The invention discloses a quick disassembly and assembly structure and method for an unmanned aerial vehicle arm, and solves the problems of quick disassembly and assembly and electromagnetic compatibility at the same time. A quick dismounting and mounting structure for an unmanned aerial vehicle arm comprises a shell, a first locking structure, a second locking structure, a shielding baffle and an electrical connection contact. The shell is of a cylinder structure with a through cavity. The first locking structure and the second locking structure are arranged on the end faces of the two shells respectively, and the two locking structures are locked in a rotating fit mode. And the shielding baffle plates respectively seal the end surfaces of the two shells and are provided with a plurality of holes. The electrical connection contacts are arranged on the holes, the two shells in the shells are rotationally locked through a locking structure, and the electrical connection contacts are in corresponding contact. By means of the structure, it can be guaranteed that the arms and the fuselage of the unmanned aerial vehicle are rapidly disassembled and assembled, and meanwhile it is guaranteed that signals of the unmanned aerial vehicle cannot affect loads.
本申请公开了一种无人机机臂快速拆装结构与方法,解决了快速拆装同时实现电磁兼容的问题。无人机机臂快速拆装结构,包含外壳、第一锁紧结构、第二锁紧结构、屏蔽挡板和电气连接触点。所述外壳为带有贯通腔的圆筒结构。所述第一锁紧结构和第二锁紧结构分别设置在两个外壳的端面,两个锁紧结构通过旋转配合锁紧。所述屏蔽挡板分别封住两个外壳的端面,上有若干孔洞。所述电气连接触点设置在孔洞上,外壳内部两个外壳通过锁紧结构旋转锁紧,电气连接触点对应接触。本申请结构既能保证无人机的机臂与机身的快速拆装,同时确保无人机本身的信号不会对载荷造成影响。
Quick disassembly and assembly structure and method for unmanned aerial vehicle arms
一种无人机机臂快速拆装结构与方法
2023-09-12
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
Europäisches Patentamt | 2021
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