Quick release mechanism for load of unmanned aerial vehicle

The invention provides an unmanned aerial vehicle load quick release mechanism, which comprises a fuselage main body, a load cabin, a transfer frame and a load, and is characterized in that the load cabin is detachably connected to the abdomen of the fuselage main body; the adapter frame is arranged in the load cabin; and the load penetrates through the bottom of the load cabin and is detachably arranged on the transfer frame. According to the technical scheme, different loads can be installed on the same load cabin, and rapid installation, rapid disassembly and rapid load replacement are achieved. 本申请提供一种无人机载荷快拆机构，包括机身主体、载荷舱、转接架和载荷，其中，所述载荷舱可拆卸地连接于所述机身主体腹部；所述转接架设置于所述载荷舱的内部；所述载荷穿过所述载荷舱的底部可拆卸地设置于所述转接架上。本申请的技术方案解决了不同载荷均可安装于同一载荷舱上，实现了可以快速安装、快速拆卸、快速更换载荷。