There is disclosed a support assembly for supporting a main accessory gearbox (82) of an aircraft turbine engine (10), said accessory gearbox (82) comprising a gear and supporting at least one facility (86) driven by the gear, the support assembly being characterized in that the support assembly comprises a structure (50) comprising at least one support element (60) for supporting the main accessory gearbox (82) of the aircraft turbine engine (10). The invention relates to a structure (50) for connecting and supporting a turbine engine (10) to a tower (32) of an aircraft, the structure (50) comprising:-an intermediate axial section (50a) for attachment to the tower (32), the intermediate axial section having an upper end defining a connection interface (P3) with the tower (32), the intermediate axial section (50a) carrying a suspension rod (62, 64) intended to be connected to the turbine engine (10); -a front axial section (50b) extending in front of the intermediate section (50a) and comprising at least one suspension member (66) intended to be connected to the turbine engine (10); and-a rear axial section (50c) extending rearward of the intermediate section (50a) and supporting the main accessory gearbox (82).
公开了一种用于对飞行器涡轮发动机(10)的主附件齿轮箱(82)进行支撑的支撑组件,所述附件齿轮箱(82)包括齿轮并支撑由齿轮驱动的至少一项设施(86),支撑组件的特征在于,支撑组件包括如下的结构(50),该结构用于将涡轮发动机(10)连接并支撑到飞行器的塔架(32),该结构(50)包括:‑中间轴向部段(50a),中间轴向部段用于附接到塔架(32),中间轴向部段具有限定了与塔架(32)的连接界面(P3)的上端部,中间轴向部段(50a)承载旨在连接到涡轮发动机(10)的悬挂杆(62,64);‑前轴向部段(50b),前轴向部段在中间部段(50a)的前方延伸,并且包括至少一个悬挂构件(66),悬挂构件旨在连接到涡轮发动机(10);以及‑后轴向部段(50c),后轴向部段延伸到中间部段(50a)的后方并且支撑主附件齿轮箱(82)。
Assembly for supporting accessory gearbox of aircraft turbine engine
用于支撑飞行器涡轮发动机的附件齿轮箱的组件
2024-01-05
Patent
Electronic Resource
Chinese
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