CN108945484A - A kind of two-way air injection aerial vehicle - Google Patents
A kind of two-way air injection aerial vehicle Download PDFInfo
- Publication number
- CN108945484A CN108945484A CN201810707865.XA CN201810707865A CN108945484A CN 108945484 A CN108945484 A CN 108945484A CN 201810707865 A CN201810707865 A CN 201810707865A CN 108945484 A CN108945484 A CN 108945484A
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- CN
- China
- Prior art keywords
- empennage
- jet
- aerial vehicle
- aircraft
- cabin
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- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/16—Aircraft characterised by the type or position of power plant of jet type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
Abstract
A kind of two-way air injection aerial vehicle, belongs to vehicle technology field.It is characterized by comprising the uniformly distributed multiple groups jet empennages of the pressurization cabin (1) for being located at center and pressurization cabin (1) surrounding annular, cabin (1) outside pressurize equipped with air inlet (3), supercharging device is installed in inside, the uniformly distributed multiple air outlets (4) being individually connected to jet empennage of annular in cabin (1) surrounding same level of pressurizeing；The jet empennage is ring jet empennage (8), and the end face of ring jet empennage (8) is equipped with multiple puff prots (12).The present invention integrally uses symmetrical structure, and weight distribution is uniform, and center warehouse is provided with the device that can produce aerodynamic energy, and overall structure improves the energy consumption ratio and stability of aircraft, aircraft is allow to make more complicated movement in the sky.The overall structure of aircraft, which makes aircraft substantially, will not occur unexpected air crash accident of turning on one's side, and improve the safety of aircraft.
Description
Technical field
A kind of two-way air injection aerial vehicle, belongs to vehicle technology field.
Background technique
Jet aircraft is main a kind of structure type in aircraft, but current jet aircraft is mostly side
Jet pushes the form of aircraft forward flight, and there is no the forms of the surrounding setting multiple groups puff prot in aircraft, moreover, by
Stability after the limitation of the structure of existing aircraft, the exceedingly difficult movements such as the stability of aircraft, and overturning is poor,
It is easy to happen rollover after overturning, therefore, especially complex movement can not be made, flexibility is not high.
Summary of the invention
The technical problems to be solved by the present invention are: overcoming the deficiencies of the prior art and provide a kind of compact-sized, design conjunction
Reason, can steadily make the two-way air injection aerial vehicle of highly difficult rotary movement.
The technical solution adopted by the present invention to solve the technical problems is: a kind of two-way air injection aerial vehicle, it is characterised in that:
The uniformly distributed multiple groups jet empennage of pressurization cabin and pressurization cabin surrounding annular including being located at center, the external side of compression chamber is set
There is air inlet, supercharging device is installed in inside, and annular is uniformly distributed multiple independent with jet empennage in cabin surrounding same level of pressurizeing
The air outlet of connection；The jet empennage is ring jet empennage, and the end face of ring jet empennage is equipped with multiple puff prots.
Aircraft of the invention is whole preferably to use carbon fiber, and high strength light plastic or light-duty alloy are made, and reduce and fly
The load of row device improves cruising ability.Aircraft integrally uses central symmetry, and structure symmetrical above and below, weight distribution is uniform, mentions
High flight stability and stablizing for front and back sides are converted.Whole includes center warehouse and multiple two-way annular puff prots.Center warehouse
It is provided with the device that can produce aerodynamic energy, in order not to break aircraft balance symmetrical above and below, air inlet is on warehouse top
Side, it is preferably symmetrical.The overall structure of aircraft improves the energy consumption ratio and stability of aircraft, and aircraft is allow to exist
More complicated movement is made in the air.The overall structure of aircraft, which makes aircraft substantially, will not occur unexpected air crash accident of turning on one's side, and mention
The high safety of aircraft.
The supercharging device is turbogenerator or turbo-dynamo.
The air inlet be equipped with it is multiple, it is radial inclination be evenly arranged on pressurization cabin top.Air is by center warehouse
The air inlet of side enters, and pressurizes in aerodynamic energy device, by the flow control and direction controlling of two-way guide pipeline, from
The puff prot in one direction of two-way annular puff prot sprays, and provides kinetic energy for aircraft.
It is equipped with gas transportation machine structure between the ring jet empennage and pressurization cabin, gas transportation machine structure includes ventilation
Pipe, empennage attachment base and air-lock, ventilation duct are straight pipe, and one end is connected to air outlet, and other end connection ring jet empennage enters
Air port, the ventilation duct and pressurization cabin junction are equipped with flow and adjust air-lock.
There are two air-locks in the controllable guide pipeline of two-way, and the air-lock close to center warehouse is by controlling annular puff prot
Jet amount, to control energy；The air-lock for being mounted on the controllable guide pipeline fork of two-way is commutated by the two-way of control gas,
To control the commutation of two-way annular puff prot.Two-way annular puff prot is in upper and lower symmetrical structure, can carry out both direction up and down
Jet, provide kinetic energy for aircraft.
The air supply tube that two-way is arranged in parallel, and ventilation duct and annular are equipped between the ventilation duct and ring jet empennage
Jet empennage junction is equipped with commutation air-lock.
The air supply tube is arc setting.
Hinged swing connecting bar between the ventilation duct and ring jet empennage is formed by swing connecting bar and is rotatablely connected.
The ring jet empennage is the shell with annular housing, is respectively equipped with multiple groups in the upper and lower end faces of shell
Puff prot, it is corresponding, annular housing inside division at upper and lower two gas circulate cavity.
The puff prot is obliquely installed or equipped with the wind deflector being obliquely installed.
Compared with prior art, the present invention has the beneficial effects that
Aircraft of the invention is whole preferably to use carbon fiber, and high strength light plastic or light-duty alloy are made, and reduce aircraft
Load, improve cruising ability.Aircraft integrally uses central symmetry, and structure symmetrical above and below, weight distribution is uniform, improves and flies
Row stability and stablizing for front and back sides are converted.Whole includes center warehouse and multiple two-way annular puff prots.Center warehouse is built-in
Have the device that can produce aerodynamic energy, in order not to break aircraft balance symmetrical above and below, air inlet in the side on warehouse top,
It is preferred that symmetrical.The overall structure of aircraft improves the energy consumption ratio and stability of aircraft, allows aircraft in the sky
Make more complicated movement.The overall structure of aircraft, which makes aircraft substantially, will not occur unexpected air crash accident of turning on one's side, and improve
The safety of aircraft.
Detailed description of the invention
Fig. 1 is two-way air injection aerial vehicle structure top view schematic diagram.
Fig. 2 is the front view schematic diagram of Fig. 1.
Fig. 3 is pressurization cabin and empennage connection relationship diagram.
Fig. 4 is ring jet tail structure schematic diagram.
Wherein, 1, pressurization cabin 2, turbogenerator 3, air inlet 4, air outlet 5, ventilation duct 6, swing connecting bar 7,
Empennage attachment base 8, ring jet empennage 9, air supply tube 10, commutation air-lock 11, flow adjust air-lock 12, puff prot.
Specific embodiment
Fig. 1 ~ 4 are highly preferred embodiment of the present invention, and 1 ~ 4 the present invention will be further described with reference to the accompanying drawing.
Referring to attached drawing 1 ~ 4: a kind of two-way air injection aerial vehicle, pressurization cabin 1 and pressurization cabin 1 including being located at center
The uniformly distributed multiple groups jet empennage of surrounding annular, pressurize cabin 1 on the outside of be equipped with air inlet 3, inside installation supercharging device, pressurize cabin
The uniformly distributed multiple air outlets 4 being individually connected to jet empennage of annular in 1 surrounding same level；The jet empennage is annular
The end face of jet empennage 8, ring jet empennage 8 is equipped with multiple puff prots 12.Supercharging device is turbogenerator or turbine electricity
Machine.Air inlet 3 be equipped with it is multiple, it is radial inclination be evenly arranged on pressurization cabin 1 top.
Ring jet empennage 8 and pressurization cabin 1 between be equipped with gas transportation machine structure, gas transportation machine structure include ventilation duct 5,
Empennage attachment base 7 and air-lock, ventilation duct 5 are straight pipe, and one end is connected to air outlet 4, and other end connection ring jet empennage 8 enters
Air port, ventilation duct 5 and pressurization 1 junction of cabin are equipped with flow and adjust air-lock 11.
The air supply tube 9 that two-way is arranged in parallel is equipped between ventilation duct 5 and ring jet empennage 8, and ventilation duct 5 and annular are sprayed
8 junction of gas empennage is equipped with commutation air-lock 10.Air supply tube 9 is arc setting.It is hinged between ventilation duct 5 and ring jet empennage 8
Swing connecting bar 6 is formed by swing connecting bar 6 and is rotatablely connected.
Ring jet empennage 8 is the shell with annular housing, is respectively equipped with multiple groups jet in the upper and lower end faces of shell
Mouthfuls 12, it is corresponding, it circulates cavity in the inside division of annular housing at upper and lower two gas.Puff prot 12 is obliquely installed or is equipped with
The wind deflector being obliquely installed.
Aircraft of the invention uses the structure of similar multi-rotor aerocraft, is illustrated with quadrotor.Aircraft is integrally preferred
Using carbon fiber, high strength light plastic or light-duty alloy are made, and reduce the load of aircraft, improve cruising ability.
Aircraft integrally uses central symmetry, and structure symmetrical above and below, weight distribution is uniform, improve flight stability and
Stablize conversion in front and back sides.Whole includes center warehouse, multiple controllable guide pipelines of two-way and multiple two-way annular puff prots.In
Heart warehouse is provided with turbogenerator, turbo-dynamo or other can produce the device of aerodynamic energy, in order not to break on aircraft
Lower symmetrical balance, air inlet are symmetrical in warehouse side.There are two air-locks in the controllable guide pipeline of two-way, close to center
The air-lock of warehouse passes through the jet amount for controlling annular puff prot, to control energy；It is mounted on the controllable guide pipeline turnout of two-way
The air-lock of mouth is commutated by the two-way of control gas, to control the commutation of two-way annular puff prot.Two-way annular puff prot is presented
Lower symmetrical structure can carry out the jet of upper and lower both direction, provide kinetic energy for aircraft.
Air is entered by the air inlet of center warehouse side, is pressurizeed in aerodynamic energy device, is passed through two-way guide pipeline
Flow control and direction controlling, sprayed from the puff prot in a direction of two-way annular puff prot, provide kinetic energy for aircraft.
The overall structure of aircraft improves the energy consumption ratio and stability of aircraft, makes that aircraft in the sky more
Complicated movement.The overall structure of aircraft, which makes aircraft substantially, will not occur unexpected air crash accident of turning on one's side, and improve aircraft
Safety.
The above described is only a preferred embodiment of the present invention, being not that the invention has other forms of limitations, appoint
What those skilled in the art changed or be modified as possibly also with the technology contents of the disclosure above equivalent variations etc.
Imitate embodiment.But without departing from the technical solutions of the present invention, according to the technical essence of the invention to above embodiments institute
Any simple modification, equivalent variations and the remodeling made, still fall within the protection scope of technical solution of the present invention.
Claims (9)
1. a kind of two-way air injection aerial vehicle, it is characterised in that: pressurization cabin (1) and pressurization cabin including being located at center
(1) the uniformly distributed multiple groups jet empennage of surrounding annular, pressurization cabin (1) outside are equipped with air inlet (3), inside installation supercharging device,
The uniformly distributed multiple air outlets (4) being individually connected to jet empennage of annular in cabin (1) surrounding same level of pressurizeing；The spray
Gas empennage is ring jet empennage (8), and the end face of ring jet empennage (8) is equipped with multiple puff prots (12).
2. a kind of two-way air injection aerial vehicle according to claim 1, it is characterised in that: the supercharging device is turbine hair
Motivation or turbo-dynamo.
3. a kind of two-way air injection aerial vehicle according to claim 1, it is characterised in that: the air inlet (3) is equipped with more
A, radial inclination is evenly arranged on the top of pressurization cabin (1).
4. a kind of two-way air injection aerial vehicle according to claim 1, it is characterised in that: the ring jet empennage (8)
Gas transportation machine structure is equipped between pressurization cabin (1), gas transportation machine structure includes that ventilation duct (5), empennage attachment base (7) are gentle
Lock, ventilation duct (5) are straight pipe, and one end is connected to air outlet (4), and the other end is connected to the air intake vent of ring jet empennage (8), described
Ventilation duct (5) and pressurization cabin (1) junction are equipped with flow and adjust air-lock (11).
5. a kind of two-way air injection aerial vehicle according to claim 4, it is characterised in that: the ventilation duct (5) and annular
The air supply tube (9) that two-way is arranged in parallel, and ventilation duct (5) and ring jet empennage (8) junction are equipped between jet empennage (8)
Equipped with commutation air-lock (10).
6. a kind of two-way air injection aerial vehicle according to claim 5, it is characterised in that: the air supply tube (9) is arc
Setting.
7. a kind of two-way air injection aerial vehicle according to claim 4, it is characterised in that: the ventilation duct (5) and annular
Hinged swing connecting bar (6) between jet empennage (8) is formed by swing connecting bar (6) and is rotatablely connected.
8. a kind of two-way air injection aerial vehicle according to claim 1, it is characterised in that: the ring jet empennage (8)
For the shell with annular housing, it is respectively equipped with multiple groups puff prot (12) in the upper and lower end faces of shell, it is corresponding, in annular chamber
The inside division of body is at upper and lower two gas circulation cavity.
9. a kind of two-way air injection aerial vehicle according to claim 1, it is characterised in that: puff prot (12) inclination is set
It sets or equipped with the wind deflector being obliquely installed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810707865.XA CN108945484A (en) | 2018-07-02 | 2018-07-02 | A kind of two-way air injection aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810707865.XA CN108945484A (en) | 2018-07-02 | 2018-07-02 | A kind of two-way air injection aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108945484A true CN108945484A (en) | 2018-12-07 |
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ID=64484868
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810707865.XA Pending CN108945484A (en) | 2018-07-02 | 2018-07-02 | A kind of two-way air injection aerial vehicle |
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| Country | Link |
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| CN (1) | CN108945484A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110481760A (en) * | 2019-07-15 | 2019-11-22 | 陈云桥 | No blade rotates air duct engine aircraft engine |
| CN112298609A (en) * | 2019-07-29 | 2021-02-02 | 之江实验室 | Jet-propelled mars detection unmanned aerial vehicle |
| CN113247258A (en) * | 2021-07-02 | 2021-08-13 | 国网福建省电力有限公司连城县供电公司 | Unmanned aerial vehicle without rotor wing |
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| CN2188544Y (en) * | 1994-04-09 | 1995-02-01 | 卢杲 | Flying disc |
| CN101857085A (en) * | 2010-06-03 | 2010-10-13 | 刘春� | Aircraft |
| CN201882248U (en) * | 2010-10-21 | 2011-06-29 | 刘新广 | Novel high-speed helicopter |
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| CN204916161U (en) * | 2015-08-19 | 2015-12-30 | 杨海涛 | No rotorcraft multiaxis aircraft |
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| CN107021235A (en) * | 2017-04-06 | 2017-08-08 | 王子墨 | A kind of low-to-medium altitude aircraft driving device, driving method and low-to-medium altitude aircraft |
| CN206456566U (en) * | 2017-02-12 | 2017-09-01 | 杨海涛 | Applied to Multi-axis aircraft without rotor air generation plants |
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2018
- 2018-07-02 CN CN201810707865.XA patent/CN108945484A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2188544Y (en) * | 1994-04-09 | 1995-02-01 | 卢杲 | Flying disc |
| CN101857085A (en) * | 2010-06-03 | 2010-10-13 | 刘春� | Aircraft |
| CN201882248U (en) * | 2010-10-21 | 2011-06-29 | 刘新广 | Novel high-speed helicopter |
| CN203528814U (en) * | 2013-11-09 | 2014-04-09 | 高伟洛 | Aircraft |
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| CN206456566U (en) * | 2017-02-12 | 2017-09-01 | 杨海涛 | Applied to Multi-axis aircraft without rotor air generation plants |
| CN107021235A (en) * | 2017-04-06 | 2017-08-08 | 王子墨 | A kind of low-to-medium altitude aircraft driving device, driving method and low-to-medium altitude aircraft |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110481760A (en) * | 2019-07-15 | 2019-11-22 | 陈云桥 | No blade rotates air duct engine aircraft engine |
| CN112298609A (en) * | 2019-07-29 | 2021-02-02 | 之江实验室 | Jet-propelled mars detection unmanned aerial vehicle |
| CN112298609B (en) * | 2019-07-29 | 2022-06-28 | 之江实验室 | Jet-propelled mars detection unmanned aerial vehicle |
| CN113247258A (en) * | 2021-07-02 | 2021-08-13 | 国网福建省电力有限公司连城县供电公司 | Unmanned aerial vehicle without rotor wing |
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