The invention relates to an aircraft assembly and an aircraft. The aircraft assembly comprises an aircraft structure; a tube assembly; a securing device attached to the aircraft structure, the securing device contacting the tube assembly via a curved bearing surface having a curvature in two orthogonal directions; the curved bearing surface is configured to enable the tube assembly to rotate about three vertical axes relative to the fixture; wherein the tube assembly comprises a stop member adjacent to the fixture, a contact surface of the stop member being configured to abut a contact surface of the fixture so as to limit axial movement of the tube assembly relative to the fixture, and wherein the stop member has a contact surface configured to abut a contact surface of the fixture. The distance between the contact surface of the securing device and the contact surface of the stop member increases radially with respect to the longitudinal tube axis.

    本发明涉及一种飞行器组件和飞行器,该飞行器组件包括:飞行器结构;管组件;固定装置,该固定装置附接至飞行器结构,固定装置经由在两个正交方向上具有曲率的弯曲的支承表面接触管组件;弯曲的支承表面构造成使得管组件能够相对于固定装置绕三个垂直轴线旋转;其中,管组件包括邻近于固定装置的止挡构件,止挡构件的接触表面构造成抵接固定装置的接触表面,以便限制管组件相对于固定装置的轴向运动,并且其中,固定装置的接触表面与止挡构件的接触表面之间的距离相对于纵向的管轴线在径向上增加。


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    Titel :

    Aircraft assembly and aircraft


    Weitere Titelangaben:

    飞行器组件和飞行器


    Beteiligte:
    JONSON CALLUM (Autor:in) / ANTHONY BRYANT (Autor:in)

    Erscheinungsdatum :

    2024-05-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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