The invention discloses a foldable wing and an unmanned aerial vehicle, the foldable wing comprises a wing main body and a foldable wing, a telescopic assembly and a rotating assembly are arranged between the wing main body and the foldable wing, the first end of the telescopic assembly is slidably connected with the wing main body, and the second end of the telescopic assembly is rotatably connected with the foldable wing; the first end of the rotating assembly is fixedly connected with the telescopic assembly, and the second end of the rotating assembly is fixedly connected with the folding wing; the telescopic assembly is used for driving the folding wing and the rotating assembly to do telescopic motion relative to the wing body, and the rotating assembly is used for overturning and folding the folding wing. According to the foldable wing, in the storage and transportation process of the unmanned aerial vehicle, the foldable wing can be directly controlled to be rapidly folded only through the telescopic assembly and the rotating assembly, the space needed by folding is small, the occupied space of the wing is reduced, damage to the wing is better avoided, repeated disassembly and assembly of the wing are not needed, and the folding efficiency is improved. The operation is simple.
本发明公开了一种可折叠机翼及无人机,可折叠机翼包括机翼主体和折叠机翼,机翼主体与折叠机翼之间设置有伸缩组件和旋转组件,伸缩组件的第一端与机翼主体滑动连接,伸缩组件的第二端与折叠机翼转动连接,旋转组件的第一端与伸缩组件固定连接,旋转组件的第二端与折叠机翼固定连接;伸缩组件用于将驱动折叠机翼以及旋转组件相对机翼主体伸缩运动,旋转组件用于对折叠机翼进行翻转折叠。采用本发明所述的可折叠机翼,在对无人机收纳及运输过程中,仅通过伸缩组件和旋转组件即可直接的控制折叠机翼进行快速折叠,折叠需要的空间小,减小机翼的占用空间,更好的避免了对机翼受到的损坏,也不需要对机翼进行反复拆装,操作简单。
Foldable wing and unmanned aerial vehicle
一种可折叠机翼及无人机
2024-02-13
Patent
Electronic Resource
Chinese
IPC: | B64U |
Foldable wing type tilting ducted unmanned aerial vehicle
European Patent Office | 2024
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