The present invention relates to an aircraft suspension interface assembly comprising: a mount assembly that attaches a suspension to a wing such that the mount assembly limits movement of the suspension relative to the wing in a heading direction X and a vertical direction Z; and a stop assembly disposed between the suspension and the wing such that the stop assembly limits movement of the suspension relative to the wing in a lateral direction Y, where the support assembly and the stop assembly form a statically indeterminate interface form that attaches the suspension to the wing. Through the statically indeterminate interface form, the aircraft hanging interface assembly can reduce the assembly difficulty and the number of joints, and has a clear disconnection mode. The invention also relates to a suspension comprising the aircraft suspension interface assembly.

    本发明涉及一种飞行器吊挂接口组件,包括:支座组件,支座组件将吊挂附连到机翼,使得支座组件限制吊挂相对于机翼在航向方向X和竖直方向Z上的运动;以及止挡组件,止挡组件设置在吊挂与机翼之间,使得止挡组件限制吊挂相对于机翼在侧向方向Y上的运动,其中,支座组件与止挡组件形成将吊挂附连到机翼的超静定接口形式。通过这种超静定接口形式,飞行器吊挂接口组件能够降低装配难度,减少接头数量,并且具有明确的断离方式。本发明还涉及包括该飞行器吊挂接口组件的吊挂。


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    Titel :

    Aircraft suspension interface assembly and aircraft hanger


    Weitere Titelangaben:

    飞行器吊挂接口组件及飞行器吊挂


    Beteiligte:
    LIN GUOZHENG (Autor:in) / YAN MINGPENG (Autor:in) / ZHANG FENGGE (Autor:in) / PENG SEN (Autor:in) / LI XIAONAN (Autor:in) / GUO HAISHA (Autor:in)

    Erscheinungsdatum :

    2021-12-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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