The invention relates to the technical field of unmanned aerial vehicles and particularly relates to an unmanned aerial vehicle with a landing buffer function. The unmanned aerial vehicle comprises aunmanned aerial vehicle body, wherein a rotating shaft is arranged at the bottom of the unmanned aerial vehicle main body; the two sides of the rotating shaft are rotationally connected with two fixing plates; connecting columns are arranged at the two ends of each fixing plate; a damping column is arranged at one end of the connecting column; a fixed disc is arranged on the damping column; a piston is arranged at one end of the damping column; a buffer device shell is arranged outside the piston; the sliding device is arranged at one end of the buffer device shell; and an air pipe is arrangedat the top of the sliding device. The unmanned aerial vehicle landing buffering device has the advantages that the unmanned aerial vehicle landing buffering device is reasonable in design and simplein structure, landing buffering functions can be realized by the unmanned aerial vehicle landing buffering device, impact during landing can be greatly reduced, the unmanned aerial vehicle can be protected, and the unmanned aerial vehicle landing buffering device is suitable for popularization.

    本发明涉及无人机技术领域,尤其是一种具有落地缓冲功能的无人机,包括无人机主体,所述无人机主体的底部设有转动轴,所述转动轴的两侧转动连接有两个固定板,每个所述固定板的两端均设有连接柱,所述连接柱的一端设有减震柱,所述减震柱上设有固定盘,所述减震柱的一端设有活塞,所述活塞的外部设有缓冲装置外壳,所述缓冲装置外壳的一端设有滑行装置,所述滑行装置的顶部设有气管,该装置设计合理结构简单,实现了落地缓冲功能,大大降低了落地时的冲击,保护了无人机,适合推广。


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    Title :

    Unmanned aerial vehicle with landing buffer function


    Additional title:

    一种具有落地缓冲功能的无人机


    Contributors:

    Publication date :

    2020-04-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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