CN104002972A - Triple warship submarine airplane - Google Patents
Triple warship submarine airplane Download PDFInfo
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- CN104002972A CN104002972A CN201310057260.8A CN201310057260A CN104002972A CN 104002972 A CN104002972 A CN 104002972A CN 201310057260 A CN201310057260 A CN 201310057260A CN 104002972 A CN104002972 A CN 104002972A
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Abstract
A triple warship submarine airplane integrates an airplane, a warship and a submarine, has the main functions of a modern jet-propelled airplane, and can realize flexible triphibian transition according to future effect demands in order to realize taking-off and landing from/on platforms comprising land, aircraft carrier, ice surface, water surface, snow surface, desert and the like and the maneuvering of trains, lorries, amphibious landing ships, pleasure boats, ro-ro passenger ships, fishing vessel group chains, deepwater drag boxes and simple ships, so technical requirements of airplane taking-off and landing platforms are reduced, the airplane action space and the maneuvering transfer efficiency, thereby the survivability, the objective environment adaptability and the practicability of the airplane are improved.
Description
Technical field
The present invention relates to aircraft, naval vessel and Submarine manufacture field, be specifically related to trisome warship submarine aircraft.
Background technology
Known modern jet plane core component turbojet engine, in the time that it turns round, temperature can reach hundreds of degree, if contact suddenly afterwards ice face, snow face, the water surface or pull the plug etc. in flight, can cause the temperature of turbojet engine sharply to decline, easily bring out blast, if turbojet engine is subject to other factor impacts, thrust, than declining and stopping, also will have influence on normally taking off and safe flight of aircraft greatly.Therefore, jet plane requires extremely strict to take-off and landing platform, take-off and landing natural conditions, the objective space of take-off and landing etc., is difficult to form the conversion of dwelling of three between aircraft, surface vessel and submarine; Be difficult to the take-off and landing under the adverse weather conditions such as ice face, the water surface, snow face and desert; The motor-driven of the platforms such as train, truck, amphibious landing warship, pleasure boat, ro-ro passenger ship, fishing boat group chain and simple and easy naval vessel can not be completed, submarine formula can not be completed motor-driven.So the action space in aircraft future is extremely restricted, this defect is never had to advanced technical scheme and solve.
Summary of the invention
The defect existing in order to solve above-mentioned aircraft, expand the following action space of aircraft, applicant is through research for many years, trisome warship submarine aircraft is designed in invention, collection aircraft, naval vessel and submarine are integrated, except having the radical function of modern jet plane, according to the demand that the act on future conversion of can flexible three dwelling, can complete land, aircraft carrier, ice face, the water surface, the take-off and landing of the kinds of platform such as snow face and desert, can complete aerial, the water surface and submarine navigation, can complete train, truck, amphibious landing warship, pleasure boat, ro-ro passenger ship, fishing boat group chain, deep water drags the motor-driven etc. of the platform such as case and simple and easy naval vessel.
In order to achieve the above object, the present invention realizes with following technical proposals: establish flat prismatic head, flat prismatic head is connected with cockpit enclosure, head triangular groove ditch is connected with flat prismatic head, right head wing is connected with flat prismatic head right side, left head wing is connected with flat prismatic head left side, flat prismatic head is connected with body slip-knot, air inlet culvert is connected with the front upper end of body, left flexible air inlet dustpan is connected with air inlet culvert left side, right flexible air inlet dustpan is connected with air inlet culvert right side, air storage cabin, loop culvert, air insulated band is connected with body air inlet culvert with foreign material escape orifice, the left semicircle that connects successively below of the air inlet culvert of body upper comes down, Left Hand Engine culvert shell, right driving engine culvert shell and right semicircle landslide, right naval vessels actuator is adsorbed on right semicircle landslide by folded sheet, left naval vessels actuator is adsorbed on left semicircle landslide by folded sheet, left large arm wing is connected with left naval vessels actuator, right large arm wing is connected with right naval vessels actuator, left winglet, left large wing is connected with left large arm wing by left wing turning joint from front to back successively with left back wing, upper rudder wing is connected with middle part on body rear end, underpart connects cabin, right side from right to left successively, trim of the right end, trim of the left end and cabin, left side, right engine nozzle is connected with right driving engine culvert shell tail end, Left Hand Engine spout is connected with Left Hand Engine culvert shell tail end, if the left air film lid of head is connected below with flat prismatic head left side, flush cabin top of the left end is connected with trim of the left end, trim air film capsule of the left end is connected with flush cabin top of the left end, trim air film lid of the left end is connected with trim air film capsule of the left end and flush cabin top of the left end respectively, if Multifunctional cabin is connected with front end in body, Left Hand Engine culvert is connected with Left Hand Engine culvert shell, Left Hand Engine sliding rail is connected with Left Hand Engine culvert, Left Hand Engine is connected with Left Hand Engine culvert track, left cooling and insulating gagger umbrella is connected with Left Hand Engine and Left Hand Engine culvert respectively, mushroom is connected with Left Hand Engine culvert tail end the sealing of Left Hand Engine culvert, before left mushroom, umbrella frame is connected with Left Hand Engine culvert and left mushroom liquid capsule pocket respectively, after left mushroom, umbrella frame is connected with Left Hand Engine culvert and left mushroom liquid capsule pocket respectively, left mushroom liquid capsule pocket respectively with left mushroom before umbrella frame, after left mushroom, umbrella frame is connected with Left Hand Engine culvert.Right back folded sheet is connected with body right side, right front folded sheet is connected with right back folded sheet, left back folded sheet is connected with body left side, left front folded sheet is connected with left back folded sheet, right naval vessels actuator is connected with right front folded sheet, left naval vessels actuator is connected with left front folded sheet, left large arm wing is connected with left naval vessels actuator, right large arm wing is connected with right naval vessels actuator, the left air film lid of head is connected with flat prismatic head left side, the left air film capsule of head is connected with the left air film lid of head and flat prismatic head left side respectively, the right air film lid of head is connected with flat prismatic head right side, the right air film capsule of head is connected with the right air film lid of head and flat prismatic head right side respectively, right side hatchcover is connected with cabin, right side, flush cabin top of the right end is connected with trim of the right end, left side hatchcover is connected with cabin, left side, cabin, right side air film lid is connected with right side hatchcover, cabin, right side air film capsule is connected with right side hatchcover and cabin, right side air film lid respectively, trim air film lid of the right end is connected with flush cabin top of the right end, trim air film capsule of the right end is connected with trim air film lid of the right end and flush cabin top of the right end respectively, cabin, left side air film lid is connected with left side hatchcover, cabin, left side air film capsule is connected with cabin, left side air film lid and left side hatchcover respectively, if left front screw propeller is connected with left naval vessels actuator front end, right front screw propeller is connected with right naval vessels actuator front end, lower rudder wing is connected with body rear end middle and lower part, left back screw propeller is connected with left naval vessels actuator rear end, right back screw propeller is connected with right naval vessels actuator rear end, right driving engine culvert sealing mushroom is connected with right driving engine culvert shell tail end, mushroom is connected with Left Hand Engine culvert tail end the sealing of Left Hand Engine culvert, dustpan type activity surfboard is connected with body tail end, if front axle is connected with left front screw propeller and front electrical motor, rear axle is connected with left back screw propeller and rear electrical motor, front stretching air sac sealing ring is connected with left naval vessels actuator outer cylinder front end inwall, rear extension airbag seal ring is connected with the outer tube rear end inwall of left naval vessels actuator, sliding nail is connected with left naval vessels actuator urceolus two ends inwall, spud pile is connected with left naval vessels actuator urceolus middle part inwall, front slide cartridge is connected with sliding nail in left naval vessels actuator is anterior, front electrical motor is connected with front slide cartridge, rear slide cartridge is connected with sliding nail in left naval vessels actuator rear portion, middle slide cartridge is fixed after stake is fixed and is connected with front slide cartridge and rear slide cartridge respectively, electrical motor before front push rod connects, electrical motor after rear push rod connects, Hydraulic Pump connects respectively front push rod and rear push rod, front seal ring air inlet/outlet is connected with front stretching air sac sealing ring, increasing back sealing ring air inlet/outlet is connected with rear extension airbag seal ring, urceolus induction opening is connected with left naval vessels actuator urceolus, inner core induction opening is connected with middle slide cartridge, liquid manhole appendix is connected with Hydraulic Pump.Right winglet, right large wing and right back wing are connected with right large arm wing from front to back successively by right wing turning joint.Front high-mobility, multipurpose, wheeled vehicle landing gear compartment is connected with flat prismatic head tail end middle part, and rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment is connected with left side, underpart rear end, and rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment is connected with right side, underpart rear end, and lower rudder wing cabin is connected with body rear end middle part.
Trisome warship submarine aircraft operation and three conversion program of dwelling:
Trisome warship submarine aircraft enters airflight, for chaufeur enters in flat prismatic head driving compartment, close cockpit enclosure, from raising up of flat prismatic head, in straight, nutation, straight in selecting in five kinds of situation of left avertence and right avertence, flat prismatic head is adjusted at 0 of body and spends position, angle, accomplish that in head triangular fovea groove and body, seam forms straight line, shrink right driving engine culvert sealing mushroom and Left Hand Engine culvert sealing mushroom, promote backward left and right driving engine by left and right driving engine culvert track, meanwhile draw left and right cooling and insulating gagger umbrella in, after right engine nozzle and Left Hand Engine spout kickoff mechanism are external, start and preheating left and right driving engine, tighten up right front folded sheet, right back folded sheet, left front folded sheet, left back folded sheet, right naval vessels actuator is adsorbed on right semicircle landslide, left naval vessels actuator is adsorbed on left semicircle landslide, launch right head wing and left head wing, launch right large arm wing and left large arm wing, by right wing turning joint and left wing turning joint, launch successively left winglet, right winglet, left large wing, right large wing, right back wing and left back wing, adjust curved surface and the loop culvert of air inlet culvert, make the curved surface of air inlet culvert become pneumatic domatic with Left Hand Engine culvert shell with right driving engine culvert hull shape, release left flexible air inlet dustpan and right flexible air inlet dustpan, shrink the left air film capsule of head and the right air film capsule of head, close the left air film lid of head and the right air film lid of head, shrink cabin, right side air film capsule, cabin, right side air film lid and right side hatchcover is next to the skin closes cabin, right side after uniting two into one, shrink trim air film capsule of the right end, after trim air film lid of the right end and next to the skin the uniting two into one of flush cabin top of the right end, close trim of the right end, shrink trim air film capsule of the left end, after trim air film lid of the left end and next to the skin the uniting two into one of flush cabin top of the left end, close trim of the left end, shrink cabin, left side air film capsule, left side cabin air film lid close after uniting two into one with left side hatchcover is next to the skin on the left of cabin, in adjustment, rudder wing is to proper orientation, strengthen left and right engine throttle, promoting trisome warship submarine aircraft runs to takeoff speed along airfield runway fast slide, flat prismatic head raises up, adjust right head wing, left head wing, left winglet, right winglet, left large wing, right large wing, right back wing and left back aliform state, open left and right driving engine assistor, promoting trisome warship submarine aircraft goes up to the air fast, in lift-off process, front high-mobility, multipurpose, wheeled vehicle landing gear compartment, rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment and rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment are sequentially packed up land wheel undercarriage, when trisome warship submarine aircraft arrives after certain altitude, straight 0 degree position during flat prismatic head is returned to, simultaneously, again adjust right head wing, left head wing, left winglet, right winglet, left large wing, right large wing, right back wing and left back aliform state, trisome warship submarine aircraft enters orthodox flight state.
Trisome warship submarine aircraft proceeds to surface vessel navigation from state of flight, for trisome warship submarine aircraft drops to after certain altitude, open the left air film lid of head, the right air film lid of head, cabin, right side air film lid, trim air film lid of the right end, trim air film lid of the left end and cabin, left side air film lid, by Multifunctional cabin to the left air film capsule of head, the right air film capsule of head, cabin, right side air film capsule, trim air film capsule of the right end, trim air film capsule of the left end and the inflation of cabin, left side air film capsule, after air film capsule inflation is combined as bottom, naval vessel, close left and right driving engine, by left and right driving engine culvert track, left and right driving engine is retracted to culvert, when driving engine is pulled back, drive and open left and right cooling and insulating gagger umbrella, form culvert Insulative umbrella, the special liquid that umbrella frame hollow circulation path provides by Multifunctional cabin absorbs heat, driving engine culvert sealing mushroom and Left Hand Engine culvert seal mushroom high-pressure delivery special liquid to Multifunctional cabin to the right simultaneously, mushroom liquid capsule pocket rapid expanding under the pressure of special liquid, squeeze before the mushroom of left and right umbrella frame after umbrella frame and left and right mushroom, the special liquid that Multifunctional cabin provides circulates in umbrella frame hollow circulation path, right driving engine culvert sealing mushroom and Left Hand Engine culvert sealing mushroom sealing left and right driving engine culvert mouth, adjust curved surface and the loop culvert of air inlet culvert, make the curved surface of air inlet culvert become wind sheltering domatic with Left Hand Engine culvert shell with right driving engine culvert hull shape, retract left flexible air inlet dustpan and right flexible air inlet dustpan, sealing admission port, in this, trisome warship submarine aircraft becomes the free parallel glide of aerodone pattern and progressively declines, trisome warship submarine aircraft is in glide decline process, progressively launch right front folded sheet and left front folded sheet, drive right naval vessels actuator to leave right semicircle landslide, drive left naval vessels actuator to leave left semicircle landslide, about point, drawing semicircle by body upper to underpart changes, simultaneously, constantly adjust right large arm wing, left large arm wing, left winglet, right winglet, left large wing, right large wing, right back wing and left back wing are with the angle of naval vessels actuator, make right large arm wing, left large arm wing, left winglet, right winglet, left large wing, right large wing, right back wing and left back wing keep horizontal parastate, reduce to greatest extent the descending speed of trisome warship submarine aircraft, right front folded sheet and left front folded sheet drive respectively left naval vessels actuator and right naval vessels actuator to move to along body both sides behind position, to stop vertically downward, right large arm wing, left large arm wing, left winglet, right winglet, left large wing, right large wing, right back wing vertically draws in to upper machine body in contacting the low vacancy of the water surface fast with left back wing, after submerging in water, laterally parallel opening becomes naval vessel flank again, naval vessels actuator is drawn in semicircle change process to underpart by body upper in point left and right, pass through liquid manhole appendix to Hydraulic Pump pumping liquid by Multifunctional cabin, promote front push rod and rear push rod moves to two ends, thereby promote front electrical motor and rear electrical motor moves, the middle slide cartridge on spud pile and sliding nail rail groove move to two ends along riveting to drive front slide cartridge and rear slide cartridge, front electrical motor and rear electrical motor move, promoting front axle and rear axle moves, front axle and rear axle move, respectively by left front screw propeller, right front screw propeller, left back screw propeller and right back screw propeller are released outside actuator two ends, then, Multifunctional cabin is by front seal ring air inlet/outlet, increasing back sealing ring air inlet/outlet, urceolus air inlet/outlet and inner core air inlet/outlet, extension airbag seal ring forward, rear extension airbag seal ring and the inflation of naval vessels actuator cylinder inner high voltage, front stretching air sac sealing ring and rear extension airbag seal ring seal naval vessels actuator two ends, naval vessels actuator cylinder is full of high pressure air and produces certain buoyancy, form the both sides hull of trisome warship submarine aircraft naval vessel situation, when trisome warship submarine aircraft approaches the water surface, flat prismatic head is kept to the state that raises up, trisome warship submarine aircraft falls into after the water surface, left naval vessels actuator and right naval vessels actuator submerge below horizon, rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment and rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment are released dustpan type activity surfboard jointly, open lower rudder wing cabin, adjust lower rudder aliform state, actuating motor drives screw propeller rotation, promote trisome warship submarine aircraft navigates by water on the water surface.
Trisome warship submarine aircraft is converted to submarine deep water by surface navigation and navigates by water, and for trisome warship submarine aircraft is in surface navigation process, flat prismatic head is adjusted to nutation state, extracts the left air film capsule of head out by Multifunctional cabin, the right air film capsule of head, cabin, right side air film capsule, trim air film capsule of the right end, air in trim air film capsule of the left end and cabin, left side air film capsule vacuum are shunk air film capsule, close the left air film lid of head, the right air film lid of head, cabin, right side air film lid, trim air film lid of the right end, trim air film lid of the left end and cabin, left side air film lid, continue to launch right front folded sheet and left front folded sheet, drive right back folded sheet and the limited expansion of left back folded sheet simultaneously, make right naval vessels actuator and left naval vessels actuator draw close and adsorb to Ce Cang bottom, both sides, simultaneously, upwards draw right large arm wing and left large arm wing in, adjust left winglet, right winglet, left large wing, right large wing, right back wing and left back wing, with the angle of naval vessels actuator, make left winglet, right winglet, left large wing, right large wing, right back wing and left back wing keep horizontal parastate to become trisome warship submarine aircraft submarine situation lateral fin, and Multifunctional cabin is by front seal ring air inlet/outlet, increasing back sealing ring air inlet/outlet, urceolus air inlet/outlet and inner core air inlet/outlet, extract front stretching air sac sealing ring out, air in rear extension airbag seal ring and naval vessels actuator cylinder, vacuum is shunk front stretching air sac sealing ring and rear extension airbag seal ring, open naval vessels actuator two ends, then, naval vessels actuator passes through the liquid of liquid manhole appendix Extract press pump by Multifunctional cabin, pull front push rod and rear push rod to move to centre, thereby pull front electrical motor and rear electrical motor to move to centre, the middle slide cartridge on spud pile and sliding nail rail groove move to centre along riveting to pull front slide cartridge and rear slide cartridge, front electrical motor and rear electrical motor move to centre, pull front axle and rear axial middle mobile, the movement of front axle and rear axle, respectively by left front screw propeller, right front screw propeller, within left back screw propeller and right back screw propeller are pulled into actuator two ends, water is drawn in naval vessel actuator through front propeller, then is released by after screw, forms the deep water navigation thrust of trisome warship submarine aircraft, high-mobility, multipurpose, wheeled vehicle landing gear compartment before opening, rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment, the hermatic door of rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment and Multifunctional cabin, forward high-mobility, multipurpose, wheeled vehicle landing gear compartment, rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment, rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment and Multifunctional cabin water filling, release is greater than the air lift force of trisome warship submarine aircraft deadweight, rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment and rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment are regained dustpan type activity surfboard jointly, the deep diving of trisome warship submarine aircraft is after certain depth, during flat prismatic head is returned to, straight 0 degree position, adjusts left winglet, right winglet, left large wing, right large wing, right back wing and left back aliform state, adjust lower rudder aliform state, and trisome warship submarine aircraft enters the conventional sail mode of deep water.
Trisome warship submarine aircraft submarine situation under any circumstance can not directly be converted to aircraft situation, the general run of thins situation of getting off the plane is not directly converted to submarine situation, in emergency circumstances, it is that trisome warship submarine aircraft cuts out left and right driving engine that aircraft situation is converted to submarine situation, by left and right driving engine culvert track, left and right driving engine is retracted to culvert, when driving engine is pulled back, drive and draw in left and right cooling and insulating gagger umbrella, form culvert Insulative umbrella, the special liquid that umbrella frame hollow circulation path provides by Multifunctional cabin absorbs heat, driving engine culvert sealing mushroom and Left Hand Engine culvert seal mushroom high-pressure delivery special liquid to Multifunctional cabin to the right simultaneously, mushroom liquid capsule pocket rapid expanding under the pressure of special liquid, squeeze before the mushroom of left and right umbrella frame after umbrella frame and left and right mushroom, the special liquid that Multifunctional cabin provides circulates in umbrella frame hollow circulation path, right driving engine culvert sealing mushroom and Left Hand Engine culvert sealing mushroom sealing left and right driving engine culvert mouth, adjust curved surface and the loop culvert of air inlet culvert, make the curved surface of air inlet culvert become wind sheltering domatic with Left Hand Engine culvert shell with right driving engine culvert hull shape, retract left flexible air inlet dustpan and right flexible air inlet dustpan, sealing admission port, in this, trisome warship submarine aircraft becomes the freely parallel glide of aerodone pattern and declines, trisome warship submarine aircraft is in glide decline process, progressively launch right front folded sheet and left front folded sheet, drive right naval vessels actuator to leave right semicircle landslide, drive left naval vessels actuator to leave left semicircle landslide, about point, drawing semicircle by body upper to underpart moves, drive right back folded sheet and the limited expansion of left back folded sheet simultaneously, make right naval vessels actuator and left naval vessels actuator draw close and adsorb to Ce Cang bottom, both sides, upwards draw right large arm wing and left large arm wing in, adjust left winglet, right winglet, left large wing, right large wing, right back wing and left back wing are with the angle of naval vessels actuator, make left winglet, right winglet, left large wing, right large wing, right back wing vertically draws in to upper machine body in contacting the low vacancy of the water surface fast with left back wing, laterally parallel the opening of submerging in water again, in water, become trisome warship submarine aircraft submarine situation lateral fin, naval vessels actuator is drawn in semicircle moving process to underpart by body upper in point left and right, straight state during flat prismatic head is adjusted to, trisome warship submarine airplane nose down enters after water, flat prismatic head is adjusted to the state of raising up, trisome warship submarine aircraft arrives shallow water top layer by coast, carrying out dive prepares, flat prismatic head is adjusted to nutation state, open lower rudder wing cabin, adjust lower rudder aliform state, actuating motor drives screw propeller rotation, water is drawn in naval vessel actuator through front propeller, released by after screw again, form the deep water navigation thrust of trisome warship submarine aircraft, high-mobility, multipurpose, wheeled vehicle landing gear compartment before opening, rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment, the hermatic door of rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment and Multifunctional cabin, high-mobility, multipurpose, wheeled vehicle landing gear compartment forward, rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment, rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment and Multifunctional cabin water filling, release is greater than the air lift force of trisome warship submarine aircraft deadweight, the deep diving of trisome warship submarine aircraft is after certain depth, straight 0 degree position during flat prismatic head is returned to, adjust left winglet, right winglet, left large wing, right large wing, right back wing and left back aliform state, adjust lower rudder aliform state, trisome warship submarine aircraft proceeds to navigation of submarine pattern.
Trisome warship submarine aircraft Land Mobile state, body is identical with aircraft situation with actuator device, different is that the right large arm wing of gathering downwards and left arm wing are greatly close to body absorption, and upwards folding left winglet, right winglet, the large wing in a left side, right large wing, right back wing and the left back wing of drawing in is close to large arm wing and adsorbs.
Trisome warship submarine aircraft water surface maneuvering condition, body is identical with naval vessel situation with actuator, different: dustpan type activity surfboard is not pushed out, air film capsule and actuator cylinder are not filled with air, upwards draw right large arm wing in and be close to body absorption with left large arm wing, downward folding left winglet, right winglet, left large wing, the large wing in the right side, right back wing and the left back wing of drawing in is close to large arm wing absorption.
Trisome warship submarine aircraft is by amphibious landing warship or drag case to carry out underwater manoeuvre state under water, body is identical with submarine situation with actuator, different: actuator and body side are point-blank, water filling cabin and actuator cylinder do not have water filling, upwards draw right large arm wing in and be close to body absorption with left large arm wing, downward folding left winglet, right winglet, left large wing, the large wing in the right side, right back wing and the left back wing of drawing in is close to large arm wing absorption.
The curved surface of air inlet culvert, loop culvert, air holding bay, air insulated band, foreign material escape orifice, the design of left flexible air inlet dustpan and right flexible air inlet dustpan, can be effectively by the flying bird being drawn in air inlet culvert, sandstone, snowflake, the foreign material such as rainwater and seawater and air insulated, and effectively lay in air, foreign material are cleaned out outside body in time, when closing after the driving engine of left and right, the curved surface of air inlet culvert, air holding bay hatch door, loop culvert, air insulated band, left flexible air inlet dustpan and right flexible air inlet dustpan sealing air inlet culvert, left and right driving engine is carried out to totally-enclosed insulation blocking.
Front high-mobility, multipurpose, wheeled vehicle landing gear compartment, the alighting gear of rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment and rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment is a kind of multi-purpose alighting gear, can be according to the trisome warship submarine aircraft platform difference of taking off and landing of living in, be changed to skates alighting gear, skis alighting gear, triangle fixed landing gear and wheel undercarriage etc., the aircraft landing of trisome warship submarine adopts high pressure airgun to spray air recoil damping while approaching platform, when trisome warship submarine aircraft landing contact platform, adopt the damping of air hydraulic bumper, trisome warship submarine aircraft is dwelt in the mutual switching process of situation three, also conventionally adopt high pressure airgun to spray air recoil damping or power-assisted lift-off.
Trisome warship submarine aircraft is converted to naval vessel state and is converted to the process of aircraft state from submarine state, being converted to naval vessel state with trisome warship submarine aircraft from aircraft state, to be converted to the process of submarine state contrary again, difference is the process difference that the trisome warship submarine aircraft water surface takes off, when trisome warship submarine aircraft is in naval vessel state during in surface navigation, curved surface at air inlet culvert is under the domatic condition of wind sheltering with Left Hand Engine culvert shell and right driving engine culvert shell, release left flexible air inlet dustpan and right flexible air inlet dustpan, shrink right driving engine culvert sealing mushroom and Left Hand Engine culvert sealing mushroom, promote backward left and right driving engine by driving engine culvert track, meanwhile draw left and right cooling and insulating gagger umbrella in, after right engine nozzle and Left Hand Engine spout kickoff mechanism are external, start left and right driving engine, close naval vessels actuator, promote trisome warship submarine aircraft in water surface quick sailing by left and right driving engine, dustpan type activity surfboard protection left and right engine nozzle be not flooded into, progressively draw right front folded sheet in, right back folded sheet, left front folded sheet, left back folded sheet, after left naval vessels actuator and right naval vessels actuator leave the water surface, Multifunctional cabin is by front seal ring air inlet/outlet, increasing back sealing ring air inlet/outlet, urceolus air inlet/outlet and inner core air inlet/outlet, extract front stretching air sac sealing ring out, air in rear extension airbag seal ring and naval vessels actuator cylinder, vacuum is shunk front stretching air sac sealing ring and rear extension airbag seal ring, open naval vessels actuator two ends, then, naval vessels actuator passes through the liquid of liquid manhole appendix Extract press pump by Multifunctional cabin, pull front push rod and rear push rod to move to centre, thereby pull front electrical motor and rear electrical motor to move to centre, the middle slide cartridge on spud pile and sliding nail rail groove move to centre along riveting to pull front slide cartridge and rear slide cartridge, front electrical motor and rear electrical motor move to centre, pull front axle and rear axial middle mobile, the movement of front axle and rear axle, respectively by left front screw propeller, right front screw propeller, within left back screw propeller and right back screw propeller are pulled into actuator two ends, then continue to draw in right front folded sheet, right back folded sheet, left front folded sheet, left back folded sheet, right naval vessels actuator is adsorbed on right semicircle landslide, left naval vessels actuator is adsorbed on left semicircle landslide, launch right head wing and left head wing, launch right large arm wing and left large arm wing, by right wing turning joint and left wing turning joint, launch successively left winglet, right winglet, left large wing, right large wing, right back wing and left back wing, left and right driving engine promote trisome warship submarine aircraft along water surface straight line quick sailing to takeoff speed, adjust right head wing, left head wing, left winglet, right winglet, left large wing, right large wing, right back wing and left back aliform state, open left and right driving engine assistor, promote trisome warship submarine aircraft and leave water surface lift-off, in lift-off process, adjust curved surface and the loop culvert of air inlet culvert, make the curved surface of air inlet culvert become pneumatic domatic with Left Hand Engine culvert shell with right driving engine culvert hull shape, shrink the left air film capsule of head and the right air film capsule of head, close the left air film lid of head and the right air film lid of head, shrink cabin, right side air film capsule, close cabin, right side air film lid, shrink trim air film capsule of the right end, close trim air film lid of the right end, shrink trim air film capsule of the left end, close trim air film lid of the left end, shrink cabin, left side air film capsule, close cabin, left side air film lid, in adjustment, rudder wing is to proper orientation, lower rudder wing is regained in lower rudder wing cabin, rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment and rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment are regained dustpan type activity surfboard jointly, when trisome warship submarine aircraft arrives after certain altitude, straight 0 degree position during flat prismatic head is returned to, simultaneously, again adjust right head wing, left head wing, left winglet, right winglet, left large wing, right large wing, right back wing and left back aliform state, trisome warship submarine aircraft enters orthodox flight state.
The invention has the beneficial effects as follows: reduce the technical requirements of taking off with landing platform, promote aircraft action space and motor-driven transition usefulness, thereby improve the viability of aircraft and the comformability of objective environment and practicality.
Brief description of the drawings
1. cockpit enclosures in figure, 2. flat prismatic head, 3. head triangular groove ditch, 4. right head wing, 5. left head wing, 6. air inlet culvert, 7. left flexible air inlet dustpan, 8. right flexible air inlet dustpan, 9. right naval vessels actuator, 10. left semicircle landslide, 11. right winglets, 12. left winglets, 13. right large arm wings, 14. Left Hand Engine culvert shells, 15 right large wings, 16. right driving engine culvert shells, 17. right back wings, 18. left large wings, rudder wing on 19., 20. left back wings, 21. left large arm wings, 22. left naval vessels actuators, 23. right semicircle landslides, 24. bodies, 25. right front folded sheets, 26. right back folded sheets, 27. left front folded sheets, 28. left back folded sheets, 29. right wing turning joints, 30. left wing turning joints, 31. cabin, right sides, 32. trims of the right end, 33. trims of the left end, 34. cabin, left sides, the left air film lid of 35. head, the left air film capsule of 36. head, the right air film lid of 37. head, the right air film capsule of 38. head, 39. cabin, right side air film lids, 40. cabin, right side air film capsules, 41. trim air film lids of the right end, 42. trim air film capsules of the right end, 43. trim air film lids of the left end, 44. trim air film capsules of the left end, 45. cabin, left side air film capsules, 46. cabin, left side air film lids, 47. right side hatchcovers, 48. flush cabin tops of the right end, 49. flush cabin tops of the left end, 50. left side hatchcovers, 51. left front screw propellers, 52. right front screw propellers, 53. lower rudder wings, 54. right engine nozzles, 55. Left Hand Engine spouts, 56. left back screw propellers, 57. right back screw propellers, 58. right driving engine culvert sealing mushrooms, 59. Left Hand Engine culvert sealing mushrooms, 60. front high-mobility, multipurpose, wheeled vehicle landing gear compartments, 61. Multifunctional cabins, 62. Left Hand Engine culverts, 63. Left Hand Engine culvert tracks, 64. Left Hand Engines, 65. left cooling and insulating gagger umbrellas, umbrella frame before 66. left mushrooms, umbrella frame after 67. left mushrooms, 68. left mushroom liquid capsule pockets, 69. front axles, 70 rear axles, 71. front stretching air sac sealing rings, 72. rear extension airbag seal rings, 73. front seal ring air inlet/outlets, 74. increasing back sealing ring air inlet/outlets, 75. sliding nails, 76. front electrical motors, 77. rear electrical motors, 78. front slide cartridges, 79. rear slide cartridges, slide cartridge in 80., 81. front push rods, 82. rear push rods, 83. Hydraulic Pumps, 84. urceolus air inlet/outlets, 85. inner core air inlet/outlets, 86. liquid manhole appendixs, 87. spud piles, 88. rear left high-mobility, multipurpose, wheeled vehicle landing gear compartments, 89. rear right high-mobility, multipurpose, wheeled vehicle landing gear compartments, 90. lower rudder wing cabins, 91. dustpan type activity surfboards, 92. air holding bays, 93. loop culverts, 94. air insulated bands, 95. foreign material escape orifices.
Fig. 1 is trisome warship submarine airplane situation birds-eye view of the present invention;
Fig. 2 is trisome warship submarine airplane situation front elevation of the present invention;
Fig. 3 is trisome warship submarine airplane situation back view of the present invention;
Fig. 4 is that cutaway view is looked on a trisome warship submarine airplane body of the present invention left side;
Fig. 5 is trisome warship submarine aircraft of the present invention naval vessel situation birds-eye view;
Fig. 6 is trisome warship submarine aircraft of the present invention naval vessel situation front elevation;
Fig. 7 is trisome warship submarine aircraft of the present invention naval vessel situation back view;
Fig. 8 is that cutaway view is looked on an actuator left side, trisome warship submarine aircraft naval vessel of the present invention;
Fig. 9 is trisome warship submarine aircraft submarine situation birds-eye view of the present invention;
Figure 10 is trisome warship submarine aircraft submarine situation front elevation of the present invention;
Figure 11 is trisome warship submarine aircraft submarine situation back view of the present invention;
Figure 12 is that cutaway view is looked on a trisome warship submarine aircraft submarine actuator of the present invention left side;
Figure 13 is trisome warship submarine aircraft upward view of the present invention.
Below in conjunction with drawings and Examples, trisome warship submarine aircraft of the present invention is described in further detail.
Detailed description of the invention
According to Fig. 1, Fig. 2, Fig. 3, trisome warship submarine airplane situation of the present invention shown in Fig. 4, if flat prismatic head 2, flat prismatic head 2 is connected with cockpit enclosure 1, head triangular groove ditch 3 is connected with flat prismatic head 2, right head wing 4 is connected with flat prismatic head 2 right sides, left head wing 5 is connected with flat prismatic head 2 left sides, flat prismatic head 2 is connected with body 24 slip-knots, air inlet culvert 6 is connected with the front upper end of body 24, left flexible air inlet dustpan 7 is connected with air inlet culvert 6 left sides, right flexible air inlet dustpan 8 is connected with air inlet culvert 6 right sides, air storage cabin 92, loop culvert 93, air insulated band 94 is connected with body air inlet culvert 6 with foreign material escape orifice 95, the left semicircle that connects successively below of the air inlet culvert 6 on body 24 tops comes down 10, Left Hand Engine culvert shell 14, right driving engine culvert shell 16 and right semicircle landslide 23, right naval vessels actuator 9 is adsorbed on right semicircle landslide 23 by folded sheet, left naval vessels actuator 22 is adsorbed on left semicircle landslide 10 by folded sheet, left large arm wing 21 is connected with left naval vessels actuator 22, right large arm wing 13 is connected with right naval vessels actuator 9, left winglet 12, left large wing 18 is connected with left large arm wing 21 by left wing turning joint 30 from front to back successively with left back wing 20, upper rudder wing 19 is connected with middle part on body 24 rear ends, body 24 bottoms connect cabin, right side 31 from right to left successively, trim of the right end 32, trim of the left end 33 and cabin, left side 34, right engine nozzle 54 is connected with right driving engine culvert shell 16 tail ends, Left Hand Engine spout 55 is connected with Left Hand Engine culvert shell 14 tail ends, if the left air film lid 35 of head is connected below with flat prismatic head 2 left sides, flush cabin top of the left end 49 is connected with trim of the left end 33, trim air film capsule 44 of the left end is connected with flush cabin top of the left end 49, trim air film lid of the left end 43 is connected with trim air film capsule 44 of the left end and flush cabin top of the left end 49 respectively, if Multifunctional cabin 61 is connected with front end in body 24, Left Hand Engine culvert 62 is connected with Left Hand Engine culvert shell 14, Left Hand Engine sliding rail 63 is connected with Left Hand Engine culvert 62, Left Hand Engine 64 is connected with Left Hand Engine culvert track 63, left cooling and insulating gagger umbrella 65 is connected with Left Hand Engine 64 and Left Hand Engine culvert 62 respectively, mushroom 59 is connected with Left Hand Engine culvert 62 tail ends the sealing of Left Hand Engine culvert, before left mushroom, umbrella frame 66 is connected with Left Hand Engine culvert 62 and left mushroom liquid capsule pocket 68 respectively, after left mushroom, umbrella frame 67 is connected with Left Hand Engine culvert 62 and left mushroom liquid capsule pocket 68 respectively, left mushroom liquid capsule pocket 68 respectively with left mushroom before umbrella frame 66, after left mushroom, umbrella frame 67 is connected with Left Hand Engine culvert 62.
According to Fig. 5, Fig. 6, Fig. 7, the naval vessel of trisome warship submarine aircraft of the present invention shown in Fig. 8 situation, right back folded sheet 26 is connected with body 24 right sides, right front folded sheet 25 is connected with right back folded sheet 26, left back folded sheet 28 is connected with body 24 left sides, left front folded sheet 27 is connected with left back folded sheet 28, right naval vessels actuator 9 is connected with right front folded sheet 25, left naval vessels actuator 22 is connected with left front folded sheet 27, left large arm wing 21 is connected with left naval vessels actuator 22, right large arm wing 13 is connected with right naval vessels actuator 9, the left air film lid 35 of head is connected with flat prismatic head 2 left sides, the left air film capsule 36 of head is connected with the left air film lid 35 of head and flat prismatic head 2 left sides respectively, the right air film lid 37 of head is connected with flat prismatic head 2 right sides, the right air film capsule 38 of head is connected with the right air film lid 37 of head and flat prismatic head 2 right sides respectively, right side hatchcover 47 is connected with cabin, right side 31, flush cabin top of the right end 48 is connected with trim of the right end 32, left side hatchcover 50 is connected with cabin, left side 34, cabin, right side air film lid 39 is connected with right side hatchcover 47, cabin, right side air film capsule 40 is connected with right side hatchcover 47 and cabin, right side air film lid 39 respectively, trim air film lid 41 of the right end is connected with flush cabin top of the right end 48, trim air film capsule of the right end 42 is connected with trim air film lid 41 of the right end and flush cabin top of the right end 48 respectively, cabin, left side air film lid 46 is connected with left side hatchcover 50, cabin, left side air film capsule 45 is connected with cabin, left side air film lid 46 and left side hatchcover 50 respectively, if left front screw propeller 51 is connected with left naval vessels actuator 22 front ends, right front screw propeller 52 is connected with right naval vessels actuator 9 front ends, lower rudder wing 53 is connected with body 24 middle and lower parts, rear end, left back screw propeller 56 is connected with left naval vessels actuator 22 rear ends, right back screw propeller 57 is connected with right naval vessels actuator 9 rear ends, right driving engine culvert sealing mushroom 58 is connected with right driving engine culvert shell 16 tail ends, mushroom 59 is connected with Left Hand Engine culvert 62 tail ends the sealing of Left Hand Engine culvert, dustpan type activity surfboard 91 is connected with body 24 tail ends, if front axle 69 is connected with left front screw propeller 51 and front electrical motor 76, rear axle 70 is connected with left back screw propeller 56 and rear electrical motor 77, front stretching air sac sealing ring 71 is connected with left naval vessels actuator 22 outer cylinder front end inwalls, rear extension airbag seal ring 72 is connected with the outer tube rear end inwall of left naval vessels actuator 22, sliding nail 75 is connected with left naval vessels actuator 22 urceolus two ends inwalls, spud pile 87 is connected with left naval vessels actuator 22 urceolus middle part inwalls, front slide cartridge 78 is connected in left naval vessels actuator 22 front portions with sliding nail 75, front electrical motor 76 is connected with front slide cartridge 78, rear slide cartridge 79 is connected in left naval vessels actuator 22 rear portions with sliding nail 75, middle slide cartridge 80 is fixed after stake 87 is fixed and is connected with front slide cartridge 78 and rear slide cartridge 79 respectively, electrical motor 76 before front push rod 81 connects, electrical motor 77 after rear push rod 82 connects, Hydraulic Pump 83 connects respectively front push rod 81 and rear push rod 82, front seal ring air inlet/outlet 73 is connected with front stretching air sac sealing ring 71, increasing back sealing ring air inlet/outlet 74 is connected with rear extension airbag seal ring 72, urceolus induction opening 84 is connected with left naval vessels actuator 22 urceolus, inner core induction opening 85 is connected with middle slide cartridge 80, liquid manhole appendix 86 is connected with Hydraulic Pump 83.
According to trisome warship submarine aircraft submarine situation of the present invention shown in Fig. 9, Figure 10, Figure 11, Figure 12, right winglet 11, right large wing 15 and right back wing 17 are connected with right large arm wing 13 from front to back successively by right wing turning joint 29.
According to the bottom of trisome warship submarine aircraft of the present invention shown in Figure 13 form, front high-mobility, multipurpose, wheeled vehicle landing gear compartment 60 is connected with flat prismatic head 2 tail end middle parts, rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment 88 is connected with body 24 left sides, rear end, bottom, rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment 89 is connected with body 24 right sides, rear end, bottom, and lower rudder wing cabin 90 is connected with body 24 middle parts, rear end.
Claims (4)
1. a trisome warship submarine airplane, it is characterized in that: establish flat prismatic head (2), flat prismatic head (2) is connected with cockpit enclosure (1), head triangular groove ditch (3) is connected with flat prismatic head (2), right head wing (4) is connected with flat prismatic head (2) right side, left head wing (5) is connected with flat prismatic head (2) left side, flat prismatic head (2) is connected with body (24) slip-knot, air inlet culvert (6) is connected with the front upper end of body (24), left flexible air inlet dustpan (7) is connected with air inlet culvert (6) left side, right flexible air inlet dustpan (8) is connected with air inlet culvert (6) right side, air storage cabin (92), loop culvert (93), air insulated band (94) is connected with body air inlet culvert (6) with foreign material escape orifice (95), after the air inlet culvert (6) on body (24) top, connect successively left semicircle landslide (10), Left Hand Engine culvert shell (14), right driving engine culvert shell (16) and right semicircle landslide (23), right naval vessels actuator (9) is adsorbed on right semicircle landslide (23) by folded sheet, left naval vessels actuator (22) is adsorbed on left semicircle landslide (10) by folded sheet, left large arm wing (21) is connected with left naval vessels actuator (22), right large arm wing (13) is connected with right naval vessels actuator (9), left winglet (12), left large wing (18) is connected with left large arm wing (21) by left wing turning joint (30) from front to back successively with left back wing (20), upper rudder wing (19) is connected with middle part on body (24) rear end, body (24) bottom connects cabin, right side (31) from right to left successively, trim of the right end (32), trim of the left end (33) and cabin, left side (34), right engine nozzle (54) is connected with right driving engine culvert shell (16) tail end, Left Hand Engine spout (55) is connected with Left Hand Engine culvert shell (14) tail end, if the left air film lid of head (35) is connected below with flat prismatic head (2) left side, flush cabin top of the left end (49) is connected with trim of the left end (33), left end trim air film capsule (44) is connected with flush cabin top of the left end (49), left end trim air film lid (43) is connected with left end trim air film capsule (44) and flush cabin top of the left end (49) respectively, if Multifunctional cabin (61) is connected with front end in body (24), Left Hand Engine culvert (62) is connected with Left Hand Engine culvert shell (14), Left Hand Engine sliding rail (63) is connected with Left Hand Engine culvert (62), Left Hand Engine (64) is connected with Left Hand Engine culvert track (63), left cooling and insulating gagger umbrella (65) is connected with Left Hand Engine (64) and Left Hand Engine culvert (62) respectively, Left Hand Engine culvert sealing mushroom (59) is connected with Left Hand Engine culvert (62) tail end, before left mushroom, umbrella frame (66) is connected with Left Hand Engine culvert (62) and left mushroom liquid capsule pocket (68) respectively, umbrella frame after left mushroom (67) is connected with Left Hand Engine culvert (62) and left mushroom liquid capsule pocket (68) respectively, left mushroom liquid capsule pocket (68) respectively with left mushroom before umbrella frame (66), umbrella frame after left mushroom (67) is connected with Left Hand Engine culvert (62).
2. a kind of trisome warship submarine aircraft according to claim 1 naval vessel, it is characterized in that: right back folded sheet (26) is connected with body (24) right side, right front folded sheet (25) is connected with right back folded sheet (26), left back folded sheet (28) is connected with body (24) left side, left front folded sheet (27) is connected with left back folded sheet (28), right naval vessels actuator (9) is connected with right front folded sheet (25), left naval vessels actuator (22) is connected with left front folded sheet (27), left large arm wing (21) is connected with left naval vessels actuator (22), right large arm wing (13) is connected with right naval vessels actuator (9), the left air film lid of head (35) is connected with flat prismatic head (2) left side, the left air film capsule of head (36) is connected with the left air film lid of head (35) and flat prismatic head (2) left side respectively, the right air film lid of head (37) is connected with flat prismatic head (2) right side, the right air film capsule of head (38) is connected with the right air film lid of head (37) and flat prismatic head (2) right side respectively, right side hatchcover (47) is connected with cabin, right side (31), flush cabin top of the right end (48) is connected with trim of the right end (32), left side hatchcover (50) is connected with cabin, left side (34), cabin, right side air film lid (39) is connected with right side hatchcover (47), cabin, right side air film capsule (40) is connected with right side hatchcover (47) and cabin, right side air film lid (39) respectively, right end trim air film lid (41) is connected with flush cabin top of the right end (48), right end trim air film capsule (42) is connected with right end trim air film lid (41) and flush cabin top of the right end (48) respectively, left side cabin air film lid (46) is connected with left side hatchcover (50), left side cabin air film capsule (45) is connected with cabin, left side air film lid (46) and left side hatchcover (50) respectively, if left front screw propeller (51) is connected with left naval vessels actuator (22) front end, right front screw propeller (52) is connected with right naval vessels actuator (9) front end, lower rudder wing (53) is connected with body (24) middle and lower part, rear end, left back screw propeller (56) is connected with left naval vessels actuator (22) rear end, right back screw propeller (57) is connected with right naval vessels actuator (9) rear end, right driving engine culvert sealing mushroom (58) is connected with right driving engine culvert shell (16) tail end, Left Hand Engine culvert sealing mushroom (59) is connected with Left Hand Engine culvert (62) tail end, dustpan type activity surfboard (91) is connected with body (24) tail end, if front axle (69) is connected with left front screw propeller (51) and front electrical motor (76), rear axle (70) is connected with left back screw propeller (56) and rear electrical motor (77), front stretching air sac sealing ring (71) is connected with left naval vessels actuator (22) outer cylinder front end inwall, rear extension airbag seal ring (72) is connected with the outer tube rear end inwall of left naval vessels actuator (22), sliding nail (75) is connected with left naval vessels actuator (22) urceolus two ends inwall, spud pile (87) is connected with left naval vessels actuator (22) urceolus middle part inwall, front slide cartridge (78) is connected in left naval vessels actuator (22) is anterior with sliding nail (75), front electrical motor (76) is connected with front slide cartridge (78), rear slide cartridge (79) is connected in left naval vessels actuator (22) rear portion with sliding nail (75), middle slide cartridge (80) is fixed after stake (87) is fixed and is connected with front slide cartridge (78) and rear slide cartridge (79) respectively, electrical motor (76) before front push rod (81) connects, electrical motor (77) after rear push rod (82) connects, Hydraulic Pump (83) connects respectively front push rod (81) and rear push rod (82), front seal ring air inlet/outlet (73) is connected with front stretching air sac sealing ring (71), increasing back sealing ring air inlet/outlet (74) is connected with rear extension airbag seal ring (72), urceolus induction opening (84) is connected with left naval vessels actuator (22) urceolus, inner core induction opening (85) is connected with middle slide cartridge (80), liquid manhole appendix (86) is connected with Hydraulic Pump (83).
3. trisome warship submarine aircraft submarine according to claim 1, is characterized in that: right winglet (11), right large wing (15) and right back wing (17) are connected with right large arm wing (13) from front to back successively by right wing turning joint (29).
4. trisome warship submarine aircraft according to claim 1 bottom, it is characterized in that: front high-mobility, multipurpose, wheeled vehicle landing gear compartment (60) is connected with flat prismatic head (2) tail end middle part, rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment (88) is connected with left side, body (24) rear end, bottom, rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment (89) is connected with right side, body (24) rear end, bottom, and lower rudder wing cabin (90) is connected with middle part, body (24) rear end.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310057260.8A CN104002972B (en) | 2013-02-25 | 2013-02-25 | Three body warship submarine aircrafts |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310057260.8A CN104002972B (en) | 2013-02-25 | 2013-02-25 | Three body warship submarine aircrafts |
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| Publication Number | Publication Date |
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| CN104002972A true CN104002972A (en) | 2014-08-27 |
| CN104002972B CN104002972B (en) | 2016-04-06 |
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| CN201310057260.8A Expired - Fee Related CN104002972B (en) | 2013-02-25 | 2013-02-25 | Three body warship submarine aircrafts |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107499486A (en) * | 2017-07-28 | 2017-12-22 | 安徽工程大学 | Mobile platform and its localization method on a kind of positioning intelligent water |
| CN108674653A (en) * | 2018-05-30 | 2018-10-19 | 佛山市神风航空科技有限公司 | A kind of multi-functional unmanned plane |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2350608A (en) * | 1942-03-19 | 1944-06-06 | James E Griffith | Combined land, air, and water vehicle |
| US2563731A (en) * | 1945-04-17 | 1951-08-07 | Wilbur L Masterson | Land, sea, and air plane |
| US4913375A (en) * | 1988-08-09 | 1990-04-03 | Fitzpatrick Peter J | Vehicle for use on land, air, or water |
| CN1235907A (en) * | 1998-05-18 | 1999-11-24 | 徐际长 | Flying dish capable of submerging under water |
| CN102774493A (en) * | 2012-08-08 | 2012-11-14 | 南昌航空大学 | Variable wing type land, sea and air triphibian aircraft |
| CN203111502U (en) * | 2013-02-25 | 2013-08-07 | 许祖勇 | Ship and submarine integrated airplane |
-
2013
- 2013-02-25 CN CN201310057260.8A patent/CN104002972B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2350608A (en) * | 1942-03-19 | 1944-06-06 | James E Griffith | Combined land, air, and water vehicle |
| US2563731A (en) * | 1945-04-17 | 1951-08-07 | Wilbur L Masterson | Land, sea, and air plane |
| US4913375A (en) * | 1988-08-09 | 1990-04-03 | Fitzpatrick Peter J | Vehicle for use on land, air, or water |
| CN1235907A (en) * | 1998-05-18 | 1999-11-24 | 徐际长 | Flying dish capable of submerging under water |
| CN102774493A (en) * | 2012-08-08 | 2012-11-14 | 南昌航空大学 | Variable wing type land, sea and air triphibian aircraft |
| CN203111502U (en) * | 2013-02-25 | 2013-08-07 | 许祖勇 | Ship and submarine integrated airplane |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107499486A (en) * | 2017-07-28 | 2017-12-22 | 安徽工程大学 | Mobile platform and its localization method on a kind of positioning intelligent water |
| CN107499486B (en) * | 2017-07-28 | 2023-05-30 | 安徽工程大学 | An intelligent water mobile platform for positioning and its positioning method |
| CN108674653A (en) * | 2018-05-30 | 2018-10-19 | 佛山市神风航空科技有限公司 | A kind of multi-functional unmanned plane |
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| Publication number | Publication date |
|---|---|
| CN104002972B (en) | 2016-04-06 |
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