The invention discloses a composite wing vertical take-off and landing unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The protection system is arranged at the top of the unmanned aerial vehicle body; the protection system comprises a first shell with one end provided with a first notch, a first movable part movably connected with the first shell, and a second movable part movably connected with the first movable part in a sleeving mode. Wherein the first shell is provided with a protruding part, the protruding part penetrates through the first notch, the second movable part comprises a second protruding part arranged at one end and a buckling part arranged at the end opposite to the second protruding part, the second protruding part penetrates through the protruding part, the second protruding part is sleeved with a first elastic mechanism, and the buckling part is provided with a second elastic mechanism. The elastic rigidity of the first elastic mechanism is larger than that of the second elastic mechanism, the image transmission system on the unmanned aerial vehicle can be greatly protected, and the image transmission system is prevented from being damaged when the unmanned aerial vehicle is impacted.

    本发明公开了一种复合翼垂直起降无人机,涉及无人机技术领域,其结构包括无人机本体;防护系统,防护系统布置在无人机本体顶部;防护系统包括一端开设有第一豁口的第一外壳、活动连接第一外壳的第一活动件以及活动套设连接第一活动件的第二活动件;其中,第一外壳设置有凸起部,凸起部穿过第一豁口,第二活动件包括设置在一端的第二凸起部和设置在背对第二凸起部一端的卡扣部,第二凸起部穿过凸起部,第二凸起部上套设有第一弹性机构,卡扣部上布置有第二弹性机构,第一弹性机构的弹性刚度大于第二弹性机构的弹性刚度,本发明中的无人机上的图像传输系统可以受到极大的保护,防止在当无人机受到撞击时损伤到图像传输系统。


    Access

    Download


    Export, share and cite



    Title :

    Composite wing vertical take-off and landing unmanned aerial vehicle


    Additional title:

    一种复合翼垂直起降无人机


    Contributors:
    XIN JINGFENG (author) / HAN FANGBO (author) / LIANG JIN (author) / MA BO (author) / XING ZHIBO (author)

    Publication date :

    2024-04-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Vertical take-off and landing fixed-wing unmanned aerial vehicle

    TIAN YU | European Patent Office | 2020

    Free access

    Vertical take-off and landing tandem wing unmanned aerial vehicle

    LIU YANG / JU WEIJIE / JU ZHUQING | European Patent Office | 2020

    Free access

    Vertical take-off and landing fixed-wing unmanned aerial vehicle

    SUN WEI | European Patent Office | 2023

    Free access

    Vertical take-off and landing fixed-wing unmanned aerial vehicle

    LIU SHIYI / XIE LING / HUANG ZIYU | European Patent Office | 2022

    Free access

    Vertical take-off and landing fixed-wing unmanned aerial vehicle

    SHI YONGKANG / WU HAO / LI PENG | European Patent Office | 2022

    Free access