The invention belongs to the technical field of unmanned aerial vehicles, and particularly discloses a carbon fiber unmanned aerial vehicle shell, which comprises an unmanned aerial vehicle housing and a bottom plate. A plurality of mounting plates are fixedly connected to the bottom end of the unmanned aerial vehicle housing, an accommodating groove for inserting the mounting plates is formed inthe top of the bottom plate, a lead screw movably runs through the mounting plates, one end of the lead screw extends out of the accommodating groove and is fixedly connected to a rotary button, and the other end of the lead screw extends to be in connection with the inner wall of the accommodating groove; buffering springs are symmetrically and fixedly connected to the inner wall of the accommodating groove and are movably arranged outside the lead screw in a sleeving mode; and a supporting mechanism is arranged at the bottom of the bottom plate. The carbon fiber unmanned aerial vehicle shellprovided by the invention is simple in structure, can reach a buffering and protection effect on the unmanned aerial vehicle housing and a chip in the vehicle body, meanwhile, the unmanned aerial vehicle housing can be conveniently disassembled and assembled, and maintenance personnel can conveniently overhaul and replace the unmanned aerial vehicle housing; in addition, the vibration force generated when the unmanned aerial vehicle lands can be reduced, so that the unmanned aerial vehicle can stably land on the ground.
本发明属于无人机技术领域,具体公开了一种碳纤维无人机壳,包括无人机壳体以及底板;所述无人机壳体的底端固接有若干安装板,底板的顶部设有用于安装板插入的容纳槽,安装板上活动贯穿有丝杆,丝杆的一端延伸至容纳槽的外部并固接有旋转钮,另一端延伸后与容纳槽的内壁连接;所述容纳槽的内壁对称固接有缓冲弹簧,且缓冲弹簧活动套设在丝杆的外部;所述底板底部设有支撑机构;本发明结构简单,能够对无人机壳体以及机身内部的芯片起到缓冲和保护的作用,同时,便于对无人机壳体进行拆装,便于维修人员对无人机壳体进行检修更换;此外,能够降低无人机降落时产生的震动力,使得无人机可以平稳降落到地面。
Carbon fiber unmanned aerial vehicle shell
一种碳纤维无人机壳
2020-06-09
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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