Safran Aircraft Engines

Christoph Marcel Lucien Perdrigeon

Regis Eugene Henri Servant

Device for distributing oil from a rolling bearing () for an aircraft turbine engine, comprising: &#x2014;a rolling bearing (), &#x2014;a body () for distributing oil, which body is configured to be mounted on a turbine engine shaft (), said body comprising: i) a first outer cylindrical surface () for mounting the inner ring () of the bearing, ii) a ring-shaped scoop () for recovering oil, iii) a ring-shaped track () of a dynamic seal (), iv) a circuit () for lubricating the bearing and cooling the track, said circuit being formed in the body, characterised in that the ring-shaped scoop is the first scoop () which supplies a first portion () of the circuit with a view to cooling the track, and in that the body comprises a second ring-shaped scoop () for recovering oil, which scoop supplies a second portion () of the circuit with a view to lubricating the bearing.

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Moissy-Cramayel, France

Christoph Marcel Lucien Perdrigeon