The invention discloses an unmanned aerial vehicle empennage. The unmanned aerial vehicle empennage comprises a first empennage, a second empennage and at least one rotation locking piece connected with the first empennage and the second empennage, and the rotation locking piece is used for rotating within a preset rotation angle and locking the first empennage and the second empennage after rotating to a preset locking angle. When the first empennage and the second empennage need to be connected with the fuselage of the unmanned aerial vehicle, the first empennage and the second empennage are locked after the rotary locking piece is rotated to a preset locking angle, so that the first empennage and the second empennage are in an inverted V shape, and when the first empennage and the second empennage do not need to be connected with the fuselage of the unmanned aerial vehicle and need to be folded, the first empennage and the second empennage are folded. The rotation locking piece can be rotated within the preset rotation angle until the first empennage and the second empennage are in the folded state, so that the occupied space of the empennage of the unmanned aerial vehicle is reduced, and transportation and storage are facilitated.
本申请公开了一种无人机尾翼。该无人机尾翼包括第一尾翼、第二尾翼及与第一尾翼和第二尾翼连接的至少一个转动锁定件,转动锁定件用于在预设转动角度内转动,并在转动至预设锁定角度后锁定第一尾翼和第二尾翼。当第一尾翼和第二尾翼需要与无人机的机身连接时,通过将转动锁定件转动至预设锁定角度后锁定第一尾翼和第二尾翼,使第一尾翼和第二尾翼呈倒“V”型,当第一尾翼和第二尾翼不需要与无人机的机身连接,而需要折叠时,可以通过将转动锁定件在预设转动角度内转动至第一尾翼和第二尾翼处于折叠状态,从而使减小无人机尾翼的占用空间,有利于运输和存储。
Unmanned aerial vehicle empennage
无人机尾翼
2022-06-17
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |