Disclosed is an assembly for supporting a main accessory gearbox (82) of an aircraft turbine engine (10), said accessory gearbox (82) comprising gears and supporting at least one item of equipment (86) driven by the gears, the support assembly being characterised in that it comprises a structure (50) for connecting and supporting the turbine engine (10) to a pylon (32) of the aircraft, the structure (50) comprising: - an intermediate axial portion (50a) for attachment to the pylon (32), having an upper end that defines a linking interface (P3) with the pylon (32), said intermediate axial portion (50a) bearing suspension rods (62, 64), which are intended to be connected to the turbine engine (10); - a front axial portion (50b) extending forward of said intermediate portion (50a) and comprising at least one suspension member (66), which is intended to be connected to the turbine engine (10); and - a rear axial portion (50c) extending rearwards of said intermediate portion (50a) and supporting the main accessory gearbox (82).


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    Titel :

    ENSEMBLE DE SUPPORTAGE D'UNE BOITE D'ACCESSOIRES D'UNE TURBOMACHINE D'AERONEF


    Weitere Titelangaben:

    ASSEMBLY FOR SUPPORTING AN ACCESSORY GEARBOX OF AN AIRCRAFT TURBINE ENGINE
    ANORDNUNG ZUR UNTERSTÜTZUNG EINES HILFSGETRIEBE EINES FLUGZEUGTURBINENTRIEBWERKS


    Beteiligte:
    BEUTIN BRUNO ALBERT (Autor:in) / PEREIRA ALEXIS (Autor:in) / ZSIGA ZOLTAN (Autor:in)

    Erscheinungsdatum :

    2024-04-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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