A rotor mounting assembly (11, 41, 51, 61) includes a rotor seat and a resilient member (118). The rotor seat comprises a base body (112, 412, 512, 612) and a locking structure (114, 414, 514, 614) arranged at the base body. The locking structure includes a groove (1242, 4242, 5242, 6242) open towards the base body and configured to receive a portion of the rotor blade assembly (12, 42, 52, 62), and a resilient member configured to provide a resilient force to the portion of the rotor blade assembly to confine the portion of the rotor blade assembly in the groove.

    一种旋翼安装组件(11,41,51,61)包括旋翼座和弹性构件(118)。所述旋翼座包括基体(112,412,512,612)和布置在所述基体处的锁定结构(114,414,514,614)。所述锁定结构包括朝向所述基体开口并且构造成接收所述旋翼叶片组件(12,42,52,62)的一部分的凹槽(1242,4242,5242,6242),所述弹性构件构造成向所述旋翼叶片组件的一部分提供弹性力,以将所述旋翼叶片组件的一部分限制在所述凹槽中。


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    Titel :

    ROTOR MOUNTING ASSEMBLY


    Weitere Titelangaben:

    旋翼安装组件


    Beteiligte:
    XIAO XIANG (Autor:in)

    Erscheinungsdatum :

    08.11.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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