CN102774493B - Variable wing type land, sea and air triphibian aircraft - Google Patents
Variable wing type land, sea and air triphibian aircraft Download PDFInfo
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- CN102774493B CN102774493B CN201210279456.7A CN201210279456A CN102774493B CN 102774493 B CN102774493 B CN 102774493B CN 201210279456 A CN201210279456 A CN 201210279456A CN 102774493 B CN102774493 B CN 102774493B
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Abstract
The invention discloses a variable wing type land, sea and air triphibian aircraft, which comprises an aircraft body, wings, an engine, a propeller and aircraft wheels, wherein deformation wings are arranged on two sides of the aircraft body and are formed by superposing more than two wings which are arranged in parallel in a staggered mode; the front ends of the wings are fixed; the rear ends of the wings are movable ends; the wings are connected with a driving joystick through connecting rods; movable flaps are arranged on outer end plates of the deformation wings; an output shaft of the engine is connected with the propeller; the propeller is arranged inside a fan duct; the rear of the aircraft body is provided with two eudipleural tail beams; and a vertical empennage and a horizontal empennage are arranged on the tail beams. The variable wing type land, sea and air triphibian aircraft is provided with the aircraft wheels and the aircraft body, so that the aircraft can be parked on the ground and the water surface and can take off and land; and the flight is controlled by controlling unfolding or folding of the deformation wings, the safety performance is high, and the propeller is arranged in the duct, so that airflow flowing through the propeller is straight, the aerodynamic efficiency and overall thrust of the propeller are improved, and the ground personnel are hardly injured or objects on the ground are hardly hit.
Description
Technical field
The present invention relates to a kind of wing formula land, water and air three that become to dwell aircraft.
Background technology
Middle-size and small-size manned craft particularly aviette is gently little because of it, park and landing without the need to large airport, obtain widespread use and develop rapidly at civil area in recent years, and hovercar also has the trend of large research great development, these represent an important development direction of future transportation instrument.In the various small-sized manned craft schemes such as aviette, ultra light aircraft, hovercar, hydroairplane class is because having good comprehensive advantage without the need to airport.But existing ground effect vehicle or hydroairplane use on land and also exist many not as people's will part in high-altitude flight.
Summary of the invention
Object of the present invention is just to provide a kind of safe and reliable, good economy performance, aircraft is dwelt in adaptable change wing formula land, water and air three.
Dwell aircraft in change wing formula land, water and air three of the present invention, comprise fuselage, wing, driving engine, screw propeller, vertical tail, tailplane, wheel, belly has the power-actuated wheel of drive, fuselage both sides dress Variable Geometry Wing, Variable Geometry Wing is made up of the superposition that interlocks of the fin of the above arrangement in parallel of two panels, the front end of fin is fixed, fin rear end is movable end, fin is all connected with drive control lever by connecting rod each other, Variable Geometry Wing outer end plate arranges movable flap, it is motor-powered machinery space above fuselage afterbody, driving engine is motor or combustion engine, engine output shaft is connected with screw propeller, carrying screws moves, it is inner that screw propeller is installed on fan duct, fuselage afterbody is provided with two symmetrical tail booms, vertical tail and tailplane tail boom be equipped with.
Dwelling aircraft in change wing formula land, water and air three of the present invention, parks ground and ground run by wheel, also can in the same landing of ground image surface fixed wing aircraft.When the water surface is parked with landing, propeller works, produce thrust, fuselage is moved ahead fast, and wing can produce lift, realizes the horizontal flight of aircraft.Can handle the distortion of both sides Variable Geometry Wings by the joystick of operator's compartment, when Variable Geometry Wing separates (or opening), Variable Geometry Wing becomes multiple wing structure, and aircraft has very large lift effect, can high-altitude flight; When Variable Geometry Wing closes (or closed), Variable Geometry Wing becomes single-blade structure, adds that outside end plate forms the both wings of ground effect vehicle, can extreme low-altitude or water surface flying; The outside flap of wing can above folding or tie, and coordinates Variable Geometry Wing to open and carries out high-altitude flight.
Change wing formula land, water and air three of the present invention aircraft of dwelling has wheel, also has hull, both can park and landing on ground, can park and landing again at the water surface, can not by the impact on airport; Launched by controlling distortion wing or closed and control flight, safety performance is high.Screw propeller is contained in duct, makes the air-flow flowing through screw propeller more straight, improves the pneumatic efficiency of screw propeller and overall thrust, is not easy injure ground staff or get to ground object when ground or low latitude travel simultaneously.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Fig. 2 is the A-A cut-away view that in Fig. 1, Variable Geometry Wing launches.
Fig. 3 is the A-A cut-away view that in Fig. 1, Variable Geometry Wing is closed.
Detailed description of the invention
Dwell aircraft in a kind of wing formula land, water and air three that become, comprise fuselage 1, wing, driving engine 5, screw propeller 7, vertical tail 9, tailplane 8, wheel 11, fuselage 1 belly has the power-actuated wheel 11 of drive, fuselage 1 both sides dress Variable Geometry Wing 2, Variable Geometry Wing 2 is made up of the superposition that interlocks of the fin of the above arrangement in parallel of two panels, the front end of fin is fixed, fin rear end is movable end, fin is all connected with drive control lever 12 by connecting rod 13 each other, Variable Geometry Wing 2 outer end plate 3 arranges movable flap 4, movable flap 4 can up be turned up, fuselage 1 rear upper is the machinery space that driving engine 5 is housed, driving engine 5 is motor or combustion engine, driving engine 5 output shaft is connected with screw propeller 7, it is inner that screw propeller 7 is installed on fan duct 6, fuselage 1 rear portion is provided with two symmetrical tail booms 10, vertical tail 9 and tailplane 8 tail boom 10 be equipped with.
Claims (2)
1. one kind becomes wing formula land, water and air three and to dwell aircraft, comprise fuselage (1), wing, driving engine (5), screw propeller (7), vertical tail (9), tailplane (8), wheel (11), fuselage (1) belly has the power-actuated wheel of drive (11), it is characterized in that: fuselage (1) both sides dress Variable Geometry Wing (2), Variable Geometry Wing (2) is made up of the superposition that interlocks of the fin of the above arrangement in parallel of two panels, the front end of fin is fixed, fin rear end is movable end, fin is all connected with drive control lever (12) by connecting rod (13) each other, Variable Geometry Wing (2) outer end plate (3) is arranged movable flap (4), fuselage (1) rear upper is for being equipped with the machinery space of driving engine (5), driving engine (5) output shaft is connected with screw propeller (7), it is inner that screw propeller (7) is installed on fan duct (6), fuselage (1) rear portion is provided with two symmetrical tail booms (10), vertical tail (9) and tailplane (8) tail boom (10) be equipped with.
2. dwell aircraft in change wing formula land, water and air three according to claim 1, it is characterized in that: driving engine (5) is motor or combustion engine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210279456.7A CN102774493B (en) | 2012-08-08 | 2012-08-08 | Variable wing type land, sea and air triphibian aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210279456.7A CN102774493B (en) | 2012-08-08 | 2012-08-08 | Variable wing type land, sea and air triphibian aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102774493A CN102774493A (en) | 2012-11-14 |
| CN102774493B true CN102774493B (en) | 2015-05-13 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210279456.7A Expired - Fee Related CN102774493B (en) | 2012-08-08 | 2012-08-08 | Variable wing type land, sea and air triphibian aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102774493B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3315404A1 (en) * | 2016-10-25 | 2018-05-02 | AeroMobil R&D, s. r. o. | Configurable tail for flying car |
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| CN102795070A (en) * | 2012-09-03 | 2012-11-28 | 张廷林 | Aeroamphibious triphibian aircraft with machine body capable of fully balancing stress |
| CN104002972B (en) * | 2013-02-25 | 2016-04-06 | 许祖勇 | Three body warship submarine aircrafts |
| US10518595B2 (en) | 2013-03-15 | 2019-12-31 | Terrafugia, Inc. | Combined flying/driving vehicle with vertical takeoff and fixed-wing cruise capabilities |
| CN104163083A (en) * | 2013-05-19 | 2014-11-26 | 刘祖学 | Multi-purpose vehicle |
| CN103692873B (en) * | 2013-12-20 | 2015-11-18 | 胡新如 | A kind of land and water hovercar |
| CN109153302A (en) | 2016-04-15 | 2019-01-04 | 特力飞车股份有限公司 | The electron gear shifting device assembly of vehicle is flown and driven for double mode |
| CN106184712B (en) * | 2016-08-10 | 2019-02-19 | 牧羽航空科技（江苏）有限公司 | A kind of amphibious aircraft with autobalance empennage |
| CN106945822B (en) * | 2017-03-09 | 2019-08-02 | 杭州米为科技有限公司 | A kind of method and apparatus for the pitching controlling aircraft |
| CN106741979B (en) * | 2017-03-09 | 2023-08-15 | 杭州米为科技有限公司 | Transmission structure for aircraft |
| CN110015400A (en) * | 2019-03-26 | 2019-07-16 | 南昌航空大学 | A kind of distributed power formula aircraft |
| CN109849604B (en) * | 2019-03-29 | 2023-10-13 | 熊子见 | Folding rotor triphibian aircraft |
| CN111845233A (en) * | 2020-08-05 | 2020-10-30 | 朱支能 | Triphibian vehicle |
| CN114180027B (en) * | 2021-12-24 | 2023-04-07 | 清华大学 | Control method and controller of morphing aircraft and application of controller |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN85104530A (en) * | 1985-06-15 | 1987-01-07 | 古飞 | Controllable wing-folded full-lift type road airplane |
| US5145129A (en) * | 1991-06-06 | 1992-09-08 | Grumman Aerospace Corporation | Unmanned boom/canard propeller v/stol aircraft |
| CN1303803A (en) * | 1999-10-26 | 2001-07-18 | 杨福顺 | Helitruck aircraft |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6848649B2 (en) * | 2000-10-03 | 2005-02-01 | Charles Gilpin Churchman | V/STOL biplane aircraft |
| US20030094536A1 (en) * | 2001-10-25 | 2003-05-22 | Labiche Mitchell G. | Flyable automobile |
| US8152096B2 (en) * | 2005-10-18 | 2012-04-10 | Smith Frick A | Apparatus and method for vertical take-off and landing aircraft |
-
2012
- 2012-08-08 CN CN201210279456.7A patent/CN102774493B/en not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN85104530A (en) * | 1985-06-15 | 1987-01-07 | 古飞 | Controllable wing-folded full-lift type road airplane |
| US5145129A (en) * | 1991-06-06 | 1992-09-08 | Grumman Aerospace Corporation | Unmanned boom/canard propeller v/stol aircraft |
| CN1303803A (en) * | 1999-10-26 | 2001-07-18 | 杨福顺 | Helitruck aircraft |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3315404A1 (en) * | 2016-10-25 | 2018-05-02 | AeroMobil R&D, s. r. o. | Configurable tail for flying car |
| WO2018077808A1 (en) * | 2016-10-25 | 2018-05-03 | Aeromobil R&D, S. R. O. | Configurable tail for flying car |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102774493A (en) | 2012-11-14 |
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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 | ||
| EE01 | Entry into force of recordation of patent licensing contract |
Application publication date: 20121114 Assignee: NANCHANG HUAMENGDA AVIATION TECHNOLOGY DEVELOPMENT CO., LTD. Assignor: Nanchang Univ. of Aviation Contract record no.: 2015360000109 Denomination of invention: Variable wing type land, sea and air triphibian aircraft Granted publication date: 20150513 License type: Exclusive License Record date: 20150625 |
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| LICC | Enforcement, change and cancellation of record of contracts on the licence for exploitation of a patent or utility model | ||
| 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: 20150513 Termination date: 20200808 |