The invention discloses an anti-collision protection structure for an unmanned aerial vehicle, and relates to the field of unmanned aerial vehicle equipment, in particular to the anti-collision protection structure for the unmanned aerial vehicle, which comprises an unmanned aerial vehicle body, an anti-collision mechanism is fixedly connected to the outer surface of the unmanned aerial vehicle body, and a leveling mechanism is fixedly connected to the top of the anti-collision mechanism. A balancing mechanism is fixedly connected to the inner surface of the unmanned aerial vehicle body, a stable buffering mechanism is fixedly connected to the bottom of the unmanned aerial vehicle body, the leveling mechanism comprises unmanned aerial vehicle wings, stand column shells are fixedly connected to the tops of the unmanned aerial vehicle wings, supporting rods are fixedly connected to the inner surfaces of the stand column shells, and second springback springs are slidably connected to the outer surfaces of the supporting rods; the tops of the second springback springs are fixedly connected with sliding blocks, the fuselage drives the unmanned aerial vehicle wings, the unmanned aerial vehicle wings drive the stand column shells, the stand column shells drive the supporting rods, the supporting rods pull the sliding blocks to drive the sliding blocks to move downwards, the second springback springs extrude the sliding blocks, the reset effect can be achieved, and the balance adjusting effect is achieved to a certain degree.

    本发明公开了一种用于无人机的防撞保护结构,涉及无人机设备领域,该发明具体为一种用于无人机的防撞保护结构,包括无人机体,无人机体的外表面固定连接有防撞机构,防撞机构的顶部固定连接有调平机构,无人机体的内表面固定连接有平衡机构,无人机体的底部固定连接有稳固缓冲机构,调平机构包括无人机机翼,无人机机翼的顶部固定连接有立柱外壳,立柱外壳的内表面固定连接有支撑杆,支撑杆的外表面滑动连接有第二回弹弹簧,第二回弹弹簧的顶部固定连接有滑动块,机身带动无人机机翼,无人机翼带动立柱外壳,立柱外壳带动支撑杆,支撑杆拉扯滑动块带动向下移动,第二回弹弹簧挤压滑动块,可以达到复位的效果,一定程度上起到调整平衡的效果。


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    Titel :

    Anti-collision protection structure for unmanned aerial vehicle


    Weitere Titelangaben:

    一种用于无人机的防撞保护结构


    Beteiligte:
    WANG CHUANGUO (Autor:in)

    Erscheinungsdatum :

    12.04.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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