The unmanned aerial vehicle rack comprises a carbon fiber middle part, a carbon fiber front main arm and a carbon fiber rear main arm, mounting sleeves are arranged at the tail ends of the carbon fiber front main arm and the carbon fiber rear main arm correspondingly, and machine arms are inserted into the mounting sleeves correspondingly; the vehicle arm comprises a left transparent cylinder, a right transparent cylinder and a cylindrical connecting part, the tail end of the left transparent cylinder and the tail end of the right transparent cylinder are closed holes and are provided with storage holes, connecting screw holes are formed in the outer wall of the cylindrical connecting part, penetrating holes are formed in the mounting sleeves, connecting bolts are inserted into the penetrating holes, and the connecting screw holes are connected with the connecting screw holes. Storage holes are formed in the carbon fiber front main arm and the carbon fiber rear main arm, first balancing weights are inserted into the storage holes, lightening holes are formed in the carbon fiber front main arm and the carbon fiber rear main arm, storage grooves are formed in the hole walls of the lightening holes, and second balancing weights are installed in the storage grooves; according to the unmanned aerial vehicle rack capable of balancing the weight, the weight can be configured according to actual conditions, so that the weight distribution is more balanced.

    本发明公开一种可配重的无人机机架及无人机,该无人机机架包括碳纤维中件、碳纤维前主臂和碳纤维后主臂,所述碳纤维前主臂和碳纤维后主臂末端均设置有安装套管,所述安装套管内均插入有机臂,所述机臂包含有左透明筒、右透明筒和柱形接驳件,所述左透明筒和右透明筒末端均为闭孔设置并形成有储存孔,所述柱形接驳件的外壁上设置有连接螺孔,所述安装套管上均设置有穿孔,所述穿孔内插入有连接螺栓,所述储存孔内插入有第一配重块,所述碳纤维前主臂和碳纤维后主臂上均设置有减重孔,所述减重孔的孔壁上设置有储存槽,所述储存槽内安装有第二配重块;该可配重的无人机机架可根据实际情况配置重量,使得重量分布得更加均衡。


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    Title :

    Unmanned aerial vehicle frame capable of balancing weight and unmanned aerial vehicle


    Additional title:

    一种可配重的无人机机架及无人机


    Contributors:
    HUANG NANMING (author) / CHEN FUMING (author)

    Publication date :

    2021-06-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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