CN104002972B - Three body warship submarine aircrafts - Google Patents
Three body warship submarine aircrafts Download PDFInfo
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- CN104002972B CN104002972B CN201310057260.8A CN201310057260A CN104002972B CN 104002972 B CN104002972 B CN 104002972B CN 201310057260 A CN201310057260 A CN 201310057260A CN 104002972 B CN104002972 B CN 104002972B
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Abstract
Three body warship submarine aircrafts, collection aircraft, naval vessel and submarine are integrated, if 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 on the right side of flat prismatic head, left head wing is connected with on the left of flat prismatic head, 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 on the left of air inlet culvert, right flexible air inlet dustpan is connected with on the right side of air inlet culvert, 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, this technology can promote aircraft action space and motor-driven transition usefulness, thus improve the viability of aircraft and the comformability of objective environment and practicality.
Description
Technical field
The present invention relates to aircraft, naval vessel and Submarine manufacture field, be specifically related to three body warship submarine aircrafts.
Background technology
Known day jet aircraft core component turbojet engine, when it operates, temperature can reach hundreds of degree, if contact suddenly ice face, snow face, the water surface afterwards in flight or pull the plug, the temperature of turbojet engine can be caused sharply to decline, easily bring out blast, if turbojet engine is subject to the impact of other factors, thrust ratio declines and stops, and 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., be difficult to form aircraft, three between surface vessel and submarine dwells conversion; 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, the technical scheme never advanced to this defect solves.
Summary of the invention
In order to solve the defect that above-mentioned aircraft exists, expand the following action space of aircraft, applicant is through studying for many years, three body warship submarine aircrafts are designed in invention, collection aircraft, naval vessel and submarine are integrated, except the radical function having day jet aircraft, can flexible three to dwell conversion according to acting on demand future, land can be completed, 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, train can be completed, 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 on the right side of flat prismatic head, left head wing is connected with on the left of flat prismatic head, 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 on the left of air inlet culvert, right flexible air inlet dustpan is connected with on the right side of air inlet culvert, 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 head left air film lid is connected below with on the left of flat prismatic head, 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 on the right side of body, right front folded sheet is connected with right back folded sheet, left back folded sheet is connected with on the left of body, 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, head left air film lid is connected with on the left of flat prismatic head, head left air film capsule is connected on the left of air film lid left with head and flat prismatic head respectively, head right air film lid is connected with on the right side of flat prismatic head, head right air film capsule is connected on the right side of air film lid right with head and flat prismatic head 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 inwall in the middle part of left naval vessels actuator urceolus, front slide cartridge is connected in left naval vessels actuator front portion with sliding nail, front electrical motor is connected with front slide cartridge, rear slide cartridge is connected in left naval vessels actuator rear portion with sliding nail, 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 front push rod and rear push rod respectively, 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 are connected with right large arm wing by right wing turning joint from front to back successively with right back wing.Front high-mobility, multipurpose, wheeled vehicle landing gear compartment is connected with in the middle part of flat prismatic head tail end, and rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment is connected with on the left of underpart rear end, and rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment is connected with on the right side of underpart rear end, and lower rudder wing cabin is connected with in the middle part of body rear end.
Three body warship submarine aircrafts run and three to dwell conversion program:
Three body warship submarine aircrafts enter 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, by flat prismatic head adjustment at 0 degree of Angle Position with body, accomplish to stitch in head triangular fovea groove and body to form straight line, shrink right driving engine culvert sealing mushroom and Left Hand Engine culvert sealing mushroom, left and right driving engine is promoted backward by left and right driving engine culvert track, meanwhile draw left and right cooling and insulating gagger umbrella in, right engine nozzle and Left Hand Engine spout kickoff mechanism external after, 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 left winglet successively, right winglet, left large wing, right large wing, right back wing and left back wing, the curved surface of adjustment air inlet culvert and loop culvert, the curved surface of air inlet culvert is made to become pneumatic domatic with Left Hand Engine culvert shell with right driving engine culvert hull shape, release left flexible air inlet dustpan and the right side to stretch air inlet dustpan, shrink head left air film capsule and the right air film capsule of head, close head left air film lid and the right air film lid of head, shrink cabin, right side air film capsule, right side cabin air film lid with right side hatchcover is next to the skin unite two into one after close on the right side of cabin, shrink trim air film capsule of the right end, trim air film lid of the right end and flush cabin top of the right end is next to the skin unite two into one after close trim of the right end, shrink trim air film capsule of the left end, trim air film lid of the left end and flush cabin top of the left end is next to the skin unite two into one after close trim of the left end, shrink cabin, left side air film capsule, left side cabin air film lid with left side hatchcover is next to the skin unite two into one after close on the left of cabin, in adjustment, rudder wing is to proper orientation, strengthen left and right engine throttle, promote three body warship submarine aircrafts to run to takeoff speed along the fast ski-running of airfield runway, raise up flat prismatic head, 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 three body warship submarine aircrafts to go up to the air fast, in lift-off process, front high-mobility, multipurpose, wheeled vehicle landing gear compartment, land wheel undercarriage sequentially packed up by rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment and rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment, after three body warship submarine aircrafts arrive certain altitude, straight 0 degree of 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, three body warship submarine aircrafts enter orthodox flight state.
Three body warship submarine aircrafts proceed to surface vessel navigation from state of flight, be after three body warship submarine aircrafts drop to 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, when air film capsule inflation is combined as after bottom naval vessel, close left and right driving engine, by left and right driving engine culvert track, left and right driving engine is retracted culvert, while 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 is provided 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, to 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 close left and right driving engine culvert mouth, the curved surface of adjustment air inlet culvert and loop culvert, the curved surface of air inlet culvert is made to become wind sheltering domatic with Left Hand Engine culvert shell with right driving engine culvert hull shape, retract left flexible air inlet dustpan and the right side to stretch air inlet dustpan, close admission port, in this, three body warship submarine aircrafts become the free parallel glide of aerodone pattern and progressively decline, three body warship submarine aircrafts are in glide decline process, progressively launch right front folded sheet and left front folded sheet, right naval vessels actuator is driven to leave right semicircle landslide, left naval vessels actuator is driven to leave left semicircle landslide, draw semicircle by body upper to underpart about point to change, simultaneously, the right large arm wing of continuous adjustment, 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 the descending speed of three body warship submarine aircrafts to greatest extent, right front folded sheet and left front folded sheet drive left naval vessels actuator and right naval vessels actuator to move to stop after the vertical down position of body both sides respectively, right large arm wing, left large arm wing, left winglet, right winglet, left large wing, right large wing, right back wing vertically draws in upper machine body in contacting the low vacancy of the water surface fast with left back wing, to submerge after in water more laterally parallel opening become naval vessel flank, naval vessels actuator is drawn in semicircle change process by body upper to underpart in point left and right, liquid manhole appendix is passed through to Hydraulic Pump pumping liquid by Multifunctional cabin, promote front push rod and rear push rod moves to two ends, thus promote front electrical motor and rear electrical motor moves, front slide cartridge and rear slide cartridge is driven to move along slide cartridge during riveting is on spud pile and sliding nail rail groove to two ends, front electrical motor and rear electrical motor move, promotion front axle and rear axle move, 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 three body warship submarine aircraft naval vessel situation, when three body warship submarine aircrafts are close to the water surface, flat prismatic head is kept the state that raises up, after three body warship submarine aircrafts fall into the water surface, left naval vessels actuator and right naval vessels actuator submerge below horizon, dustpan type activity surfboard released jointly by rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment and rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment, open lower rudder wing cabin, adjustment lower rudder aliform state, actuating motor carrying screws rotates, promote three body warship submarine aircrafts to navigate by water on the water surface.
Three body warship submarine aircrafts are converted to submarine deep water by surface navigation and navigate by water, be three body warship submarine aircrafts in surface navigation process, flat prismatic head is adjusted to nutation state, extracts head left air film capsule 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 constriction 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, right naval vessels actuator and left naval vessels actuator is made to draw close to Ce Cang bottom, both sides and adsorb, 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 three body warship submarine aircraft submarine situation lateral fins, 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 constriction front stretching air sac sealing ring and rear extension airbag seal ring, open naval vessels actuator two ends, then, naval vessels actuator is by the liquid of Multifunctional cabin by liquid manhole appendix Extract press pump, front push rod and rear push rod is pulled to move to centre, thus pull front electrical motor and rear electrical motor to move to centre, front slide cartridge and rear slide cartridge is pulled to move along slide cartridge during riveting is on spud pile and sliding nail rail groove to centre, front electrical motor and rear electrical motor move to centre, pull in the middle of front axle and rear axis mobile, the movement of front axle and rear axle, respectively by left front screw propeller, right front screw propeller, left back screw propeller and right back screw propeller are pulled within actuator two ends, and water is drawn in naval vessel actuator through front propeller, then is released by after screw, form the deep water sail thrust of three body warship submarine aircrafts, 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 three body warship submarine aircraft deadweights, dustpan type activity surfboard regained jointly by rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment and rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment, after three body warship submarine aircraft deep divings to certain depth, in being returned to by flat prismatic head, straight 0 degree of position, adjusts left winglet, right winglet, left large wing, right large wing, right back wing and left back aliform state, adjustment lower rudder aliform state, three body warship submarine aircrafts enter the conventional sail mode of deep water.
Three body warship submarine aircraft submarine situation under any circumstance can not directly be converted to aircraft situation, general run of thins situation of getting off the plane directly is not converted to submarine situation, in emergency circumstances, it is that three body warship submarine aircrafts cut 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 culvert, while driving engine is pulled back, drive and draw left and right cooling and insulating gagger umbrella in, form culvert Insulative umbrella, the special liquid that umbrella frame hollow circulation path is provided 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, to 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 close left and right driving engine culvert mouth, the curved surface of adjustment air inlet culvert and loop culvert, the curved surface of air inlet culvert is made to become wind sheltering domatic with Left Hand Engine culvert shell with right driving engine culvert hull shape, retract left flexible air inlet dustpan and the right side to stretch air inlet dustpan, close admission port, in this, three body warship submarine aircrafts become the freely parallel glide decline of aerodone pattern, three body warship submarine aircrafts are in glide decline process, progressively launch right front folded sheet and left front folded sheet, right naval vessels actuator is driven to leave right semicircle landslide, left naval vessels actuator is driven to leave left semicircle landslide, draw semicircle by body upper to underpart about point to move, drive right back folded sheet and the limited expansion of left back folded sheet simultaneously, right naval vessels actuator and left naval vessels actuator is made to draw close to Ce Cang bottom, both sides and adsorb, 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 upper machine body in contacting the low vacancy of the water surface fast with left back wing, to submerge laterally parallel again in water opening, three body warship submarine aircraft submarine situation lateral fins are become in water, naval vessels actuator is drawn in semicircle moving process by body upper to underpart in point left and right, straight state during flat prismatic head is adjusted to, after three body warship submarine airplane nose downs enter water, flat prismatic head is adjusted to the state of raising up, three body warship submarine aircrafts by coast to shallow water top layer, carry out dive to prepare, flat prismatic head is adjusted to nutation state, open lower rudder wing cabin, adjustment lower rudder aliform state, actuating motor carrying screws rotates, water is drawn in naval vessel actuator through front propeller, released by after screw again, form the deep water sail thrust of three body warship submarine aircrafts, 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 three body warship submarine aircraft deadweights, after three body warship submarine aircraft deep divings to certain depth, straight 0 degree of 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, adjustment lower rudder aliform state, three body warship submarine aircrafts proceed to navigation of submarine pattern.
Three body warship submarine aircraft Land Mobile states, body is identical with aircraft situation with actuator device, be close to body unlike the right large arm wing of downward gathering and left large arm wing and adsorb, upwards the left winglet of folding gathering, right winglet, left wing greatly, the right side large wing, right back wing and left back wing are close to large arm wing and adsorb.
Three body warship submarine aircraft water surface maneuvering conditions, body is identical with naval vessel situation with actuator, unlike: 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 left large arm wing is close to body and adsorbs, folding draw left winglet in downwards, right winglet, left large wing, right large wing, right back wing and left back wing be close to large arm wing and adsorb.
Three body warship submarine aircrafts are by amphibious landing warship or drag case to carry out underwater manoeuvre state under water, body is identical with submarine situation with actuator, unlike: 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 left large arm wing is close to body and adsorbs, folding draw left winglet in downwards, right winglet, left large wing, right large wing, right back wing and left back wing be close to large arm wing and adsorb.
The curved surface of air inlet culvert, loop culvert, air storage cabin, air insulated band, foreign material escape orifice, stretch the design of air inlet dustpan in left flexible air inlet dustpan and the right side, the flying bird that can effectively will be 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 after the driving engine of closedown left and right, the curved surface of air inlet culvert, air storage cabin door, loop culvert, air insulated band, air inlet culvert closed by left flexible air inlet dustpan and the right side air inlet dustpan that stretches, totally-enclosed insulation blocking is carried out to left and right driving engine.
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 different according to the platform of takeoff and anding residing for three body warship submarine aircrafts, be changed to skates alighting gear, skis alighting gear, triangle fixed landing gear and wheel undercarriage etc., three body warship submarine aircraft landings spray air recoil damping close to adopting high pressure airgun during platform, during three body warship submarine aircraft landing contact platforms, adopt the damping of air hydraulic bumper, three body warship submarine aircrafts are dwelt in the mutual switching process of situation three, also high pressure airgun is usually adopted to spray air recoil damping or power-assisted lift-off.
Three body warship submarine aircrafts are the process that naval vessel state is converted to aircraft state again from submarine State Transferring, being converted to naval vessel state with three body warship submarine aircrafts from aircraft state, to be converted to the process of submarine state more contrary, difference is that the process that the three body warship submarine aircraft waters surface take off is different, when three body warship submarine aircrafts are in naval vessel state in surface navigation, under the curved surface of air inlet culvert is 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 the right side to stretch air inlet dustpan, shrink right driving engine culvert sealing mushroom and Left Hand Engine culvert sealing mushroom, left and right driving engine is promoted backward by driving engine culvert track, meanwhile draw left and right cooling and insulating gagger umbrella in, right engine nozzle and Left Hand Engine spout kickoff mechanism external after, start left and right driving engine, close naval vessels actuator, three body warship submarine aircrafts are promoted 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 constriction front stretching air sac sealing ring and rear extension airbag seal ring, open naval vessels actuator two ends, then, naval vessels actuator is by the liquid of Multifunctional cabin by liquid manhole appendix Extract press pump, front push rod and rear push rod is pulled to move to centre, thus pull front electrical motor and rear electrical motor to move to centre, front slide cartridge and rear slide cartridge is pulled to move along slide cartridge during riveting is on spud pile and sliding nail rail groove to centre, front electrical motor and rear electrical motor move to centre, pull in the middle of front axle and rear axis mobile, the movement of front axle and rear axle, respectively by left front screw propeller, right front screw propeller, left back screw propeller and right back screw propeller are pulled within actuator two ends, then continue to draw right front folded sheet in, 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 left winglet successively, right winglet, left large wing, right large wing, right back wing and left back wing, left and right driving engine promotes three body warship submarine aircrafts after 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 three body warship submarine aircrafts and leave water surface lift-off, in lift-off process, the curved surface of adjustment air inlet culvert and loop culvert, the curved surface of air inlet culvert is made to become pneumatic domatic with Left Hand Engine culvert shell with right driving engine culvert hull shape, shrink head left air film capsule and the right air film capsule of head, close head left air film lid 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, dustpan type activity surfboard regained jointly by rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment and rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment, after three body warship submarine aircrafts arrive certain altitude, straight 0 degree of 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, three body warship submarine aircrafts enter orthodox flight state.
The invention has the beneficial effects as follows: reduce and take off the technical requirements with landing platform, promote aircraft action space and motor-driven transition usefulness, thus improve the viability of aircraft and the comformability of objective environment and practicality.
Accompanying drawing explanation
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, cabin on the right side of in the of 31., 32. trims of the right end, 33. trims of the left end, cabin on the left of in the of 34., 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, air film lid in cabin on the right side of in the of 39., air film capsule in cabin on the right side of in the of 40., 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, air film capsule in cabin on the left of in the of 45., air film lid in cabin on the left of in the of 46., hatchcover on the right side of in the of 47., 48. flush cabin tops of the right end, 49. flush cabin tops of the left end, hatchcover on the left of in the of 50., 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, high-mobility, multipurpose, wheeled vehicle landing gear compartment before 60., 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, extension airbag seal ring after 72., seal ring air inlet/outlet before 73., 74. increasing back sealing ring air inlet/outlets, 75. sliding nails, electrical motor before 76., electrical motor after 77., slide cartridge before 78., slide cartridge after 79., slide cartridge in 80., push rod before 81., push rod after 82., 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 storage cabins, 93. loop culverts, 94. air insulated bands, 95. foreign material escape orifices.
Fig. 1 is three body warship submarine airplane situation birds-eye vieies of the present invention;
Fig. 2 is three body warship submarine airplane situation front elevations of the present invention;
Fig. 3 is three body warship submarine airplane situation back views of the present invention;
Fig. 4 is that cutaway view is looked on three body warship submarine airplane body left sides of the present invention;
Fig. 5 is three body warship submarine aircraft naval vessel situation birds-eye vieies of the present invention;
Fig. 6 is three body warship submarine aircraft naval vessel situation front elevations of the present invention;
Fig. 7 is three body warship submarine aircraft naval vessel situation back views of the present invention;
Fig. 8 is that cutaway view is looked on three actuator left sides, body warship submarine aircraft naval vessel of the present invention;
Fig. 9 is three body warship submarine aircraft submarine situation birds-eye vieies of the present invention;
Figure 10 is three body warship submarine aircraft submarine situation front elevations of the present invention;
Figure 11 is three body warship submarine aircraft submarine situation back views of the present invention;
Figure 12 is that cutaway view is looked on three body warship submarine aircraft submarine actuator left sides of the present invention;
Figure 13 is three body warship submarine aircraft upward views of the present invention.
Below in conjunction with drawings and Examples, the present invention three body warship submarine aircraft is described in further detail.
Detailed description of the invention
According to Fig. 1, Fig. 2, Fig. 3, the body of the present invention three shown in Fig. 4 warship submarine airplane situation, 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 on the right side of flat prismatic head 2, left head wing 5 is connected with on the left of flat prismatic head 2, 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 on the left of air inlet culvert 6, right flexible air inlet dustpan 8 is connected with on the right side of air inlet culvert 6, 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 top 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 end, body 24 bottom connects cabin 31, right side 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 head left air film lid 35 is connected below with on the left of flat prismatic head 2, flush cabin top of the left end 49 is connected with trim of the left end 33, trim air film capsule of the left end 44 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 of the left end 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, mushroom 59 is connected with Left Hand Engine culvert 62 tail end 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 body of the present invention three shown in Fig. 8 warship submarine aircraft naval vessel situation, right back folded sheet 26 is connected with on the right side of body 24, right front folded sheet 25 is connected with right back folded sheet 26, left back folded sheet 28 is connected with on the left of body 24, 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, head left air film lid 35 is connected with on the left of flat prismatic head 2, head left air film capsule 36 is connected on the left of air film lid 35 left with head and flat prismatic head 2 respectively, head right air film lid 37 is connected with on the right side of flat prismatic head 2, head right air film capsule 38 is connected on the right side of air film lid 37 right with head and flat prismatic head 2 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 of the right end 41 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 of the right end 41 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 end, right front screw propeller 52 is connected with right naval vessels actuator 9 front end, lower rudder wing 53 is connected with middle and lower part, body 24 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, mushroom 59 is connected with Left Hand Engine culvert 62 tail end the sealing of Left Hand Engine culvert, 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 inwall in the middle part of left naval vessels actuator 22 urceolus, front slide cartridge 78 is connected in left naval vessels actuator 22 front portion 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, front push rod 81 connects front electrical motor 76, rear push rod 82 connects rear electrical motor 77, Hydraulic Pump 83 connects front push rod 81 and rear push rod 82 respectively, 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 the body of the present invention three shown in Fig. 9, Figure 10, Figure 11, Figure 12 warship submarine aircraft submarine situation, right winglet 11, right large wing 15 are connected with right large arm wing 13 by right wing turning joint 29 from front to back successively with right back wing 17.
According to form bottom the body of the present invention three shown in Figure 13 warship submarine aircraft, front high-mobility, multipurpose, wheeled vehicle landing gear compartment 60 is connected with in the middle part of flat prismatic head 2 tail end, rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment 88 is connected with on the left of rear end, body 24 bottom, rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment 89 is connected with on the right side of rear end, body 24 bottom, and lower rudder wing cabin 90 is connected with in the middle part of body 24 rear end.
Claims (4)
1. a body warship submarine aircraft, 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 body (24) front upper end, 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), the left semicircle that connects successively below of the air inlet culvert (6) on body (24) top 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 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 head left air film lid (35) is connected below with flat prismatic head (2) left side, flush cabin top of the left end (49), was connected with trim of the left end (33), left end trim air film capsule (44) was 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, 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).
2. a kind of three body warship submarine aircrafts according to claim 1, 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), head left air film lid (35) is connected with flat prismatic head (2) left side, head left air film capsule (36) respectively air film lid (35) left with head and flat prismatic head (2) left side is connected, head right air film lid (37) is connected with flat prismatic head (2) right side, head right air film capsule (38) respectively air film lid (37) right with head and flat prismatic head (2) right side is connected, right side hatchcover (47) is connected with cabin, right side (31), flush cabin top of the right end (48), was connected with trim of the right end (32), left side hatchcover (50) is connected with cabin, left side (34), cabin air film lid, right side (39) is connected with right side hatchcover (47), cabin air film capsule, right side (40) is connected with right side hatchcover (47) and cabin, right side air film lid (39) respectively, right end trim air film lid (41) was 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, cabin air film lid, left side (46) is connected with left side hatchcover (50), cabin air film capsule, left side (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 inwall in the middle part of left naval vessels actuator (22) urceolus, front slide cartridge (78) is connected in left naval vessels actuator (22) front portion with sliding follow closely (75), front electrical motor (76) is connected with front slide cartridge (78), rear slide cartridge (79) is followed closely (75) with cunning and is connected in left naval vessels actuator (22) rear portion, 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 front push rod (81) and rear push rod (82) respectively, 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. three body warship submarine aircrafts according to claim 1, is characterized in that: right winglet (11), right large wing (15) are connected with right large arm wing (13) by right wing turning joint (29) from front to back successively with right back wing (17).
4. three body warship submarine aircrafts according to claim 1, it is characterized in that: front high-mobility, multipurpose, wheeled vehicle landing gear compartment (60) is connected with in the middle part of flat prismatic head (2) tail end, rear left high-mobility, multipurpose, wheeled vehicle landing gear compartment (88) is connected with on the left of body (24) rear end, bottom, rear right high-mobility, multipurpose, wheeled vehicle landing gear compartment (89) is connected with on the right side of body (24) rear end, bottom, and lower rudder wing cabin (90) is connected with in the middle part of 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 |
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| CN201310057260.8A CN104002972B (en) | 2013-02-25 | 2013-02-25 | Three body warship submarine aircrafts |
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| CN104002972B true CN104002972B (en) | 2016-04-06 |
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| 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 |
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 |
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| CN104002972A (en) | 2014-08-27 |
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