A suspension assembly for a turbine engine includes a beam that attaches to an aircraft pylon. The beam has first and second portions, each carrying a half-housing together defining a ball joint housing. A ball joint nut is hingedly engaged to rotate in the ball joint housing, and a cylindrical part is configured to be attached to a fixed portion of the turbine engine, hinged in the ball joint housing, and mounted so as to be pivotable about its axis in the ball joint nut. The suspension assembly further includes a support ring surrounding the two half-housings around their entire circumference. The support ring performs a safety function in the event of failure of at least one element of the suspension assembly.


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    Title :

    SUSPENSION ASSEMBLY FOR A TURBINE ENGINE



    Publication date :

    2025-06-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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