The invention relates to a tilting folding wing variant unmanned aerial vehicle, which consists of a fuselage, tilting folding wings, an undercarriage, an empennage, a main rotor wing and a tail rotor wing, vertical take-off and landing and fixed wing state cruising can be achieved through tilting of the tilting folding wings, and the wings can be folded to reduce the space occupied by ground parking. The tilting folding wings move backwards while tilting to the fixed wing state from the vertical take-off and landing state, so that the focuses of the wings are located behind the gravity center when the aircraft flies in the fixed wing state, and the whole aircraft has static stability. According to the tilting folding wing variant unmanned aerial vehicle, through reasonable cooperation and connection of all the components, the problems that an existing tilting wing unmanned aerial vehicle does not have static stability in the fixed wing state and the wing cannot be folded, so that the occupied space is large when the unmanned aerial vehicle is parked on the ground are solved.
一种倾转折叠翼变体无人机,由机身、倾转折叠机翼、起落架、尾翼、主旋翼、尾旋翼组成。通过倾转折叠机翼的倾转可实现垂直起降与固定翼状态巡航,机翼可折叠以降低地面停放所占用的空间。倾转折叠机翼在由垂直起降状态倾转至固定翼状态的同时向后移动,使固定翼状态飞行时机翼焦点位于重心后方,使整机具备静稳定性。本发明的倾转折叠翼变体无人机通过各部件合理的配合与连接,解决了现有倾转翼无人机固定翼状态不具静稳定性以及机翼不可折叠导致的地面停放时占用空间大的问题。
Tilting folding wing variant unmanned aerial vehicle
一种倾转折叠翼变体无人机
2023-07-14
Patent
Electronic Resource
Chinese
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