The foldable electrically-driven tilting large manned aircraft comprises a fuselage, tilting driving motors are arranged on the front portion and the rear portion of the fuselage correspondingly, tilting shafts are connected to the tilting driving motors, folding arms are rotationally connected to the ends, on the two sides of the fuselage, of the tilting shafts correspondingly, and paddles and folding driving motors are arranged at the ends of the folding arms. The folding aircraft has the beneficial effects that the blades are locked to be parallel to the folding arms before folding, the blades are prevented from rotating, the folding arms of the aircraft arms at the front part of the aircraft body are folded backwards, the folding arms at the rear part of the aircraft body are folded forwards, the structure is more compact, and the problems that the aircraft body is damaged due to the fact that the aircraft is too large in size and the blades are easily bumped or scratched during transportation are solved. And when the aircraft is stored or transported indoors, the occupied space is large, and the cost is high. And the front folding arm and the rear folding arm have a certain height difference, so that the problems of large attitude angle change and limited wind resistance of the aircraft in a high-speed forward flying state are solved.
本发明涉及一种可折叠式电驱动倾转大型载人飞行器,包括:机身,机身前后部的均设有一个倾转驱动电机,倾转驱动电机连接有倾转轴,倾转轴在机身两侧的端部分别转动连接有折叠臂,折叠臂的端部设有桨叶和折叠驱动电机。本发明的有益效果是:在折叠前将桨叶锁定在与折叠臂平行的状态,防止桨叶转动,机身前部的机臂折叠臂向后折叠,机身后部的折叠臂向前折叠,使结构更加紧凑,解决了因飞行器体积过大,在运输时桨叶容易磕碰或刮蹭损坏飞机本体,从而影响飞行器可靠性,且在室内储放或运输时所占空间很大,导致成本较高的问题;前折叠臂与后折叠臂有一定的高度差,解决了飞行器大速度前飞状态下姿态角变化大及抗风能力有限的难题。
Foldable electrically-driven tilting large manned aircraft
一种可折叠式电驱动倾转大型载人飞行器
2024-05-10
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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