The invention concerns a suspension system (7) for a turbomachine, comprising a beam (10) intended to be attached to a pylon of an aircraft, and a cylindrical part (15) articulated on a ball joint housing, the ball joint housing comprising a body (11), and a ball joint nut (16) articulated on the body (11), the cylindrical part (15) being mounted so as to pivot about its axis in the ball joint nut, characterized in that the cylindrical part (15) is intended to be integral with a fixed part (8) of the turbomachine (1), the body (11) of the ball joint housing being integral with the beam (10).


    Access

    Download


    Export, share and cite



    Title :

    ENSEMBLE DE SUSPENSION POUR UNE TURBOMACHINE


    Additional title:

    SUSPENSION ASSEMBLY FOR A TURBOMACHINE
    TURBOMASCHINENAUFHÄNGUNGSANORDNUNG



    Publication date :

    2023-11-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



    ENSEMBLE DE SUSPENSION POUR UNE TURBOMACHINE

    GARNAUD QUENTIN MATTHIAS EMMANUEL / HELLEGOUARCH ANTOINE ELIE | European Patent Office | 2020

    Free access

    ENSEMBLE DE SUSPENSION POUR UNE TURBOMACHINE

    GARNAUD QUENTIN MATTHIAS EMMANUEL / HELLEGOUARCH ANTOINE ELIE | European Patent Office | 2020

    Free access

    ensemble de suspension pour une turbomachine

    CAPASSO VALERIO / GLEMAREC GUILLAUME / VIGNES JEAN-BAPTISTE MANUEL NICOLAS | European Patent Office | 2023

    Free access

    ENSEMBLE DE SUSPENSION POUR UNE TURBOMACHINE

    CAPASSO VALERIO / GLEMAREC GUILLAUME / VIGNES JEAN-BAPTISTE | European Patent Office | 2023

    Free access

    ENSEMBLE DE SUSPENSION POUR UNE TURBOMACHINE

    GARNAUD QUENTIN / HELLEGOUARCH ANTOINE | European Patent Office | 2020

    Free access