The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle buffer mechanism with a landing protection structure, which comprises a frame body, the frame body comprises a mounting plate, a supporting rod is arranged at the bottom end of the mounting plate, and a bottom frame is fixedly connected to the lower surface of the supporting rod; a buffering mechanism is arranged on the inner side of the supporting rod and comprises a sliding groove, and the sliding groove is formed in the inner wall of the supporting rod. Through arrangement of first springs, when the unmanned aerial vehicle lands, the first springs are impacted to deform, the effect of relieving impact force is achieved, damage to the unmanned aerial vehicle by impact can be reduced, the unmanned aerial vehicle is protected, meanwhile, through deformation of second springs, the impact force is further relieved, and the unmanned aerial vehicle is protected. And through the cooperation effect of the first spring and the second spring, the buffering effect during landing is better, damage caused by impact to internal parts of the unmanned aerial vehicle can be reduced, and then the service life of the unmanned aerial vehicle is prolonged.

    本发明涉及无人机技术领域,具体为一种无人机具有落地保护结构的缓冲机构,包括架体,所述架体包括安装板,所述安装板的底端设置有支撑杆,所述支撑杆的下表面固定连接有底架;所述支撑杆的内侧设置有缓冲机构,所述缓冲机构包括滑槽,所述滑槽开设在支撑杆的内壁。本发明通过第一弹簧的设置,可以实现当无人机落地时,第一弹簧受到冲击发生形变,达到对冲击力进行缓解的效果,可以减少冲击对无人机的损伤,实现对无人机进行防护,同时通过第二弹簧发生形变,实现对冲击力进行进一步的缓解,通过第一弹簧和第二弹簧的配合作用,使得对落地时的缓冲效果更好,可以减少冲击对无人机内部零件造成的损坏,进而延长无人机使用寿命。


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    Title :

    Buffer mechanism with landing protection structure for unmanned aerial vehicle


    Additional title:

    一种无人机具有落地保护结构的缓冲机构


    Contributors:

    Publication date :

    2023-04-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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