Oil-cooled exhaust turbine apparatus
According to embodiments described herein, an oil-cooled exhaust turbine apparatus is provided. The exhaust turbine apparatus comprises a rotatable shaft with a turbine wheel, a bearing member comprising a bearing, a bearing housing comprising a sealing bush portion for providing a first sealing device axially between the turbine wheel and the bearing member; an oil cooling chamber for cooling an inner face of the bearing housing, an oil channel for providing oil into the oil cooling chamber, an oil drainage chamber arranged axially between the bearing member and the sealing bush portion and an oil barrier wall surrounding, in at least a vertically top circumferential segment, a radially outer side of the oil drainage chamber for covering the oil drainage chamber from the oil cooling chamber.
1. An oil-cooled exhaust turbine apparatus, the exhaust turbine apparatus comprising:
a rotatable shaft with a turbine wheel;
a bearing member comprising a bearing for rotatably supporting the shaft;
a bearing housing accommodating the bearing member therein and comprising a sealing bush portion extending radially inwardly towards the shaft at an axial position between the turbine wheel and the bearing member for providing a first sealing device axially between the turbine wheel and the bearing member; and
an oil cooling chamber for cooling an inner face of the bearing housing; wherein
the exhaust turbine apparatus comprises an oil channel for providing oil into the oil cooling chamber for cooling the inner wall of the bearing housing using the oil as cooling medium; and
an oil drainage chamber arranged axially between the bearing member and the sealing bush portion; and wherein
the exhaust turbine apparatus further comprises an oil barrier wall surrounding, in at least a vertically top circumferential segment, a radially outer side of the oil drainage chamber for covering the oil drainage chamber from the oil cooling chamber;
wherein the oil barrier wall is formed integrally with one of the sealing bush portion and the bearing member; and
wherein the oil barrier wall further comprises a wall tip section axially overlapping with the other one of the sealing bush portion and the bearing member, wherein the wall tip section integrally formed with the sealing bush portion axially overlaps only a portion of the bearing member.
2. The oil-cooled exhaust turbine apparatus according to claim 1 , wherein the oil drainage chamber extends radially outwardly from the shaft and/or from a bearing bush of the bearing member.
3. The oil-cooled exhaust turbine apparatus according claim 1 , wherein the oil barrier wall comprises an axial wall section extending axially from a wall base at the one of the sealing bush portion and the bearing member.
4. The oil-cooled exhaust turbine apparatus according to claim 1 , wherein the oil barrier wall further comprises a radial wall section extending radially outwardly from the wall portion.
5. The oil-cooled exhaust turbine apparatus according to claim 1 , wherein the oil drainage chamber is at least formed by a turbine-facing side wall of the bearing member and a bearing-member-facing side wall of the sealing bush portion and optionally by the shaft.
6. The oil-cooled exhaust turbine apparatus according to claim 1 , wherein the oil cooling chamber is axially delimited by the bearing housing and the bearing member and wherein the sealing bush portion delimits the oil cooling chamber at least partially from radially inwards and axially from the turbine wheel.
7. The oil-cooled exhaust turbine apparatus according to claim 1 , wherein the oil drainage chamber has an oil drainage opening at a vertically bottom side of the oil drainage chamber.
8. The oil-cooled exhaust turbine apparatus according to claim 1 , wherein the oil cooling chamber comprises an oil recess for receiving oil from the oil cooling chamber and wherein the oil recess forms a drainage channel, the drainage channel extending at least partially circumferentially for guiding the cooling oil downwards along the oil drainage channel around the rotatable shaft.
9. The oil-cooled exhaust turbine apparatus according to claim 1 , wherein an oil drainage is arranged vertically below the shaft and wherein the oil drainage channel is configured to guide oil received from the oil cooling chamber and/or the oil barrier wall to the oil drainage.
10. The oil-cooled exhaust turbine apparatus according to claim 1 , wherein the first sealing device comprises a sealing element and wherein the shaft comprises a cavity for supporting the sealing element.
11. The oil-cooled exhaust turbine apparatus according to claim 1 , wherein a second sealing device is provided between the oil barrier wall and the bearing member and/or between the oil barrier wall and the sealing bush portion.
12. The oil-cooled exhaust turbine apparatus according to claim 1 , wherein the oil barrier wall is arranged radially inwardly of the oil channel.
13. The oil-cooled exhaust turbine apparatus according to claim 11 , wherein the second sealing device is selected from the group consisting of a sealing gap, a sealing ring, a labyrinth seal, a contact seal, seal air and/or combinations thereof.
14. The oil-cooled exhaust turbine apparatus according to claim 1 , wherein the bearing member comprises an oil deflection plate at the turbine-facing side wall of the bearing member and wherein the oil barrier wall axially overlaps with the oil deflection plate.
15. The oil-cooled exhaust turbine apparatus according to claim 1 , wherein the oil-cooled exhaust turbine apparatus is a turbocharger or a power turbine.
16. The oil-cooled exhaust turbine apparatus according to claim 1 , wherein the sealing bush portion is comprised of the turbine-facing side wall of the bearing housing.
17. The oil-cooled exhaust turbine apparatus according to claim 1 , wherein the sealing bush portion is comprised of a separate component of the bearing housing.
18. An oil-cooled exhaust turbine apparatus, the exhaust turbine apparatus comprising:
a rotatable shaft with a turbine wheel;
a bearing member comprising a bearing for rotatably supporting the shaft;
a bearing housing accommodating the bearing member therein and comprising a sealing bush portion extending radially inwardly towards the shaft at an axial position between the turbine wheel and the bearing member for providing a first sealing device axially between the turbine wheel and the bearing member; and
an oil cooling chamber for cooling an inner face of the bearing housing; wherein the exhaust turbine apparatus comprises an oil channel for providing oil into the oil cooling chamber for cooling the inner wall of the bearing housing using the oil as cooling medium; and
an oil drainage chamber arranged axially between the bearing member and the sealing bush portion; and wherein
the exhaust turbine apparatus further comprises an oil barrier wall surrounding, in at least a vertically top circumferential segment, a radially outer side of the oil drainage chamber for covering the oil drainage chamber from the oil cooling chamber;
wherein the oil barrier wall is formed integrally with one of the sealing bush portion and the bearing member;
wherein the oil barrier wall further comprises a wall tip section axially overlapping with the other one of the sealing bush portion and the bearing member; and
wherein the bearing member comprises an oil deflection plate at a turbine-facing side wall of the bearing member and wherein the oil barrier wall axially overlaps with the oil deflection plate.
19. An oil-cooled exhaust turbine apparatus, the exhaust turbine apparatus comprising:
a rotatable shaft with a turbine wheel;
a bearing member comprising a bearing for rotatably supporting the shaft;
a bearing housing accommodating the bearing member therein and comprising a sealing bush portion extending radially inwardly towards the shaft at an axial position between the turbine wheel and the bearing member for providing a first sealing device axially between the turbine wheel and the bearing member, wherein the sealing bush portion is comprised of a separate component of the bearing housing; and
an oil cooling chamber for cooling an inner face of the bearing housing; wherein
the exhaust turbine apparatus comprises an oil channel for providing oil into the oil cooling chamber for cooling the inner wall of the bearing housing using the oil as cooling medium; and
an oil drainage chamber arranged axially between the bearing member and the sealing bush portion; and wherein
the exhaust turbine apparatus further comprises an oil barrier wall surrounding, in at least a vertically top circumferential segment, a radially outer side of the oil drainage chamber for covering the oil drainage chamber from the oil cooling chamber;
wherein the oil barrier wall is formed integrally with one of the sealing bush portion and the bearing member; and
wherein the oil barrier wall further comprises a wall tip section axially overlapping with the other one of the sealing bush portion and the bearing member.