Safran Aircraft Engines

Snecma

Benoit Guillaume Farvacque

Catherine Pikovsky

Serge Rene Morreale

Serge René Morreale

Mathieu Jean Pierre Trohel

An annular cap for collecting lubricating oil for turbomachine equipment is configured to extend around the equipment and to rotate about an axis. The cap includes through-orifices through which the oil can pass radially under the effect of spinning. The cap further includes means of deflecting the oil leaving the orifices in a direction substantially transverse to the axis and substantially tangential to the cap.

Lubricating-oil collection cap for turbomachine equipment

The invention relates to a turbine engine module comprising a rotating device () having a cover (), said cover () comprising radial through ports () for the passage of the oil escaping by centrifugation and means () for guiding the oil leaving said ports () radially outwards, and a casing () defining at least one portion of a lubrication enclosure of said device (), said casing () comprising at least one gutter (), arranged to recover the oil, characterized in that the gutter () comprises an annular bottom wall () having at least one discharge port, and in that the casing () comprises at least one other port located on the outside of the gutter (), said at least one other port and said at least one discharge port being connected to common discharge means.

Growing community of inventors

Moissy-Cramayel, France

Benoit Guillaume Farvacque