A support assembly for supporting a main accessory gearbox of an aircraft turbine engine, the accessory gearbox including gears and supporting at least one item of equipment driven by the gears. The support assembly can include a structure for connecting and supporting the turbine engine to a pylon of the aircraft including: an intermediate axial portion for attachment to the pylon, having an upper end that defines a linking interface with the pylon, the intermediate axial portion bearing suspension rods, which are intended to be connected to the turbine engine; a front axial portion extending forward of the intermediate portion and having at least one suspension member configured to be connected to the turbine engine; and a rear axial portion extending rearwards of the intermediate portion and supporting the main accessory gearbox.
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
10.04.2024
Patent
Elektronische Ressource
Französisch
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