CN103708038B - Double-dragon aircraft - Google Patents
Double-dragon aircraft Download PDFInfo
- Publication number
- CN103708038B CN103708038B CN201210378058.0A CN201210378058A CN103708038B CN 103708038 B CN103708038 B CN 103708038B CN 201210378058 A CN201210378058 A CN 201210378058A CN 103708038 B CN103708038 B CN 103708038B
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- CN
- China
- Prior art keywords
- aircraft
- dragon
- double
- electromotor
- wind
- 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.)
- Expired - Fee Related
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Classifications
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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
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Wind Motors (AREA)
Abstract
The present invention is a kind of type aircraft, is named as double-dragon aircraft.Double-dragon aircraft need not aviation fuel, and it drives by electric motor, and electromotor can do vector variation upwards, backward.The sustainable electric energy supplement of wind-driven generator carried on aircraft, the electric energy that electromotor sends even can be directly output to electric motor group by following superior technique.Double-dragon aircraft uses the new type propeller that two or more wing tips tilt.
Description
Art
Technical field
The present invention is a kind of novel aerospace craft
Background technology
Gyroplane needs aviation fuel, and the cost of aviation fuel is the highest.The huge wing of gyroplane still suffers from the weight of electromotor
Measuring, this makes system structure extremely complex, and anti-fatigue performance is poor, and stability is the most undesirable.So gyroplane should now
Little.
Summary of the invention
The present invention is a kind of type aircraft.This aircraft need not aviation fuel, and it uses electric motor to drive, and electromotor can
To do vector variation upwards, backward.Being disposed with wind powered generator system at fuselage rear, the impeller of wind-driven generator is two rotations
The centre of the wing, the high velocity air that it can utilize two rotors to produce when electromotor is in level backward is implemented wind-force and is sent out
Electricity, electric energy is stored in battery the supply of electric power ensureing that the electric motor of aircraft has abundance, and following superior technique is even
The electric energy that electromotor sends can be directly output to electromotor use.Double-dragon aircraft uses two or more wing tips to tilt
New type propeller, this is to strengthen the paddle working area to air, thus obtains more kinetic energy, and this is compared with the longest
Paddle more saves space.Double-dragon aircraft is different from gyroplane, and it is not placed on electromotor on fixed-wing.Double dragon formulas fly
Machine is different from helicopter, and his electromotor is outside fuselage, and electromotor itself can do change vector action.
The invention has the beneficial effects as follows and solve the problem that aircraft engine relies on aviation fuel.Double-dragon aircraft has preferably
Stability, higher kinetic energy, this also means that this aircraft will have bigger lifting capacity, more carrying capacity.Due to double
The electromotor of dragon formula aircraft is outside fuselage, it is simple to maintenance, so self supportability of double-dragon aircraft is the highest, and Ke Yiyou
Longer service life.
Accompanying drawing explanation
Basic structure
Fig. 1 is the structural representation of double-dragon aircraft, wherein: 1-operating system display；2-fuselage trousers；3-is preposition
Power generator fan；The preposition electromotor of 4-；5-accumulator；6-flight signal lamp；7-paddle；8-electromotor；9-electromotor connects seat；
10-engine spindle；11-changes horizontally disposed electromotor into；The rearmounted electromotor of 12-；13-rearmounted generator drive paddle；14-
Empennage；15-control handle；16-pilot seat；17-front-wheel；18-seat；19-trailing wheel；20-is plug-in.
Fig. 2 is the rearview of double-dragon aircraft.Fig. 3 is the top view of double-dragon aircraft.
Detailed description of the invention
The structural representation of double-dragon aircraft is shown in accompanying drawing 1.Double-dragon aircraft deploys wind-power electricity generation above fuselage
Machine and electromotor connect seat.What electromotor connected seat carrying is engine spindle, and main shaft two ends are the electromotors of variable vector.This
Two airscrew engines are all electric motors.Electric motor, by the storage battery power supply after wind-driven generator, carries for aircraft
For power.In the inside of engine spindle equipped with micro-machine and thumb wheel.Thumb wheel rotates under control of the control system and promotes to send out
Motivation turns an angle by regulation, thus realizes becoming the action of vector.Another set of generating is also deployed after the fuselage of aircraft
Unit.The driving paddle of this generating set is in the centre of two main paddles.When two main paddles change into horizontally disposed backward,
The rotation direction of two main oars is identical, just has the strongest wind in the periphery of two main paddles, and the driving paddle of generating set is just
Being rotated by this high wind, generating set just obtains kinetic energy to start generating and charges for accumulator, it is ensured that aircraft has
Lasting electric energy supply.
Double-dragon aircraft is when main paddle is for being arranged vertically, and aircraft will have the mobility as helicopter.For protecting
Card aircraft will not deflect, and two paddle one the first from left are right, and the spin that fuselage is produced by they is relative, and two power offset
Aircraft would not be made to produce deflection.The engine power of side is the most suitably decreased or increased, makes both sides crosswind
Producing different spins, fuselage is necessarily affected by the side that wind-force is strong to be deflected towards opposite side, so that it may realize changing aircraft flight
The purpose in direction, this mode even can be carried out with original place.Therefore changing two electromotors is that different vector revolution can
Obtain more mobility.
Double-dragon aircraft, when electromotor is arranged horizontally, the rotation direction changing paddle just can realize propeller use
The pulling force that the thrust advanced is slowed down the most backward, this has very great help for the horizontal maneuver performance improving aircraft.
Claims (1)
1. double-dragon aircraft, uses electric motor to drive, and it is mainly characterized by this aircraft and is disposed with wind-force at fuselage rear
Generator system, the impeller of wind-driven generator is in the centre of two rotors, and when electromotor is in level backward, it is permissible
The high velocity air utilizing two rotors to produce implements wind-power electricity generation, and electric energy is stored in battery the electric motor ensureing aircraft
There is the supply of electric power of abundance.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210378058.0A CN103708038B (en) | 2012-10-09 | 2012-10-09 | Double-dragon aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210378058.0A CN103708038B (en) | 2012-10-09 | 2012-10-09 | Double-dragon aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103708038A CN103708038A (en) | 2014-04-09 |
| CN103708038B true CN103708038B (en) | 2016-08-17 |
Family
ID=50401463
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210378058.0A Expired - Fee Related CN103708038B (en) | 2012-10-09 | 2012-10-09 | Double-dragon aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103708038B (en) |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2229413A (en) * | 1989-03-22 | 1990-09-26 | Michael John Leigh Chapman | Rotating circular wing aircraft |
| CN2420228Y (en) * | 2000-02-29 | 2001-02-21 | 韩玮 | High performance propeller |
| MX2007000821A (en) * | 2004-07-21 | 2007-09-11 | Delta T Corp | Fan blades and modifications. |
| CN102582819B (en) * | 2010-08-03 | 2016-01-20 | 王庆源 | Wind power airplane |
| CN201864038U (en) * | 2010-10-31 | 2011-06-15 | 王治岳 | Self-feeding electric air vehicle |
-
2012
- 2012-10-09 CN CN201210378058.0A patent/CN103708038B/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN103708038A (en) | 2014-04-09 |
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Legal Events
| Date | Code | Title | Description |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| DD01 | Delivery of document by public notice | ||
| DD01 | Delivery of document by public notice |
Addressee: Jiang Yinzhi Document name: payment instructions |
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| DD01 | Delivery of document by public notice | ||
| DD01 | Delivery of document by public notice |
Addressee: Jiang Yinzhi Document name: Notice of termination of patent right |
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160817 Termination date: 20211009 |