CN102166931A - New energy multifunctional airplane - Google Patents
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- CN102166931A CN102166931A CN2011101513701A CN201110151370A CN102166931A CN 102166931 A CN102166931 A CN 102166931A CN 2011101513701 A CN2011101513701 A CN 2011101513701A CN 201110151370 A CN201110151370 A CN 201110151370A CN 102166931 A CN102166931 A CN 102166931A
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/16—Information or communication technologies improving the operation of electric vehicles
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Abstract
The invention discloses a new energy multifunctional airplane. As shown in a figure, the two ends of a hydraulic movable frame on the middle-rear part in a cabin are provided with two jet aircraft engines 8; the engines can be driven to move from the inside of the cabin to a flying working position outside the cabin in a parallel telescopic way by using a hydraulic device, and can be moved back into the cabin when not used; wings 4 are provided with two or more electric propeller engines 3; the two types of engines can be driven to deflect by certain angles in a reciprocating way by using the hydraulic device according to taking-off and landing requirements; the airplane is suitable for gliding and vertically taking off and landing at different natural environment occasions; the surface of an airplane body is provided with a solar film cell; multiple groups of high-voltage super capacitors are arranged below a solar cell layer; multiple groups of storage batteries and a fuel tank are arranged in the cabin; and the top of the cabin is provided with multiple layers of combined parachutes. The wings can be filled with compressed air or water according to the water surface and underwater diving environment requirements. The airplane has amphibious functions. An electric engine and a jet engine can be driven to work by using a new energy such as solar energy, wind energy and electric energy. The new energy multifunctional airplane has a very good application prospect.
Description
Technical field:
The present invention makes relevant with the new multi-purpose amphibious aircraft.
Background technology:
Generally all more single in function and landing mode in the world at present with aircraft, that can glide landing can not take into account vertical takeoff and landing, can vertical takeoff and landing can not take into account the glide landing, that uses on land can not use on the water, the land of can not arriving of Shi Yonging is used on the water.In order to produce buoyancy, hydroairplane commonly used now generally adopts at the big iron floating drum of two heavinesses of body lower device, and this class hydroairplane is very backward should be eliminated.Existing in a word aircraft all is that function is more single, the landing mode is more single, one airplane can not be taken into account the landing of can gliding and can vertical takeoff and landing fly again, therefore the natural environment place scope of aircraft utilization is extremely restricted, the existing aircraft of not energy-conservation high oil consumption high pollution discharging can not adapt to the development new demand of following environmental emission reduction, the type aircraft of multifunctional and multipurpose new energy source energy-saving environment-friendly type just can be complied with this development tendency, a kind of Application and Development of new forms of energy multifunction aircraft will produce huge benefit for socio-economic development, has boundless application prospect.
Summary of the invention:
The technology of the present invention is to have above problems and complete innovative design scheme in order to solve present airplane design manufacturing, expand the range of use and the function of following type aircraft, make a kind of aircraft can have multifunctional and multipurpose, can adapt to multiple environment place uses, it can not only can or move under water at water surface landing, water surface flying (containing adjoined water surface flight) again under water in terrestrial space landing and the vertical takeoff and landing flight (containing hedgehopping) of gliding.The fuel oil jet engine of airborne device and electric propeller formula driving engine are through the manipulation of hydraulic efficiency gear, but by flight landing requirements of one's work deflected as desired angle, thereby aircraft can select glide landing or vertical takeoff and landing according to the place flexibly at the landing scene, and restriction and the influence of avoiding aircraft to be subjected to the natural environment place in use reduce range of use.
Energy applied solar energy, wind energy, electric energy drive electric propeller formula engine operation, and he is the amphibious new forms of energy hybrid power aeroplane of a kind of Multifunction high-mobility, multipurpose, wheeled vehicle.
That the technology of the present invention can be used for making is little, in, large-scale all kinds of multifunctional and multipurpose amphibious aircrafts.This type aircraft purposes is very extensive, can on airfield, the highway, on the level land, the landing of gliding on the water surface, aircraft carrier.In level land, hospital, campus, station, harbour, street, square vertical takeoff and landing on the warship deck, on the aircraft carrier, before and after the military camp sentry post, mansion roof, room, private Residence roof.Can be at rivers,lakes and seas water surface landing water surface flying.On warplane, be equipped with guided missile, laser weapon can be tackled enemy's aircraft, guided missile, warship, aircraft carrier, submarine, military target such as tank, armored motor car, also can make long-range bomber, electronic reconnaissance communication patrol early warning plane, fuel charger, military transportation airplane etc., warplane can adopt the fuselage stealth technique.Aircraft is civilian makes engineering lifting handling construction, passenger-cargo commercial transport, rescue and relief work, fire-fighting fire extinguishing, fly to spill sowing, the aerial survey of taking photo by plane, communication, mine locating, medical aid, public security patrol, public affair, private savings are gone sightseeing etc.
The present invention is achieved in that principle of work is as follows, as shown in Figure 2, now overlapping back and forth flexible parallel mobile fluid pressure linkage stand arrangement with postmedian device in the cabin of aircraft one, two end device jet engines 1 (solid line) in frame, through parallel telescopic (dotted line) flight station outside the cabin that moves to of hydraulic efficiency gear 6 maneuver energies, driving engine does not need the time spent can cut out after operating hydraulically operated device 6 is moved back in the cabin.Through the manipulation control of hydraulic efficiency gear as shown in Figure 4, can make respectively that two electric propeller formula driving engines 13 on 1 (dotted line) jet engine and preceding wing 16 are at the scene according to the needs deflection angle of working environment landing flight among Fig. 2, the use that makes aircraft can adapt to multiple natural environment place is flown.In drop in water surface, flight, in wing 16, fill 10-12 kilogram pressurized air earlier according to water surface working environment needs, wing is immersed produce buoyancy picking-up body in the water.The operation hydraulic efficiency gear is opened the jet engine cabin door before water surface glide in land is taken off, as shown in Figure 2 through hydraulic efficiency gear 6 handle with jet engine 1 (solid line) from the parallel driving engine flight station that moves to out of my cabin in the cabin shown in 1 (dotted line) the figure, at this moment can handle use start jet engine 1 and handle use start before electric propeller formula driving engine 13 on the wing make aircraft in airfield or water surface gliding flight.Need move under water under water, aircraft is parked on the water surface to be handled hydraulic efficiency gear 6 jet engine 1 is moved back in the cabin, hermetically closing cabin door and window, operation is manipulated electric propeller formula driving engine 13 work drowneds and is moved under water with the water pump of installing in wing water-filling and discharge pressurized air in the wing (during dive be stored in when waiting to float in the accumulator unit emit again air) in wing 16.
As shown in figure 10,2 electric propeller formulas of two end devices driving engine 9 of the mmi machine wing, two jet engines 5 of postmedian both sides device on body, 2 in minicomputer such as Fig. 1 mmi machine wing two end device electric propeller formula driving engines, on afterbody normal limb 9 device jet engine shown among the figure 8, medium-sized as shown in Figure 9 machine on the afterbody horizontal tail two end device jet engines each one shown among the figure 1.In the time of need taking off vertically, handle principle hydraulic efficiency gear as shown in Figure 4, make as about 90 degree of 5 deflections of jet engine among Figure 10, air nozzle vertically downward, engine condition is shown in 5 dotted lines among Figure 10, handle principle as shown in Figure 4 and be installed in hydraulic efficiency gear in the wing and make on wing 2 two ends about 90 degree of electronic propeller type driving engine 9 deflections shown in dotted line, make electric propeller formula driving engine screw propeller upwards, driving engine presents this state and can prepare to take off vertically or vertical landing.The thrust that does not need fully to advance forward because aircraft only need obtain maximum lift when taking off vertically, so at this moment with after all driving engine deflection about 90 is spent on the machine, owing to changed the direction of driving engine generation thrust, so the forward thrust that driving engine produced just changes lift vertically upward fully into, according to aerodynamic principle, the lift vertically upward that driving engine produced is greater than aircraft weight gravity vertically downward, aircraft just can parked vertically slowly rising of original place, after aircraft rises to suitable flying height, handling as shown in Figure 4, the deflection hydraulic efficiency gear makes slowly about 90 degree of deflection of institute's mounted engine, among state such as Figure 10 5, shown in 9 solid lines, the driving engine air nozzle slightly is level backward, propeller turning direction head working direction, go up driving engine this opportunity and all be used to produce thrust, producing lift by preceding wing 2 can normally fly forward.Because of aircraft adopts the maximum lift that need obtain driving engine when taking off vertically, so the driving engine of airborne device needs to use simultaneously.When the landing environment has glide landing condition, operate the same, wherein a kind of driving engine glide landing of installing on wing or the body postmedian before can selecting to use with aircraft commonly used.When needing high-speed flight, electric propeller formula driving engine and jet engine can be used simultaneously.Aircraft can be according to engine installation type position, possess the local glide landing of glide condition landing on land, can not adopt vertical takeoff and landing when not possessing the glide condition, can also be on the water surface glide or vertical takeoff and landing and move under water under water.
When flight arrives the landing destination, select landing modes according to the geographical nature environment in landing place.As on airport, highway, spacious level land, aircraft carrier are first-class possesses the landing of can gliding of glide condition place, handle identical with existing common aircraft commonly used.When not having the glide condition, need vertical landing on smooth ground, land, on the warship, targets such as front and back, house, roof, the operation during landing is basic identical with operating process of taking off vertically and principle.Handle driving engine that deflection hydraulic efficiency gear as shown in Figure 4 makes on the machine to be equipped with slowly to about 90 degree of clockwise direction deflection, as among Figure 10 5, shown in 9 dotted lines, control aircraft and landing target approaching height flying speed well, when reducing height speed, handle hydraulic efficiency gear control tail vane wing control heading in the tail vane wing 7, when aircraft is arrived in the height of the overhead suitable landing of landing target and suitable location by plane, at this moment control reduces the throttle of jet engine 5 and reduces the power of electric propeller formula driving engine 9, make jet-propelled start 5 and the vertical lift that produced of electric propeller formula driving engine 9 gradually less than the gravity of aircraft, aircraft just slowly safe vertical landing in the target location.Use above vertical takeoff and landing operating sequence, can make the motionless enforcement of the hang positioning operation that hovers aloft.
Reciprocating type parallel telescopic moving of jet engine and reciprocating type deflection angle principle of work, as shown in Figure 3, two driving engines 1 be installed in hydraulic pressure parallel telescopic move and reciprocating type deflection work housing two ends on, device is by driving engine U type frame 2, parallel telescopic mobile bearing and support 3, the parallel telescopic shifting axle 4 of hydraulic pressure, fixed type bearing and support 5, parallel telescopic mobile hydraulic efficiency gear 6, hydraulic efficiency gear deflection gears 7, the parallel telescopic mobile hydraulic efficiency gear transmission gear bar 8 of the reciprocating type deflection of driving engine, chute mount 9, hydraulic oil control and regulation valve 10, oil pipe 11 is formed.When needing the parallel telescopic mobile working of driving engine, operation hydraulic efficiency gear 6 is with hydraulic efficiency gear axle 4 parallel shifting out, at this moment drive parallel telescopic mobile bearing 3 and support and follow translation, driving engine and U type frame be together parallel to move to driving engine flight station outside the cabin, the time spent reversing sense is parallel to be moved back in the cabin not needing but handle this hydraulic efficiency gear driving engine, and device is used as shown in Figure 2.
The reciprocating type deflection angle hydraulic efficiency gear of driving engine operation element theory structure as shown in Figure 4, device connects telescopic parallel traveling gear bar 3 by the piston rod of hydraulic efficiency gear 1, rack 3 again with Fig. 3 in the work that matches of gear 7 on the telescopic parallel mobile hydraulic efficiency gear 6 of driving engine, make piston rod parallel backward forward when mobile when operating as shown in Figure 4 hydraulic efficiency gear 1, rack 3 just interlock drives the reciprocating type deflection angle of body skin gear of another set of hydraulic efficiency gear 2 (in this way among Fig. 3 7), because of the hydraulic piston in the hydraulic efficiency gear 2 is square, be that the reciprocating type deflection angle of hydraulic efficiency gear 2 body skin gears is followed the reciprocating type mobile of rack 3 and deflection angle with regard to making hydraulic efficiency gear 2 integral body, therefore drive be contained in hydraulic efficiency gear 2 two ends start function by need of work reciprocating type deflection angle, can adapt to the purpose that can both take off under the multiple different natural environments place and land to reach aircraft.
As shown in Figure 5,2 electric propeller formula driving engines 10 of device on the mmi machine wing 2 handle to use electric propeller formula genemotor to drive screw propeller 9 rotations, the aircraft landing flight of can gliding.The hydraulic pressure inflector assembly as shown in Figure 4 of device is handled and is made electric propeller formula driving engine 2 deflection an angle of 90 degrees degree in wing 3 as shown in Figure 8, state is shown in 2 dotted lines, handling the interior hydraulic efficiency gear of normal limb turn 90 degrees jet engine 7 partially, state is shown in 7 solid lines among the figure, but driving engine is this state microminiature machine vertical takeoff and landing, when only using fuel engines 7 work, the electrical motor of electric propeller formula driving engine 2 can be exchanged into the electrical generator mode of operation and uses, utilize screw propeller when flight, to produce wind energy screw propeller 1 is rotated, drive electrical motor 2 generatings lithium battery group charging in the cabin.
Aircraft can utilize solar power, wind energy, the multiple new forms of energy of electric energy to drive electric propeller formula engine operation, according to the working environment needs, electric propeller formula driving engine and jet engine can be worked respectively and be worked simultaneously jointly becomes the new forms of energy hybrid power aeroplane.Shown in all dices among Fig. 5,10, all device one deck solar film batteries or organic thin film solar cells (except the glass port) on the surface of body, when aircraft is parked on ground, aerial, the water surface or flown, can both utilize solar film battery in the cabin as Fig. 2 in 11 lithium battery groups charge.As shown in Figure 9, at body solar cell layer 8 lower devices many group multi-layer high-voltage ultracapacitors 9 are arranged, at flight forward direction storage battery 11 and ultracapacitor 9 sufficient electrical energies, when electric energy abundance during aloft with water surface flying, can use electrodynamic type airscrew engine 13 work flight saving fuel oil earlier, fuel engines 1 is done standby and is used during vertical takeoff and landing.As shown in Figure 2, before drop in water surface, the air of 10--12 kilogram pressure is filled in the Air compressor work in the wing manipulated in wing 16, the buoyancy that the wing compressed air is immersed in the water to be produced can land aircraft to park, take off and at water surface flying on the water surface.When water surface glide is taken off and is pressed close at water surface flying, electric propeller formula driving engine 13 work before using on the wing 16.When needing to accelerate flying speed, electric propeller formula driving engine and jet engine can be used simultaneously and reach than hypersonic flight shown in Fig. 9,10.
Be aircraft and personal security; at top, cabin medium position parachute compartment 5 is set as shown in Figure 6; one group in interior dress multi-layer combined type parachute; among umbrella mode of operation such as the figure 1; shown in 2; launch out earlier the guiding drogue-parachute 1 of the combination parachute the superiors when critical at the bridge operation button; take compound parachute 2 out of after opening by umbellule and go up the ground floor gamp most; because of every layer of gamp is connected with rope; the ground floor gamp opens and drives lower floor's gamp more successively and all open work up to whole group gamp; be equipped with at hour of danger immediately with umbrella protection aircraft and personal security; one group in minicomputer device, medium-and-large-sized machine are pressed load carrying ability suitable many devices group number and every group of compound parachute number of plies.
Description of drawings:
Fig. 1 is a microminiature machine working flight view, 1 screw propeller among the figure, 2 hydraulic pressure axis of deflection, 3 electric propeller formula motor of engine, 4 wings, 5 operator'ies compartment, top, 6 cabin parachute compartment, 7 bodies, 8 jet engines, 9 normal limbs, 10 horizontal tails.
Fig. 2 is that Medium Plane is arranged front elevation, 1 fuel oil jet engine among the figure, 2 driving engine U type framves, the parallel telescopic shifting axles of 3 driving engines (dotted line), parallel telescopic mobile movable axis bearing of 4 driving engines and support, 5 hydraulic efficiency gear fixed type bearing and supports, the parallel telescopic mobile hydraulic efficiency gear of 6 driving engines, the reciprocating type deflection gears of the parallel telescopic mobile hydraulic efficiency gear of 7 driving engines, 8 hydraulic efficiency gear pistons, the parallel telescopic mobile reciprocating deflection hydraulic efficiency gear transmission gear bar of 9 driving engines, 10 chutes, 11 lithium battery groups, 12 fuel tanks, 13 electric propeller formula motor of engine, 14 screw propellers, 15 solar cell layers, 16 wings (needing can fill pressurized air or water in the wing the suitable work of moving under water of this type by working environment under water).
Fig. 3 is the parallel telescopic mobile reciprocating deflection angle hydraulic actuated schematic diagram of jet engine, 1 driving engine among the figure, 2U type frame, 3 parallel telescopic mobile bearing and supports, the parallel telescopic mobile reciprocating deflection hydraulic control unit axle of 4 driving engines, 5 hydraulic efficiency gear fixed installation bearing and support, the parallel telescopic mobile reciprocating deflection hydraulic efficiency gear of 6 driving engines, the parallel telescopic mobile reciprocating deflection hydraulic efficiency gear gear of 7 driving engines, the parallel telescopic mobile reciprocating deflection hydraulic actuator rack of 8 driving engines, 9 chutes, 10 oil pressure adjusting valve doors, 11 oil pipes.
Fig. 4 is the reciprocating type deflection angle hydraulic actuated of a driving engine schematic diagram, 1 hydraulic efficiency gear among the figure, parallel telescopic mobile reciprocating deflection hydraulic efficiency gear of 2 driving engines and gear, 3 parallel telescopic mobile hydraulic efficiency gear transmission gear bars, 4 hydraulic efficiency governing valves, 5 fuel tanks, 6 oil pipes, 7 safety valves, 8 oil pumps, 9 support slippers.
Fig. 5 is medium-and-large-sized machine body surface device solar film battery and working flight view, 1 operator's compartment among the figure, 2 wings, top, 3 cabin parachute compartment, 4 bodies, 5 jet engine cabin doors, 6 jet engines, 7 tail horizontal tails, the 8 tail steering rudder wings, 9 screw propellers, 10 electrodynamic type motor of engine.
Fig. 6 is a microminiature machine compound type parachute work scheme drawing, 1 guiding drogue-parachute among the figure, the big parachute of 2 multi-layer combined types, 3 wings, 4 operator'ies compartment, 5 parachute compartments, 6 bodies, the 7 tail steering rudder wings, 8 jet engines, 9 tail horizontal tails, 10 screw propellers, 11 electric propeller formula motor of engine.
Fig. 7 is a solar film battery supercapacitor device site plan, and figure a is a cross-sectional view, 1 solar battery apparatus layer among the figure, 2 supercapacitor device layers, 3 cabins.Figure b is solar cell supercapacitor device body (part) section plan, and sign is identical with 7a among the figure.
Fig. 8 is a minicomputer vertical takeoff and landing flight lateral plan, 1 screw propeller among the figure, 2 electric propeller formula driving engines (energy deflection angle), 3 wings, 4 driving compartments, 5 parachute compartments, 6 tail normal limbs, 7 jet engines, 8 tail horizontal tails, 9 bodies.
Fig. 9 is medium-sized machine equipment layout front elevation, 1 jet engine among the figure, 2U type support, 3 hydraulic pressure axis of deflection (dotted line), 4 tail horizontal tails, the 5 tail steering rudder wings, 6 axis of deflection gears, 7 deflection hydraulic efficiency gear (hydraulic telescopic type rack), 8 solar cell layers, 9 ultracapacitor layers, 10 bodies, 11 storage batterys, 12 fuel tanks, 13 electric propeller formula driving engines, 14 screw propellers, 15 wings, 16 Partition board for fuel tank.
Figure 10 is that medium-and-large-sized machine main device is arranged scheme drawing, 1 driving compartment among the figure, 2 wings, 3 parachute compartments, 4 bodies, 5 jet engines, 6 horizontal tails, 7 normal limbs, 8 screw propellers, 9 electric propeller formula motor of engine.
The specific embodiment:
Embodiment example 1: shown in 1 (solid line) among Fig. 2, two jet engines are installed on back and forth telescopic parallel the moving and reciprocal deflection frame two ends of postmedian hydraulic pressure in the cabin, two three-phase alternating current high-tension high-power electric propeller formula driving engines 13 are installed at wing 16 two ends, shown in dice among Fig. 5,10, the military machine of using is installed stealthy layer under the solar film battery layer at body outside face device solar film battery.Organize multi-layer high-voltage ultracapacitor 9 at solar cell layer 8 lower devices as shown in Figure 9 more, in the cabin shown in some groups 11 of device fuel tank 12 and the lithium batteries, at drive end unit normal limb 5 and horizontal tail 4 are set, flight forward direction storage battery 11 and ultracapacitor 9 sufficient electrical energies.
As shown in Figure 2, when the needs glide is taken off, the front control hydraulic efficiency gear that takes off is opened double-deck jet engine cabin door, through hydraulic efficiency gear 6 handle with jet engine 1 (solid line) from the parallel flight station that moves in the cabin shown in 1 (dotted line) the figure, at this moment can handle to use and start jet engine 1 (dotted line) and handle simultaneously and use electric propeller formula driving engine 13 that the aircraft glide is taken off.According to landing environment needs vertical takeoff and landing, handling deflection hydraulic efficiency gear (as Fig. 4) as shown in figure 10 turn 90 degrees jet engine 5 partially, handling wing intrinsic deflection hydraulic efficiency gear (as Fig. 4) turn 90 degrees electronic propeller type driving engine 9 on the wing partially, engine condition is shown in 5,9 dotted lines among Figure 10, manipulation starts to use 4 driving engines to produce lift, make body slowly rise to suitable flight space, the operational deflection hydraulic efficiency gear slowly turn 90 degrees driving engine 5,9 partially once more, state is shown in 5,9 solid lines among the figure, and flight can normal flight.The operating process of aircraft vertical landing with take off vertically identical.Before needing as shown in Figure 2 to move under water under water, aircraft is parked in water pump to wing 16 in the water-filling of the water surface (wing has been filled with 10 kilograms with the upward pressure pressurized air in the wing in face of cutting off the water) with dress in the wing, meanwhile discharge pressurized air in the wing 16 (putting back to wing when air is stored in the accumulator unit come-up entirely), close jet engine 1, operation is retracted driving engine 1 in the cabin with hydraulic efficiency gear 6, hermetically closing hatch door window is handled and is used electric propeller formula driving engine 13 to move under water under water.With the hydraulic efficiency gear operation tail normal limb yaw rudder regulating control direction of moving under water under water, handle with dive on the attached wing control of the adjusting lifting of installing on the wing aircraft, dive moves under water with parallel.Also available deflection hydraulic efficiency gear is gone up the control and regulation of electric propeller deflection angle adjusting current direction and is dived, dive is moved under water or emerged with parallel.Need emerge and need and park, when come-up, in wing, fill compression air (emitting) and discharge water in the wing simultaneously by accumulator unit at the water surface.
Moving under water aircraft under water also needs device diving instrument, sonar, telecommunications radar, homing advice, air filtration processing equipment and oxygen unit, bavin electrical propulsion unit etc. except that aircraft Common Instrument and handling device are housed.
Because of the moving airscrew engine work 2 hours of only powering of the high-voltage super cond of design apparatus on the machine and storage battery electric energy, surpass 2 hours and need join the bavin electrical propulsion unit if move under water.The direct current energy inversion that stores is used for the moving airscrew engine of three-phase alternating current high voltage electric energy power supply.
Body adopts and adds crisscross strengthening rib making between the multilayer aluminium alloy layer, and the design body can bear depth of water 200--300 rice depth of water static pressure.
In operator's compartment device instrument and operating control, handle control manual and automatic two cover management systems all are set, operation control system makes and computerizes control automatically.
Embodiment example 2:
As shown in figure 10, two three-phase alternating current high-tension high-power electric propeller formula driving engines 9 of device on the mmi machine wing 2, the device jet engine is 5 two on body postmedian body, each one on limit, the left and right sides, at afterbody horizontal tail 6 and normal limb 7 are set, near driving engine 5, in the body of position fuel tank are set.Embodiment example 2 aircrafts suit on land, the water surface glides or vertical takeoff and landing, can not move under water under water.
Need take off vertically and use as shown in Figure 4, device is being handled about 90 degree of jet engine 5 deflections on the body postmedian top shown in 5 dotted lines among the figure near the hydraulic pressure inflector assembly of driving engine in the cabin, handle about 90 degree of 9 deflections among the electric propeller formula driving engine on the wing 2 such as Figure 10 shown in dotted line with as shown in Figure 4 hydraulic efficiency gear in the preceding wing, handle engine on when taking off, the power that strengthens jet engine throttle and increasing electric propeller formula driving engine is until maximum, the lift that produces with driving engine slowly rises to body in the air, after rising to suitable flying height, operating hydraulically operated device makes slowly about 90 degree of deflection of driving engine, among state such as Figure 10 9, shown in 5 solid lines, aircraft can advance by normal flight, at this moment can use as 9 electric propeller formula driving engines flight among Figure 10 for saving fuel oil, close jet engine 5.Basic identical during vertical landing with the operating process of taking off vertically, when near the landing target, operating hydraulically operated device slowly changes jet engine and electrodynamic type driving engine into the vertical landing state from the flight forward travel state, be about to all about 90 degree of deflection slowly of driving engine, as 5,9 dotted line states among Figure 10, the power that reduces driving engine gradually reduces lift, and controls flying height and direction well, make aircraft slowly vertical landing in the target location.
Before drop in water surface, with 16 air that fill 10 to 12 kilograms of air pressure in wing such as Fig. 2 of the Air compressor in the wing, preceding wing is immersed in and produces buoyancy in the water and hold up body at the water surface.
Personnel and aircraft safety when aloft flying for protecting, shown in 5 positions among Fig. 6, device has one group of multi-layer combined type parachute at middle part, top, cabin, can install the load carrying ability of organizing more or increasing each group umbrella number of plies increase parachute according to the load-carrying needs.Medium-and-large-sized machine is organized more, when a machine has many group umbrellas to use, is docile and obedient preface behind the slave and uses before machine.
Remove body is topped intactly at body outside face device solar film battery outside glass window, organize the high-voltage super cond of multilayer at the solar cell layer lower device more, minicomputer device 2,000 to 3,000 ampere-hours are during medium-and-large-sized machine 5,000 to 1 Wan An.The lithium battery pool-size is during according to required energy device 1,000 to 2 kilo-amperes of flight load-carrying and design flying distance 2 hours, and the storage battery of airborne device and capacitor stores electric energy total volume can make electric propeller formula engine operation more than 2 hours.Is that high-tension high-power electric propeller formula engine operation is used with the electric energy inversion of storage battery and capacitor stores for the three-phase alternating current high potential, use fuel oil after when space, water surface flying, using electric energy earlier, fuel engines is done standby, when only using fuel engines, electric propeller formula driving engine can be converted to the electrical generator mode of operation to battery charge by the electrical motor mode of operation.When needing high-speed flight and vertical takeoff and landing, electric propeller formula and jet engine will be used simultaneously.Two fuel tanks are set in the cabin, the horizontal tail adjustment are set, normal limb regulating control direction at tail.In operator's compartment device instrument and operating control, handle control manual and automatic two cover management systems all are set, operation control system makes and computerizes control automatically.
Body employing multilayer aluminum alloy light metal or multilayer strengthened plastics, carbon fiber composite material, interlayer add crisscross strengthening rib to be made.
Claims (4)
1. the amphibious use of a new forms of energy multifunction aircraft energy, its structure is: have solar film battery to organize at body outside face device more, there is ultracapacitor to organize at the solar cell layer lower device more, under capacitor layer, be body, the device storage battery is organized more in the cabin, fuel tank is set in the cabin, postmedian is equiped with back and forth telescopic parallel mobile reciprocating deflection stand arrangement of hydraulic pressure in the cabin, 2 jet engines are housed at the frame two ends, at body middle front part position extreme lower position installing wing, two end devices at wing have 2 electric propeller formula driving engines, and ejection device has the multi-layer combined type parachute at the middle part, cabin.It is characterized by: install one deck solar film battery (or organic thin film solar cell) outside glass window entirely the most surperficial the removing of body, military affairs are equiped with stealthy layer with machine under solar cell layer, the many groups of tight connection multi-layer high-voltage ultracapacitor under stealthy layer, tight online body under the capacitor layer, body is made by multilayer aluminum alloy light metal material or multilayer carbon fiber composite material or reinforced plastic, and the body interlayer has crisscross strengthening rib to constitute.The aircraft function and usage has the type that moves under water under water and the type that do not move under water under water by the difference of jet engine setting position, and the type that moves under water under water device has equipment such as sonar, diving instrument and dive computer, navigation communication apparatus, diesel-engine generator, people living.The power capacity that the device storage battery is organized storage more in many groups high-voltage super cond that installs on the body and cabin can make aircraft flight or the work 2 hours of moving under water under water, and the direct current energy of storage must inversion be that the moving propeller type driving engine of three-phase high-voltage AC-powered uses.2 of fuel tanks are set in the cabin.At driving compartment device aircraft instrument, manual, automatic two cover operating controls are set, two kinds of operating mode that automatic guidance is controlled with computer.
2. according to right 1, postmedian is equiped with back and forth telescopic parallel the moving and reciprocating type deflection stand arrangement of hydraulic pressure in the cabin, 2 jet engines are housed at the frame two ends, it is characterized by: device is by driving engine U type frame, parallel telescopic mobile bearing and support, the parallel telescopic shifting axle of hydraulic pressure, fixed type bearing and support, parallel telescopic mobile hydraulic pressure deflection gears, the parallel telescopic mobile fluid transmission gear bar of the reciprocating type deflection of driving engine, chute mount, compositions such as hydraulic oil control and regulation valve.Need driving engine parallel telescopic when mobile, operating hydraulically operated device shifts out frame two ends hydraulic pressure translation shaft, axle shifts out the drive parallel telescopic mobile bearing in two ends and support is followed translation, the parallel together jet engine flight station out of my cabin that moves to of driving engine and U type frame is handled the landing flight of can gliding of engine on aircraft.Need vertical takeoff and landing, handle telescopic mobile hydraulic efficiency gear rack and drive reciprocating type parallel mobile reciprocating deflection hydraulic compressor rack device gear, make device need slowly deflection an angle of 90 degrees degree by the landing working flight in the jet engine at frame two ends.Operate this hydraulic efficiency gear and can make driving engine not need the time spent parallelly to be moved back in the cabin, close the double-layer seal cabin door and be convenient to aircraft and move under water under water.Before handling in the wing hydraulic pressure inflector assembly of device make electric propeller formula driving engine deflection an angle of 90 degrees degree slowly on the wing, be used to complete the aircraft vertical takeoff and landing with jet engine with work.Aircraft has multifunctional and multipurpose, and landing mode and range of use are not limited by natural environmental condition, can be vertical at the terrestrial space water surface, glide landing and moving under water under water.
3. according to right 1, at body middle front part position extreme lower position installing wing, two end device electric propeller formula driving engines at wing is characterized by: wing is the low wing of putting, for adapting to the needs of the water surface and underwater operation, wing can fill pressurized air or water-filling.Before need drop to the water surface, in wing, fill pressurized air more than 10 kilograms, make wing in water, produce buoyancy and hold up body with the Air compressor of device in wing.Before the work of need moving under water under water, be parked on the water surface with the water pump of device in wing water-filling and discharge pressurized air (needing to emit when emerging when aircraft moves under water under water) in wing with the storage device stores air.The time of moving under water under water is equipped with diesel-engine generator than needing on the lead aircraft, and for electric propeller formula driving engine provides electric energy, the military machine diesel generation machine of using is between the vacuum interlayer between the sound insulation specialized equipment.Two end devices of wing have 2 three-phase alternating current high-tension high-power electric propeller formula driving engines, the hydraulic pressure inflector assembly that installs in wing is handled, start function by the needs of landing mode deflection an angle of 90 degrees degree slowly, electric propeller formula and the jet engine deflection angle that works together is finished the vertical takeoff and landing process.When only using fuel engines, the wind energy that screw propeller produces when utilizing flight to advance is rotated screw propeller, and electrical motor can be exchanged into the work of electrical generator mode and charges to closed-center system.Only use electric propeller formula driving engine, the aircraft work of can moving under water in the underwater.
4. according to right 1, be top-loaded with the multi-layer combined type parachute in the cabin, it is characterized by: top, cabin medium position be provided with parachute compartment one or more, adorn one group of multi-layer combined type parachute in one cabin, one group of multi-layer umbrella is become by several layers umbrella phase joint group, and there is a guiding umbellule in the umbrella the superiors, launch out earlier umbellule during use, open the back guiding by umbellule and take the superiors' gamp out of, one group of umbrella opens according to level from top to bottom.
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| CN2011101513701A CN102166931A (en) | 2011-06-08 | 2011-06-08 | New energy multifunctional airplane |
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| CN2011101513701A CN102166931A (en) | 2011-06-08 | 2011-06-08 | New energy multifunctional airplane |
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| CN102424107A (en) * | 2011-09-29 | 2012-04-25 | 北京航空航天大学 | Manufacture method of solar airplane |
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| CN103204237A (en) * | 2013-03-19 | 2013-07-17 | 北京航空航天大学 | Aerial propelling device suitable for amphibious unmanned aerial vehicle |
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| CN105947197A (en) * | 2016-04-28 | 2016-09-21 | 上海牧羽航空科技有限公司 | Amphibious aircraft with double-rectification planing-step structure |
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| CN102424107A (en) * | 2011-09-29 | 2012-04-25 | 北京航空航天大学 | Manufacture method of solar airplane |
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| CN103204237A (en) * | 2013-03-19 | 2013-07-17 | 北京航空航天大学 | Aerial propelling device suitable for amphibious unmanned aerial vehicle |
| CN103171756A (en) * | 2013-03-19 | 2013-06-26 | 北京航空航天大学 | Wing rib-free rapid water injection and drainage wing suitable for sea and air across amphibious unmanned aerial vehicle |
| CN103171756B (en) * | 2013-03-19 | 2014-12-10 | 北京航空航天大学 | Wing rib-free rapid water injection and drainage wing suitable for sea and air across amphibious unmanned aerial vehicle |
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| CN104029813A (en) * | 2014-06-04 | 2014-09-10 | 深圳市万博鑫科技有限公司 | Aeronautic amphibious transport plane |
| CN105109682A (en) * | 2015-09-18 | 2015-12-02 | 江苏科技大学 | Wing ship |
| CN105446357A (en) * | 2015-12-31 | 2016-03-30 | 深圳伟思创信息开发有限公司 | Control system and method of amphibious manned aircraft |
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| CN107554783A (en) * | 2017-09-03 | 2018-01-09 | 佛山市龙远科技有限公司 | A kind of amphibious unmanned plane of VTOL |
| CN107554778A (en) * | 2017-09-03 | 2018-01-09 | 佛山市海茂聚航科技有限公司 | A kind of land and water unmanned plane of VTOL |
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| CN107696811A (en) * | 2017-09-03 | 2018-02-16 | 佛山市龙远科技有限公司 | A kind of VTOL amphibious unmanned plane of more power |
| CN108312795A (en) * | 2018-02-05 | 2018-07-24 | 中国船舶科学研究中心（中国船舶重工集团公司第七0二研究所） | Aerial-underwater paleocinetic amphibious aircraft and sailing method can be achieved in one kind |
| CN108312795B (en) * | 2018-02-05 | 2019-06-11 | 中国船舶科学研究中心（中国船舶重工集团公司第七0二研究所） | Aerial-underwater paleocinetic amphibious aircraft and sailing method can be achieved in one kind |
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Application publication date: 20110831 |