snorkel 163 of nominal gas jet port Universal-head in runway；It is answered in runway Anxious gas ejection ports Universal-head laterally on defeated snorkel 164, is respectively equipped with refrigeration, heating sensing modulator 207；It is normal in runway Fork sliding sleeve 165 is stirred in the swing of gas ejection ports transverse pipe；Fork sliding sleeve is stirred in the swing of emergency gas ejection ports transverse pipe in runway 166；And the normal control of mechanical linkage and road face temperature is constituted normally with emergency transverse pipe sealing-plug stifled 167 in runway.Such as Shown in Figure 75, Figure 76, Figure 98, Figure 99, Figure 101 and Figure 102.

In jet runway normally with meet an urgent need and storage deflation bucket electromagnet cut off valve interval freewheeling diode 168, each valve body plate module Interior soft or hard snorkel is coupled quick combination hub 169, normally stirs fork 170 in runway with emergency transverse pipe swing, is normal in runway It is stirred in fork connection locking plate 171 and runway with emergency transverse pipe swing and normally stirs fork locking with emergency transverse pipe swing Plate and handspike fixing bolt 172, constitute each air supply system on demand by the accurate regulation in freewheeling diode intellectual moment, And each spout angle is made to guarantee accurate, flexible weave control.Such as Figure 75, Figure 76, Figure 98, Figure 99, Figure 101 and Figure 102 institute Show.

It is described in the lower part shape chamber of 73 inner frame structure of jet runway valve body plate main body module sub-unit, be respectively equipped with interior normal The automatically controlled travel switch 177 of jet port advance stop artificial intelligence formula；Interior normal injection mouth retreats the automatically controlled row of stop artificial intelligence formula Cheng Kaiguan 178；The automatically controlled travel switch 179 of interior emergency jet port advance stop artificial intelligence formula；Interior emergency jet port retreats stop The automatically controlled travel switch 180 of artificial intelligence formula constitutes the automatically controlled control of signal.As Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Shown in Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49 and Figure 76.

When normal injection mouth in the automatically controlled travel switch 177 of normal injection mouth advance stop artificial intelligence formula in jet runway, runway Retreat the interior automatically controlled stroke of jet port advance stop artificial intelligence formula of meeting an urgent need of the automatically controlled travel switch 178 of stop artificial intelligence formula, runway Emergency jet port retreats the automatically controlled travel switch 180 of stop artificial intelligence formula in switch 179 and runway, when a certain signal is out of control, The mechanically automatically controlled travel switch 173 of normal injection mouth advance stop in jet runway, normal injection mouth retreats stop machine in runway It is met an urgent need in the mechanically automatically controlled travel switch 175 of jet port advance stop and runway in the automatically controlled travel switch 174 of tool formula, runway Jet port of meeting an urgent need retreats the mechanically automatically controlled travel switch 176 of stop, plays the role of dual fail-safe control.Such as Figure 76 and Figure 100 institute Show.

It is described in frame bottom shape chamber, to be respectively equipped in jet runway just in jet runway valve body plate main body module sub-unit 73 Normal jet port advances and retreats artificial intelligence formula angle sensor controller 181；Emergency jet port advances artificial with retrogressing in runway Intellectual angle sensor controller 182；Normal servo motor impeller-hub feed rod connects locking transition plates 183 in runway；In runway Servo motor impeller-hub feed rod of meeting an urgent need connects locking transition plates 184；Normal servo motor or promotion oil cylinder 185 in runway；Runway Interior emergency servo motor pushes oil cylinder 186；In runway normally with emergency impeller-hub feed rod 187；In runway normally with answer hitch Moving axis feed rod guiding axis sliding sleeve 188.Its optimum efficiency can normal each jet port of artificial intelligence control ejected it is various needed for Timing, level pressure, quantitative gas needed for precise angle, 100% safe landing is reached to landing aircraft.Such as Fig. 1 a, Fig. 2, figure 3, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Figure 76 and Figure 100 institute Show.

The shape chamber in 73 inside casing of jet runway valve body plate main body module sub-unit, interior lower outer portion jet runway pavement lower part In the melt pit on basis, be respectively equipped with normally with emergency and spare three sets independent manuals intelligence and can the confession that switches of mutual numerical control The non-control system and runway auxiliary equipment of gas system, power supply system, the various safety operation control systems of flight control system and safety Compressor air accumulator air supply system 189 goes to the spare gas storage cylinder air supply system 190 of interior current collecting tier, in the spare gas storage of current collecting tier On steel cylinder air supply system 190, it is equipped with refrigeration, heating sensing modulator 207, low pressure colored gas and the preheating main gas ejection ports of oxygen 226.It acts on the Normal Take-Off And Landing that can guarantee on runway, which, which can be used as, flies school to check and accept the various of various type aircrafts Pneumatic dynamic and the pneumatic static state of various actual measurements are surveyed, is that the optimal detection school in the field flies to equip line, can reach 100% Accurately actual measurement go out；By itself can be produced in jet runway it is a variety of can be to extraneous landing aircraft environment runway Covered face of Smooth Slide Above, it can release various one hundred point avenge, ice making, make than the manufacture oxygenation of different proportion, manufacture anoxic, refrigeration, heating, making drugs into frostlike powder, system The functions such as rain, the various random wind for manufacturing cyclone, manufacture flow-disturbing wind, the aircraft model performance technologies that can be dispatched from the factory to various coming of new The winged test in landing school of the standard parameter on jet runway and detection are checked and accepted.As Fig. 1 a, Fig. 2, Fig. 9, Figure 33, Figure 40, Figure 41, Shown in Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Figure 75 and Figure 76.

In the shape chamber of the frame bottom in jet runway valve body plate main body module sub-unit 73, it is equipped with external right side gas in runway The curtain intellectual air control switch 227 of normal injection gas solenoid valve；And the external right side air curtain normal injection gas solenoid valve in runway On intellectual air control switch 227, it is equipped with the intellectual Regulation Control valve 228 of external right side air curtain normal injection gas in runway；Simultaneously It is additionally provided with external right side air curtain emergency injection gas solenoid valve air control switch 229 in runway；And external right side air curtain is met an urgent need in runway It sprays on gas solenoid valve air control switch 229, is equipped with the external right side air curtain emergency injection intellectual Regulation Control valve of gas in runway 230；In runway external right side normally with the longitudinal defeated snorkel 231 of emergency air curtain Universal-head jet port；With left and right sides gas inside and outside runway Longitudinally fork sliding sleeve 232 is stirred in defeated snorkel swing to curtain Universal-head jet port.Its maximum actual effect prevents the outer left side wind pair of runway Interference when Normal Take-Off And Landing of the landing aircraft in runway.Such as Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, figure 43, shown in Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49 and Figure 77.

In the shape chamber of the frame bottom in jet runway valve body plate main body module sub-unit 73, it is respectively equipped with inside and outside runway left The intellectual air control switch 233 of side air curtain normal injection gas solenoid valve；And the left side air curtain normal injection gas electricity inside and outside runway On the intellectual air control switch 233 of magnet valve, it is equipped with the inside and outside left side intellectual Regulation Control valve 234 of air curtain normal injection gas of runway； And it is additionally provided with the inside and outside left side air curtain emergency injection intellectual air control switch 235 of gas solenoid valve of runway；And it is left inside and outside runway On the side air curtain emergency injection intellectual air control switch 235 of gas solenoid valve, it is equipped with the inside and outside left side air curtain emergency injection gas of runway Intellectual Regulation Control valve 236；With left side inside and outside runway normally with the longitudinal defeated snorkel 237 of emergency air curtain Universal-head jet port. Its maximum actual effect is the interference for preventing runway external right side wind to landing aircraft in runway when landing.Such as Fig. 1 a, Fig. 2, figure 3, shown in Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49 and Figure 77.

In the shape chamber of the frame bottom in each piece of valve body plate main body module sub-unit 73 of jet runway, it is respectively equipped with runway Inside normally receive communication far infrared and spectrum or Beidou intelligent sensing controller 238；It is received with emergency in runway and communicates far infrared Between spectrum or Beidou intelligent sensing controller 239, the navigation of three's far and near distance can mutually switch, the scope of heading whole world Communication, the winged various flying objects of control cannot any, arbitrarily, freely rise and fall on jet runway between domestic various airports, the race Road there is intelligence software to recognize it difference various flyers after receive function naturally, and to the complete of mobile flyer Ball navigation locating function, especially to various guided missiles or commit suiside unmanned plane or have it is man-machine attack, which can be each by it The flyers such as kind unacquainted various unmanned planes or someone's airborne missile quickly exclude to blow winged, effectively protect jet runway The great advantage of safe normal operation.As Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Shown in Figure 46, Figure 47, Figure 48, Figure 49 and Figure 77.

In the shape chamber of the frame bottom heart in jet runway valve body plate main body module sub-unit 73, it is respectively equipped in runway Outer left and right sides and the green instruction lamp driver of middle left and right sides reddish yellow input six hole power sockets 240；The right outside of coupled runway is red Yellowish green indicator light wiring conversion terminal 241；With reddish yellow green indicator light wiring conversion terminal 242 in side in the runway right side；The left side of runway The green indicator light wiring conversion terminal 243 of reddish yellow；And the green indicator light wiring conversion terminal 244 of runway left-external side reddish yellow.It is maximum Effect be can normal supply each group indicator light power supply, and it is safer to pilot eye-catching in night landing.Such as Fig. 1 a, Fig. 2, figure 3, shown in Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Figure 78 and Figure 79.

In the shape chamber of the frame bottom heart in jet runway valve body plate main body module sub-unit 73, it is being respectively equipped with runway just Often four hole power sockets 245 are inputted with emergency air curtain electromagnetic valve circuit with emergency main jet port and normally；Just with outside right in runway Often with emergency main jet port and normally with meet an urgent need each solenoid valve control connecting terminal 259 of air curtain；With in runway in the right side normally with answer Anxious each solenoid valve wiring conversion terminal 260 of main jet port；And in runway it is left normally with emergency each solenoid valve wiring of main jet port Conversion terminal 261；In runway left-external side normally with emergency main jet port and normally with meet an urgent need each solenoid valve wiring change-over terminal of air curtain Son 262.Its maximum efficiency is to guarantee that each electric-controlled parts and electronic signal can have the control of normal safety standard to it.Such as figure 1a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Tu78He Shown in Figure 79.

In the shape chamber of the lower part heart in 73 bearing wall and frame structure of jet runway valve body plate main body module sub-unit, set respectively Have in runway and normally inputs five hole power sockets 246 with emergency gas receiver solenoid valve x far-infrared spectrum x Beidou x heat tracing line；And runway Inside normally with emergency gas receiver solenoid valve x far-infrared spectrum x Beidou x heat tracing line connecting terminal 263；With in runway normally with emergency Gas receiver solenoid valve x far-infrared spectrum x Beidou x heat tracing line connecting terminal 264.Its maximum efficiency is to guarantee that gas source is led for giving The accurate and ice and snow of signal, the combustion hot weather of navigating 100% can have a good normal temperature control intelligently to adjust on runway It is whole.As Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Shown in Figure 78 and Figure 79.

It is described in the lower part shape chamber of 73 bearing wall and frame structure of jet runway valve body plate main body module sub-unit, be respectively equipped with runway The interior normal 1-2 servo motor for pushing main injection port inputs four hole power sockets 247；With normally main jet is pushed to emanate in runway Mouth No. 1 motor of front and rear angles connects on 1-2 contact wiring conversion terminal 265, for the closure electricity for controlling No. 1 servo motor Road；And it normally pushes No. 2 motors of main injection port front and rear angles to meet the 1-2-3 on 4-5 contact and connect in runway and is laid flat in deflector On wiring conversion terminal 266, for a closed circuit for controlling No. 2 servo motors.Its effect ensures the normal of each servo motor Defeated power supply.As Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Shown in Figure 49, Figure 78 and Figure 79.

It is described in the lower part shape chamber of 73 bearing wall and frame structure of jet runway valve body plate main body module sub-unit, be respectively equipped with runway Interior emergency pushes the 3-4 servo motor of main jet loophole to input four hole power sockets 248；Main jet port is pushed with emergency in runway No. 3 motors of front and rear angles connect on the wiring conversion terminal 267 of 1-2 contact, for the closure electricity for controlling No. 3 servo motors Road；It pushes No. 4 servo motors of main injection port front and rear angles to meet 1-2 point 3-4-5 with emergency in runway and connects connecing for deflector standing On line conversion terminal 278, for a closed circuit for controlling No. 4 servo motors.Its effect ensures the normal defeated of each servo motor Power supply.Such as Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 41, Figure 48, figure 49, shown in Figure 78 and Figure 79.

It is described in the lower part shape chamber of 73 bearing wall and frame structure of jet runway valve body plate main body module sub-unit, be respectively equipped with runway Interior normal main jet port front and rear angles control No. 1 servo motor and input four hole power sockets 249；Before main jet port normal in runway Angle controls No. 1 servo motor wiring conversion terminal 268 afterwards, for normal main jet port No. 1 servo of front and rear angles in control runway The closed circuit of motor signal sensor；Normal main jet port front and rear angles control No. 2 servo motors and input four holes electricity in runway Source(-)holder 256；No. 2 servo motor wiring conversion terminals 269 are controlled with main jet port front and rear angles normal in runway；It is answered in runway Anxious main jet port front and rear angles control No. 4 servo motors and input four hole power sockets 257；Emergency main jet port front and rear angles in runway Control No. 4 motor wiring conversion terminals 277；Emergency main jet port front and rear angles control No. 3 servo motors and input four holes in runway Power socket 250；No. 3 servo motor wiring conversion terminals 270 are controlled with main jet port front and rear angles of meeting an urgent need in runway.Its effect is Guarantee the normal of input power and various signal transducers.Such as Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, figure 43, shown in Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Figure 78 and Figure 79.

It is described in the lower part shape chamber of 73 bearing wall and frame structure of jet runway valve body plate main body module sub-unit, be respectively equipped with runway Interior normal close or retrogressing of advancing inputs six hole power sockets 251 close to No. 1 servo motor sensitive switch；With normally advance in runway It approaches or retreats close to No. 1 servo motor sensitive switch wiring conversion terminal 271；Close or retrogressing connects with normally advancing in runway Nearly No. 2 servo motor sensitive switches input six hole power sockets 255；It approaches or is retreated close to No. 2 servos with normally advancing in runway Motor sensitive switch wiring conversion terminal 272；And emergency is advanced close or is retreated close to No. 3 servo motor sensitive switches in runway Input six hole power sockets 252；Advance close with emergency in runway or retreats close to No. 3 servo motor sensitive switch wiring change-over terminals Son 273；Advance close with emergency in runway or retreats close to No. 4 servo motor sensitive switches six hole power sockets 254 of input；With Emergency is advanced close or is retreated close to No. 4 servo motor sensitive switch wiring conversion terminals 274 in runway.Its effect ensures respectively to watch Take the power supply and each puff prot angle of intelligent signal normal control of motor.As Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Shown in Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Figure 78 and Figure 79.

It is described in the lower part shape chamber of 73 bearing wall and frame structure of jet runway valve body plate main body module sub-unit, be respectively equipped with and connect sky Air compressor inputs four hole power sockets 253 with current collecting tier is connect；And it connects compressor and connects wiring under current collecting tier gas supply electromagnetic valve gas control Conversion terminal 275；And it connects compressor and connects wiring conversion terminal 276 on current collecting tier gas supply electromagnetic valve gas control.Its maximum efficiency is protected Demonstrate,prove the match control of the normal gentle source stream of power supply.Such as Fig. 1 a, Fig. 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, figure 44, shown in Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Figure 78 and Figure 79.

It is described in the lower part shape chamber of 73 bearing wall and frame structure of jet runway valve body plate main body module sub-unit, be respectively equipped with pre- road Deflector erects input and is laid flat six hole power sockets 258 of input with pre- road deflector；Emergency pushes main jet port front-and-back angle in runway Spend No. 4 servo motors connect 1-2 point 3-4-5 connect deflector standing wiring conversion terminal 278 on, for pre- road deflector erect One automatically controlled closed circuit；And pre- road deflector erects input and is laid flat six hole power sockets 258 of input with pre- road deflector；Connect race No. 2 servo motors of main injection port front and rear angles are normally pushed to connect on 4-5 contact in road, 1-2-3 connects to be laid flat in deflector and connect It is input and the output circuit of the automatically controlled closure that pre- road deflector is laid flat on 266 position of line conversion terminal.Such as Fig. 1 a, figure 2, Fig. 3, Fig. 9, Figure 33, Figure 40, Figure 41, Figure 42, Figure 43, Figure 44, Figure 45, Figure 46, Figure 47, Figure 48, Figure 49, Figure 78 and Figure 79 It is shown.

The efficient short distance of band slides or the dedicated jet runway of VTOL aircraft is in type aircraft carrier deck, naval vessel, land and water platform jet Device on runway includes：Runway first area to District 7 domain electromagnet cut off valve or pneumatic regulation whiff pressure alleviates valve assembly 200 to 206 and type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport.When various airport aircrafts or ship-board aircraft Warship slided when landing 140 meters long 199 into jet runway, continental rise airfield runway, continental rise sky body panel runway, land and water fix or The extension type air bag platform runway of mobile independent air bags platform runway and naval vessel ship side left and right sides or after run, Constitute landing safely and fast.Such as Fig. 3, Figure 76, Figure 80, Figure 81, Figure 82, Figure 83, Figure 84, Figure 85, Figure 86, Figure 87, Figure 88, figure Shown in 89 and Figure 90.

A variety of gas supply gas sources of the use, the gas laminar flow short distance formed by compressed air gas injection are slided, or vertical On dedicated each region of jet runway of landing aircraft, it is equipped with that type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport.In aircraft carrier Deck is carrier-borne or each dedicated jet runway 191 in airport on, be respectively equipped with it is seven 20 meters long, 140 meters of overall length × wide 15-20,30 or 40 meters of wide type aircraft carrier decks are carrier-borne or each dedicated jet runway in airport, constitute the safe falling condition of carrier-borne aircraft.Such as Figure 80, figure 81, shown in Figure 82, Figure 83, Figure 84, Figure 85, Figure 86, Figure 87, Figure 88, Figure 89 and Figure 90.

When taking off, when carrier-borne aircraft is slided into 20 meter long 192 of jet runway, the carrier-borne aircraft that takes off is slided into jet carrier-borne aircraft At 40 meter long 193 of runway, when the carrier-borne aircraft that takes off is slided into 60 meter long 194 of jet runway, the carrier-borne aircraft that takes off slides entrance At 80 meter long 195 of jet runway, at this moment, the carrier-borne aircraft that takes off is type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport On, the natural flying height of gas outstanding support when whole second-mission aircrafts for being detached from dedicated jet runway take off has been constituted, has been constituted Fly the safely and fast natural flying speed of aircraft.As Figure 80, Figure 81, Figure 82, Figure 83, Figure 84, Figure 85, Figure 86, Figure 87, Figure 88, Shown in Figure 89 and Figure 90.

Carrier-borne aircraft is when warship lands, and is first 45 degree when carrier-borne aircraft is slided into the 20-40 rice long 196 of jet runway The film grade laminar flow gas enclosure body at angle blocks landing；Warship carrier-borne aircraft when sliding into the 60-80 rice long 197 of jet runway, constituted The film grade laminar flow at second 45 degree of angle that carrier-borne aircraft blocks presss from both sides；At this moment warship carrier-borne aircraft continue to slide into jet runway At 100-120 meters long 198, the film grade laminar flow gas enclosure body for having constituted 45 degree of angles of third blocks landing；At this moment warship carrier-borne aircraft after It is continuous when sliding into 140 meter long 199 of jet runway, constitute the 4th film grade laminar flow folder that carrier-borne aircraft blocks；At this moment warship Carrier-borne aircraft type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, finally, carrier-borne aircraft or various aircrafts are in dedicated jet Nature is realized on runway, stable gas hangs support formula 100% and blocks landing.Such as Figure 80, Figure 81, Figure 82, Figure 83, Figure 84, figure 85, shown in Figure 86, Figure 87, Figure 88, Figure 89 and Figure 90.

Type aircraft carrier deck is carrier-borne or each dedicated jet runway 191 in airport on, be respectively equipped with first region electromagnet cut off valve of runway Or pneumatic regulation whiff pressure alleviates valve assembly 200, runway Two Areas electromagnet cut off valve or pneumatically regulation whiff pressure is slow It solves valve assembly 201, runway third region electromagnet cut off valve or pneumatic regulation whiff pressure and alleviates valve assembly 202, runway the 4th A region electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly 203, runway the 5th region electromagnet cut off valve or gas Dynamic regulation whiff pressure alleviates valve assembly 204, the 6th region electromagnet cut off valve of runway or pneumatic regulation whiff pressure graduated release valve The 7th region electromagnet cut off valve of assembly 205 and runway or pneumatic regulation whiff pressure alleviate valve assembly 206.For carrier-borne Seven region electromagnet cut off valve of dedicated jet runway or pneumatic regulation and air pressure, can be by the need of each region air pressure size and flow It carries out quick, the safe uniform constant pressure effect that 100% can reach to region gas source and matches regulation with artificial intelligence formula Supply and distribution.As shown in Fig. 3 and Figure 76.

Carrier-borne aircraft is adjusted to 2-3 when taking off on jet runway, by the gas source air pressure of first region entirety pressure of runway Technical atmosphere；Valve assembly 200 is alleviated by first region electromagnet cut off valve or pneumatic regulation whiff pressure, by artificial intelligence regulating It completes, the air pressure of the gas source of second region entirety is adjusted to 3-4 technical atmosphere；By Two Areas electromagnet cut off valve Or pneumatic regulation whiff pressure alleviates valve assembly 201, is completed by artificial intelligence regulating, by the gas source of third region entirety Air pressure is adjusted to 4-5 technical atmosphere；Valve assembly is alleviated by third region electromagnet cut off valve or pneumatic regulation whiff pressure 202, it is completed by artificial intelligence regulating, the air pressure of the gas source of the 4th region entirety is adjusted to 5-6 technical atmosphere；By 4th region electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly 203, are completed by artificial intelligence regulating, by the 5th The air pressure of the gas source of a region entirety is adjusted to 6-7 technical atmosphere；By the 5th region electromagnet cut off valve or pneumatic regulation Whiff pressure alleviates valve assembly 204, is completed by artificial intelligence regulating, the air pressure of the gas source of the 6th region entirety is adjusted to 7-8 technical atmosphere；Valve assembly 205 is alleviated by the 6th region electromagnet cut off valve or pneumatic regulation whiff pressure, by artificial intelligence It is adjustable completion, the air pressure of the gas source of the 7th region entirety is adjusted to 8-10 technical atmosphere；By the 7th region electricity Magnetic shut-off valve or pneumatic regulation whiff pressure alleviate valve assembly 206, are completed by artificial intelligence regulating.Finally, carrier-borne aircraft is in jet When taking off on runway, the distribution pressure of the gas source of seven region entireties on jet runway is regulated and controled by artificial intelligence.Such as Fig. 3 and Shown in Figure 76.

Carrier-borne aircraft on jet runway warship when, by the pressure of the gas source of first region entirety of jet runway, by first A region electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly 200, are completed by artificial intelligence regulating, by first area The air pressure of the gas source of domain entirety is adjusted to 8-10 technical atmosphere；By Two Areas electromagnet cut off valve or pneumatic regulation spray Atmospheric pressure alleviates valve assembly 201, is completed by artificial intelligence regulating, the air pressure of the gas source of second region entirety is adjusted to 7- 8 technical atmospheres；Third region electromagnet cut off valve or pneumatic regulation whiff pressure are alleviated into valve assembly 202, by artificial intelligence It adjusts and completes, the air pressure of the gas source of third region entirety is adjusted to 6-7 technical atmosphere；4th region electromagnetism is cut Only valve or pneumatic regulation whiff pressure alleviate valve assembly 203, are completed by artificial intelligence regulating, by the main gas of the 4th region entirety The air pressure in source is adjusted to 5-6 technical atmosphere；5th region electromagnet cut off valve or pneumatic regulation whiff pressure graduated release valve is total It at 204, is completed by artificial intelligence regulating, the air pressure of the gas source of the 5th region entirety is adjusted to 4-5 technical atmosphere；It will 6th region electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly 205, are completed by artificial intelligence regulating, by the 6th The air pressure of the gas source of a region entirety is adjusted to 3-4 technical atmosphere；By the 7th region electromagnet cut off valve or pneumatic regulation Whiff pressure alleviates valve assembly 206, is completed by artificial intelligence regulating, the air pressure of the gas source of the 7th region entirety is adjusted to 2-3 technical atmosphere.Finally, carrier-borne aircraft on jet runway warship when, to the main gas of seven region entireties on jet runway The uniform constant pressure in source can be carried out supply quickly, safe and be divided by the needs of each region air pressure size and flow to each region Regulate and control with artificial intelligence.Note：Operating condition when using 10-25 technical atmosphere on jet runway.As shown in Fig. 3 and Figure 76.

It is described before and after each puff prot in each region of jet runway, be all respectively equipped with low pressure colored gas and preheating the main gas of oxygen Body jet port 226, maximum efficiency are height and the angle of the injection ray in adjustment, each each puff prot of region high pressure of whole runway Whether degree, each puff prot by jet runway each region high pressure spray port drive low pressure good luck or fortune and preheating oxygen master in work or failure Gas jet mouth, formed to each region puff prot mixing good luck or fortune spray angle with highly formed the inspection of eye-catching formula with it is more acurrate, Judgement is directed to the debugging of each jet port.As shown in Fig. 1 a, Fig. 2.

Claims (13)

1. a kind of efficient very-short-reach of band slides or the aircraft carrier of VTOL aircraft device, naval vessel, land and water platform jet runway；Packet Included efficient very-short-reach slide or the type aircraft carrier deck jet runway or VTOL of VTOL aircraft or unmanned plane device fly Machine jet stage apparatus, and the management system to jet runway or jet stage apparatus, it is characterised in that：In the boat On female deck, on continental rise airport or various platforms can second-mission aircraft landing jet runway device, and outside each jet runway On left and right sides outside the preceding bow tail end position on side and runway, it is respectively equipped with symmetrical hidden horizontal liftable flexion-extension or hidden horizontal and road Face horizontal 0-90 degree angle, and 0-30 meters of the formula that is laid flat high lifting tubular type heavy caliber injection gas laminar flow apparatus, the liter can be erected It drops tubular type heavy caliber and sprays gas laminar flow apparatus, be that emergency when preventing landing aircraft out of control suddenly during take-off and landing safely is assisted Fly or emergency is blocked；The type aircraft carrier deck jet runway or continental rise airport and various jet runway stage apparatus and manipulation and control system System is connected；

The platform jet runway be one kind can inflation/deflation sea lifting gasbag float type jet runway stage apparatus, the jet run Stage apparatus can inversely the meet an urgent need aircraft that lands in road ejects the gas laminar flow of various different angles to block aircraft, and will Aircraft inertia force of landing is eliminated on the natural coastdown jet runway stage apparatus waterborne of lifting gasbag floating body at sea, described to fill The platform-type jet runway device of deflation lifting air utricule continental rise air bag nature coastdown is connected with management system；

The platform jet runway is slided on various naval vessels by the very-short-reach that blast injection gas blanket stream is formed to be a kind of, Or it VTOL aircraft or the dedicated jet runway stage apparatus of unmanned plane or itself moves for a kind of sea-going tug drawing type or independently Dynamic jet runway platform, slided by the short distance that blast injection gas blanket stream is formed VTOL aircraft or nobody The dedicated jet runway stage apparatus of machine is a kind of and various naval vessel Contiuum types, is formed by blast injection gas blanket stream super Short distance is slided or VTOL aircraft or the dedicated jet runway stage apparatus of unmanned plane, on the various various towboats in naval vessel If the dedicated jet runway stage apparatus of dress is connected with management system；

The platform jet runway be it is a kind of naval vessel rearward end be equipped with extension type it is waterborne can independent floating gasbag platform, or it is left On certain side at right ship side two side ends position or on each position in left and right ship side two sides, extension type is equipped with by blast injection The very-short-reach that gas blanket stream is formed slides or VTOL aircraft or the dedicated jet runway device of unmanned plane, described on naval vessel Rearward end is equipped on certain side at extension type or left and right ship side two side ends position or each position in left and right ship side two sides, is equipped with ultrashort Distance slides or VTOL aircraft or the dedicated jet runway stage apparatus of unmanned plane, the device are connected with management system It connects；

The platform jet runway is a kind of fixed offshore platform, and the very-short-reach formed by blast injection gas blanket stream is sliding Capable or VTOL aircraft or the dedicated jet runway stage apparatus of unmanned plane, the dedicated jet runway of fixed platform at sea Device, it is described in island short distance airfield runway, it is islands and reefs short distance airfield runway, oil platform short distance airfield runway, artificial Short distance airfield runway on chinampa, each frontier sentry dispense various goods and materials 5-10 ton wing type unmanned plane or unmanned helicopter, Vertical boosting landing unmanned helicopter platform is sprayed by compressed air gas, and will not be by weather misty rain, ice and snow, frost Frigid zone-low temperature that the small equal environment of geographic areas are limited in subzero 60 degree, the torrid zone-high temperature in 80 degree above freezing regional or mountain vallages, especially At sea aircraft carrier, naval vessel, land and water platform, the jet-propelled short distance of the various wing type unmanned planes on the high-altitude aerodrome of Qinghai-Tibet frigid zone are run for it Road or device to unmanned helicopter VTOL platform, the device are connected with management system；

The platform jet runway is that one kind may be provided on marine or rivers and lakes floating body platform, by blast injection gas laminar flow The very-short-reach of formation slides or VTOL aircraft or the dedicated jet runway stage apparatus of unmanned plane, it is described at sea or river Lake floating body platform-specific jet runway device is in each logistics area very short takeoff and landing runway, tourist district's very short takeoff and landing runway, each Desert mountain area very short takeoff and landing runway, Concealable cavern very short takeoff and landing runway or island, the water surface, cavern or extension airbag Formula very short takeoff and landing runway device, the device are connected with management system；

The platform jet runway is a kind of land airplane field, and the very-short-reach formed by blast injection gas blanket stream is sliding Capable or VTOL aircraft or the dedicated jet runway stage apparatus of unmanned plane；Or it is flexible for a kind of continental rise Moveable foldable skeleton Charge-discharge air bag cushion jet runway stage apparatus, is slided by the very-short-reach that blast injection gas blanket stream is formed, or vertical Landing aircraft or the dedicated jet runway stage apparatus of unmanned plane, described in land airplane field, continental rise Moveable foldable skeleton is flexible Charge-discharge air bag cushion platform jet runway device is connected with management system；

The platform jet runway will be for a kind of future in town-dweller-rural-family's individual's baby plane in continental rise or continental rise sky airplane platform Frontier sentry, and may extend to the landing with international adaptability standard or store the current supermarket on family's aircraft airport, by pressing The very-short-reach that contracting air injection gas blanket stream is formed slides or VTOL aircraft or the dedicated jet runway device of unmanned plane, A kind of frigid zone-the low temperature limited by environment such as weather, geographic areas subzero 60 degree, the torrid zone-high temperature 80 degree variously Area, is slided by the very-short-reach that blast injection gas blanket stream is formed or VTOL aircraft or unmanned plane private track are put down Platform device, it is described in the personal big baby plane of town-dweller-rural-family or large, medium and small unmanned plane, continental rise or continental rise sky airplane platform, Carrier-borne fixed-wing unmanned plane landing when can 100% auxiliary recycling do not fall unmanned fuselage and head, each dedicated jet in frontier sentry Runway stage apparatus, someone or unmanned helicopter landing gas injection stage apparatus are connected with management system.

Forming the platform jet runway can be used whirlpool spray, turbofan, axial flow blower formula, air compressor, the liquid change of current maturation The gas supply gas source technology of gas various ways, the power source of the essential core as the jet runway will above several gas supply gas A certain gas source in source is input to each gas storage of the jet-propelled runway of the platform, supplies in artificial intelligent control system, can shape At the structure of the jet platform runway device of the safe landing aircraft of a very-short-reach.

2. platform jet runway according to claim 1, it is characterized in that：Overall structure is made of seven regions；Each region On, respectively as being provided with seven regions made of muti-piece valve body plate main body module sub-unit (73) is combined, the valve body plate main body Tangible chamber is arranged in the lower part of the bearing wall and frame structure of module sub-unit (73)；The first area of jet runway is 20 meters long (1), jet 20 meters of second area long (2) of runway, the third region of jet runway is 20 meters long (3), and 20 meters of the fourth region of jet runway are long (4), the 5th region of jet runway is 20 meters long (5), the District 7 of the 6th region of jet runway 20 meters long (6) and jet runway Domain is 20 meters long (7), respectively sets on each airfield runway each region or type aircraft carrier deck is carrier-borne or each dedicated jet runway in airport (191) on, one to seven region constitutes 140 meters long of each airport, and dedicated length is set as needed for a variety of different types, or It sets a kind of jet runway that size type is mutually compatible with or type aircraft carrier deck is whole to carrier-borne aircraft or the dedicated jet runway of unmanned plane landing The structure of body；

The left-external side in the first area of jet runway 20 meters long (1) is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；On the left outside cliche frame longitudinal direction batten seat (16) of runway, it is respectively equipped with the left outside green warning lamp of cliche frame longitudinal direction reddish yellow of runway (24)；Cushion connecting sewing (13) and private track left fixed under-chassis (8) are installed between each region valve body plate module of runway；

The left-external side in the first area of jet runway 20 meters long (1) is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；In the left outside lower part of the left outside cliche frame longitudinal direction batten seat (16) of runway, it is equipped with the left outside 1-7 region turnbarrel valve of runway Gate slot shape puff prot or circle hole shape puff prot servo pushing motor (30)；On the right side of the first area of jet runway 20 meters long (1) Outside, it is equipped with the right outer cliche frame longitudinal direction batten seat (17) of runway；In the right outer lower part of the right outer cliche frame longitudinal direction batten seat (17) of runway, Equipped with the right outer 1-7 region rotary sleeve valve flute profile puff prot of runway or circle hole shape puff prot servo pushing motor (31)；

The laterally inboard in the first area of jet runway 20 meters long (1) is equipped with the green warning of runway rear left wheel road reddish yellow Lamp (28)；After the left-external side of the first area of jet runway 20 meters long (1) between longitudinal direction, the second area equipped with jet runway 20 meters long (2)；Preceding longitudinally outboard in the first area of jet runway 20 meters long (1) is equipped with cliche frame transverse direction press strip before runway Sealing and dustproof outer cover (14)；Before runway on cliche frame transverse direction press strip sealing and dustproof outer cover (14), it is respectively equipped with Normal Take-Off And Landing storage Deposit defeated deflation bucket connecting tube (10)；Defeated deflation bucket connecting tube (11) is stored with emergency landing；Defeated deflation bucket is stored with spare landing Connecting tube (12)；And cliche frame transverse direction press strip sealing and dustproof outer cover seat fixing bolt (18) before runway, it is whole to constitute jet runway The unblocked fixed reasonable bindiny mechanism of sealing with cliche frame transverse direction press strip in three sets of independent gas transmission sources.

3. platform jet runway according to claim 2, it is characterized in that：In the green warning lamp of runway rear left wheel road reddish yellow (28) inside between is respectively equipped with each spout in left first region of runway and opens 1-2 millimeters (33)；In runway left first A each spout in region opens the Right Inboard of 1-2 millimeters (33), is equipped with the green warning lamp of runway front left wheel road reddish yellow (26) and runway The green warning lamp of front right wheel road reddish yellow (27)；The outside in the right side of the runway front right wheel green warning lamp of road reddish yellow (27), is equipped with and runs Each spout in first region opens 1-2 millimeters (35) in the road right side；Each spout in first region opens 1-2 millimeters in the runway right side (35) right side is equipped with the green warning lamp of right wheel road reddish yellow (29) after runway；

The right outside of the green warning lamp of right wheel road reddish yellow (29) after dedicated jet runway is equipped with right outer first area of runway Each spout in domain opens 1-2 millimeters (34)；1-2 millimeters of (34) right outsides are opened in the right outer each spout in first region of runway, are equipped with The right inside and outside multiple air curtain puff prots (61) in longitudinal direction of runway；It is right outer in the right inside and outside multiple air curtain puff prots (61) in longitudinal direction of runway Side is equipped with the right outer cliche frame longitudinal direction batten seat (17) of runway；On the right outer cliche frame longitudinal direction batten seat (17) of runway, it is respectively equipped with The runway right side green warning lamp of outer cliche frame longitudinal direction reddish yellow (25) and the fixed spiral shell of the right outer cliche frame longitudinal direction press strip sealing and dustproof outer cover of runway Bolt (21)；With the right fixed under-chassis (9) of private track；And cushion connecting sewing is installed between each region valve body plate module of runway (13)；Constitute that the consistent property of each component reasonable coordination repairs the connection of convenient for disassembly and assembly and jet protection gas source and warning rises with safety The manipulation and control of drop；

The left-external side of 20 meters of second area long (2) in jet runway is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；On the left outside cliche frame longitudinal direction batten seat (16) of runway, it is respectively equipped with the left outside green warning lamp of cliche frame longitudinal direction reddish yellow of runway (24)；Cushion connecting sewing (13) are installed between each region valve body plate module of runway；The left fixed under-chassis (8) of private track is constituted Integrally each portion position is fixedly connected with the structural compatibility with warning to jet runway；

20 meters of second area long (the horizontal left side 2), equipped with the green police of runway rear left wheel road reddish yellow in jet runway Show lamp (28)；After the left-external side of 20 meters of second area long (2) of jet runway between longitudinal direction, the third area equipped with jet runway Domain is 20 meters long (3)；Between the preceding longitudinal direction of 20 meters of second area long (2) of jet runway, the first area equipped with jet runway 20 meters long (1) constitutes the consistency of the whole cooperation control to one to three region of jet runway part runway mechanism；

The left-external side in the third region of jet runway 20 meters long (3) is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；On the left outside cliche frame longitudinal direction batten seat (16) of runway, it is respectively equipped with the left outside green warning lamp of cliche frame longitudinal direction reddish yellow of runway (24)；Cushion connecting sewing (13) and the left fixed under-chassis (8) of private track are installed between each region valve body plate module of runway；

The left side of transverse direction in the third region of jet runway 20 meters long (3) is equipped with the green warning of runway rear left wheel reddish yellow Lamp (28)；After the left-external side of the third region of jet runway 20 meters long (3) between longitudinal direction, the fourth region equipped with jet runway 20 meters long (4)；Between the preceding longitudinal direction of the third region of jet runway 20 meters long (3), the second area 20 equipped with jet runway Rice long (2) constitutes the consistency of structure connection Proper Match between each region in one to four region；

The left-external side of 20 meters of the fourth region long (4) in jet runway is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；On the left outside cliche frame longitudinal direction batten seat (16) of runway, it is respectively equipped with the left outside green warning lamp of cliche frame longitudinal direction reddish yellow of runway (24), cushion connecting sewing (13) and the left fixed under-chassis (8) of private track are installed between each region valve body plate module of runway；

The left side of transverse direction of 20 meters of the fourth region long (4) in jet runway is equipped with the green police of runway rear left wheel road reddish yellow Show lamp (28)；After the left-external side of 20 meters of the fourth region long (4) of jet runway between longitudinal direction, the 5th area equipped with jet runway Domain is 20 meters long (5)；Between the preceding longitudinal direction of 20 meters of the fourth region long (4) of jet runway, the third region equipped with jet runway 20 meters long (3) are constituted to the interconnection of each section components of jet runway and the reliability of security warning；

The left-external side in the 5th region 20 meters long (5) in jet runway is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；On the left outside cliche frame longitudinal direction batten seat (16) of runway, it is respectively equipped with the left outside green warning lamp of cliche frame longitudinal direction reddish yellow of runway (24), cushion connecting sewing (13) and the left fixed under-chassis (8) of private track are installed between each region valve body plate module of runway；

The left side of transverse direction in the 5th region 20 meters long (5) in jet runway is equipped with the green police of runway rear left wheel road reddish yellow Show lamp (28)；After the left-external side in the 5th region 20 meters long (5) of jet runway between longitudinal direction, the 6th area equipped with jet runway Domain is 20 meters long (6)；Between the preceding longitudinal direction in the 5th region 20 meters long (5) of jet runway, the fourth region equipped with jet runway 20 meters long (4)；

The left-external side in the 6th region 20 meters long (6) in jet runway is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；On the left outside cliche frame longitudinal direction batten seat (16) of runway, it is respectively equipped with the left outside green warning lamp of cliche frame longitudinal direction reddish yellow of runway (24), cushion connecting sewing (13) and the left fixed under-chassis (8) of private track are installed between each region valve body plate module of runway；

The left side of transverse direction in the 6th region 20 meters long (6) in jet runway is equipped with the green police of runway rear left wheel road reddish yellow Show lamp (28)；After the left-external side in the 6th region 20 meters long (6) of jet runway between longitudinal direction, the District 7 equipped with jet runway Domain is 20 meters long (7)；Between the preceding longitudinal direction in the 6th region 20 meters long (6) of jet runway, the 5th region equipped with jet runway 20 meters long (5), constitute each regional body and each region cooperates between each movement mechanism and fixed mechanism part in practical application It is advanced reasonable handling；

The left-external side in the District 7 domain of jet runway 20 meters long (7) is equipped with the left outside cliche frame longitudinal direction batten seat of runway (16)；On the left outside cliche frame longitudinal direction batten seat (16) of runway, it is respectively equipped with the left outside green warning lamp of cliche frame longitudinal direction reddish yellow of runway (24), cushion connecting sewing (13) and the left fixed under-chassis (8) of private track are installed between each region valve body plate module of runway, Constituting each section components of jet runway can the fixed security warning of entire combination.

4. platform jet runway according to claim 2, it is characterized in that：On the platform jet runway, it is respectively equipped with normal Landing stores defeated deflation bucket connecting tube (10), stores defeated deflation bucket connecting tube (11) with emergency landing and spare landing storage is defeated Cliche frame transverse direction press strip sealing and dustproof outer cover fixing bolt (19) after deflation bucket connecting tube (12) and runway is constituted to whole spray The three sets of individual secure air distribution systems sealing the most complete of gas runway and the smooth safe and practical property of gas source；

The left fixed under-chassis (8) of dedicated jet runway, the right fixed under-chassis (9) of private track, Normal Take-Off And Landing store defeated deflation bucket Connecting tube (10), emergency landing store defeated deflation bucket connecting tube (11), and spare landing stores defeated deflation bucket connecting tube (12), runway Cliche frame transverse direction press strip sealing and dustproof outer cover before installation cushion connecting sewing (13), runway between each region valve body plate module (14), the left outside cliche frame longitudinal direction batten seat (16) of cliche frame transverse direction press strip sealing and dustproof outer cover (15), runway, runway are right after runway It is inlayed after cliche frame transverse direction press strip sealing and dustproof outer cover fixing bolt (18), runway before outer cliche frame longitudinal direction batten seat (17), runway The fixed spiral shell of the left outside cliche frame longitudinal direction press strip sealing and dustproof outer cover of bezel transverse direction press strip sealing and dustproof outer cover fixing bolt (19), runway The right outer cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt (21) of bolt (20), runway；

It is described on the left outside cliche frame longitudinal direction batten seat (16) of dedicated jet runway, be respectively equipped with each region valve body plate module of runway Between installation cushion connecting sewing (13) run with the left outside cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt 20 of runway On the bottom position of the left outside cliche frame longitudinal direction batten seat (16) in road, it is equipped with the left fixed under-chassis (8) of private track；

It is described on the right outer cliche frame longitudinal direction batten seat (17) of dedicated jet runway, it is green to be equipped with the outer cliche frame longitudinal direction in runway right side reddish yellow Warning lamp (25)；On the bottom position of the right outer cliche frame longitudinal direction batten seat (17) of runway, it is equipped with the right fixed under-chassis of private track (9), with the right outer cliche frame longitudinal direction press strip sealing and dustproof outer cover fixing bolt (21) of runway；Cliche frame transverse direction press strip is close before runway Seal dustproof encloser 14) on, it is respectively equipped with the first green warning lamp of cliche frame transverse direction reddish yellow (22) before runway, stores defeated put with Normal Take-Off And Landing Gas bucket connecting tube (10), and emergency landing stores defeated deflation bucket connecting tube (11) and spare landing stores defeated deflation bucket connecting tube (12) and before runway cliche frame transverse direction press strip sealing and dustproof outer cover fixing bolt (18), composition consolidate jet runway entirety Fixed layout is connect and the controllability of safe Normal Take-Off And Landing with the layout closure of valve actuating mechanism；

It is described on cliche frame transverse direction press strip sealing and dustproof outer cover (15), to be respectively equipped with Normal Take-Off And Landing storage after dedicated jet runway Defeated deflation bucket connecting tube (10) stores defeated deflation bucket connecting tube (11) with emergency landing and spare landing stores defeated deflation bucket and connects The sealing of cliche frame transverse direction press strip is anti-after taking over (12) and the runway rear molding green warning lamp of cliche frame transverse direction reddish yellow (23) and runway Dirt outer cover fixing bolt (19)；

The first green warning lamp of cliche frame transverse direction reddish yellow (22), the green police of runway rear molding cliche frame transverse direction reddish yellow before the dedicated jet runway Show lamp (23), the left outside green warning lamp of cliche frame longitudinal direction reddish yellow (24) of runway, the green warning lamp of the runway right side outer cliche frame longitudinal direction reddish yellow (25), the green warning lamp of runway front left wheel road reddish yellow (26), the runway front right wheel green warning lamp of road reddish yellow (27), runway rear left machine It takes turns the green warning lamp of road reddish yellow (28), the green warning lamp of right wheel road reddish yellow (29) after runway, constitutes automatic letter whole to jet runway Number warning and the controllability of safe active.

5. platform jet runway according to claim 2, it is characterized in that：The left outside 1-7 region turnbarrel of runway Valve flute profile puff prot or circle hole shape puff prot servo pushing motor (30), each spout in the 7th region opens 7-8 in the runway right side Millimeter (59), if mounted in type aircraft carrier deck is carrier-borne or each dedicated jet runway (191) in airport on；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, it is longitudinal to be respectively equipped with the left outside cliche frame of runway Batten seat (16)；In the interior lower part of the left outside cliche frame longitudinal direction batten seat (16) of runway, it is equipped with the left outside 1-7 region rotary sleeve of runway Cylinder valve flute profile puff prot or circle hole shape puff prot servo pushing motor (30)；In the right outer cliche frame longitudinal direction batten seat (17) of runway Interior lower part is equipped with the right outer 1-7 region rotary sleeve valve flute profile puff prot of runway or circle hole shape puff prot servo pushing motor (31)；

It is described to open 1-2 millimeters (32) in each spout in left outside first region of jet runway, it is each in left first region of runway Spout opens 1-2 millimeters (33), 1-2 millimeters (34) is opened in the right outer each spout in first region of runway, first in the runway right side A each spout in region opens 1-2 millimeters (35)；

It is described to open 2-3 millimeters (36) in each spout of the left outside Two Areas of jet runway, it is each in the left Two Areas of runway Spout opens 2-3 millimeters (37), 2-3 millimeters (38) is opened in the right outer each spout of Two Areas of runway, second in the runway right side A each spout in region opens 2-3 millimeters (39)；

It is described to open 3-4 millimeters (40) in each spout in the left outside third region of jet runway, it is each in the left third region of runway Spout opens 3-4 millimeters (41), opens 3-4 millimeters (42) in the right outer each spout in third region of runway, the third in the runway right side A each spout in region opens 3-4 millimeters (43)；

It is described to open 4-5 millimeters (44) in each spout in left outside 4th region of jet runway, it is each in left 4th region of runway Spout opens 4-5 millimeters (45), 4-5 millimeters (46) is opened in the right outer each spout in 4th region of runway, the 4th in the runway right side A each spout in region opens 4-5 millimeters (47)；

It is described to open 5-6 millimeters (48) in each spout in left outside 5th region of jet runway, it is each in left 5th region of runway Spout opens 5-6 millimeters (49), 5-6 millimeters (50) is opened in the right outer each spout in 5th region of runway, the 5th in the runway right side A each spout in region opens 5-6 millimeters (51)；

It is described to open 6-7 millimeters (52) in each spout in left outside 6th region of jet runway, it is each in left 6th region of runway Spout opens 6-7 millimeters (53), 6-7 millimeters (54) is opened in the right outer each spout in 6th region of runway, the 6th in the runway right side A each spout in region opens 6-7 millimeters (55)；

It is described to open 7-8 millimeters (56) in each spout in left outside 7th region of jet runway, it is each in left 7th region of runway Spout opens 7-8 millimeters (57), 7-8 millimeters (58) is opened in the right outer each spout in 7th region of runway, the 7th in the runway right side Each spout in a region opens 7-8 millimeters (59), constitute first region to the 7th region on whole jet runway, to each area Domain puff prot gap opens size and meets landing aircraft in the security control of the quick landing in each region, each region jet size all with The control system of pilot and jet runway control tower mutually switches in machine, the finally completion whole in aircraft by pilot Manipulate control of the jet runway to landing aircraft.

6. platform jet runway according to claim 2, it is characterized in that：In each region valve body plate main body of the jet runway On module sub-unit (73), it is respectively equipped with the left inside China and foreign countries of runway longitudinally multiple air curtain puff prots (60), the right inside and outside longitudinal direction of runway Outer laterally four flute profiles or round puff prot are positive normal landing puff prot (62), runway before multiple air curtain puff prots (61), runway Four flute profiles of preceding middle transverse direction or round puff prot are lateral four flute profiles or circular jetting before and after spare landing puff prot (63), runway Port is emergency landing puff prot (64)；Runway longitudinally injection 50-400 mesh intelligence hydraulic spray nozzle (72), if being mounted in type aircraft carrier deck On carrier-borne or each dedicated jet runway (191) in airport；

It is described in the left inside China and foreign countries of jet runway longitudinally multiple air curtain puff prots (60), the right inside and outside multiple air curtain jets in longitudinal direction of runway Outer laterally four flute profiles or round puff prot are positive middle transverse direction four before normal landing puff prot (62), runway before mouthful (61), runway Flute profile or round puff prot are that laterally four flute profiles or round puff prot are to meet an urgent need for spare landing puff prot (63), runway front and back Drop puff prot (64), constitute whole runway is not influenced by external wind interference, and in runway each region be designed with it is normal, The normal work of each region main jet loophole of intelligent control of the respective independent switching system of three of emergency power landing aircraft；

The position all around of the seat under each piece of valve body plate main body module sub-unit (73) template of jet runway, all distinguishes Equipped with the longitudinal road face horizontal adjustment cushion (65) of each valve body plate main body module of installation or so；Runway installs each valve body plate main body mould Lateral road face horizontal adjustment cushion (66), runway install the self-locking fixing bolt of each valve body plate main body module dedicated buffering before and after block (67)；The various bufferings and damping after overloading to whole runway in takeoff and landing are constituted, it will not when reaching to landing aircraft Cause the vibration to runway；

In from jet runway first area to the 7th of jet runway the region, it is equipped with muti-piece valve body plate main body module sub-unit 73；On valve body plate main body module sub-unit 73, it is equipped with outer rotary shaft flute profile mouth or round hole axle outer shaft in multiple runways and connects Fork library (68) is connect, outer rotary shaft flute profile mouth or round hole axle internal axle sleeve connecting fork library (69), universal globe shell type 180- in runway 360 degree of angle rotary oscillating type puff prot amendment takeoff and landing " inclination of the yaw biasing heart, righting of rising and falling up and down " (70), inner rotary shaft Flute profile puff prot 97 is covered,；Oxygenation or manufacture anoxic puff prot (71) are manufactured, runway longitudinally sprays 50-400 mesh intelligence hydraulic spray nozzle (72)；Constitute to exterior and interior axle sleeves connecting fork library to each rotary shaft flute profile jet port or circle hole shape jet port, each jet port it is coaxial Degree and steering angle up to 100% it is accurate；

First region 20 meters long (1) on jet runway valve body plate main body module sub-unit (73) to the 7th region On 20 meters long (7), the left inside China and foreign countries of runway longitudinally multiple air curtain puff prots (60) are respectively equipped with, it is multiple with the right inside and outside longitudinal direction of runway Outer laterally four flute profiles or round puff prot are positive normal landing puff prot (62) and runway before air curtain puff prot (61) and runway Four flute profiles of preceding middle transverse direction or round puff prot are lateral four flute profiles or circle before and after spare landing puff prot (63) and runway Shape puff prot is emergency landing puff prot (64), constitutes the independent switching manipulation control of three sets of air curtains protection in each region of jet runway System, and constitute interfering it for the whole various high wind of runway external environment；

The position all around of the seat under every piece of valve body plate main body module sub-unit (73) template of jet runway, all pacifies respectively Fill the longitudinal road face horizontal adjustment cushion (65) of each valve body plate main body module or so；Each valve body plate main body module front and back is installed laterally Road face horizontal adjustment cushion (66)；The self-locking fixing bolt of each valve body plate main body module dedicated buffering (67) is installed；The above, Constitute whole jet runway, the security performance during realizing integrated buffer and damping use to landing aircraft；

It is described on jet runway valve body plate main body module sub-unit 73, be respectively equipped with outer rotary shaft flute profile mouth or circle in runway Hole axle outer shaft connecting fork library (68), interior outer rotary shaft flute profile mouth or round hole axle internal axle sleeve connecting fork library (69) with runway； Constitute whole each region of jet runway laterally each interior outer rotary shaft it is in office what when being driven, each jet port angle opens size all 100% on an axis, precise angle, sealing when each puff prot switch closes prevent dirt object, rainwater or seawater from entering Each puff prot and shutoff valve shape are intracavitary；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with universal globe shell type 180- 360 degree of angle rotary oscillating type puff prot amendment takeoff and landing " inclination of the yaw biasing heart, righting of rising and falling up and down " (70)；Inner rotary shaft It covers flute profile puff prot (97), longitudinally sprays 50-400 mesh intelligent water with manufacture oxygenation or manufacture anoxic puff prot (71) and runway Atomizing nozzle (72)；Whole each region of jet runway is constituted actively to the secure safety manipulation and control of emergency landing aircraft, and It can the various large aircraft safe fallings of safety barrage.

7. platform jet runway according to claim 2, it is characterized in that：It is described in each region valve body plate main body of jet runway On module sub-unit (73), it is respectively equipped with outer rotary shaft flute profile mouth or round hole axle outer shaft connecting fork library in jet runway (68)；Outer rotary shaft flute profile mouth or round hole axle internal axle sleeve connecting fork library (69) in runway；Universal globe shell type 180-360 degree angle Rotary oscillating type puff prot corrects takeoff and landing " inclination of the yaw biasing heart, righting of rising and falling up and down " (70)；Inner rotary shaft covers flute profile Puff prot (97)；With manufacture oxygenation or manufacture anoxic puff prot (71)；50-400 mesh intelligence hydraulic spray nozzle is longitudinally sprayed with runway (72)；Whole each region of jet runway is constituted actively to emergency landing aircraft " eccentric biasing boat inclination, righting of rising and falling up and down " It constantly corrects, warship control is blocked using water mist gas is with high safety to 600 tons heavy or more aircraft landing, and to jet Runway gas source constitutes manipulation of the secure safety to landing aircraft under Reasonable Protection utilization and recycling effect；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be equipped with 0-180 degree angle spray circle hole shape mouth Interior rotation solid shaft (98)；0-180 degree angle injection circle hole shape mouth in rotate solid shaft (98) on, be equipped with interior rotation solid shaft or Hollow axle sleeve circle hole shape puff prot (99)；The both ends that solid shaft (98) are rotated in 0-180 degree angle injection circle hole shape mouth, are equipped with rotation Shaft flute profile mouth or round hole axle outer shaft head end card slot (113) are set respectively mounted in type aircraft carrier deck is carrier-borne or each dedicated jet in airport On runway (191)；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be equipped with runway valve body plate main body module install Electromagnet cut off valve or gas control jet air storage chamber phase through slot room (74)；Electromagnet cut off valve or gas are installed in runway valve body plate main body module It controls under jet air storage chamber phase through slot room (74), is equipped with runway valve body plate main body module lower plate pedestal (86)；In runway valve body plate Main body module is installed in electromagnet cut off valve or gas control jet air storage chamber phase through slot room (74), and universal globe injector head or inside and outside is equipped with Rotary sleeve sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or pneumatic regulation whiff pressure graduated release valve sub-unit (137)；In universal globe injector head or inside and outside rotary sleeve sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or gas On dynamic regulation whiff pressure graduated release valve sub-unit (137), it is equipped with universal globe injector head and is oriented to jet appendix single sleeve (136)；With compressed air gas source blowing mouth or the quick plug receptacle seat (139) of hose connector, extraneous input gas source is constituted to entirety The manipulation and control of the normal safe landing of injection gas source in jet runway.

8. platform jet runway according to claim 2, it is characterized in that：It is described in each region valve body plate main body of jet runway On module sub-unit (73), it is equipped with Pneumatic extension and hydraulic cylinder flexible control mechanism installation room maintenance blind patch (89)；In gas It is dynamic flexible under hydraulic cylinder flexible control mechanism installation room maintenance blind patch (89), oil cylinder (75) are pushed equipped with Pneumatic extension； It is pushed on oil cylinder (75) in Pneumatic extension, pushes hydraulic cylinder equipped with Pneumatic extension and stretch interlocking lever (76)；With flexible interlocking lever Arm connecting plate (77) are oriented to each control rotary axle valve；With fixed pin shaft above and below flexible interlocking lever and each guiding arm connecting plate And pin card dottle pin (78) constitutes the safe manoeuvring control mechanism that whole jet runway pneumatically moves cylinder mixing fast and flexible with oil；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be equipped with rotary shaft flute profile mouth or round hole axle Outer shaft fixing seat (94)；On rotary shaft flute profile mouth or round hole axle outer shaft fixing seat (94), it is equipped with inside and outside compressed air The outer swing arm fixing groove handle seat (79) of rotary sleeve sleeve；The swing arm fixing groove handle outside rotary sleeve sleeve inside and outside the compressed air On seat (79), it is equipped with swing arm and fixing bolt (80) outside outer rotary shaft set sleeve fork library；Outside outer rotary sleeve sleeve fork library The lower end of swing arm and fixing bolt (80) is equipped with swing arm and fixing bolt (81) outside inner rotary shaft set sleeve fork library；Inside Rotary sleeve sleeve is pitched under the outer swing arm in library and fixing bolt (81), is equipped with and is oriented to active support plate swing linking arm or rotary shaft The whole jet runway of lateral pressure swivel bearing (138) composition pneumatically pushes oil cylinder Hybrid connections part and flexibly swings inside and outside set sleeve The operating-controlling mechanism reliably used of guiding freely；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, push oil cylinder (75) equipped with Pneumatic extension； It is pushed on oil cylinder (75) in Pneumatic extension, is equipped with inside and outside rotary sleeve sleeve and pushes rack gear or connection gib block (82)；Inside and outside Rotary sleeve sleeve pushes in rack gear or connection gib block (82), is equipped with flexible interlocking lever and each control rotary axle valve is oriented to arm Connecting plate (77)；With fixed pin shaft and pin card dottle pin (78) above and below flexible interlocking lever and each guiding arm connecting plate；With interior rotation Bushing sleeves pitch swing arm and fixing bolt (81) outside library；And the active support plate of guiding is swung in linking arm or rotary sleeve sleeve Outer lateral pressure swivel bearing (138)；On each 73 inside casing of region valve body plate main body module sub-unit of jet runway, it is equipped with control Cylinder is connected and fixed seat (83)；It is connected and fixed on seat (83) in master cylinder, is connected and fixed hinged shaft (84) equipped with master cylinder；With pneumatically stretch Contracting pushes the flexible realization that oil cylinder (75) constitute each control unit of whole jet runway, is swinging the sliding peace closed in precision of shaft The stability of full manipulation service life；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be equipped with runway longitudinally injection 50-400 mesh intelligence It can hydraulic spray nozzle (72)；Runway pavement panel (85)；The longitudinal multiple air curtain puff prots (60) in the left inside China and foreign countries of runway；In runway transverse direction Centre to bilateral symmetry is equipped with universal globe shell type 180-360 degree angle rotary oscillating type puff prot amendment takeoff and landing " yaw biasing Heart inclination, righting of rising and falling up and down " (70) constitutes and corrects takeoff and landing " inclination of the yaw biasing heart, upper sinking on whole jet runway Floating righting " puff prot to aircraft trace can adjustment constantly control；

The lower part in each region valve body plate main body module sub-unit (73) of jet runway is equipped with jet runway valve body plate main body Module lower plate pedestal (86)；On jet runway valve body plate main body module lower plate pedestal (86), it is equipped with runway valve body plate master Module installs electromagnet cut off valve or gas control jet air storage chamber phase through slot room (74)；Runway valve body plate main body module I-shaped support rib Stand (87)；Fixing threaded hole (91) above and below subject runway module air inlet air storage chamber transverse sealing end cap；Normal Take-Off And Landing storage is defeated to put Gas bucket connecting tube (10)；Landing of meeting an urgent need stores defeated deflation bucket connecting tube (11) and spare landing stores defeated deflation bucket connecting tube (12), the unimpeded control with the fixed support performance of sealing of air distribution system gas transmission of whole jet three sets of self-insurances of runway is constituted；

The lower part in each region valve body plate main body module sub-unit (73) of jet runway is equipped with jet runway valve body plate main body Module I-shaped support rib stand (87)；On jet runway valve body plate main body module I-shaped support rib stand (87), it is equipped with runway Fixing threaded hole (91) above and below main body module air inlet air storage chamber transverse sealing end cap；The flexible manipulation of hydraulic cylinder is pushed with Pneumatic extension Room (88) are installed by mechanism；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, it is flexible to be equipped with Pneumatic extension and hydraulic cylinder Operating mechanism installs room maintenance blind patch overlap joint mouth (90)；It is repaired in Pneumatic extension and hydraulic cylinder flexible control mechanism installation room Blind patch overlaps on mouth (90) left and right sides, is respectively provided with Pneumatic extension and hydraulic cylinder flexible control mechanism installation room maintenance port lid Plate (89)；Under jet runway valve body plate main body module lower plate pedestal (86), it is equipped in runway valve body plate main body module air inlet Pipe installs room transverse sealing end cap inner panel (92)；Transverse sealing end cap inner panel in room is installed in runway valve body plate main body module air inlet pipe (92) it on, is respectively equipped with Normal Take-Off And Landing and stores defeated deflation bucket connecting tube (10)；Landing of meeting an urgent need stores defeated deflation bucket connecting tube (11)； Spare landing stores defeated deflation bucket connecting tube (12)；A variety of interior main each gas transmission storages deflation bucket interface bore (140) of air supply source；Pressure Contracting air gas source blowing mouth or the quick plug receptacle seat (139) of hose connector；With subject runway module air inlet air storage chamber transverse sealing Fixing threaded hole (91), the air distribution system and Pneumatic extension for constituting whole three sets of runway of jet push hydraulic cylinder and stretch end cap up and down Installation and maintenance operating control mechanism easy to use.

9. platform jet runway according to claim 2, it is characterized in that：It is described in each region valve body plate main body of jet runway On module sub-unit (73), it is equipped with rotation solid shaft or hollow shaft sleeve (96) in 0-180 degree angle injection flute profile mouth；In 0-180 It spends in angle injection flute profile mouth and rotates on solid shaft or hollow shaft sleeve (96), be equipped with inner rotary shaft set flute profile puff prot (97)；If It sets in the 0-180 degree angle injection circle hole shape mouth on the valve body plate main body module sub-unit (73) in rotation solid shaft (98), if There are interior rotation solid shaft or hollow axle sleeve circle hole shape puff prot (99), each jet port air-flow of whole jet runway is constituted, by axis The Internal control structure of bar and axle sleeve gap seal standard precision, which cooperates, to be adjusted；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be equipped with manufacture oxygenation or manufacture anoxic jet Mouth (71)；In manufacture oxygenation or manufacture anoxic puff prot (71), it is respectively equipped with 30 degree of dead angles spray by 30-90 degree fixed angle Loophole rotates solid shaft or hollow shaft sleeve (100)；By 30-90 degree fixed angle 40 degree of dead angle jet ports rotate solid shaft or Hollow shaft sleeve (101)；Solid shaft or hollow shaft sleeve (102) are rotated by 50 degree of dead angle jet ports of 30-90 degree fixed angle； Solid shaft or hollow shaft sleeve (103) are rotated by 60 degree of dead angle jet ports of 30-90 degree fixed angle；By 30-90 degree fixed angles The 70 degree of dead angle jet ports rotation solid shaft or hollow shaft sleeve (104) of degree；It is sprayed by 80 degree of dead angles of 30-90 degree fixed angle Mouth rotation solid shaft or hollow shaft sleeve (105)；Solid shaft or sky are rotated by 90 degree of dead angle jet ports of 30-90 degree fixed angle Mandrel sleeve (106) constitutes each jet port rotary shaft axle sleeve clearance seal in one to seven region and storage inside whole jet runway The standard controllability of air chamber structure；

On each region valve body plate main body module sub-unit (73) of jet runway, it is equipped with by 0-180 degree angle injection flute profile mouth Rotate solid shaft or hollow shaft sleeve (96)；Solid shaft or hollow shaft sleeve (96) are rotated in 0-180 degree angle injection flute profile mouth On, it is equipped with rotation axis seal packing mounting groove (107)；On rotation axis seal packing mounting groove (107), it is equipped with rotation axis seal Packing (108)；It is described on each region valve body plate main body module sub-unit (73) of jet runway, be equipped with rotary shaft flute profile mouth or circle Shape hole axle internal axle sleeve fixing seat mouth (109)；On rotary shaft flute profile mouth or round hole axle internal axle sleeve fixing seat mouth (109), respectively Equipped with rotary shaft flute profile mouth or round hole axle exterior and interior axle sleeves or upper and lower gas transmission room sealing FE Tiler (110)；With rotary shaft flute profile mouth or Round hole axle exterior and interior axle sleeves or FE Tiler cage bolt hole (95) constitute whole jet runway internal spray mouth rotary shaft to gas supply Gas source sealing structure precision closes the manipulation of the reliability of gas source；

It is described on each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with rotary shaft flute profile mouth or circle Hole axle outer shaft fixing seat (94)；On rotary shaft flute profile mouth or round hole axle outer shaft fixing seat (94), it is respectively equipped with rotation Axial trough shape mouth or round hole axle outer shaft (93)；With rotary shaft flute profile mouth or round hole axle exterior and interior axle sleeves or FE Tiler cage bolt Hole (95)；On each region valve body plate main body module sub-unit (73) of jet runway, it is provided with manufacture oxygenation or manufacture anoxic spray Port (71)；It is manufactured in oxygenation or manufacture anoxic puff prot (71) in runway, is equipped with rotation in 0-180 degree angle injection circle hole shape mouth Solid shaft (98)；It is rotated on solid shaft (98) in 0-180 degree angle injection circle hole shape mouth, is equipped with rotary shaft flute profile mouth or round hole Axis outer shaft head end card slot (113)；On rotary shaft flute profile mouth or round hole axle outer shaft head end card slot (113), rotation can be respectively equipped with Shaft flute profile mouth or round hole axle unofficial biography dynamic crankshaft swing angle axis (111)；It is dynamic with rotary shaft flute profile mouth or round hole axle unofficial biography D-axis swing angle axis (112) constitutes the ensuring smooth transmission after being connected between each rotary shaft and head both ends, easy to assembly, use The manipulation of safe and reliable property.

10. platform jet runway according to claim 2, it is characterized in that：Each region valve body plate main body of jet runway On module sub-unit (73), it is equipped with universal globe shell type gas-sparging head list sleeve or double telescopic sub-units (114)；Multi-directional ball Face injector head outward flange disk seat fixing bolt (141)；If mounted in type aircraft carrier deck is carrier-borne or each dedicated jet runway (191) in airport On；

The universal globe shell type gas-sparging head list sleeve or double telescopic sub-units (114), in universal globe shell type gas On injector head list sleeve or double telescopic sub-units (114), fixing seat (116) are positioned outside equipped with universal globe injector head；With ten thousand To spherical sleeve type injector head flange seat (115)；Jet appendix single sleeve (136) are oriented to universal globe injector head；With ten thousand To spherical surface injector head or inside and outside rotary sleeve sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or pneumatically regulate and control jet Pressure relief valve sub-unit (137)；

It is described on the valve body plate main body module sub-unit (73) in each region of jet runway, be respectively equipped with outside universal globe injector head It positions fixing seat (116)；With universal globe injector head outward flange disk seat fixing bolt (141)；It is solid with longitudinal motor or pneumatic linear actuator Fixed rack (121)；And universal globe injector head guiding leading screw or guiding pneumatic control thick stick fixed plate (126)；

It is described to be positioned outside universal globe injector head on fixing seat (116), it is respectively equipped with universal globe injector head rotary oscillation ball Surface cover seat is fixed inner shield ring (117)；Spherical surface set fixing seat (118) is swung with universal globe jet port spinning ball；And multi-directional ball Face jet port rotary oscillation spherical surface body (119)；Constitute universal globe shell type rotary oscillation 0-360 degree can angle-adjustable, spray The connection and flexible manipulation and control of the fixation position for body sub-unit entirety of emanating；

It is described in universal globe jet port rotary oscillation spherical surface body (119), be respectively equipped with universal globe shell type injection head flange Seat (115)；Jet appendix single sleeve (136) are oriented to universal globe injector head；With universal globe injector head or interior outward turning Shaft covers sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or pneumatic regulation whiff pressure graduated release valve sub-unit (137)；Constitute universal globe shell type rotary oscillation 0-360 degree can angle-adjustable, realize that injection gas sub-unit is whole The safer manipulation and control of gas source control system；

It is described to be positioned outside universal globe injector head on fixing seat (116), it is respectively equipped with longitudinal motor or the fixed bracket of pneumatic linear actuator (121)；Motor is driven with lateral driving lever or the transmission of Pneumatic extension cylinder pushes driving lever (122)；It is controlled with longitudinal motor or pneumatic linear actuator (123)；

Described to control on (123) in longitudinal motor or pneumatic linear actuator, longitudinal dial can arbitrarily be adjusted by being respectively equipped with universal globe 0-360 degree Actuator push rod (120) are stretched in moving gear or pneumatic control；With universal globe injector head guiding leading screw worm gear pairs or guiding air valve control Processed group (127)；

It is described to be positioned outside universal globe injector head on fixing seat (116), it is respectively equipped with universal globe injection headstock gasket (124)；With universal globe injector head locknut (125)；It is fixed with universal globe injector head guiding leading screw or guiding pneumatic control thick stick Plate (126) constitutes universal globe shell type rotary oscillation 0-360 degree, can arbitrarily adjust each angle injection gas gas sub-unit entirety Fixed support and control；

It is described universal globe injector head guiding leading screw or guiding pneumatic control thick stick fixed plate (126) on, be respectively equipped with multi-directional ball Face injector head guiding leading screw worm gear pairs or guiding Air Valve Control group (127), with universal globe injector head guiding leading screw or guiding gas Valve controls flexible thick stick (128) and universal globe injector head guiding locking screw (129) and universal globe injector head guiding is lived Network support plate swings linking arm pin shaft and plum blossom latch card (134), is oriented to active support plate with universal globe injector head and swings company It connects arm (130) and universal globe injector head is oriented to active support plate and swings linking arm sliding pin (131), sprayed with universal globe It penetrates head and is oriented to active support plate swing linking arm adjustment upper arm reinforcing rib (132) and the active support of universal globe injector head guiding Plate swing linking arm pin hole (133) constitute universal globe shell type rotary oscillation 0-360 degree can angle-adjustable, and will injection The control of gas entirety, and reliable and stable control when transmission guide swinging；

It is described to be oriented on jet appendix single sleeve (136) in universal globe injector head, it is respectively equipped with universal globe injector head It is oriented to active support plate and swings linking arm driving lever support base (135), with universal globe injector head or inside and outside rotary sleeve sleeve groove Shape mouth or each region electromagnet cut off valve of circle hole shape mouth or pneumatic regulation whiff pressure graduated release valve sub-unit (137) and universal globe Injector head is oriented to active support plate and swings linking arm pin hole (133), is oriented to active support plate with universal globe injector head and swings Linking arm adjusts upper arm reinforcing rib (132) and universal globe injector head is oriented to active support plate and swings linking arm sliding pin (131) and universal globe injector head is oriented to active support plate and swings linking arm (130) and the guiding work of universal globe injector head Network support plate swings linking arm pin shaft and plum blossom latch card (134), constitutes extraneous input gas source to spraying gas source in jet runway Normal safe landing control, and the reliable manipulation of active support plate flexible swinging is oriented to universal globe injector head；

It is described that the both ends that active support plate swings linking arm (130) are oriented in universal globe injector head, it is active to be respectively equipped with guiding Support plate swings lateral pressure swivel bearing (138) inside and outside linking arm or rotary sleeve sleeve；It is swung being oriented to active support plate Inside and outside linking arm or rotary sleeve sleeve in lateral pressure swivel bearing (138), it is equipped with universal globe injector head and is oriented to active branch Fagging swings linking arm pin shaft and plum blossom latch card (134), and constituting universal globe shell type rotary oscillation 0-360 degree can arbitrarily adjust Angle, and whole the fixing of injection gas are supported and are controlled the guiding movement more flexibility of gas；

It is described on the valve body plate main body module sub-unit (73) in each region of jet runway, be respectively equipped with outside universal globe injector head It positions fixing seat (116)；It positions on fixing seat (116), is respectively equipped with outside universal globe injector head outside universal globe injector head Flange holder fixing bolt (141)；

It is described in universal globe injector head or inside and outside rotary sleeve sleeve flute profile mouth or each region electromagnet cut off valve of circle hole shape mouth or On pneumatic regulation whiff pressure graduated release valve sub-unit (137), it is respectively equipped with universal globe injector head guiding jet appendix list set Cartridge type (136), with compressed air gas source blowing mouth or the quick plug receptacle seat (139) of hose connector；Constitute extraneous input gas source pair The normal safe landing supportive control of injection gas source in jet runway；

It is described on universal globe shell type gas-sparging head list sleeve or double telescopic sub-units (114), be equipped with universal globe spray Penetrate pressure locking block set (209) of collaborating under turnbarrel in the double sleeves of head；The turnbarrel in the double sleeves of universal globe injector head Under collaborate in pressure locking block set (209), be respectively equipped with turnbarrel waterproof and dustproof in the double sleeves of universal globe injector head, anti- Turnbarrel collaborates downwards pressure buffer bearing (211) in frozen oil envelope or the double sleeves of packing (208) and universal globe injector head, Pressure locking block set (209) is collaborated outside under turnbarrel in the double sleeves of universal globe injector head, is equipped with universal globe injector head Buffing pad (210) on turnbarrel in double sleeve fixed sleeves cylinders；In the double sleeve fixed sleeves cylinder inward turnings of universal globe injector head On rotaring sleeve outside buffing pad 210, it is equipped with universal globe jet port rotary oscillation spherical surface body (119), constitutes universal globe injector head Turnbarrel flexible rotation and 360 degree of swings and dust-proof, anti-water management in double bush outer sleeve cylinders are fixed；

It is described on universal globe shell type gas-sparging head list sleeve or double telescopic sub-units (114), be respectively equipped with multi-directional ball The double sleeve fixed sleeves cylinders (212) of face injector head, with single sealing gland or the packing of collaborating on universal globe injector head inside and outside sleeve (213) slot (214) and universal globe injector head inside and outside sleeve in the defeated deflation of turnbarrel and in universal globe injector head Middle part is collaborated single sealing gland or packing (215), constitute in universal globe injector head turnbarrel flexible rotation and fixed sleeves cylinder it Between leakproofness control；

It is described on universal globe shell type gas-sparging head list sleeve or double telescopic sub-units (114), be respectively equipped with multi-directional ball Face injector head fixed sleeves cylinder gas transmission air inlet (217) open in usual；In the gas transmission open in usual of universal globe injector head fixed sleeves cylinder In air inlet (217), it is equipped with turnbarrel (225) in the double sleeves of universal globe injector head；In the double sleeves of universal globe injector head On interior turnbarrel (225), air inlet blowing mouth (216) and universal globe in turnbarrel are equipped in universal globe injector head It collaborates under injector head inside and outside sleeve double sealing glands or packing (218), constitutes the normal injection in defeated ventilation source and the normal opening of gas source With the flexible control of the normal leakproofness for closing gas source and gas source；

It is described on turnbarrel (225), to be equipped with turnbarrel in universal globe injector head in the double sleeves of universal globe injector head It collaborates compressive resistance buffering bearing (219), collaborates upwards anti-pressure locking flange with turnbarrel in universal globe injector head upwards Turnbarrel in turnbarrel locking screw tooth (221) and universal globe injector head in nut (220) and universal globe injector head Turnbarrel swing arm (223) in swing arm fixing bolt (224) and universal globe injector head, with universal globe injector head inward turning Rotaring sleeve swing arm pushes and pulls bulb (222), constitutes the flexible control of the rotation input gas source of interior turnbarrel and fixed sleeves cylinder, Swing angle it is accurate, reliable；

It is described on universal globe injector head fixed sleeves cylinder gas transmission air inlet (217) open in usual, be equipped with each valve body plate module in Soft or hard snorkel is coupled quick combination hub (169), with the defeated soft or hard coupling connecting tube of deflating of nominal gas jet port in runway (157), and can 360 degree rotation swing nominal gas jet port electromagnet cut off valve switch in connecting bend (162) and runway (151), the normal on and off of defeated ventilation source is constituted.

11. platform jet runway according to claim 2, it is characterized in that：It is described in each region valve body plate master of jet runway The interior lower part of module sub-unit (73) is respectively equipped with normal storage deflation bucket (146) in runway, puts with emergency storage in runway Gas bucket (147) is met an urgent need in storage deflation bucket (147) in normal storage deflation bucket (146) and runway in jet runway, is respectively set Some refrigeration, heating sensing modulator (207) act on the enough landing aircraft institutes of flow that can guarantee that each jet port of runway sprays Gas source, and guarantee that runway pavement temperature Normal Take-Off And Landing aircraft can be made under cold, tropical environment, it constitutes whole jet runway and exists The safe manoeuvring of normally safe landing when misty rain, ice and snow or hot weather controls；

The interior lower part in each region valve body plate main body module sub-unit (73) of jet runway is respectively equipped with multiple main gas of conveying Deflation bucket appendix (143) are stored in source Quick connector plug (142) and more runways, are put with normal storage in multiple runways Emergency storage deflation bucket check valve (145), controls the general gas of each autonomous system in gas bucket check valve (144) and multiple runways It can still Normal Take-Off And Landing, the gas supply air supply machine for constituting whole jet runway be driven when source and the switching of individual gas sources system or failure The safety guarantee of control, circuit system control；

The interior lower part in each region valve body plate main body module sub-unit (73) of jet runway, is respectively equipped in jet runway just Air pressure is regarded outside normal storage deflation bucket in often storage deflation bucket (146), with emergency storage deflation bucket (147) in runway and runway Normal injection gas pressure regulation in air gauge (149) and runway is regarded outside emergency storage deflation bucket in table (148) and runway to cut Emergency injection gas tune in only valve (150), with nominal gas jet port electromagnet cut off valve switch (151) in runway and runway In pressure cutoff valve (152) and runway in emergency gas ejection ports electromagnet cut off valve switch (153) and runway normally with emergency Gas source switching electromagnet cut off valve switch (154) in deflation bucket is stored, guarantees the normal control of each air supply source；

It is described in the interior lower part of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped in runway normally with answer Anxious storage deflation bucket current collecting tier gas supply check valve (155), deflation bucket is compressor gas supplied unidirectional with normally storing with emergency in runway Emergency gas injection in nominal gas jet port defeated deflate soft or hard coupling connecting tube (157) and runway in valve (156) and runway Normal storage deflation bucket is mutually ventilated soft or hard coupling connecting tube in mouthful defeated deflate soft or hard coupling connecting tube (158) and runway (159), it mutually ventilates soft or hard coupling connecting tube (160) with emergency storage deflation bucket in runway, composition can each gas source of safety assurance The normal gas supply of constant-pressure stable can the more selective distribution control to gas source；

The interior lower part in each region valve body plate main body module sub-unit (73) of jet runway, is respectively equipped with gas in jet runway Body pressure regulation stop valve and electromagnet cut off valve switch connection outside screw (161), and can 360 degree rotation swing connecting bend (162), with race Laterally defeated snorkel (163) and the interior emergency gas ejection ports Universal-head of runway are laterally defeated for nominal gas jet port Universal-head in road Snorkel (164) meets an urgent need gas ejection ports Universal-head laterally on defeated snorkel (164) in runway, is respectively equipped with intellectual system Fork sliding sleeve (165) is stirred in the swing of nominal gas jet port transverse pipe in cold, heating sensing modulator (207) and runway, and is run Fork sliding sleeve (166) is stirred in gas ejection ports transverse pipe of meeting an urgent need in road swing, and normally stifled with emergency transverse pipe sealing-plug in runway (167), it is ensured that the normal output and the landing of runway pavement normal temperature of each air supply system；

It is described on the low inside of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with jet runway Inside normally with meet an urgent need and storage deflation bucket electromagnet cut off valve interval freewheeling diode (168)；It is soft or hard in each valve body plate module of runway Snorkel is coupled quick combination hub (169)；Fork (170) normally are stirred with emergency transverse pipe swing in runway；In runway normally with Fork connection locking plate (171) is stirred in emergency transverse pipe swing；In runway normally with emergency transverse pipe swing stir fork locking plate with Handspike fixing bolt (172), it is ensured that the constant and transverse pipe swinging fork angle of each storage deflation bucket air pressure is controlled positive and negative In the range of 0.5 degree of angle, constituting can the more smart accurate flexible effect of safe landing using gas source and saving gas source.

12. platform jet runway according to claim 2, it is characterized in that：It is described in each region valve body plate master of jet runway On the low inside of module sub-unit (73), it is respectively equipped with the mechanically automatically controlled stroke of normal injection mouth advance stop in runway and opens It closes (173)；Normal injection mouth retreats the mechanically automatically controlled travel switch (174) of stop in runway；Emergency jet port advances in runway The mechanically automatically controlled travel switch (175) of stop；Emergency jet port retreats the mechanically automatically controlled travel switch (176) of stop in runway, Spare and setting a kind of stroke electric-controlled switch after ensuring angle sensor Signal-controlled switch failure, constitutes dual fail-safe circuit mould The artificial intelligence control of formula；

It is described on the low inside of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped in runway just The normal jet port advance automatically controlled travel switch of stop artificial intelligence formula (177)；Normal injection mouth retreats stop artificial intelligence in runway The automatically controlled travel switch of formula (178)；The automatically controlled travel switch of jet port advance stop artificial intelligence formula (179) are met an urgent need in runway；Runway Interior emergency jet port retreats the automatically controlled travel switch of stop artificial intelligence formula (180), it is ensured that the accuracy of each jet port angle is constituted It controls to form mechano-electronic dual fail-safe circuit-mode and artificial intelligence manipulation and control with electronic signal sensitive switch；

It is described on the low inside of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped in runway just Normal jet port advances and retreats artificial intelligence formula angle sensor controller (181)；Emergency jet port advances and retreats people in runway The intellectual angle sensor controller (182) of work；Normal servo motor impeller-hub feed rod connection locking transition plates (183) in runway； Emergency servo motor impeller-hub feed rod connection locking transition plates (184) in runway；Normal servo motor or promotion oil cylinder in runway (185)；Emergency servo motor or promotion oil cylinder (186) in runway；In runway normally with emergency impeller-hub feed rod (187)；Runway Inside normally with emergency impeller-hub feed rod guiding axis sliding sleeve (188), optimum efficiency can normal each jet port institute of artificial intelligence control Timing, level pressure, quantitative gas needed for the various required precise angles ejected, the safety for reaching 100% to landing aircraft rise Drop；

The shape chamber in jet runway valve body plate main body module sub-unit (73) inside casing, under interior lower outer portion jet runway pavement It is respectively equipped in the melt pit on portion basis；Normally with emergency and spare three sets independent manuals intelligence and can mutual numerical control switch The non-control system of new model of air supply system, power supply system, the various safety operation control systems of flight control system and safety is run in jet In road melt pit, it is respectively equipped with runway auxiliary equipment compressor air accumulator air supply system (189)；Current collecting tier gas storage cylinder air supply system (190)；On current collecting tier gas storage cylinder air supply system (190), the refrigeration, heating sensing modulator (207) that are equipped with；Low pressure is colored Gas and the preheating main gas ejection ports of oxygen (226), act on the Normal Take-Off And Landing that can guarantee on runway.The jet runway can be used as school Fly the pneumatic dynamic of various actual measurements of examination new architecture aircraft and the static state that various actual measurements are pneumatic, this runway is that the field is optimal One detection school flies equipment line, can reach 100% accurately actual measurement and goes out；By itself can be produced in jet runway it is various can To on extraneous landing aircraft environment runway pavement, can release various one hundred point than the oxygenation processed of different proportion, anoxic processed, refrigeration, Heating, making drugs into frostlike powder, system are avenged, are made ice, rain processed, manufacture cyclone, manufacturing the functions such as various random wind, can be flown to various coming of new factory Machine model-performance and the landing Test And Checkout of technical standard and various technical parameters on jet runway；

It is described in the shape chamber of jet runway valve body plate main body module sub-unit (73) interior frame bottom, be respectively equipped with inside and outside runway The right side intellectual air control switch of air curtain normal injection gas solenoid valve (227)；And the external right side air curtain normal injection gas in runway On the intellectual air control switch of body solenoid valve (227), it is equipped with the intellectual Regulation Control of external right side air curtain normal injection gas in runway Valve (228)；It is additionally provided with external right side air curtain emergency injection gas solenoid valve air control switch (229) in runway simultaneously；And in runway In external right side air curtain emergency injection gas solenoid valve air control switch (229), it is equipped with external right side air curtain emergency injection gas in runway Intellectual Regulation Control valve (230)；In runway external right side normally with the longitudinal defeated snorkel of emergency air curtain Universal-head jet port (231)；Longitudinally fork sliding sleeve (232) is stirred in defeated snorkel swing with left and right sides air curtain Universal-head jet port inside and outside runway, maximum Actual effect prevents bad interference of the runway external right side wind to Normal Take-Off And Landing of the landing aircraft in runway when；

It is described in the shape chamber of the interior frame bottom of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with race The inside and outside left side intellectual air control switch of air curtain normal injection gas solenoid valve (233) in road；And left side air curtain is normal inside and outside runway It sprays on the intellectual air control switch of gas solenoid valve (233), is equipped with the inside and outside left side intellectual tune of air curtain normal injection gas of runway Pressure control valve (234)；And it is additionally provided with the inside and outside left side air curtain emergency injection intellectual air control switch of gas solenoid valve of runway (235)；And the left side air curtain emergency injection intellectual air control switch of gas solenoid valve (on 235) inside and outside runway, it is equipped in runway The outer left side air curtain emergency injection intellectual Regulation Control valve (236) of gas；It is normally universal with emergency air curtain with left side inside and outside runway Longitudinally defeated snorkel (237), maximum actual effect are to prevent the outer left side wind of runway to landing aircraft in runway to head jet port The bad interference of left side wind outside the road landing Shi Dui；

It is described in the shape chamber of the interior frame bottom of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with race Communication far infrared and spectrum or Beidou intelligent sensing controller (238) are normally received in road, are received and are communicated far with emergency in runway It is infrared between spectrum or Beidou intelligent sensing controller (239), the navigation of three's far and near distance can mutually switch, and various Flying object cannot any, arbitrarily, freely rise and fall on jet runway, which has intelligence software to recognize it various flyers Receive function naturally after knowing difference, and to the global navigation locating function of mobile flyer, especially to various guided missiles Commit suiside unmanned plane or have it is man-machine attack, which can lead its various unacquainted various unmanned plane or someone's aircraft The flyers such as bullet quickly exclude to blow winged, effectively protect the great advantage of the safe normal operation of jet runway；

It is described in the shape chamber of the interior frame bottom of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with race Left and right sides and the green instruction lamp driver of middle left and right sides reddish yellow input six hole power sockets (240) inside and outside road, and coupled runway is right Reddish yellow green indicator light wiring conversion terminal (242) in side in the green indicator light wiring conversion terminal (241) of outside reddish yellow and the runway right side, And the green indicator light wiring conversion terminal (243) of the left side reddish yellow of runway and the green indicator light wiring of runway left-external side reddish yellow are transferred Terminal (244), maximum efficiency be can normal supply each group indicator light power supply, and night landing it is safer to pilot wake up Mesh；

It is described in the shape chamber of the interior frame bottom of each region valve body plate main body module sub-unit (73) of jet runway, be respectively equipped with spray Gas runway normally inputs four hole power sockets (245) with emergency air curtain electromagnetic valve circuit with emergency main jet port and normally, with runway Interior right outside is normally with emergency main jet port and normally and in each solenoid valve control connecting terminal (259) of emergency air curtain and runway It is normally normally led with emergency with left in each solenoid valve control wiring conversion terminal (260) of emergency main jet port and runway in the right side Each solenoid valve wiring conversion terminal (261) of puff prot, in runway left-external side normally with emergency main jet port and normally with gas of meeting an urgent need Each solenoid valve wiring conversion terminal (262) of curtain；Its maximum efficiency is to guarantee that each electric-controlled parts and electronic signal can have just it The control of normal safety standard；

It is described in the lower part shape chamber of each region valve body plate main body module sub-unit (73) bearing wall and frame structure of jet runway, respectively Equipped in runway normally with emergency gas receiver solenoid valve x far-infrared spectrum x Beidou x heat tracing line input five hole power sockets (246), and In runway normally with it is normal in emergency gas receiver solenoid valve x far-infrared spectrum x Beidou x heat tracing line connecting terminal (263) and runway With emergency gas receiver solenoid valve x far-infrared spectrum x Beidou x heat tracing line connecting terminal (264), maximum efficiency is to guarantee that gas source supplies Giving the accurate and ice and snow of navigation signal, combustion hot weather 100% can have a good normal temperature control intelligence to runway It can adjustment；

It is described in the lower part shape chamber of each region valve body plate main body module sub-unit (73) bearing wall and frame structure of jet runway, respectively It normally pushes the 1-2 servo motor of main injection port to input in four hole power sockets (247) and runway equipped with runway normally to push No. 1 servo motor of main jet port front and rear angles connects on 1-2 contact wiring conversion terminal (265), to control No. 1 servo motor A closed circuit and runway in normally push No. 2 servo motors of main injection port front and rear angles to meet the 1- on 4-5 contact 2-3 connects to be laid flat on wiring conversion terminal (266) in deflector, and for a closed circuit for controlling No. 2 servo motors, effect is true Protect the normal power supply of each servo motor；

It is described in the lower part shape chamber of each region valve body plate main body module sub-unit (73) bearing wall and frame structure of jet runway, respectively It pushes the 3-4 servo motor of main injection port to input in four hole power sockets (248) and runway equipped with runway emergency and answers hitch Dynamic No. 3 motors of main injection port front and rear angles connect on the wiring conversion terminal (267) of 1-2 contact, to control No. 3 servo motors A closed circuit and runway in emergency push No. 4 servo motors of main injection port front and rear angles to meet 1-2 point 3-4-5 and connect to lead On the wiring conversion terminal (278) that flowing plate erects, for a closed circuit for controlling No. 4 servo motors, effect ensures respectively to watch Take the control of the normal defeated power supply of motor；

It is described in the lower part shape chamber of each region valve body plate main body module sub-unit (73) bearing wall and frame structure of jet runway, respectively No. 1 servo motor is controlled equipped with main jet port front and rear angles normal in runway to input in four hole power sockets (249) and runway normally Main jet port front and rear angles control No. 1 servo motor wiring conversion terminal (268), before and after normal main jet port in control runway Angle pushes the closed circuit of No. 1 servo motor signal transducer, and normal main jet port front and rear angles control No. 2 servos in runway Motor inputs normal main jet port front and rear angles in four hole power sockets (256) and runway and controls No. 2 servo motor wiring change-over terminals Sub (269) control No. 4 servo motors with main jet port front and rear angles of meeting an urgent need in runway and input four hole power sockets (257), in runway Main jet port front and rear angles of meeting an urgent need control No. 4 motor wiring conversion terminals (277), main jet port front and rear angles control of meeting an urgent need in runway It makes No. 3 servo motors and inputs emergency main jet port front and rear angles No. 3 servo motors of control in four hole power sockets (250) and runway Wiring conversion terminal (270), effect are guarantee input power and various electronic signal sensors normal；

It is described in the lower part shape chamber of each region valve body plate main body module sub-unit (73) bearing wall and frame structure of jet runway, respectively Six hole power sockets (251) and runway are inputted close to No. 1 servo motor sensitive switch equipped with close or retrogressing is normally advanced in runway Interior normal close or retrogressing of advancing normally is advanced close to No. 1 servo motor sensitive switch wiring conversion terminal (271) in runway It is close or retreat inputted in six hole power sockets (255) and runway close to No. 2 servo motor sensitive switches normally advance it is close or after It moves back close to No. 2 servo motor sensitive switch wiring conversion terminals (272), and connects emergency in runway and advance close or retreat close to 3 Number servo motor sensitive switch inputs emergency in six hole power sockets (252) and runway and advances close or retreat close to No. 3 servo electricity Emergency is advanced close or is retreated close to No. 4 servo motor sensitive switches in machine sensitive switch wiring conversion terminal (273) and runway It inputs in six hole power sockets (254) and runway to meet an urgent need to advance to approach or retreat and transfer close to No. 4 servo motor sensitive switch wiring Terminal (274), effect ensure each puff prot angle of normal control of the power supply and intelligent signal of each servo motor；

It is described in the lower part shape chamber of each region valve body plate main body module sub-unit (73) bearing wall and frame structure of jet runway, respectively Four hole power sockets (253) are inputted equipped with connecing air compressor and connecing current collecting tier, and connects compressor and connects current collecting tier gas supply electromagnetic valve Wiring conversion terminal (275) under gas control, and connect compressor and connect wiring conversion terminal on current collecting tier gas supply electromagnetic valve gas control (276), maximum efficiency can guarantee the match control of the normal gentle source stream of power supply；

It is described in the lower part shape chamber of jet runway valve body plate main body module sub-unit (73) bearing wall and frame structure, be respectively equipped with pre- Road deflector erects input and is laid flat six hole power sockets (258) of input with pre- road deflector, before emergency pushes main jet port in runway No. 4 servo motors of angle meet 1-2 point 3-4-5 and connect on the wiring conversion terminal (278) of deflector standing afterwards, vertical for pre- road deflector An automatically controlled closed circuit and pre- road deflector erect input with pre- road deflector be laid flat input six hole power sockets (258), No. 2 servo motors of main injection port front and rear angles are normally pushed to connect on 4-5 contact in runway, 1-2-3 connects to be laid flat in deflector It is the automatically controlled closed circuit that pre- road deflector is laid flat on wiring conversion terminal (266) position；

It is described to be slided with efficient short distance or the dedicated jet runway of VTOL aircraft, in type aircraft carrier deck, naval vessel, the spray of land and water platform Gas runway device includes that type aircraft carrier deck is carrier-borne or first the dedicated jet runway (191) in each airport, runway region are to the 7th Region electromagnet cut off valve or pneumatic regulation whiff pressure graduated release valve (200)-(206), carrier-borne in type aircraft carrier deck or each airport is dedicated Slided on jet runway (191), equipped with carrier-borne aircraft the 60-80 rice long (197) into jet runway, on continental rise airfield runway, land On base sky body panel runway, land and water fix or mobile independent air bags platform runway on, naval vessel ship side left or right side or stern end On portion's extension type air bag platform runway, the jet runway of the multi-purpose landing aircraft of sea Lu Pingtai is constituted.

13. platform jet runway according to claim 2, it is characterized in that：It is described to use a variety of gas supply gas sources, it is empty by compression Gas gas injection formed the short distance of gas laminar flow slide or VTOL aircraft or the dedicated each region of jet runway of unmanned plane on, if There is type aircraft carrier deck carrier-borne or each dedicated jet runway (191) in airport；Type aircraft carrier deck is carrier-borne or each dedicated jet runway in airport (191) on, it is respectively equipped with that seven 20 meters long, 140 meters × 30 meters of overall length wide or 40 meters of wide type aircraft carrier decks are carrier-borne or each airport is special With jet runway, the jet runway of the multi-purpose landing aircrafts such as airport, the land and water platform in various environment areas also may make up；

It is described when carrier-borne aircraft is when taking off, when carrier-borne aircraft is slided into 20 meters long (192) of jet runway；The carrier-borne aircraft that takes off slides When into 40 meters long (193) of jet runway；When the carrier-borne aircraft that takes off is slided into 60 meters long (194) of jet runway；Take off warship When carrier aircraft is slided into 80 meters long (195) of jet runway；At this moment the carrier-borne aircraft that takes off is carrier-borne or each airport is dedicated in type aircraft carrier deck On jet runway (191), constitutes and be detached from the outstanding support of the gas of dedicated jet runway and jet runway when second-mission aircraft takes off By departing aeroplane accelerate to nature flying speed and height, realize departing aeroplane safely and fast naturally flight, constitute The lift-off of quickly taking off of jet runway paving take-off-helping aircraft；

It is described in carrier landing landing, be first when carrier-borne aircraft is slided into 20-40 rice long (196) of jet runway The film grade laminar gas at a 45 degree of angles blocks landing, warship carrier-borne aircraft when sliding into 60-80 rice long (197) of jet runway, Constituted the film grade laminar flow at second 45 degree of angle that carrier-borne aircraft blocks, at this moment warship carrier-borne aircraft continue to slide into jet runway When 100-120 meters long (198), the film grade laminar gas for having constituted third 45 degree of angles blocks landing, warship carrier-borne aircraft in aircraft carrier Deck is carrier-borne or each dedicated jet runway (191) in airport on, constituted various airport aircrafts or ship-board aircraft in warship landing It slides and enters on 140 meters long (199) on jet runway, realize the outstanding support formula of the naturally stable gas of safety and block landing, structure The outstanding support of gas when landing aircraft is helped at jet runway paving or is blocked；

It is described type aircraft carrier deck is carrier-borne or each dedicated jet runway (191) in airport on, be respectively equipped with first region electromagnetism of runway Shut-off valve or pneumatic regulation whiff pressure alleviate valve assembly (200), runway Two Areas electromagnet cut off valve or pneumatic regulation spray Atmospheric pressure alleviates valve assembly (201), runway third region electromagnet cut off valve or pneumatic regulation whiff pressure and alleviates valve assembly (202), the 4th region electromagnet cut off valve of runway or pneumatic regulation whiff pressure alleviate the 5th valve assembly (203), runway area Domain electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly (204), the 6th region electromagnet cut off valve of runway or pneumatic Regulate and control whiff pressure and alleviates valve assembly (205), the 7th region electromagnet cut off valve of runway or pneumatic regulation whiff pressure graduated release valve Assembly (206) is constituted to carrier-borne or each airport seven region electromagnet cut off valve of dedicated jet runway or pneumatic regulation and air pressure quilt The safety distribution manipulation of constant pressure after alleviation；

The aircraft is when taking off, the auto-control situation of change of each region atmospheric pressure of runway：When departing aeroplane is slided to first When a area, valve assembly (200) are alleviated by first region electromagnet cut off valve or pneumatic regulation whiff pressure, first region is whole The air pressure of body gas source is adjusted to 2-3 technical atmosphere；When departing aeroplane is slided to second area, by Two Areas electromagnetism Shut-off valve or pneumatic regulation whiff pressure alleviate valve assembly (201), and the air pressure of second region entirety gas source is adjusted to 3-4 A technical atmosphere；When departing aeroplane is slided to third area, by third region electromagnet cut off valve or pneumatic regulation jet pressure Power alleviates valve assembly (202), and the air pressure of third region entirety gas source is adjusted to 4-5 technical atmosphere；Work as departing aeroplane When sliding to the 4th area, valve assembly (203) are alleviated by the 4th region electromagnet cut off valve or pneumatic regulation whiff pressure, by the The air pressure of four region entirety gas sources is adjusted to 5-6 technical atmosphere；When departing aeroplane is slided to the 5th area, by the 5th A region electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly (204), by the gas of the 5th region entirety gas source Pressure is adjusted to 6-7 technical atmosphere；When departing aeroplane is slided to the 6th area, by the 6th region electromagnet cut off valve or pneumatic Regulate and control whiff pressure and alleviate valve assembly (205), the air pressure of the 6th region entirety gas source is adjusted to 7-8 technical atmosphere； When departing aeroplane is slided to the 7th area, the 7th region electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly (206), the air pressure of the 7th region entirety gas source is adjusted to 8-10 technical atmosphere, constitutes carrier-borne aircraft on jet runway When taking off, seven region entirety gas sources on runway alleviated after air pressure, protect forever the distribution pressure constancy in each region by Artificial intelligence regulation.Used on jet runway 10-25 technical atmosphere to take off carrier-borne aircraft when operating condition various controls, structure It boards a plane at jet runway when taking off, the air pressure in each region is incremental；

The aircraft is when warship lands, the auto-control situation of change of each region atmospheric pressure of runway：When landing aircraft taxi extremely When first region, valve assembly (200) are alleviated by first region electromagnet cut off valve or pneumatic regulation whiff pressure, by first The air pressure of region entirety gas source is adjusted to 8-10 technical atmosphere；When land aircraft taxi to Two Areas when, by second A region electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly (201), by the gas of second region entirety gas source Pressure is adjusted to 7-8 technical atmosphere；When land aircraft taxi to third region when, by third region electromagnet cut off valve or gas Dynamic regulation whiff pressure alleviates valve assembly (202), and the air pressure of third region entirety gas source is adjusted to 6-7 engineering gas Pressure；When land aircraft taxi to the 4th region when, alleviated by the 4th region electromagnet cut off valve or pneumatic regulation whiff pressure The air pressure of 4th region entirety gas source is adjusted to 5-6 technical atmosphere by valve assembly (203)；When landing aircraft taxi extremely When the 5th region, valve assembly (204) are alleviated by the 5th region electromagnet cut off valve or pneumatic regulation whiff pressure, by the 5th The air pressure of region entirety gas source is adjusted to 4-5 technical atmosphere；When land aircraft taxi to the 6th region when, by the 6th Region electromagnet cut off valve or pneumatic regulation whiff pressure alleviate valve assembly (205), by the air pressure of the 6th region entirety gas source It is adjusted to 3-4 technical atmosphere；When land aircraft taxi to the 7th area Ge Yu when, by the 7th region electromagnet cut off valve or pneumatic Regulate and control whiff pressure and alleviate valve assembly (206), the air pressure of the 7th region entirety gas source is adjusted to 2-3 technical atmosphere, Constitute to it is carrier-borne on jet runway warship when runway on seven region entirety gas sources distribution pressure；It is adopted on jet runway Operating condition when with 10-25 technical atmosphere constitutes the air pressure in each region in landing of boarding a plane of jet runway and successively decreases.

Before and after each puff prot in each region on jet runway longitudinal direction, it is all respectively equipped with low pressure colored gas and pre- The hot main gas ejection ports of oxygen (226) are constituted to each injection gas laminar flow of adjustment each region high pressure spray loophole of jet runway The actual height of ray, with angle can vision whether reach within the scope of the various Aircraft Standards of landing.