CN108715223A - Efficient aircraft power source - Google Patents
Efficient aircraft power source Download PDFInfo
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- CN108715223A CN108715223A CN201810042001.0A CN201810042001A CN108715223A CN 108715223 A CN108715223 A CN 108715223A CN 201810042001 A CN201810042001 A CN 201810042001A CN 108715223 A CN108715223 A CN 108715223A
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Abstract
The present invention relates to a kind of efficient aircraft power sources, belong to space flight and aviation technical field.This disc-shaped flying craft has low latitude, low speed, VTOL, the features such as hovering, have both the function of helicopter and fixed-wing an ancient type of spoon machine, technical support can be provided for multiple fields, flight is without geographical restrictions, accident illumination and rescue rescue etc. are provided, the aircraft is by chassis, cluster engine, cockpit, and idler wheel composition, the disc-shaped flying craft uses laser, the technologies such as electricity injection effectively promote the flight efficiency of disc-shaped flying craft, it avoids the sky using rotor as flight engine occupancy aircraft and asks excessive disadvantage, the sky for effectively reducing engine is asked, flight efficiency can be improved, with good development potentiality.
Description
Technical field
The present invention is divisional application, and the application number of female case is：2014100464858.The present invention relates to a kind of efficient
Aircraft power source belongs to space flight and aviation technical field.
Background technology
Disc-shaped flying craft has the characteristics that low latitude, low speed, VTOL, hovering, has both helicopter and fixed wing aircraft
Function can provide technical support for multiple fields, and without geographical restrictions, flight track can be preset, also can at any time more for flight
Change, can be widely applied to aviation take pictures, geological survey, ultra-high-tension power transmission line tour, oil filed pipeline inspection, freeway management,
Forest fire protection cruising, poison gas are reconnoitred, are enforced the drug law, accident illumination, building the side such as temporary communications platform and emergency management and rescue, rescue
Face.The space that disc-shaped flying craft often uses rotor to occupy aircraft as flight engine is excessive, how to reduce the space of engine,
Improve flight efficiency, using high-tech come promoted these problems of the flight efficiency of disc-shaped flying craft have it is to be solved.
Invention content
The purpose of the present invention is to provide a kind of efficient aircraft power sources.
The technical scheme is that：The aircraft is Dished aircraft, by chassis 24, cluster engine 26, and cockpit 27,
And the composition such as idler wheel 25, cockpit shape are hemisphere, are constituted using three cluster engines, three engines are with axial symmetry point
Cloth is in equilateral triangle vertex, and three idler wheels are distributed with axial symmetry, is in equilateral triangle vertex, the top of two triangles
Point is uniformly distributed, and cluster engine is by water system, oil supply system, laser emitter, combustion chamber, jet system, gas handling system
It constitutes；Gas enters combustion chamber 15 after turbocharging first from air entry 13 by check valve, and laser emits laser at this time
Violent high temperature is generated in heat build-up meniscus 5, air instantaneous expansion arrives air inlet cavity 4 through jet pipe 16, sprayed, reached by puff prot 1
To the purpose departed；When airship accelerates, fuel liquid enters spray chamber 20 by woven hose 22, and electromagnetic valve coil 18 is logical
Electricity, EFI piston press fuel liquid are sprayed to heat build-up meniscus 5 from spray-hole and are expanded by laser heating combustion generated gas,
Air inlet cavity 4 is arrived through jet pipe 16, is sprayed by puff prot 1, flying saucer accelerates；Smooth motion when, using fuel oil
It is worked alternatively for power with vapor, i.e., when the use of vapor being power source, water enters injection from water tank 12 to woven hose 22
Chamber 20, electromagnetic valve coil 18 are powered, and EFI piston press water is sprayed from spray-hole to heat build-up meniscus 5 to be heated by laser, wink
Between generate high-pressure steam through jet pipe 16 arrive air inlet cavity 4, sprayed by puff prot 1, generate power.
The invention jet system turns to ball cover 3 by puff prot 1, steering ball 2, and air inlet cavity 4 is constituted, wherein turning to ball cover 3
For spherical shape, on spherical top, there are one windows, so that puff prot is in the rotation of wide-angle, the slave window of gas is injected into
In the cavity of steering ball 2, in this way, can freely control the heading of airship when sprinkler rotation.
Electronic spray-head 6 is by resetting spring 17, electromagnetic valve coil 18, injector head wall 19, spray chamber 20, spray-hole 21, infusion
Pipe 22, EFI piston 23 are constituted, and when liquid is entered by woven hose 22 in spray chamber 20, electromagnetic valve coil 18 is powered, EFI
Piston 23 squeezes the liquid in spray chamber 20, and liquid is made to be sprayed from spray-hole 21, AEI After End of Injection, and EFI piston 23 is resetting bullet
It resets and bounces back under the action of spring 17, during retraction, aspirate air from spray-hole 21 is interior, on the one hand can clear up the spray of nozzle
Perforation 21, pre- anti-clogging；Another aspect partial air enters in spray chamber 20, causes cavity part low density gas vacuum, next
Secondary liquid, which is spurted into from the gap between woven hose 22 and piston in spray chamber 20, forms the first air-fuel mixture of misty liquid droplets realization,
So that having more good atomizing effect when really spraying.
Air inlet uses electronic supercharging, when air enters air entry 13, drives fan 39 right by primary motor 29 first
Air is pressurized, and air is pressurized by the fan that secondary motor is driven again later, and air after supercharged passes through unidirectional
After valve 33, into wind conveying pipe 14, for preventing from going here and there on air-flow, motor is fixed on using holder 31 on air entry wall check valve.
Laser：The semiconductor laser that the present invention uses be substance is worked with certain semi-conducting material and generate by
The device of effect is penetrated in excitation.Its operation principle is by certain energisation mode, in energy band (conduction band and the valence of semiconductor substance
Band) between or energy band and impurity (acceptor or donor) energy level of semiconductor substance between, realize the particle of nonequilibrium carrier
Number reversion just generates stimulated emission effect when a large amount of electronics in population inversion state are with hole-recombination.Semiconductor swashs
There are mainly three types of the energisation modes of light device, i.e. electrical pumping formula, optical pumping formula and high-power electron beam Exciting-simulator system.Electrical pumping formula semiconductor swashs
Light device, usually made of GaAs (GaAs), cadmium sulfide (CdS), indium phosphide (I nP), zinc sulphide (ZnS) etc. material
Semiconductor junction diode generates stimulated emission along forward bias Injection Current into row energization in junction plane region.Optical pumping formula
Semiconductor laser generally uses N-type or P-type semiconductor monocrystalline (such as GaAS, I nAs, I nSb etc.) substance of working, with other
The laser that laser is sent out makees optical pumping excitation.High-power electron beam Exciting-simulator system semiconductor laser is typically also with N-type or p-type
Semiconductor monocrystal (such as PbS, CdS, ZhO etc.) substance of working, by injecting high-power electron beam into row energization by outside.Partly leading
In volumetric laser device, better performances, application it is wider be the electrical pumping formula GaAs diode lasers with double-heterostructure.
The advantages of laser diode, has：Efficient, small, light-weight and price is low.Especially multiple quantum well type
Efficiency has 20%-40%, P-N types also to reach several 0-25%, and all in all energy efficiency height is its greatest feature.In addition, it
Continuous output wavelength covers infrared ray to visible-range.
Advantageous effect
The disc-shaped flying craft of the present invention avoids excessive scarce in space for occupying aircraft as flight engine using rotor
Point effectively reduces the space of engine, improves flight efficiency, and dish is effectively promoted using technologies such as laser, electrosprays and is flown
The flight efficiency of row device has good development potentiality.
Description of the drawings
Fig. 1 is main view diagrammatic cross-section of the present invention；
Fig. 2 is top cross-sectional view of the present invention；
Fig. 3 cluster engine structural schematic diagrams；
Fig. 4 electromagnetic injection valve diagrammatic cross-sections；
Fig. 5 plenum mouth structure schematic diagrames.
In figure respectively marked as：1：Puff prot, 2：Steering ball, 3：Steering ball cover, 4：Air inlet cavity, 5. heat build-up meniscus, 6：
Electronic spray-head, 7：Seal nipple, 8：Petroleum pipeline, 9：Laser transfer tube, 10：Laser emitter, 11：Fuel tank, 12：Water tank, 13：It inhales
Gas port, 14：Wind conveying pipe, 15：Combustion chamber, 16：Jet pipe, 17 resetting springs, 18：Electromagnetic valve coil, 19：Injector head wall, 20：Spray
Penetrate chamber, 21：Spray-hole, 22：Woven hose, 23：EFI piston, 24：Chassis, 25：Idler wheel, 26：Cluster engine, 27：Cockpit,
28：Air blow check valve, 29：Primary motor, 30：Fan, 31：Holder, 32：Air entry wall, 33：Check valve.
Specific implementation mode
With reference to the accompanying drawings and examples, the invention will be further described, but present disclosure be not limited to it is described
Range.
Embodiment 1：The aircraft is Dished aircraft, by chassis 24, cluster engine 26, cockpit 27 and idler wheel 25
Deng composition, cockpit shape is hemisphere, is constituted using three cluster engines, and three engines are distributed with axial symmetry, in equilateral
Triangular apex.Three idler wheels are distributed with axial symmetry, are in equilateral triangle vertex, and two vertexs of a triangle are uniformly distributed,
Its cluster engine is made of water system, oil supply system, laser emitter, combustion chamber, jet system, gas handling system；Gas is first
From air entry 13, combustion chamber 15 is entered by check valve after turbocharging, laser emits laser in heat build-up half a month at this time
Plate 5 generates violent high temperature, and air instantaneous expansion arrives air inlet cavity 4 through jet pipe 16, sprayed by puff prot 1, reach and depart
Purpose；When airship accelerates, fuel liquid enters spray chamber 20 by woven hose 22, and electromagnetic valve coil 18 is powered, EFI piston
Fuel liquid is squeezed to spray to heat build-up meniscus 5 by laser heating combustion generated gas expansion, through jet pipe 16 from spray-hole
It to air inlet cavity 4, is sprayed by puff prot 1, flying saucer accelerates；Smooth motion when, use fuel oil and vapor for
Power works alternatively, and when the use of vapor being power source, water enters spray chamber 20, solenoid valve from water tank 12 to woven hose 22
Coil 18 is powered, and EFI piston press water is sprayed from spray-hole to heat build-up meniscus 5 to be heated by laser, and moment generates high pressure water
Steam arrives air inlet cavity 4 through jet pipe 16, is sprayed by puff prot 1, generates power.
Embodiment 2：The aircraft is Dished aircraft, by chassis 24, cluster engine 26, cockpit 27 and idler wheel 25
Deng composition, cockpit shape is hemisphere, is constituted using three cluster engines, and three engines are distributed with axial symmetry, in equilateral
Triangular apex.Three idler wheels are distributed with axial symmetry, are in equilateral triangle vertex, and two vertexs of a triangle are uniformly distributed,
Its cluster engine is made of water system, oil supply system, laser emitter, combustion chamber, jet system, gas handling system；Gas is first
From air entry 13, combustion chamber 15 is entered by check valve after turbocharging, laser emits laser in heat build-up half a month at this time
Plate 5 generates violent high temperature, and air instantaneous expansion arrives air inlet cavity 4 through jet pipe 16, sprayed by puff prot 1, reach and depart
Purpose；When airship accelerates, fuel liquid enters spray chamber 20 by woven hose 22, and electromagnetic valve coil 18 is powered, EFI piston
Fuel liquid is squeezed to spray to heat build-up meniscus 5 by laser heating combustion generated gas expansion, through jet pipe 16 from spray-hole
It to air inlet cavity 4, is sprayed by puff prot 1, flying saucer accelerates；Smooth motion when, use fuel oil and vapor for
Power works alternatively, and when the use of vapor being power source, water enters spray chamber 20, solenoid valve from water tank 12 to woven hose 22
Coil 18 is powered, and EFI piston press water is sprayed from spray-hole to heat build-up meniscus 5 to be heated by laser, and moment generates high pressure water
Steam arrives air inlet cavity 4 through jet pipe 16, is sprayed by puff prot 1, generates power.
The invention jet system turns to ball cover 3 by puff prot 1, steering ball 2, and air inlet cavity 4 is constituted, wherein turning to ball cover 3
For spherical shape, on spherical top, there are one windows, so that puff prot is in the rotation of wide-angle, the slave window of gas is injected into
In the cavity of steering ball 2, in this way, can freely control the heading of airship when sprinkler rotation.
Electronic spray-head 6 is by resetting spring 17, electromagnetic valve coil 18, injector head wall 19, spray chamber 20, spray-hole 21, infusion
Pipe 22, EFI piston 23 are constituted, and when liquid is entered by woven hose 22 in spray chamber 20, electromagnetic valve coil 18 is powered, EFI
Piston 23 squeezes the liquid in spray chamber 20, and liquid is made to be sprayed from spray-hole 21, AEI After End of Injection, and EFI piston 23 is resetting bullet
It resets and bounces back under the action of spring 17, during retraction, aspirate air from spray-hole 21 is interior, on the one hand can clear up the spray of nozzle
Perforation 21, pre- anti-clogging；Another aspect partial air enters in spray chamber 20, causes cavity part low density gas vacuum, next
Secondary liquid, which is spurted into from the gap between woven hose 22 and piston in spray chamber 20, forms the first air-fuel mixture of misty liquid droplets realization,
So that having more good atomizing effect when really spraying.
Air inlet uses electronic supercharging, when air enters air entry 13, drives fan 39 right by primary motor 29 first
Air is pressurized, and air is pressurized by the fan that secondary motor is driven again later, and air after supercharged passes through unidirectional
After valve 33, into wind conveying pipe 14, for preventing from going here and there on air-flow, motor is fixed on using holder 31 on air entry wall check valve.
The present invention has been described in detail through specific embodiments, but these not constitute the limit to the present invention
System.Without departing from the principles of the present invention, those skilled in the art can also make many modification and improvement, these are also answered
It is considered as protection scope of the present invention.
Claims (1)
1. a kind of efficient aircraft power source, it is characterised in that：The aircraft is Dished aircraft, by chassis, engine
The compositions such as group, cockpit and idler wheel, cockpit shape are hemisphere, are constituted using three cluster engines, three engines are with axis
It is symmetrical, it is in equilateral triangle vertex, three idler wheels are distributed with axial symmetry, are in equilateral triangle vertex, two triangles
The vertex of shape is uniformly distributed, and cluster engine is by water system, oil supply system, laser emitter, combustion chamber, jet system, into
Gas system is constituted；
Electronic spray-head is made of resetting spring, electromagnetic valve coil, injector head wall, spray chamber, spray-hole, woven hose, EFI piston,
Electronic spray-head is divided into water spray and the nozzle of oil spout, and structure is identical, electric when liquid is entered by woven hose in spray chamber
Magnet valve coil is powered, and the liquid in EFI piston press spray chamber makes liquid be sprayed from spray-hole, and oil spout or water spray terminate
Afterwards, EFI piston resets retraction under the action of resetting spring, and during retraction, air is aspirated out of spray-hole, on the one hand
The spray-hole of nozzle, pre- anti-clogging can be cleared up, another aspect partial air enters in spray chamber, causes local low density gas true
Sky, gap of the liquid between woven hose and piston, which is spurted into spray chamber, next time forms misty liquid droplets and realizes that first oil gas is mixed
It closes, really there is when injection more good spray effect；
Air inlet uses electronic supercharging, when air enters air entry, drives fan to increase air by primary motor first
Pressure, air is pressurized by the fan that secondary motor is driven again later, after air after supercharged is by check valve, is entered
Wind conveying pipe, for preventing from going here and there on air-flow, motor is fixed on using holder on air entry wall check valve.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810042001.0A CN108715223B (en) | 2014-02-10 | 2014-02-10 | Aircraft power source |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810042001.0A CN108715223B (en) | 2014-02-10 | 2014-02-10 | Aircraft power source |
| CN201410046485.8A CN103754365B (en) | 2014-02-10 | 2014-02-10 | It is a kind of using laser and the butterfly aircraft power source of EFI |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410046485.8A Division CN103754365B (en) | 2014-02-10 | 2014-02-10 | It is a kind of using laser and the butterfly aircraft power source of EFI |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108715223A true CN108715223A (en) | 2018-10-30 |
| CN108715223B CN108715223B (en) | 2021-08-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410046485.8A Active CN103754365B (en) | 2014-02-10 | 2014-02-10 | It is a kind of using laser and the butterfly aircraft power source of EFI |
| CN201810042001.0A Active CN108715223B (en) | 2014-02-10 | 2014-02-10 | Aircraft power source |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN201410046485.8A Active CN103754365B (en) | 2014-02-10 | 2014-02-10 | It is a kind of using laser and the butterfly aircraft power source of EFI |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN109502037A (en) * | 2018-11-14 | 2019-03-22 | 哈尔滨工程大学 | A kind of urgent descending mechanism of the reversed jet bubbling crystallzation aviation aircraft water surface |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947199B (en) * | 2016-05-03 | 2017-03-22 | 王西银 | Autoroatation self-flinging antigravity butterfly-shaped aircraft |
| KR101885640B1 (en) * | 2016-12-01 | 2018-08-07 | 박형수 | Drones |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109502037A (en) * | 2018-11-14 | 2019-03-22 | 哈尔滨工程大学 | A kind of urgent descending mechanism of the reversed jet bubbling crystallzation aviation aircraft water surface |
| CN109502037B (en) * | 2018-11-14 | 2021-11-09 | 三亚哈尔滨工程大学南海创新发展基地 | Water surface forced landing mechanism of reverse air-jet ventilation cavitation aviation aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103754365A (en) | 2014-04-30 |
| CN108715223B (en) | 2021-08-10 |
| CN103754365B (en) | 2018-03-02 |
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