Double-rotor tilting aircraft and flight control method thereof
Double-rotor tilting aircraft and flight control method thereof
- Neue Suche nach: LIU ZEFENG
- Neue Suche nach: LIU ZEFENG
The invention provides a double-rotor tilting aircraft and a flight control method thereof. The aircraft comprises a fuselage main body, a left tilting rotor fixed to the left side of the fuselage main body, a left rotor fixed to the left tilting rotor, a right tilting rotor fixed to the right side of the fuselage main body, a right rotor fixed to the right tilting rotor and an empennage set fixed to the tail of the fuselage main body. The empennage group comprises a vertical empennage, a horizontal empennage and a horizontal tail rotor; wherein the left rotor wing and the right rotor wing realize flight power and attitude control of vertical take-off and landing and cruising of the aircraft. The unmanned aerial vehicle is separated left and right, independently tilts, and has various different actions according to flight conditions; the wingspan of the aircraft not only can tilt, but also can be folded; according to the invention, vertical take-off and landing, high-speed cruise, transition stability between vertical hovering and high-speed cruise can be obtained, and the method has the advantage of very high use economy.
本发明提供一种双旋翼倾转飞行器及其飞行控制方法，飞行器包括机身主体、固定在所述机身主体左侧的左倾转翼、固定在所述左倾转翼上的左旋翼、固定在所述机身主体右侧的右倾转翼、固定在所述右倾转翼上的右旋翼、以及固定在所述机身主体尾部的尾翼组，所述尾翼组包括垂直尾翼、水平尾翼以及水平尾桨；其中所述左旋翼和右旋翼实现飞行器垂直起降和巡航的飞行动力和姿态控制。本发明左右分开且独立倾转，并且依据飞行条件有各种不同的作动；本发明飞行器的翼展不仅倾转，还可以折叠；实施本发明可以获得垂直起降，高速巡航，垂直悬停与高速巡航之间过渡平稳，同时具备非常高的使用经济性之好处。
Dokumentinformationen
Double-rotor tilting aircraft and flight control method thereof
一种双旋翼倾转飞行器及其飞行控制方法
2023-04-07
Patent
Elektronische Ressource
Chinesisch
| IPC: | B64C AEROPLANES , Flugzeuge |
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