The invention concerns a suspension assembly (7) for a turbine engine, comprising a beam (10) intended to be attached to a pylon of an aircraft, and a cylindrical part (15) hinged to a ball-joint housing, the ball-joint housing comprising a body (11), and a ball-joint yoke (16) hinged to the body (11), the cylindrical part (15) being mounted so as to be able to pivot about its axis in the ball-joint yoke, characterised in that the cylindrical part (15) is intended to be secured to a fixed part (8) of the turbine engine (1), the body (11) of the ball-joint housing being secured to the beam (10).

    本发明涉及用于涡轮机的悬挂系统(7),其包括旨在附接到飞机挂架上的横杆(10)和铰接在球形接头外壳上的圆柱形部件(15),所述球形接头外壳包括主体(11)和铰接在所述主体(11)上的球形接头螺母(16),所述圆柱形部件(15)安装成在所述球形接头螺母中围绕其轴线枢转,其特征在于,所述圆柱形部件(15)旨在与所述涡轮机(1)的固定部分(8)成一体,所述球形接头外壳的主体(11)与所述横杆(10)成一体。


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    Titel :

    SUSPENSION ASSEMBLY FOR A TURBINE ENGINE


    Weitere Titelangaben:

    用于涡轮机的悬挂系统



    Erscheinungsdatum :

    2021-06-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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