Abstract: 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.

Abstract: The invention relates to a turbine engine module comprising a rotating device (1) having a cover (5), said cover (5) comprising radial through ports (8) for the passage of the oil escaping by centrifugation and means (10) for guiding the oil leaving said ports (8) radially outwards, and a casing (2) defining at least one portion of a lubrication enclosure of said device (1), said casing (2) comprising at least one gutter (13), arranged to recover the oil, characterized in that the gutter (13) comprises an annular bottom wall (12) having at least one discharge port, and in that the casing (2) comprises at least one other port located on the outside of the gutter (13), said at least one other port and said at least one discharge port being connected to common discharge means.

Abstract: 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.

Abstract: The invention relates to a turbine engine module comprising a rotating device (1) having a cover (5), said cover (5) comprising radial through ports (8) for the passage of the oil escaping by centrifugation and means (10) for guiding the oil leaving said ports (8) radially outwards, and a casing (2) defining at least one portion of a lubrication enclosure of said device (1), said casing (2) comprising at least one gutter (13), arranged to recover the oil, characterised in that the gutter (13) comprises an annular bottom wall (12) having at least one discharge port, and in that the casing (2) comprises at least one other port located on the outside of the gutter (13), said at least one other port and said at least one discharge port being connected to common discharge means.

Abstract: The main object of the invention is an assembly forming a seal (1) for a turbomachine (10), used to provide a seal between two elements of the turbomachine (10) rotating relative to one another, and being rotationally symmetrical around an axis (X) of the assembly forming a seal (1), characterised in that it includes a brush seal (2), which is annular around the axis (X) of the assembly forming a seal (1), having multiple elastic sealing bristles (5, 5a, 5b) intended to be attached to one of the two elements of the turbomachine (10) rotating relative to one another, and at least one lip (3, 3a, 3b, 3c), which is annular around the axis (X) of the assembly forming a seal (1), extending radially in the direction of the brush seal (2), intended to be attached to the other of the two elements of the turbomachine (10) rotating relative to one another, where the said at least one lip (3, 3a, 3b, 3c) penetrates at least partially into the brush seal (2).