The invention relates to an assembly between an aircraft pylon (30) and a turbine (20) having a longitudinal axis (X), the pylon (30) and the turbine (20) each comprising a forward longitudinal region and a rearward longitudinal region, the assembly comprising a rearward support (40) configured to connect the rearward region of the turbine (20) to the rearward region of the pylon (30), the assembly being characterized in that the pylon (30) and the turbine (20) are supported by the rearward support (40). The rear support (40) comprises a sliding pivot connection arranged between a rear region of the turbine (20) and a rear region of the pylon (30), the turbine (20) can be moved in translation along the longitudinal axis (X) and in rotation about the longitudinal axis (X), in translation along the vertical axis (Z) and in rotation about the vertical axis (Z), and in rotation about the transverse axis (Y).

    本发明涉及一种在飞行器挂架(30)与具有纵向轴线(X)的涡轮机(20)之间的组件,挂架(30)和涡轮机(20)各自包括前部纵向区域和后部纵向区域,该组件包括后支撑件(40),后支撑件被构造成将涡轮机(20)的后部区域连接到挂架(30)的后部区域,该组件的特征在于,后支撑件(40)包括滑动枢转连接部,滑动枢转连接部被布置在涡轮机(20)的后部区域与挂架(30)的后部区域之间,以使得涡轮机(20)仅能够沿着纵向轴线(X)进行平移移动并围绕纵向轴线进行旋转移动、沿着竖直轴线(Z)进行平移移动并围绕竖直轴线进行旋转移动、以及围绕横向轴线(Y)进行旋转移动。


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    Title :

    Assembly between aircraft pylon and turbine


    Additional title:

    飞行器挂架与涡轮机之间的组件



    Publication date :

    2022-08-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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