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).
ENSEMBLE DE SUPPORTAGE D'UNE BOITE D'ACCESSOIRES D'UNE TURBOMACHINE D'AERONEF
ASSEMBLY FOR SUPPORTING AN ACCESSORY GEARBOX OF AN AIRCRAFT TURBINE ENGINE
ANORDNUNG ZUR UNTERSTÜTZUNG EINES HILFSGETRIEBE EINES FLUGZEUGTURBINENTRIEBWERKS
2024-04-10
Patent
Elektronische Ressource
Französisch
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