The invention provides an unmanned aerial vehicle protection structure, an unmanned aerial vehicle and an unmanned aerial vehicle protection method, and belongs to the technical field of unmanned aerial vehicles, the unmanned aerial vehicle protection structure comprises a support, a stall detection module and a protection pad, the support comprises a transverse support, a second inclined support and a first inclined support, and the transverse support is fixedly arranged at the bottom end of the unmanned aerial vehicle; the second inclined support is movably connected with the transverse support through a first hinge, the first inclined support is movably connected with the transverse support through a second hinge, a flexible hollow pipe body is arranged in each of the second inclined support, the first inclined support and the transverse support, and the flexible hollow pipe bodies arranged in the second inclined support, the first inclined support and the transverse support are communicated with one another. The flexible hollow pipe body is filled with compressed gas; the protective pad is attached to the outer wall of the bottom of the transverse support, and the protective pad is in through connection with a flexible hollow pipe body arranged in the transverse support through an electromagnetic valve to form a first air path; the stall detection module is arranged in the unmanned aerial vehicle and used for controlling compressed air to enter the protection pad to open the protection pad.

    本发明提供了一种无人机防护结构、无人机以及无人机防护方法,属于无人机技术领域,包括支架、失速检测模块、防护垫组成,支架包括横向支架、第二斜支架和第一斜支架,横向支架固定设定在无人机底端,第二斜支架与横向支架通过第一活页活动连接,第一斜支架通过第二活页与横向支架活动连接,第二斜支架、第一斜支架、横向支架内分别设置有1个柔性空心管体,所述第二斜支架、第一斜支架以及横向支架内设的柔性空心管体互通,柔性空心管体内灌注有压缩气体;防护垫贴敷设置在横向支架底部外壁上,防护垫通过电磁阀与横向支架内设置的柔性空心管体贯通连接形成第一气路;失速检测模块设置在无人机内,用于控制压缩气体进入防护垫内撑开防护垫。


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    Titel :

    Unmanned aerial vehicle protection structure, unmanned aerial vehicle and unmanned aerial vehicle protection method


    Weitere Titelangaben:

    一种无人机防护结构、无人机以及无人机防护方法


    Beteiligte:
    CAO KAI (Autor:in) / ZHANG BAI (Autor:in) / JIANG CHAOWEI (Autor:in) / WU JIANNING (Autor:in) / YANG JIONG (Autor:in) / PAN WEIFENG (Autor:in) / LI NING (Autor:in) / LI BO (Autor:in) / ZHANG LIANG (Autor:in) / ZHANG YUAN (Autor:in)

    Erscheinungsdatum :

    2024-04-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




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