According to the wing folding structure for the unmanned aerial vehicle, the unmanned aerial vehicle comprises a fuselage and two wings arranged on the two sides of the fuselage in a folded mode, the wings are hinged to the fuselage, and a telescopic assembly arranged in the length direction of the fuselage in a sliding mode is arranged on the fuselage; the two ends of the telescopic assembly are hinged to the wings through connecting shafts, an arc groove is formed in the fuselage, and the connecting shafts are movably arranged in the arc groove in a penetrating mode. According to the wing folding structure, the wing of the unmanned aerial vehicle can be unfolded and folded by adopting a simple mechanical structure, so that the wing folding structure is suitable for small unmanned aerial vehicles, can be popularized to large unmanned aerial vehicles and can also realize large-angle wing backsweep.
本发明公开了一种用于无人机的机翼折叠结构,包括:所述无人机包括机身和折叠设置在所述机身两侧的两个机翼,所述机翼与所述机身铰接,所述机身上设置有沿所述机身的长度方向滑动设置的伸缩组件,所述伸缩组件的两端与所述机翼通过连接轴铰接,所述机身上设置有一圆弧槽,所述连接轴活动穿设于所述圆弧槽。该机翼折叠结构采用简单地机械结构即能够实现无人机机翼的打开与折叠,既适用于小型无人机,又可以推广至大型无人机使用,还可以实现大角度的机翼后掠。
Wing folding structure for unmanned aerial vehicle
一种用于无人机的机翼折叠结构
2022-07-29
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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