The invention provides an anti-shake folding unmanned aerial vehicle cantilever. The anti-shake folding unmanned aerial vehicle cantilever comprises a cantilever body, a first locking assembly and a reinforcing assembly. The cantilever body comprises a first connecting rod and a second connecting rod, a first connector is arranged on the first connecting rod, a splicing groove and a connecting shaft are arranged on the first connector, a second connector is arranged on the second connecting rod, and the second connector is hinged to the connecting shaft. The first locking assembly comprises a locking block and a locking rod, the locking rod is arranged in the splicing groove in a sliding mode, and the locking block is arranged on the second connector. The reinforcing assembly comprises a reinforcing piece, the reinforcing piece is arranged on the locking block in a liftable mode, and after the locking block is inserted into the splicing groove, the reinforcing piece can abut against the inner wall of the splicing groove. According to the anti-shake folding unmanned aerial vehicle cantilever created in the invention, the gap of the splicing part of the folding cantilever can be reduced, and then the splicing stability of the cantilever is improved.
本发明创造提供了一种防抖型折叠无人机悬臂,包括:悬臂本体、第一锁止组件和加固组件。所述悬臂本体包括第一连接杆和第二连接杆,所述第一连接杆上设有第一接头,在第一接头上设有拼接槽和连接轴,所述第二连接杆上设有第二接头,所述第二接头与连接轴相铰接。所述第一锁止组件包括锁止块和锁止杆,所述锁止杆滑动设置在拼接槽内部,所述锁止块设置在第二接头上。所述加固组件包括加固片,所述加固片可升降的设置在锁止块上,当锁止块插入拼接槽后,所述加固片能与拼接槽的内壁相抵持。本发明创造所述的一种防抖型折叠无人机悬臂,能够降低折叠悬臂拼接部位的间隙,从而提升悬臂的拼接稳定性。
Anti-shake folding unmanned aerial vehicle cantilever
一种防抖型折叠无人机悬臂
2021-06-15
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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