The invention provides an unmanned aerial vehicle power module, the unmanned aerial vehicle power module comprises a system control box, a power supply system, a cruise system and a vertical take-off and landing system, the power supply system is arranged on the system control box, the system control box is mounted on a system mounting part of a connecting pipe, the cruise system comprises a front pull propeller and an empennage, the front pull propeller and the empennage are connected based on the connecting pipe; the vertical take-off and landing system comprises a plurality of rotor wings, each rotor wing is fixed to the corresponding rotor wing installation position on the connecting pipe, the system control box is provided with a battery pack and a control system, and the unmanned aerial vehicle power module components are connected based on the connecting pipes, so that the components are convenient to replace. The unmanned aerial vehicle power module is provided with an independent power supply and an independent control system, a plurality of unmanned aerial vehicle power modules are carried, and safe return flight of the unmanned aerial vehicle can be guaranteed when the unmanned aerial vehicle breaks down.

    本发明提供了一种无人机动力模块,所述无人机动力模块包括系统控制箱、电源系统、巡航系统和垂直起降系统,所述电源系统设置在所述系统控制箱,所述系统控制箱安装在连接管的系统安装部位上,所述巡航系统包括前拉桨和尾翼,所述前拉桨和所述尾翼之间基于所述连接管连接;所述垂直起降系统包括若干个旋翼,所述若干个旋翼中的每一旋翼固定在所述连接管上所对应的旋翼安装部位上,所述系统控制箱设置有电池组和控制系统,所述无人机动力模块部件之间基于连接管连接,便于更换部件,所述无人机动力模块具有独立的电源和控制系统,搭载多个该无人机动力模块,在无人机发生故障时能够保证无人机安全返航。


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    Title :

    Unmanned aerial vehicle power module


    Additional title:

    一种无人机动力模块


    Contributors:
    LIU SHIYI (author) / XIE LING (author) / HUANG ZIYU (author)

    Publication date :

    2022-02-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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