The invention provides an unmanned aerial vehicle power arm quick release structure and an unmanned aerial vehicle. The unmanned aerial vehicle power arm quick release structure comprises an arm connection assembly for mounting a socket assembly, and an arm assembly which is used for mounting the plug assembly, and the first end of the arm assembly and the first end of the arm connection assemblyare installed in a matched mode; the structure further comprises a disassembling and assembling assembly which is used for disassembling and assembling the arm connection assembly and the arm assemblyand is arranged at the first end of the arm assembly and the first end of the arm connection assembly in a sleeving mode, the socket assembly which is used for being connected with the plug assemblyin an inserted mode and is arranged at the first end of the arm connection assembly, and the plug assembly which is used for being connected with the socket assembly in an inserted mode and is arranged at the first end of the arm assembly. According to the invention, axial, radial and circumferential positioning of the connecting portion of the arm and the vehicle body can be achieved at the sametime, and axial positioning, radial positioning and circumferential positioning of the whole connecting structure are still effective even if a part of threads of sleeving nuts are loosened.

    一种无人机动力机臂快拆结构及无人机,所述无人机动力机臂快拆结构包括:机臂连接组件,用于安装插座组件;机臂组件,用于安装插头组件;所述机臂组件的第一端与所述机臂连接组件的第一端适配安装;拆装组件,用于拆装所述机臂连接组件和所述机臂组件;所述拆装组件套设于所述机臂组件的第一端和所述机臂连接组件的第一端;插座组件,用于与所述插头组件插接;所述插座组件设置于所述机臂连接组件的第一端;插头组件,用于与所述插座组件插接;所述插头组件设置于所述机臂组件的第一端。本申请能同时实现机臂与机身连接部位的轴向、径向和周向定位,即使套接螺母有一部分螺纹松脱,整个连接结构的轴向定位、径向定位和周向定位依然有效。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Unmanned aerial vehicle power arm quick release structure and unmanned aerial vehicle


    Weitere Titelangaben:

    一种无人机动力机臂快拆结构及无人机


    Erscheinungsdatum :

    2021-02-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge




    Quick release device and unmanned aerial vehicle

    CONG BAOWEI / YANG JUNJIE / CONG WANG | Europäisches Patentamt | 2020

    Freier Zugriff

    Quick-release undercarriage for unmanned aerial vehicle

    JI JINGJING | Europäisches Patentamt | 2021

    Freier Zugriff


    Holder quick-release structure and unmanned aerial vehicle thereof

    LU ZHIHUI / LIU XINGHANG / CHEN FUHAI et al. | Europäisches Patentamt | 2021

    Freier Zugriff