CN108528712A - A kind of jet-propelled unmanned aerial vehicle of bull - Google Patents
A kind of jet-propelled unmanned aerial vehicle of bull Download PDFInfo
- Publication number
- CN108528712A CN108528712A CN201710118609.2A CN201710118609A CN108528712A CN 108528712 A CN108528712 A CN 108528712A CN 201710118609 A CN201710118609 A CN 201710118609A CN 108528712 A CN108528712 A CN 108528712A
- Authority
- CN
- China
- Prior art keywords
- jet
- unmanned aerial
- aerial vehicle
- water hydrogen
- hydrogen
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 244000309464 bull Species 0.000 title claims abstract description 28
- 239000001257 hydrogen Substances 0.000 claims abstract description 78
- 229910052739 hydrogen Inorganic materials 0.000 claims abstract description 78
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims abstract description 75
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 47
- 230000005611 electricity Effects 0.000 claims abstract description 11
- 239000002994 raw material Substances 0.000 claims abstract description 11
- 238000003032 molecular docking Methods 0.000 claims abstract description 5
- 239000007789 gas Substances 0.000 claims description 27
- 238000002347 injection Methods 0.000 claims description 19
- 239000007924 injection Substances 0.000 claims description 19
- 210000000078 claw Anatomy 0.000 claims description 12
- 238000010438 heat treatment Methods 0.000 claims description 10
- 239000000446 fuel Substances 0.000 claims description 9
- 239000007788 liquid Substances 0.000 claims description 7
- GBMDVOWEEQVZKZ-UHFFFAOYSA-N methanol;hydrate Chemical compound O.OC GBMDVOWEEQVZKZ-UHFFFAOYSA-N 0.000 claims description 7
- 238000000926 separation method Methods 0.000 claims description 5
- 239000007921 spray Substances 0.000 claims description 5
- 239000000463 material Substances 0.000 claims description 4
- 230000005484 gravity Effects 0.000 claims description 3
- 230000008054 signal transmission Effects 0.000 claims description 3
- 238000004804 winding Methods 0.000 claims description 3
- 150000002431 hydrogen Chemical class 0.000 abstract description 3
- 239000000243 solution Substances 0.000 description 10
- 238000000034 method Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 3
- 230000033001 locomotion Effects 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 208000035473 Communicable disease Diseases 0.000 description 1
- 241001465754 Metazoa Species 0.000 description 1
- 235000004443 Ricinus communis Nutrition 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000009331 sowing Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/12—Propulsion using turbine engines, e.g. turbojets or turbofans
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- 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
- Y02T90/40—Application of hydrogen technology to transportation, e.g. using fuel cells
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Jet Pumps And Other Pumps (AREA)
Abstract
The invention discloses a kind of jet-propelled unmanned aerial vehicles of bull comprising body, from the outwardly extending multiple cantilevered legs of body, correspond multiple jet thrusts set on the outer end of cantilevered leg, the water hydrogen machine set on body, be connected to docking with each jet thrust respectively and be connected to docking with the hot output terminal of water hydrogen machine and the jet plane connected, the support leg on the downside of body be connected with the electricity output end of water hydrogen machine；The jet plane includes that electronic jet plane and heat drive jet plane.It is produced electricl energy and thermal energy using water hydrogen machine consumption water hydrogen feedstock, forming support with jet plane rises air-flow and promote air-flow, pushes aircraft flight, without carrying hydrogen, relative safety is higher, and water hydrogen feedstock is carried and purchased conveniently, raw material is supplemented whenever and wherever possible, exempts the worry to problem of continuing a journey.
Description
Technical field
The present invention relates to a kind of aircraft more particularly to a kind of bull as unmanned means of transport it is jet-propelled nobody
Aircraft.
Background technology
In endoatmosphere, flight is known as aircraft, such as balloon, dirigible, aircraft.They lean on the quiet buoyancy or sky of air
The air force lift-off flight that gas relative motion generates.Wherein, referred to as " unmanned plane ", english abbreviation is UAV
" UAV " is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself.It is defined from technical standpoint
It can be divided into：Unmanned fixed-wing aircraft, unmanned VTOL machine, unmanned airship, unmanned helicopter, unmanned multi-rotor aerocraft, nothing
People's parasol etc..The application field of unmanned plane can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.
Civilian aspect, unmanned plane+sector application, which is unmanned plane, really just have been needed；At present take photo by plane, it is agricultural, plant protection, miniature self-timer, fast
Pass transport, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making,
The purposes of unmanned plane itself has greatly been expanded in the application for manufacturing romance etc. field, and developed country is also in actively extension industry
Using with development unmanned air vehicle technique.
Currently, unmanned plane is most of to be run using storage battery power supply, since the weight of accumulator itself is bigger, take
Charged pool itself needs to consume larger energy, thus there are the short defects of course continuation mileage.Also there is new-type use hydrogen fuel electricity
Battery-powered dynamic mode, however carry hydrogen and need gas cylinder and store enough hydrogen and carry movement, but also there are hydrogen
The inflation problem of the hydrogen supply of safety issue and long-distance travel process that gas carries（Hydrogen fuel cell needs purity sufficient
Enough high hydrogen）.
In addition, the thermal energy that generates of hydrogen production process there is also can not utilize and the phenomenon that waste so that the cost of gas station hydrogen manufacturing
It is high, could not energy-saving and emission-reduction enough be better achieved.
Invention content
In view of the deficiencies of the prior art, the technical problem to be solved in the present invention is to provide a kind of energy-saving safety continue a journey it is carefree
The jet-propelled unmanned aerial vehicle of bull.
In order to solve the above-mentioned technical problem, the technical solution adopted in the present invention is：A kind of jet-propelled unmanned aerial vehicle of bull,
It include body, from the outwardly extending multiple cantilevered legs of body, correspond set on cantilevered leg outer end multiple jet thrusts, set
Be connected in the water hydrogen machine of body, respectively with each jet thrust dock and be connected to the hot output terminal of water hydrogen machine dock and with water hydrogen machine
Electricity output end conducting connection jet plane, the support leg on the downside of body；The jet plane includes electronic jet plane and heat
Drive jet plane；The body is additionally provided with the flight control being connect respectively with water hydrogen machine, jet plane, each jet thrust signal transmission
Device.
A kind of improvement of technical solution as the jet-propelled unmanned aerial vehicle of bull of the present invention, it includes pair that the heat, which drives jet plane,
The air inlet of water receiving hydrogen machine hot output terminal and water hydrogen mechatronics simultaneously suck the gas injection device of ambient atmos, are respectively communicated with air inlet
With the heat exchanger of gas injection device, positioned at heat exchanger rear end and dock the gas outlet of jet thrust；The jet thrust is located on the downside of cantilevered leg
And it can universal rotational.
A kind of improvement of technical solution as the jet-propelled unmanned aerial vehicle of bull of the present invention, the heating channel of the heat exchanger
The interior electricity output end electricity for being equipped with electric heater or/and electric booster pump, the electric heater or/and electric booster pump and the water hydrogen machine
Connection.
A kind of improvement of technical solution as the jet-propelled unmanned aerial vehicle of bull of the present invention, the jet thrust are equipped with tapered injection
Gas port, it is placed in the middle set on puff prot and can axial stretching adjusting taper guide head.
A kind of improvement of technical solution as the jet-propelled unmanned aerial vehicle of bull of the present invention, the jet thrust, which is equipped with, is located at end
The annular-jet that portion is arranged circumferentially and the direct-injection mouth positioned at end face center；The jet thrust is equipped with control annular-jet and and direct-injection
The control valve of mouth opening and closing.
A kind of improvement of technical solution as the jet-propelled unmanned aerial vehicle of bull of the present invention, the jet thrust have hemispherical
The jet portion and jet portion has been evenly arranged multiple gas ports.
A kind of improvement of technical solution as the jet-propelled unmanned aerial vehicle of bull of the present invention, the gas injection device include mutually interconnecting
Logical air pump and check valve, the other side connection heating channel of check valve.
A kind of improvement of technical solution as the jet-propelled unmanned aerial vehicle of bull of the present invention, the water hydrogen machine includes for taking out
It inhales the liquid pump of methanol-water raw material, using piping connection liquid pump delivery outlet and by methanol-water raw material heating and gasifying and reform the weight of separation
Whole device receives separation hydrogen by pipeline and exports battery residual air and produce electricl energy the fuel cell of output, and fuel cell is constituted
The electricity output end of water hydrogen machine, it is to constitute hot output terminal that reformer, which exports high-quality hot gas,；The body is additionally provided with positioned at center of gravity position
The material box for the receiving water hydrogen feedstock set.
A kind of improvement of technical solution as the jet-propelled unmanned aerial vehicle of bull of the present invention, the top of the body, which is equipped with, erects
The standpipe set is erected, riser top ends are equipped with air bag, and the air bag is connected and set by the hydrogen delivery tube of hydrogen Guan Yushui hydrogen machines
Air pump driving is set, air bag top is connected with drag-line, and drag-line passes through standpipe connection to be located at the receipts rope device in body.
A kind of improvement of technical solution as the jet-propelled unmanned aerial vehicle of bull of the present invention, the hydrogen pipe are equipped with bypass and return
Pump is received, and reverse circuit is formed with air pump；The riser top ends be hinged with one group it is circumferentially distributed and hold up air bag prevent it is inclined
Claw；It is correspondingly connected with air bag on the inside of the claw；The top of the claw is connected with lanyard, and lanyard passes through opposite support
Pawl is simultaneously connected to the winding shuttle set by body.
The beneficial effects of the present invention are：It is produced electricl energy and thermal energy using water hydrogen machine consumption water hydrogen feedstock, recycles jet
Machine forms Jet Stream, including the support sprayed downwards rises air-flow and propulsion air-flow backward, to push aircraft flight, without taking
Band hydrogen, relative safety is higher, and water hydrogen feedstock carries and purchase all very convenient, supplements raw material whenever and wherever possible, exempts to continuous
The worry of boat problem.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of the jet-propelled unmanned aerial vehicle solid of bull of the present invention.
Fig. 2 is a kind of planar structure schematic diagram of the jet-propelled unmanned aerial vehicle of bull of the present invention.
Fig. 3 is the organigram of the water hydrogen machine in unmanned plane.
Fig. 4 is a kind of organigram of jet plane in unmanned plane.
Fig. 5 is claw folding structure schematic diagram.
Fig. 6 is the structural schematic diagram of cone mouth jet thrust.
Fig. 7 is a kind of structural schematic diagram of more mouthfuls of jet thrusts.
Specific implementation mode
Specific implementation mode to further illustrate the present invention below in conjunction with the accompanying drawings.
As shown in Figure 1 and Figure 2, a kind of jet-propelled unmanned aerial vehicle of bull of the present invention comprising body 11 prolongs outward from body
Multiple cantilevered legs 12 for stretching correspond multiple jet thrusts 72, the water hydrogen machine set on body 11 set on the outer end of cantilevered leg 12
31, it is connected to respectively with each jet thrust 72 and docks and be connected to the hot output terminal of water hydrogen machine 31 docking and electric defeated with water hydrogen machine 31
Jet plane 71, the support leg 19 positioned at 11 downside of body of outlet conducting connection.The jet plane 71 includes electronic jet plane 73
Jet plane 74 is driven with heat, electric energy is consumed respectively and thermal energy generates air-flow recoil driving force.The body 11 be additionally provided with respectively with water
The flight controller 99 that hydrogen machine 31, jet plane 71,72 signal transmission of each jet thrust connect.It is former that water hydrogen is consumed using water hydrogen machine 31
Material produces electricl energy and thermal energy, and jet plane 71 is recycled to form Jet Stream, including the support sprayed downwards rises air-flow and pushing away backward
Inlet air flow, to push aircraft flight, without carrying hydrogen, relative safety is higher, and water hydrogen feedstock is carried and purchased all very
It is convenient, raw material is supplemented whenever and wherever possible, exempts the worry to problem of continuing a journey.The quantity of jet thrust can be 4,6,8 synchronizations
The flight operation process for controlling aircraft, to more efficiently utilize the energy of water hydrogen.The quantity of general jet thrust be even numbers and
It is symmetrical.Jet plane 71 therein can be turbofan engine, and water hydrogen machine internal exhaust passages setting certain pressure is simultaneously connected to
To the driving chamber of turbofan engine, the effect of forming it into fanjet；Castor can be arranged in support leg 19 therein.
More preferably, refering to what is shown in Fig. 4, it includes the air inlet to 31 hot output terminal of water receiving hydrogen machine that the heat, which drives jet plane 74,
21, the gas injection device 22 of ambient atmos is electrically connected and sucked with water hydrogen machine 31, is respectively communicated with the heat exchanger of air inlet and gas injection device 22
23, positioned at 23 rear end of heat exchanger and the gas outlet 24 of jet thrust 72 is docked, the recoil air-flow of thermal drivers can be generated.
Wherein, the jet thrust 72 be located at the downside of cantilevered leg 12 and can universal rotational, to concentrated when taking off and being lifted to
Lower jet, makes aircraft be lifted steadily, then adjusts jet angle, can generate the propulsion of horizontal direction, comprehensive to constitute flight
Process.
More preferably, electric heater 33 or/and electric booster pump, the electrical heating are equipped in the heating channel of the heat exchanger 23
Device 33 or/and electric booster pump are electrically connected with the electricity output end of the water hydrogen machine.It can be converted electrical energy into using electric heater 33
Thermal energy utilizes together as the energy of promotion air-flow；Jet plane inner cavity can also be pressurized using electric booster pump, it is provided
Air-flow motive force, also by electric energy together using as the power capacity source of buoyancy lift and propulsive force.It thus can be by water hydrogen
The electric energy and thermal energy of raw material conversion utilize together, have the effect of preferable energy-saving and emission-reduction, improve the efficiency of using energy source.
More preferably, refering to what is shown in Fig. 6, the jet thrust 72 is equipped with taper puff prot 75, it is set to puff prot 75 and can between two parties
The guide head 76 for the taper that axial stretching is adjusted sprays the direct-injection gas of recoil strength bigger so as to adjust the airflow shaped of jet
Stream or the better conical flow of stability.
More preferably, refering to what is shown in Fig. 7, the jet thrust 72 is equipped with the annular-jet 77 and position for being located at that end is arranged circumferentially
Direct-injection mouth 78 in end face center；The control valve 79 that the jet thrust 72 is equipped with control annular-jet 77 and is opened and closed with direct-injection mouth 78.
Independent direct-injection mouth 78 opens the direct-injection air-flow that can spray recoil strength bigger；It opens simultaneously annular-jet 77 or individually opens annular-jet
77, the better homogeneous radiation air-flow of stability can be generated.
More preferably, the jet thrust 72 has hemispherical jet portion and the jet portion has been evenly arranged multiple gas ports, can
The shape of Jet Stream is selected to regulate and control the opening and closing of gas port, sprays the direct-injection air-flow or stability of recoil strength bigger
Better conical flow.
More preferably, refering to what is shown in Fig. 4, the gas injection device 22 includes the air pump 26 being interconnected and check valve 27, check valve
27 other side connection heating channel, can discontinuously inject air using air pump 26, can be to avoid liter in conjunction with setting check valve 27
Gas expansion forms recoil in warm channel, to form smooth single way jet formula air-flow.
More preferably, refering to what is shown in Fig. 3, the water hydrogen machine 31 includes for aspirating the liquid pump 33 of methanol-water raw material, using pipe
Road connect 33 delivery outlet of liquid pump and by methanol-water raw material heating and gasifying and reform separation reformer 35, by pipeline receive detach
Hydrogen simultaneously exports battery residual air and produces electricl energy the fuel cell 36 of output, and fuel cell constitutes the electricity output end of water hydrogen machine, weight
It is to constitute hot output terminal that whole device 35, which exports high-quality hot gas,；The body 11 is additionally provided with the receiving water hydrogen feedstock positioned at position of centre of gravity
Material box 18.Entering reformer by the extraction methanol-water raw material of liquid pump 33 to be detached, the exhaust gas of discharge carries amount of heat,
It can use it to and push jet plane operating, realize the efficient utilization of energy.The hydrogen generated simultaneously can pass through fuel cell
Electric energy, the equipment operations such as driving heater, booster are converted to, or drives fan wing operating to generate air-flow formation using motor and pushes away
Into power, the flight of unmanned plane is realized.
More preferably, the top of the body 11 is equipped with the standpipe 51 for erectting setting, and 51 top of standpipe is equipped with air bag 52, institute
It states air bag 52 and the driving of air pump 53 or setting Air Valve Control, air bag 52 is connected and be arranged by the hydrogen delivery tube of hydrogen Guan Yushui hydrogen machines
Top is connected with drag-line 55, and drag-line 55 passes through the connection of standpipe 51 to be located at the receipts rope device 56 in body 11.It is defeated that air pump 53 extracts hydrogen
Being sent to air bag 52 makes it generate buoyancy lift and suspend unmanned plane in midair, and the interim of unmanned plane may be implemented and hover or go slowly, reduce slow
Energy consumption in row operational process enables its activity duration to extend, and the operation of water hydrogen machine can also be made to produce electricl energy supply at this time attached
Belong to equipment to use, such as the agricultural application such as sowing, spray.Setting air valve can also replace air pump control hydrogen to be transported in air bag
Generate suspending power.Standpipe 51, which is arranged, can improve the installation position of air bag 52, prevent air bag from being interfered with rotor, to improve
The safety of unmanned plane.
More preferably, with reference to shown in Fig. 5, the hydrogen pipe is equipped with bypass and recovery pump 57, and is formed inversely with air pump 53
Circuit.After hovering or going slowly, the hydrogen recycling in air bag is got up to utilize again, further increases the effect of using energy source
Rate.51 top of the standpipe be hinged with one group it is circumferentially distributed and hold up air bag 52 and prevent inclined claw 58, avoid air bag from tilting
And interfere with rotor, improve the safety of unmanned plane.58 inside of the claw is correspondingly connected with air bag 52, is vented convenient for air bag 52
It receives folded, avoids receiving folded process air bag 52 and drift and interfere with rotor.Refering to what is shown in Fig. 5, the top of the claw 58 is connected with receipts
Tight rope 59, lanyard 59 pass through opposite claw 58 and are connected to the winding shuttle set by body 11, facilitate the gathering of claw 58,
Folded air bag 52 is preferably received to avoid drifting.
It is above disclosed to be merely a preferred embodiment of the present invention, the right of the present invention cannot be limited with this certainly
Range, therefore according to equivalent variations made by scope of the present invention patent, be still within the scope of the present invention.
Claims (10)
1. a kind of jet-propelled unmanned aerial vehicle of bull, it is characterised in that：Including body, from the outwardly extending multiple cantilevered legs of body,
It corresponds multiple jet thrusts set on the outer end of cantilevered leg, be connected to set on the water hydrogen machine of body, respectively with each jet thrust pair
It connects and is connected to docking with the hot output terminal of water hydrogen machine and the jet plane of connection is connected with the electricity output end of water hydrogen machine, is located under body
The support leg of side；The jet plane includes that electronic jet plane and heat drive jet plane；The body be additionally provided with respectively with water hydrogen machine, spray
The flight controller that mechanism of qi, each jet thrust signal transmission connect.
2. the jet-propelled unmanned aerial vehicle of bull according to claim 1, it is characterised in that：It includes docking that the heat, which drives jet plane,
The air inlet of water hydrogen machine hot output terminal, with water hydrogen mechatronics and suck the gas injection device of ambient atmos, be respectively communicated with air inlet and
The heat exchanger of gas injection device positioned at heat exchanger rear end and docks the gas outlet of jet thrust；The jet thrust is located on the downside of cantilevered leg simultaneously
It can universal rotational.
3. the jet-propelled unmanned aerial vehicle of bull according to claim 2, it is characterised in that：In the heating channel of the heat exchanger
Equipped with electric heater or/and electric booster pump, the electricity output end of the electric heater or/and electric booster pump and the water hydrogen machine is electrically connected
It connects.
4. the jet-propelled unmanned aerial vehicle of bull according to claim 1 or 2, it is characterised in that：The jet thrust is equipped with taper
Puff prot, it is placed in the middle set on puff prot and can axial stretching adjusting taper guide head.
5. the jet-propelled unmanned aerial vehicle of bull according to claim 1 or 2, it is characterised in that：The jet thrust, which is equipped with, to be located at
The annular-jet that end is arranged circumferentially and the direct-injection mouth positioned at end face center；The jet thrust is equipped with control annular-jet and and directly
The control valve of spout opening and closing.
6. the jet-propelled unmanned aerial vehicle of bull according to claim 1 or 2, it is characterised in that：The jet thrust has hemisphere
The shape jet portion and jet portion has been evenly arranged multiple gas ports.
7. the jet-propelled unmanned aerial vehicle of bull according to claim 1, it is characterised in that：The gas injection device includes being interconnected
Air pump and check valve, check valve the other side connection heating channel.
8. the jet-propelled unmanned aerial vehicle of bull according to claim 1, it is characterised in that：The water hydrogen machine includes for aspirating
The liquid pump of methanol-water raw material using piping connection liquid pump delivery outlet and by methanol-water raw material heating and gasifying and reforms the reformation of separation
Device receives separation hydrogen by pipeline and exports battery residual air and produce electricl energy the fuel cell of output, and fuel cell constitutes water
The electricity output end of hydrogen machine, it is to constitute hot output terminal that reformer, which exports high-quality hot gas,；The body is additionally provided with positioned at position of centre of gravity
Receiving water hydrogen feedstock material box.
9. the jet-propelled unmanned aerial vehicle of bull according to claim 1, it is characterised in that：The top of the body, which is equipped with, erects
The standpipe of setting, riser top ends are equipped with air bag, and the air bag is connected and is arranged by the hydrogen delivery tube of hydrogen Guan Yushui hydrogen machines
Air pump drives, and air bag top is connected with drag-line, and drag-line passes through standpipe connection to be located at the receipts rope device in body.
10. the jet-propelled unmanned aerial vehicle of bull according to claim 9, it is characterised in that：The hydrogen pipe is equipped with bypass and returns
Pump is received, and reverse circuit is formed with air pump；The riser top ends be hinged with one group it is circumferentially distributed and hold up air bag prevent it is inclined
Claw；It is correspondingly connected with air bag on the inside of the claw；The top of the claw is connected with lanyard, and lanyard passes through opposite support
Pawl is simultaneously connected to the winding shuttle set by body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710118609.2A CN108528712A (en) | 2017-03-01 | 2017-03-01 | A kind of jet-propelled unmanned aerial vehicle of bull |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710118609.2A CN108528712A (en) | 2017-03-01 | 2017-03-01 | A kind of jet-propelled unmanned aerial vehicle of bull |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108528712A true CN108528712A (en) | 2018-09-14 |
Family
ID=63488720
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710118609.2A Pending CN108528712A (en) | 2017-03-01 | 2017-03-01 | A kind of jet-propelled unmanned aerial vehicle of bull |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108528712A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3835213A1 (en) * | 2019-12-09 | 2021-06-16 | 2706649 Ontario Ltd | Lift and drive unit, aircraft and submarine vehicle |
| US11652226B2 (en) | 2020-02-19 | 2023-05-16 | 2706649 Ontario Ltd | Hydrogen developing body and process of making the same |
| US11881577B2 (en) | 2019-11-28 | 2024-01-23 | 2706649 Ontario Ltd | Active element, hydrogen generating apparatus, and electrical energy generating apparatus |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030230671A1 (en) * | 2000-08-24 | 2003-12-18 | Dunn James P. | Fuel cell powered electric aircraft |
| US20080070078A1 (en) * | 2006-09-19 | 2008-03-20 | Hamilton Sundstrand Corporation | Jet fuel based high pressure solid oxide fuel cell system |
| CN101367435A (en) * | 2008-09-16 | 2009-02-18 | 广州伟韬电子科技有限公司 | Novel air injection aerial vehicle |
| CN104362359A (en) * | 2014-11-07 | 2015-02-18 | 广东合即得能源科技有限公司 | Electric generator based on methanol water hydrogen-making system and electricity generation method thereof |
| CN104993162A (en) * | 2015-06-24 | 2015-10-21 | 上海合既得动氢机器有限公司 | Methanol hydrogen electric aircraft |
| US20160325834A1 (en) * | 2015-05-07 | 2016-11-10 | Curtis Asa Foster | In-flight battery recharging system for an unmanned aerial vehicle |
| CN206645009U (en) * | 2017-03-01 | 2017-11-17 | 广东合即得能源科技有限公司 | A kind of jet-propelled unmanned aerial vehicle of bull |
-
2017
- 2017-03-01 CN CN201710118609.2A patent/CN108528712A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030230671A1 (en) * | 2000-08-24 | 2003-12-18 | Dunn James P. | Fuel cell powered electric aircraft |
| US20080070078A1 (en) * | 2006-09-19 | 2008-03-20 | Hamilton Sundstrand Corporation | Jet fuel based high pressure solid oxide fuel cell system |
| CN101367435A (en) * | 2008-09-16 | 2009-02-18 | 广州伟韬电子科技有限公司 | Novel air injection aerial vehicle |
| CN104362359A (en) * | 2014-11-07 | 2015-02-18 | 广东合即得能源科技有限公司 | Electric generator based on methanol water hydrogen-making system and electricity generation method thereof |
| US20160325834A1 (en) * | 2015-05-07 | 2016-11-10 | Curtis Asa Foster | In-flight battery recharging system for an unmanned aerial vehicle |
| CN104993162A (en) * | 2015-06-24 | 2015-10-21 | 上海合既得动氢机器有限公司 | Methanol hydrogen electric aircraft |
| CN206645009U (en) * | 2017-03-01 | 2017-11-17 | 广东合即得能源科技有限公司 | A kind of jet-propelled unmanned aerial vehicle of bull |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11881577B2 (en) | 2019-11-28 | 2024-01-23 | 2706649 Ontario Ltd | Active element, hydrogen generating apparatus, and electrical energy generating apparatus |
| EP3835213A1 (en) * | 2019-12-09 | 2021-06-16 | 2706649 Ontario Ltd | Lift and drive unit, aircraft and submarine vehicle |
| US11652226B2 (en) | 2020-02-19 | 2023-05-16 | 2706649 Ontario Ltd | Hydrogen developing body and process of making the same |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11530036B2 (en) | Fixed-wing aerial underwater vehicle and control method thereof | |
| CN108528712A (en) | A kind of jet-propelled unmanned aerial vehicle of bull | |
| CN105217033B (en) | Amphibious rotor wing unmanned aerial vehicle | |
| CN106218849A (en) | Aerial wind energy power station formula aircraft and aerial fixing aircraft device | |
| CN110667838A (en) | Solar energy telescopic wing water-air dual-purpose unmanned aerial vehicle | |
| CN108622384A (en) | A kind of rotor air-jet combinatorial formula mother aircraft | |
| CN206645009U (en) | A kind of jet-propelled unmanned aerial vehicle of bull | |
| CN211107984U (en) | Solar energy telescopic wing water-air dual-purpose unmanned aerial vehicle | |
| CN107021235B (en) | A kind of low-to-medium altitude aircraft driving device, driving method and low-to-medium altitude aircraft | |
| CN206544596U (en) | A kind of many rotor unmanned aerial vehicles | |
| CN108622373A (en) | A kind of jet-propelled mother aircraft of bull | |
| CN107554351A (en) | To the aerogenerator device people of high electric air commercial aircraft wireless power | |
| CN108688785A (en) | A kind of rotor push type power airship | |
| CN105109695A (en) | Multifunctional aircraft with hybrid of oil and electricity | |
| CN108688788A (en) | A kind of Powered Propulsion fire balloon | |
| CN108528697A (en) | A kind of more rotor unmanned aerial vehicles | |
| CN108528696A (en) | A kind of rotor air-jet combinatorial formula unmanned aerial vehicle | |
| CN211810220U (en) | Air-drop device for water search and rescue | |
| CN207045715U (en) | A kind of novel and multifunctional unmanned plane | |
| CN206645025U (en) | A kind of jet-propelled unmanned aerial vehicle of single rotor | |
| CN206645005U (en) | A kind of rotor air-jet combinatorial formula unmanned aerial vehicle | |
| CN108528733A (en) | A kind of jet-propelled unmanned aerial vehicle of single rotor | |
| CN206900643U (en) | A kind of agricultural spraying unmanned plane | |
| CN207826544U (en) | A kind of manned unmanned exchange aircraft of double ducts | |
| CN108622407A (en) | A kind of jet-propulsion formula power glider |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |