The invention relates to the field of miniature unmanned aerial vehicles, in particular to a miniature unmanned aerial vehicle power system vibration isolation device and a miniature unmanned aerial vehicle. Wherein the power system vibration isolation device comprises a motor mounting seat and a vibration reduction ring, and the vibration reduction ring is connected with the motor mounting seat; wherein a concave notch is formed in the middle of the outer ring of the damping ring, and the motor mounting seat is embedded into the concave notch. According to the miniature unmanned aerial vehicle, the power unit is connected with the motor mounting base through the damping ring and fixed to the vehicle body through the motor mounting base, the damping ring is made of a compressible material, axial and radial vibration caused by the power unit can be reduced at the same time, and stable flight of the miniature unmanned aerial vehicle is facilitated.

    本发明涉及微型无人机领域,具体涉及一种微型无人机动力系统隔振装置及微型无人机。其中,所述动力系统隔振装置包括电机安装座、减振环,减振环与电机安装座相连接;其中,减振环外圈中间部位具有一凹型缺口,电机安装座嵌入该凹型缺口。本发明中,动力单元通过减振环与电机安装座连接,并通过电机安装座固定于机体,该减振环为可压缩材质,能同时减小动力单元造成的轴向和径向振动,有利于微型无人机的平稳飞行。


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    Titel :

    Miniature unmanned aerial vehicle power system vibration isolation device and miniature unmanned aerial vehicle


    Weitere Titelangaben:

    一种微型无人机动力系统隔振装置及微型无人机


    Beteiligte:
    DENG CHAO (Autor:in) / YIN JIAO (Autor:in) / CHENG RUYUAN (Autor:in)

    Erscheinungsdatum :

    15.09.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / F16F SPRINGS , Federn / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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