Fan module for an aircraft turbine engine, the module including a fan having variable-pitch blades and an oil-transfer device configured to transfer oil between a stator and a rotor. The device includes a stator ring having internal oil ducts, a shaft engaged in the ring and having internal oil ducts, and a plain bearing and rolling bearings which are mounted between the ring and the shaft, the ring including first fluidic-connection ports which are configured to cooperate by male-female engagement with ends of oil-supply sockets during blind assembly of the device by axial translation downstream of the device as a whole.
MODULE DE SOUFFLANTE EQUIPE D'UN DISPOSITIF DE TRANSFERT D'HUILE
FAN MODULE EQUIPPED WITH AN OIL-TRANSFER DEVICE
LÜFTERMODUL MIT ÖLÜBERTRAGUNGSVORRICHTUNG
2024-01-24
Patent
Elektronische Ressource
Französisch
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