The invention discloses a quick-release and quick-lock structure and method and an unmanned aerial vehicle. Through cooperation of a limiting structure on a connecting structure and a locking assemblyarranged in a shell, when the connecting structure penetrates through the through hole in the locking assembly to reach the locking position, the upper end face of a groove formed in the through holeabuts against the lower end face of the limiting structure, and tool-free quick automatic locking is achieved. In the process that the abutting force is gradually removed, the lower end face of the limiting structure can be gradually separated from the upper end face of the groove, so that the locking structure is separated. All parts of the unmanned aerial vehicle can be quickly disassembled andassembled without special tools, and the unmanned aerial vehicle is simple and convenient to operate due to a self-locking mechanism. By setting an angle on the surface, in contact with the edge of the lower side of the limiting bulge, of the locking assembly, a gap between quick-release and quick-lock structures can be automatically eliminated, so that the quick-release and quick-lock structureis safer and more reliable in connection.
一种快拆快锁结构、方法及无人机。本发明通过连接结构上的限位结构与壳体内部所设置的锁止组件的配合,在所述连接结构穿过所述锁止组件内的通孔到达锁止位置时,通过通孔所开凹槽的上端面抵接于所述限位结构的下端面,实现免工具的快速自动锁定。在上述抵接力逐渐被撤销的过程中,本发明限位结构的下端面能够逐渐脱离所述凹槽的上端面,以使得所述锁定结构分离。本发明无需专用工具即可实现无人机各部件时间的快速拆装,自锁机构,操作简单方便。本发明通过在锁止组件上与所述限位凸起下侧边缘接触的表面设置角度,可自动消除快拆快锁结构之间的间隙,使得本发明连接更为安全更可靠。
Quick-release and quick-lock structure and method and unmanned aerial vehicle
一种快拆快锁结构、方法及无人机
19.03.2021
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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