The invention discloses a control surface connecting mechanism and method, a wing and an aircraft, and belongs to the field of unmanned aerial vehicles. The control surface can automatically compensate for coaxiality errors caused by control surface installation through a knuckle bearing, and can bear large radial loads, is high in impact resistance. The mechanism comprises a control surface connecting joint, a control surface connecting piece and a knuckle bearing; wherein the control surface connecting joint is used for embedding and connecting the wing surface; the knuckle bearing is used for embedding and connecting the wing ribs on two sides of the control surface; the control surface connecting joint is pivoted with the joint bearing, or the control surface connecting joint is pivoted with the joint bearing through the control surface connecting piece; the control surface connecting joint is provided with a protruding part used for being connected with a control surface connecting piece, and the protruding part is provided with a through hole or a shaft body.

    本发明公开了一种舵面连接机构、方法、机翼及飞行器,属于无人机领域,舵面可以通过关节轴承自动补偿舵面安装造成的同轴度误差,同时可以承受较大的径向载荷,抗冲击能力强,包括舵面连接接头、舵面连接件和关节轴承,舵面连接接头用于嵌入并连接翼面,关节轴承用于嵌入并连接舵面两侧的翼肋;舵面连接接头枢接关节轴承,或舵面连接接头通过舵面连接件枢接关节轴承;舵面连接接头具有用于连接舵面连接件的突起部,突起部设有贯通的孔,或突起部设有轴体。


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    Titel :

    Control surface connecting mechanism and method, wing and aircraft


    Weitere Titelangaben:

    一种舵面连接机构、方法、机翼及飞行器


    Beteiligte:
    WANG RUI (Autor:in) / ZHENG YANA (Autor:in) / WU JUNWEI (Autor:in) / WANG CHAOSHENG (Autor:in)

    Erscheinungsdatum :

    03.11.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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