A structure for linking and supporting a turbine engine on an aircraft pylon, the structure having a first longitudinal axis intended to extend parallel to a second longitudinal axis of the pylon, the structure including a first axial portion for fastening to the pylon, the first portion having an upper end that defines a substantially horizontal plane of interface with the pylon, and a lower end bearing suspension rods for suspending the turbine engine, which extend in a rear vertical plane; and a second axial portion that is intended to extend forward of the pylon and includes at least one suspension member of the turbine engine in a front vertical plane.


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    Title :

    STRUCTURE DE LIAISON ET DE SUPPORT D'UNE TURBOMACHINE A UN PYLONE D'AERONEF


    Additional title:

    STRUCTURE FOR LINKING AND SUPPORTING A TURBINE ENGINE ON AN AIRCRAFT PYLON
    STRUKTUR ZUR VERBINDUNG UND STÜTZE EINES TURBINENMOTORS AUF EINEM FLUGZEUGPYLON



    Publication date :

    2024-04-10


    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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