The invention provides a multi-propeller 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, at least one left front power paddle and at least one left rear power paddle which are fixed to the two opposite sides of the left tilting rotor respectively, and a right tilting rotor fixed to the right side of the fuselage main body. The at least one right front power paddle and the at least one right rear power paddle are respectively fixed on two opposite sides of the right tilting wing; the empennage group is fixed at the tail part of the fuselage main body; the empennage group comprises a vertical empennage, a horizontal empennage and a horizontal tail paddle; wherein the left front power paddle, the left rear power paddle, the right front power paddle and the right rear power paddle 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 vertical take-off and landing, high-speed cruising and transition stability between vertical hovering and high-speed cruising can be achieved, and meanwhile the advantage of very high use economy is achieved.
本发明提供一种多桨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、分别固定在所述左倾转翼相对两侧的至少一个左前动力桨和至少一个左后动力桨、固定在所述机身主体右侧的右倾转翼、分别固定在所述右倾转翼相对两侧的至少一个右前动力桨和至少一个右后动力桨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;其中所述左前动力桨、左后动力桨、右前动力桨和右后动力桨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。
Multi-propeller tilting aircraft and flight control method thereof
一种多桨倾转飞行器及其飞行控制方法
2023-03-31
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
MULTI-PROPELLER TILTING AIRCRAFT AND FLIGHT CONTROL METHOD THEREFOR
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