The invention relates to the field of unmanned aerial vehicles, in particular to a rotor unmanned aerial vehicle landing auxiliary balancing device which comprises a vehicle body, blades arranged on the periphery of the vehicle body, supporting rods mounted at the bottoms of the blades and a driving mechanism, a fluted disc is arranged in the center of the bottom of the vehicle body, and a sliding groove, an inserting groove and a transmission part are arranged at the bottom of the vehicle body. A base is arranged in the sliding groove. The follow-up mechanism comprises a fixing block and a T-shaped block which are arranged in the sliding groove, a pulling part and a locking part are arranged on the T-shaped block, and an unlocking part is arranged on the base; the adjusting mechanism comprises a tooth groove in the T-shaped block, an overturning rod is arranged on the base, a tooth block is arranged on the arc-shaped side wall of the overturning rod and meshed with the tooth groove, one end of the overturning rod is connected with a telescopic part, and a reset part, a limiting part and an adjusting part are arranged on the telescopic part. And through the arrangement of the driving mechanism, the follow-up mechanism and the adjusting mechanism, the unmanned aerial vehicle can be adjusted according to the supporting surface of the ground.

    本发明涉及无人机领域,尤其是一种旋翼无人机降落辅助平衡装置,包括机体,机体的四周设置有桨叶,桨叶底部安装有支撑杆,还包括,驱动机构,机体的底部的中心位置设置有齿盘,机体的底部设置有滑槽、插槽和传动部,滑槽的内部设置有底座;随动机构,包括滑槽的内部设置的固定块和T形块,T形块上设置有拉动部和锁定部,底座上设置解锁部;调节机构,包括T形块上的齿槽,底座上设置有翻转杆,翻转杆的弧形侧壁上设置有齿块,齿块与齿槽啮合,翻转杆的一端连接有伸缩部,伸缩部上设置有复位部、限制部和调节部。通过驱动机构、随动机构和调节机构的设置,可以使得无人机可以根据地面的支撑面进行调节。


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    Titel :

    Rotor wing unmanned aerial vehicle landing auxiliary balancing device


    Weitere Titelangaben:

    一种旋翼无人机降落辅助平衡装置


    Beteiligte:
    FANG CHUANBAO (Autor:in) / LIU WENPING (Autor:in) / LI NENGFEI (Autor:in) / XIE JUN (Autor:in)

    Erscheinungsdatum :

    21.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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