The invention relates to an aircraft piping system assembly comprising: an aircraft structure; a piping system; the fixing device is located between the pipeline system and the aircraft structure; a tie rod connecting the piping system to the aircraft structure; a first tie rod support connecting the tie rod to the piping system; and a second tie rod support connecting the tie rod to the aircraft structure. The fixture includes a spherical support including a ball mounted to the piping system and a housing coupled to the aircraft structure. The ball comprises a convex spherical bearing surface; and the housing includes a concave spherical bearing surface cooperating with the convex spherical bearing surface of the ball. The fixture is configured to enable translation of the piping system relative to the ball in an axial direction aligned with a longitudinal axis of the piping system.
本发明涉及一种飞行器管道系统组件,该飞行器管道系统组件包括:飞行器结构;管道系统;固定装置,该固定装置位于管道系统与飞行器结构之间;拉杆,该拉杆将管道系统连接至飞行器结构;第一拉杆支承件,该第一拉杆支承件将拉杆连接至管道系统;以及第二拉杆支承件,该第二拉杆支承件将拉杆连接至飞行器结构。固定装置包括球形支承件,该球形支承件包括安装至管道系统的球,以及联接至飞行器结构的壳体。球包括凸球形支承表面;并且壳体包括与球的凸球形支承表面配合的凹球形支承表面。固定装置构造成使得管道系统能够相对于球在与管道系统的纵向轴线对准的轴向方向上平移。
Aircraft duct system assembly
飞行器管道系统组件
2024-05-28
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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