The invention relates to a suspension assembly (11) for a turbine engine (10), comprising:-a crossbar (12) for attaching the suspension assembly to an aircraft pylon (13), the crossbar (12) comprising a first portion (12a) and a second portion (12b) each carrying a half-shell (16a, 16b), the half-shells together defining a ball joint shell (17),-a ball joint nut (16) hingedly engaged for rotation in the ball joint shell (17), and-a cylindrical part (14) intended to be attached to a fixed part (15) of the turbine engine (10), articulated in the ball joint housing (17) and mounted so as to be pivotable about its axis (X) in the ball joint nut (16), in which the suspension assembly (11) further comprises a support ring (23) surrounding the two half-shells (16a, 16b) around the entire circumference thereof, the support ring (23) is arranged to perform a safety function in the event of a failure of at least one element of the suspension assembly (11).
本发明涉及用于涡轮发动机(10)的悬挂组件(11),其包括:‑横杆(12),其用于将悬挂组件附接到飞机挂架(13),横杆(12)包括各自承载半壳体(16a、16b)的第一部分(12a)和第二部分(12b),半壳体一起界定球形接头壳体(17),‑球形接头螺帽(16),其铰接地接合以在球形接头壳体(17)中旋转,和‑圆柱形零件(14),其旨在附接到涡轮发动机(10)的固定部分(15),铰接于球形接头壳体(17)中且安装成能够在球形接头螺帽(16)中围绕其轴线(X)枢转,其中悬挂组件(11)进一步包括支撑环(23),其环绕两个半壳体(16a、16b)的整个圆周包围两个半壳体,支撑环(23)设置成在悬挂组件(11)的至少一个元件发生故障的情况下执行安全功能。
Suspension assembly for turbine engine
用于涡轮发动机的悬挂组件
2024-11-29
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |