The electric vertical take-off and landing aircraft with the improved motor vibration isolation structure comprises a plurality of propeller structures, each propeller structure comprises a motor, a base, a vibration isolator and blades, the motors are connected to the blades, the vibration isolators are in a circular ring shape and are made of manganese-copper alloy materials, the vibration isolators are arranged between the motors and the bases, and the vibration isolators are arranged on the bases. A plurality of hollowed-out grooves are formed in the face, close to the base, of the vibration isolator.

    提供了一种改进电机隔振结构的电动垂直起降飞行器,其包括多个螺旋桨结构,所述螺旋桨结构包括电机、基座、隔振器、桨叶,所述电机连接到所述桨叶,所述隔振器为圆环形并采用锰铜合金材质,所述隔振器设置于所述电机与所述基座之间,所述隔振器靠近所述基座的一面形成有多个镂空槽。


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    Titel :

    Electric vertical take-off and landing aircraft with improved motor vibration isolation structure


    Weitere Titelangaben:

    改进电机隔振结构的电动垂直起降飞行器


    Beteiligte:
    HAN QI (Autor:in) / JIN JUN (Autor:in) / ZHANG YIDING (Autor:in) / DONG MING (Autor:in) / DANG TIEHONG (Autor:in)

    Erscheinungsdatum :

    2023-05-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



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