The assembly comprises an aircraft turbine engine (10) and a pylon (32) for mounting the turbine engine to an element of the aircraft, the pylon comprising members (34, 36) for suspending the turbine engine (10), these members being connected to the turbine engine in at least one plane (P1) perpendicular to an axis (A) and upstream of a combustion chamber (18) of the turbine engine, the turbine engine (10) is mounted on the pylon (32) such that the turbine engine (10) is attached in a cantilevered manner to the pylon (32), characterised in that the assembly further comprises at least one damper (40) connecting the turbine engine (10) to the pylon (32) and lying in a plane (P2) perpendicular to the axis (A) downstream of the combustion chamber (18), the damper (40) is configured to limit relative displacement between the turbine engine (10) and the pylon (32) without transmitting forces.

    组件包括飞行器涡轮发动机(10)和用于将涡轮发动机安装到飞行器的元件上的吊架(32),吊架包括用于使涡轮发动机(10)悬挂的构件(34,36),这些构件在垂直于轴线(A)且位于涡轮发动机的燃烧室(18)的上游的至少一个平面(P1)中连接到涡轮发动机,使得涡轮发动机(10)以悬臂方式附接到吊架(32),其特征在于,该组件还包括至少一个阻尼器(40),至少一个阻尼器将涡轮发动机(10)连接到吊架(32),并且位于垂直于轴线(A)的平面(P2)中,该平面位于燃烧室(18)的下游,所述阻尼器(40)被构造成在不传递力的情况下限制涡轮发动机(10)和吊架(32)之间的相对移位。


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    Title :

    Assembly comprising aircraft turbine engine and mounting pylon therefor


    Additional title:

    包括飞行器涡轮发动机及其安装吊架的组件



    Publication date :

    2023-09-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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