The invention relates to a suspension assembly for a turbomachine (10), the assembly comprising: • - a beam (12) for the attachment thereof to an aircraft pylon (13), the beam (12) comprising a first portion (12a) and a second portion (12b) each carrying a half-housing (16a, 16b) jointly defining a ball joint housing (17); • - a ball joint nut (16) rotatably hingedly enaged in the ball joint housing (17); and • - a cylindrical portion (14) intended to be attached to a fixed portion (15) of the turbomachine (10) hinged to the ball joint housing (17) and mounted so as to be pivotable about its axis (X) in the ball joint nut (16), wherein the suspension assembly (11) further comprises a retaining ring (23) surrounding the two half-housings (16a, 16b) around the entire circumference thereof, the retaining ring (23) being provided to perform a safety function in the event of the failure of at least one element of the suspension assembly (11).


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    Title :

    ENSEMBLE DE SUSPENSION POUR UNE TURBOMACHINE


    Additional title:

    SUSPENSION ASSEMBLY FOR A TURBOMACHINE
    AUFHÄNGUNGSANORDNUNG FÜR EINE TURBOMASCHINE



    Publication date :

    2025-02-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



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