The invention relates to the technical field of unmanned aerial vehicle auxiliary devices and discloses a control device for safe landing of the unmanned aerial vehicle. A machine body is included. Wings are fixedly mounted on an outer side of the machine body; a first hinge shaft is fixedly mounted at the bottom of the machine body; a bearing rod is movably mounted in the first hinge shaft; whenthe unmanned aerial vehicle lands, supporting legs of the unmanned aerial vehicle firstly contact with the ground and are affected by an impact force, after being impacted, the supporting legs extrudea first springs along second sliding rods; the supporting legs can drive s first rotating rod to rotate through a third hinge shaft fixedly mounted at the tops of the supporting legs; and a height between the supporting legs and a bearing block can be reduced, the bearing block drives the bearing rod to rotate towards one side through the first hinge shaft, the first sliding rod drive the slidingblock to extrude a second spring, the impact force of the unmanned aerial vehicle is reduced, and damage to internal components of the unmanned aerial vehicle is avoided.

    本发明涉及无人机辅助装置技术领域,且公开了一种无人机安全着陆的控制装置,包括机体,所述机体的外侧固定安装有机翼,所述机体的底部固定安装有第一铰链轴,所述第一铰链轴的内部活动安装有承重杆,通过在无人机降落时,无人机的支撑脚会与地面首先接触,并且会受到冲击力,支撑脚在受到冲击力之后会沿着第二滑动杆挤压第一弹簧,并且支撑脚会通过顶部固定安装的第三铰链轴带动第一转动杆转动,这样支撑脚与承重块之间的高度将会减小,并且承重块通过第一铰链轴带动承重杆向一侧转动,并通过第一滑动杆带动滑动块挤压第二弹簧,从而减小无人机的冲击力,避免无人机内部部件的损坏。


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    Titel :

    Control device for safe landing of unmanned aerial vehicle


    Weitere Titelangaben:

    一种无人机安全着陆的控制装置


    Beteiligte:
    ZHANG HONGBO (Autor:in) / KUANG YINHU (Autor:in)

    Erscheinungsdatum :

    2020-10-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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