The invention relates to the field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle and a wing assembly thereof, the wing assembly is used for being installed on a fuselage of the unmanned aerial vehicle, and the wing assembly comprises a wing and a wing assembly, the rotating lock cylinder is provided with a rotating axis, one end of the rotating lock cylinder is installed on the wing, and the other end of the rotating lock cylinder is used for being installed on the fuselage; wherein the rotating lock cylinder can rotate around the rotating axis relative to the wings, so that the other end of the rotating lock cylinder is detached from the fuselage. The rotary lock cylinder is mounted on the wing, and the rotary lock cylinder is rotated to be detached from the fuselage, so that the wing can be detached from the fuselage conveniently.
本发明涉及无人飞行器领域,公开了一种无人飞行器及其机翼组件,其中所述机翼组件用于安装于无人飞行器的机身,所述机翼组件包括:机翼;以及旋转锁芯,所述旋转锁芯具有旋转轴线,所述旋转锁芯的一端安装于所述机翼,所述旋转锁芯的另一端用于安装于所述机身;其中,所述旋转锁芯可绕所述旋转轴线相对于所述机翼旋转,以使得所述旋转锁芯的另一端与所述机身相拆卸。通过在所述机翼上安装所述旋转锁芯,通过旋转所述旋转锁芯与所述机身相拆卸,以方便将机翼从机身上拆卸下来。
Unmanned aerial vehicle and wing assembly thereof
一种无人飞行器及其机翼组件
2024-08-09
Patent
Electronic Resource
Chinese
IPC: | B64U |
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