The invention discloses a pressing buckle type unmanned aerial vehicle folding arm structure, and relates to the technical field of unmanned aerial vehicles, the pressing buckle type unmanned aerial vehicle folding arm structure comprises a pressing buckle assembly, a fixing seat assembly and a folding piece assembly, and the pressing buckle assembly comprises a clamping hook rotating shaft, a clamping hook, a clamping hook spring and a pressing buckle; the two ends of the pressing buckle are provided with an end buckling part and a side stirring part respectively, the pressing buckle is provided with a hinge hole, and the upper end of the pressing buckle is provided with mounting holes used for containing the clamping hook and the clamping hook spring. The clamping hook is hinged in the mounting hole through a clamping hook rotating shaft, and the clamping hook and the end buckling part are distributed at the two ends of the mounting hole; a clamping hook fixing buckle and a hinge end are arranged at the upper end of the fixing base assembly, the pressing buckle type folding machine arm structure is simple and convenient in folding operation mode, and the problems that the folding mode is tedious and the unfolding and folding efficiency is low are solved. The clamping hooks and the end part clamping parts are adopted for double-clamping-buckle type matching, the clamping buckles are stressed in a balanced manner, and the reliability of the buckling structure of the pressing buckle type folding machine arm structure is ensured.
本发明公开了一种压扣式无人机折叠机臂结构,涉及无人机技术领域,包括压扣组件、固定座组件、折叠件组件,压扣组件包括卡钩转轴、卡钩、卡钩弹簧、压扣;压扣的两端分别设置有端部卡扣部、侧部拨动部,压扣设置有铰接孔,压扣的上端设有用于放置卡钩、卡钩弹簧的安装孔;卡钩通过卡钩转轴铰接于安装孔内,卡钩、端部卡扣部分布于安装孔的两端;固定座组件的上端设置有卡钩固定扣、铰接端,压扣式折叠机臂结构折叠操作方式简单便捷,解决了折叠方式繁琐、展开折叠效率低的问题。采用所述卡钩、端部卡扣部进行双重卡扣形式配合,卡扣受力均衡,保证了压扣式折叠机臂结构扣合结构的可靠性。
Pressing buckle type folding arm structure of unmanned aerial vehicle
压扣式无人机折叠机臂结构
2022-03-01
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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