The invention provides a mounting apparatus for mounting a gas turbine engine to an aircraft. The mounting apparatus includes a thrust strut operably connected to the gas turbine engine and the aircraft. The thrust strut defines a thrust strut axis. The mounting apparatus further includes a restraining structure. The restraining structure includes a bracket circumferentially disposed on the thruststrut and at least one elongate member connected to the bracket and the gas turbine engine. The restraining structure radially and circumferentially constrains the thrust strut with respect to the thrust strut axis of the thrust strut while allowing the thrust strut to move in the direction of thrust strut axis.
本发明提供了一种用于将气体涡轮引擎安装到飞行器上的安装设备。所述安装设备包括可操作地连接到所述气体涡轮引擎和所述飞行器的推力支柱。所述推力支柱限定推力支柱轴线。所述安装设备还包括约束结构。所述约束结构包括周向设置在所述推力支柱上的托架以及连接到所述托架和所述气体涡轮引擎的至少一个细长构件。所述约束结构相对于所述推力支柱的所述推力支柱轴线径向和周向地约束所述推力支柱,同时允许所述推力支柱沿推力支柱轴线的方向移动。
Mounting apparatus for gas turbine engine
用于气体涡轮引擎的安装设备
2020-07-24
Patent
Elektronische Ressource
Chinesisch