System for sealing and draining oil leaks for a turbomachine bearing enclosure
A sealing system for a turbomachine bearing enclosure includes bearing with a stator carrying a rotor; a seal carried by the stator and surrounding the rotor; an external peripheral groove carried by the stator in the vicinity of the seal for collecting oil which exits the enclosure running along the rotor through the seal and which is centrifuged by the rotor towards this groove; and a drain at the bottom for discharging the oil from the groove. This groove is open towards the inside and is delimited by a base extended by two side walls, the side wall opposite the seal is extended by a skirt oriented obliquely towards the base to delimit a gutter opening towards the base.
1 . A system for sealing and draining leaks of oil for a turbine-engine chamber enclosing a bearing, the system comprising:
the bearing which comprises a stator and a rotor which is carried by the stator, the stator rotating about a rotation axis;
a seal carried by the stator and surrounding the rotor;
an external circumferential groove carried by the stator while being contiguous with the seal to collect leaking oil travelling along the rotor through the seal and which is centrifuged by the rotor towards the external circumferential groove; and
a drain located at a lowest point of the external circumferential groove with respect to a vertical direction for collecting the oil recovered by the external circumferential groove, the external circumferential groove being open towards the rotation axis while being delimited by a bottom extended by upstream and downstream lateral walls, the downstream lateral wall that is opposite to the seal along the rotation axis terminating in a gutter opening towards the bottom.
2 . The system according to claim 1 , wherein the gutter is absent at the lowest point of the external circumferential groove with respect to the vertical direction.
3 . The system according to claim 1 , wherein the bottom is formed by a frustoconical wall, and an inside diameter of the frustoconical wall decreases on moving away from the seal.
4 . The system according to claim 1 , further comprising an internal circumferential groove formed in the rotor facing the external circumferential groove, the internal circumferential groove having a length along the rotation axis that is less than a length of the external circumferential groove along the rotation axis.
5 . The system according to claim 4 , wherein the internal circumferential groove has a frustoconically shaped bottom, and an inside diameter of the frustoconically shaped bottom decreases on moving away from the seal.
6 . The system according to claim 4 , wherein the rotor includes a circumferential rib terminating the internal circumferential groove.
7 . The system according to claim 1 , further comprising knife-edge seals secured to the rotor and sliding along a radially internal face of the gutter that is provided with abradable elements, to form a labyrinth seal.
8 . A turbine engine comprising a bearing chamber that is equipped with a sealing system according to claim 1 .
9 . The system according to claim 1 , wherein the gutter presents a trapezoidal cross-section.
10 . The system according to claim 1 , wherein the upstream wall runs along the seal.