CN104229153A - Automatic acceleration and deceleration sloping runway for aircraft carrier - Google Patents
Automatic acceleration and deceleration sloping runway for aircraft carrier Download PDFInfo
- Publication number
- CN104229153A CN104229153A CN201310253910.6A CN201310253910A CN104229153A CN 104229153 A CN104229153 A CN 104229153A CN 201310253910 A CN201310253910 A CN 201310253910A CN 104229153 A CN104229153 A CN 104229153A
- Authority
- CN
- China
- Prior art keywords
- runway
- aircraft
- deck
- sloping
- aircraft carrier
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000001133 acceleration Effects 0.000 title abstract 2
- 238000010276 construction Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 description 5
- 230000000979 retarding effect Effects 0.000 description 5
- IWEDIXLBFLAXBO-UHFFFAOYSA-N dicamba Chemical compound COC1=C(Cl)C=CC(Cl)=C1C(O)=O IWEDIXLBFLAXBO-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229920000136 polysorbate Polymers 0.000 description 2
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 230000006855 networking Effects 0.000 description 1
Landscapes
- Road Paving Structures (AREA)
- Traffic Control Systems (AREA)
Abstract
An automatic acceleration and deceleration sloping runway for an aircraft carrier is characterized in that a sloping runway and a runway vessel are connected in order behind a deck of the aircraft carrier, the deck is connected to the upper section of sloping runway, the runway vessel is connected to the lower section of the sloping runway, and the sloping runway is Z shaped. The sloping runway plays a role mainly; during takeoff of an aircraft, the aircraft can automatically accelerate just by moving from the deck to an warping takeoff segment of the runway vessel; during landing, the aircraft is not directly landed on the deck but landed on the runway vessel at the low position and automatically decelerates through a slope; the takeoff and landing distance is automatically shortened. As to the construction of the runway, a land airport test is recommended to be performed before the runway is applied to the aircraft carrier; the runway is also applicable to variously sized airports on lands, mountainous areas and isles.
Description
Art
The present invention relates to and be a kind ofly added in the automatic acceleration-deceleration abrupt slope runway that aircraft carrier also can be used on land, especially not needing to add brake appts just can automatic retarding, and shorten and shut down distance, not adding ejector can accelerate automatically, energy short field take-off.
Background technology
Present aircraft lands as allowing aircraft stop as early as possible on aircraft carrier, employing cable wire draws, for improving takeoff speed just with ejector, but the shortcoming one of these methods is that aviator is in distance landing short like this, inertia large is like this difficult to adapt to, two is just in case cable wire is out of joint, aircraft will pour sea, just in case ejector is out of joint, aircraft does not rise and flies, be exactly burden in wartime, separately that aircraft lands on airfield, stop as early as possible for allowing those military fast aircrafts, below also in tow one, two parachutes, this method that parachute can be adopted to drag is shut down apart from still long especially, various places home airdrome just can only solve with adding long runway for welcoming large aircraft.Existing straight runway is not suitable for mountain area and island builds airport.The landing distance of aircraft be no matter on aircraft carrier or airfield landing distance more short safer.Present aircraft is made larger and larger, also more and more faster, and manufacturing technology is also more and more advanced, and just shutdown technology does not still catch up with far away in original place.
Summary of the invention
For solve the landing on the aircraft carrier of limited area of large fast aircraft difficult and on land the short and difficult problem for the large fast aircraft that cannot land of medium and small airfield runway.The invention provides a kind of acceleration-deceleration abrupt slope runway automatically; aircraft landing on this new abrupt slope runway can be accelerated and automatic retarding automatically; the method is used on aircraft carrier; both dragged without cable wire when can allow on this runway of aircraft landing and just can stop very soon; greatly shorten and shut down distance; can not add ejector when taking off again just can automatically raise speed; take off in very short distance; the runway in this way built is short especially, and each medium and small airfield reconstruction becomes this runway also can to land large fast aircraft on land.
The technical solution adopted for the present invention to solve the technical problems is: the abrupt slope runway building an automatic acceleration-deceleration of energy at the rear portion of aircraft carrier, company's type aircraft carrier deck that this runway is high, low one connects the runway ship floated on the surface, centre is one section of abrupt slope road, whole runway becomes Yi shape, the section of taking off of runway ship is tilted upward, and regulate and control to take off trend.Aircraft all when taking off and land will firmly raise speed and slow down.The ultromotivity that this runway produces utilizes terrestrial attraction, the namely weight of aircraft itself exactly.The condition manufacturing this power is exactly the height of type aircraft carrier deck to sea.As shown in Figure 2, aircraft puts into high gear when type aircraft carrier deck is taken off, after arriving lower slope section, under terrestrial attraction effect, two power are unified, the speed of aircraft is run faster and faster, when arrive runway ship upwarp the section of taking off time, aircraft has just had enough takeoff speeds, without ejector, also can realize short field take-off.When aircraft landing, can not directly fall above deck, fall on lower runway ship, on runway ship, aircraft is only walked a bit of level road and is just entered upward slope section, under gravitational effect, the speed goes of aircraft is slow, aircraft does not just have much inertia to during type aircraft carrier deck, can stop voluntarily, landing notice: 1, aircraft can not drop on slope, in case form head-on collision.2, can not shutting down on slope, as shut down on abrupt slope, can fall back.This will aviator oneself control, and method is in the switch of throttle and brake, and be separately that type aircraft carrier deck can with double-deck, last layer reaches helicopter, also can add one section of movable runway as shown in Figure 9, reaches and carries a fighter plane.
The invention has the beneficial effects as follows: 1, aircraft takes off on aircraft carrier does not need, with ejector, can automatically raise speed, and reaches short range lift-off.2, do not draw with cable wire during aircraft landing, can automatic retarding, realize short range and shut down.3, opportunity of combat lift-off is fast, and aircrafts all on aircraft carrier can be almost take off in tens seconds simultaneously, can increase and get the time.Although 4, takeoff and landing distance is very short, because this inertia utilizes terrestrial attraction to overcome, so can not because inertia brings injury as automobile emergency brake to people and aircraft.5, safe and reliable, there is no contingency.6, this abrupt slope shape runway is applicable equally at airfield, and various large fast aircraft can be allowed everywhere can to fall on medium and small airport, facilitate passenger, can produce economic benefit again, namely present said aviation economy, medium and small airport also can communicate with the networking of global airport.As needed to land nearby at wartime military aircraft, there is the middle-size and small-size airport of this abrupt slope runway can fall everywhere, can bring convenience.7, because not needing the just energy landing of oversize runway aircraft, Mountainous region and island all can build airport.8, fuel-economizing.9, owing to deck not being stayed runway just can nearly carry some aircrafts.10, double deck can be done and reach a year more aircraft.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the present invention is further described
In figure 1, sea, 2, sea to altitude above deck, 3, pipe link, 4, runway ship, 5, the section of taking off is upwarped, 6, landing section, 7, steep slope section, 8, lower floor's point of connection, 9, upper strata movable runway, 10, signal runway slings, 11, upper strata movable runway point of connection, 12, aircraft carrier promenade deck, 13, aircraft carrier lower tween deck
Accompanying drawing schematic illustration
This figure is an automatic lifting stick principle schematic, mainly illustrate and utilize sea this highly manufactures an abrupt slope runway to type aircraft carrier deck, allow aircraft take off above deck to go down hill and automatically accelerate, not directly fall in type aircraft carrier deck during landing, but drop on the runway ship below aircraft carrier, by raise automatic retarding.
Detailed description of the invention
In this figure embodiment; runway ship 4, pipe link 3, steep slope section 7; lower floor's point of connection 8 is connected with aircraft carrier; steep slope section 7 is entered once a few section level line when aircraft landing is only walked in the landing section 6 of runway ship; aircraft carrier promenade deck 12 is arrived in conjunction with brake; now airplane inertial disappears automatically, realizes short range auto-stop.As promenade deck aircraft is fully parked with, sling by upper strata movable runway, as shown in Figure 10, the aircraft at this moment dropped on the runway ship of below just can change its course and enter aircraft carrier lower tween deck 13, equally can auto-stop.Here it is walks upward slope energy automatic retarding.The section of taking off that upwarps of putting into high gear when taking off to rush at runway ship from deck downwards along steep slope section 7 is accelerated to take off automatically, the order that takes off of levels deck aircraft is identical with the method for landing, mainly upper strata movable runway is sling, put down allowing the aircraft of levels can landing on same runway.
Claims (1)
1. an aircraft carrier automatic acceleration-deceleration abrupt slope runway, at the rear portion of type aircraft carrier deck, abrupt slope runway, runway ship be linked in sequence, and it is characterized in that: above runway, one connects type aircraft carrier deck, below one be connected with runway ship, centre is one section of abrupt slope, and whole runway circuit becomes Yi shape.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310253910.6A CN104229153A (en) | 2013-06-12 | 2013-06-12 | Automatic acceleration and deceleration sloping runway for aircraft carrier |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310253910.6A CN104229153A (en) | 2013-06-12 | 2013-06-12 | Automatic acceleration and deceleration sloping runway for aircraft carrier |
Publications (1)
Publication Number | Publication Date |
---|---|
CN104229153A true CN104229153A (en) | 2014-12-24 |
Family
ID=52218234
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201310253910.6A Pending CN104229153A (en) | 2013-06-12 | 2013-06-12 | Automatic acceleration and deceleration sloping runway for aircraft carrier |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN104229153A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104963251A (en) * | 2015-07-03 | 2015-10-07 | 贡茅 | Runway and hangar integrated mushroom umbrella type slope airport |
CN113320668A (en) * | 2021-07-02 | 2021-08-31 | 易志勇 | Scale anchor chain type combined catamaran aircraft carrier and using method thereof |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1557678A (en) * | 2004-02-10 | 2004-12-29 | 通 刘 | Airplane inertial taking off and landing technology |
US20090200421A1 (en) * | 2006-08-08 | 2009-08-13 | Vinayak Virkar | Efficient airport runway management system |
CN202345921U (en) * | 2011-10-13 | 2012-07-25 | 王力丰 | Shipboard aircraft lifting system for aircraft carrier |
CN102826231A (en) * | 2012-08-31 | 2012-12-19 | 赵天烁 | Slope downward-sliding takeoff platform for carrier-based aircraft, application aircraft carrier and realization method |
-
2013
- 2013-06-12 CN CN201310253910.6A patent/CN104229153A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1557678A (en) * | 2004-02-10 | 2004-12-29 | 通 刘 | Airplane inertial taking off and landing technology |
US20090200421A1 (en) * | 2006-08-08 | 2009-08-13 | Vinayak Virkar | Efficient airport runway management system |
CN202345921U (en) * | 2011-10-13 | 2012-07-25 | 王力丰 | Shipboard aircraft lifting system for aircraft carrier |
CN102826231A (en) * | 2012-08-31 | 2012-12-19 | 赵天烁 | Slope downward-sliding takeoff platform for carrier-based aircraft, application aircraft carrier and realization method |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104963251A (en) * | 2015-07-03 | 2015-10-07 | 贡茅 | Runway and hangar integrated mushroom umbrella type slope airport |
CN113320668A (en) * | 2021-07-02 | 2021-08-31 | 易志勇 | Scale anchor chain type combined catamaran aircraft carrier and using method thereof |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN111356633A (en) | Tram system and method for autonomous take-off and landing of aircraft | |
CN106379552B (en) | The retractable method of small UAV based on tethered balloon | |
CN105867413B (en) | A kind of parachuting unmanned plane voluntary recall method | |
CN103224031B (en) | Fixed Wing AirVehicle landing gear | |
CN107161354A (en) | A kind of high aspect ratio solar energy unmanned plane is without undercarriage landing system | |
CN105564663A (en) | Airplane suspension type full-automatic take-off and landing system and take-off and landing method | |
CN106228500A (en) | Airplane intelligent automatic braking method and system based on data sharing | |
CN101256410B (en) | A method for transitioning flight phases of unmanned aerial vehicles | |
CN104229153A (en) | Automatic acceleration and deceleration sloping runway for aircraft carrier | |
US1706065A (en) | Airplane-launching gear | |
CN116198737A (en) | Automatic collection system of temporary airport emergency navigation light unmanned aerial vehicle | |
CN104210669A (en) | Plane takeoff mode and device | |
CN110733664A (en) | seaplane takeoff performance verification method | |
CN102363447A (en) | Method for reducing sliding distance of airplane during landing and taking off | |
RU2111896C1 (en) | Polyfuselage seaplane | |
CN204737021U (en) | Solar energy dirigible of double dynamical dual fail -safe | |
JP2005138641A (en) | Transportation facilities | |
CN205524983U (en) | Push -button aircraft system | |
Ragauskas et al. | Research of remotely piloted vehicles for cargo transportation | |
RU2406652C2 (en) | Vtol aircraft | |
CN104890850A (en) | Dual-power dual-insurance solar airship | |
CN105752351A (en) | Auxiliary device for safe landing of aircraft and safe landing method | |
Fujiwara et al. | Flight plan and flight test results of experimental SST vehicle NEXST-1 | |
CN101088864B (en) | Flying squirrel simulating flyer | |
US11649069B2 (en) | Airport capable of saving energy and resources and improving take-off and landing safety of airplane |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WD01 | Invention patent application deemed withdrawn after publication | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20141224 |