The invention discloses a detachable unmanned aerial vehicle arm device. The device comprises a vehicle body; a mounting seat which is connected to the vehicle body, wherein a connecting hole is formed in the front side of the mounting seat, the connecting hole is a conical hole with a large front part and a small rear part, and a first connecting structure is arranged on the outer side wall of the mounting seat; a connecting rod, wherein a connecting head is arranged at one end of the connecting rod, the connecting head is inserted into the connecting hole, and the shape of the connecting head is matched with that of the connecting hole; and a connecting piece, wherein the front side of the connecting piece is connected to the connecting rod, a second connecting structure is arranged on the rear side of the connecting piece, and the second connecting structure is detachably connected with the first connecting structure so that the outer side wall of the connecting head can be tightly attached to the inner side wall of the connecting hole. According to the detachable unmanned aerial vehicle arm device, the pressure direction of the inner side wall of the connecting hole to the outer side wall of the connecting head is converged at the axis of the connector, so that the connecting head is stably fixed in the connecting hole, the connecting head is prevented from shaking in the connecting hole, and the stability of the arm is improved. The device can be applied to the field of unmanned aerial vehicles.

    本发明公开了一种可拆卸无人机机臂装置,包括:机身;安装座,其连接于机身,安装座的前侧设有连接孔,连接孔为前大后小的锥形孔,安装座的外侧壁上设有第一连接结构;连接杆,其一端设有连接头,连接头插入连接孔中,连接头的外形与连接孔的形状相匹配;连接件,其前侧连接于连接杆,连接件的后侧设有第二连接结构,第二连接结构与第一连接结构可拆卸连接使连接头的外侧壁紧贴于连接孔的内侧壁。本发明的可拆卸无人机机臂装置,连接孔的内侧壁对连接头的外侧壁的压力方向汇集于连接头的轴线处,从而使得连接头被稳固固定于连接孔中,防止连接头在连接孔中晃动,提高机臂的稳定性。本发明可应用于无人机领域中。


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    Titel :

    Detachable unmanned aerial vehicle arm device


    Weitere Titelangaben:

    可拆卸无人机机臂装置


    Beteiligte:
    WU TAO (Autor:in) / ZHANG JINGUANG (Autor:in) / ZHOU LONG (Autor:in) / ZENG NENG (Autor:in) / PAN SHICHUN (Autor:in) / ZHOU WEICAI (Autor:in)

    Erscheinungsdatum :

    2021-12-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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