Pressurized seal system for a power turbine unit

Patent metadata

Field	Value
Publication number	US-9932848-B2
Application number	US-201214438619-A
Country	US
Kind code	B2
Filing date	Nov 21, 2012
Priority date	Nov 21, 2012
Publication date	Apr 3, 2018
Grant date	Apr 3, 2018

Abstract

A power turbine unit includes a turbine housing, an exhaust duct, a turbine wheel with blades positioned in the exhaust duct, a shaft rigidly connected to the turbine wheel and rotatably supported in the housing, and an oil sealing system. The oil sealing system includes a sealing arrangement positioned in the vicinity of the turbine wheel for preventing oil from escaping from the turbine housing along the shaft to the exhaust duct. The oil sealing system further includes a buffer gas duct that is arranged to supply exhaust gas from the exhaust duct to the sealing arrangement for pressurizing the sealing arrangement.

First claim

The invention claimed is:

1. Power turbine unit comprising
a turbine housing,
an exhaust duct,
a turbine wheel with blades positioned in the exhaust duct,
a shaft rigidly connected to the turbine wheel and rotatably supported in the housing, and
an oil sealing system comprising a sealing arrangement positioned in the vicinity of the turbine wheel for preventing oil from escaping from the turbine housing along the shaft to the exhaust duct, wherein the oil sealing system comprises a buffer gas duct that is arranged to supply exhaust gas from the exhaust duct to the sealing arrangement for pressurizing the sealing arrangement, and
the buffer gas duct is formed partly by an outer buffer gas duct wall and an inner buffer gas duct wall, each of which being separate from the housing, wherein the buffer gas duct Is formed by at least an outer buffer gas duct wall, which is fastened to the housing by means of at least one fastener.

2. The power turbine unit according to claim 1 , wherein the buffer gas duct is formed of the outer buffer gas duct wall and an inner buffer gas duct wall, each of which being fastened to the housing by means of at least one of the at least one fasteners.

3. The power turbine unit according to claim 1 , wherein the outer buffer gas duct wall forms an inner wall of the exhaust duct.

4. The power turbine unit according to claim 1 , wherein the inner and/or outer buffer gas duct wall is formed of sheet metal.

5. The power turbine unit according to claim 1 , wherein the inner and/or outer buffer gas duct wall is at least partly formed of an annular conical sleeve section that surrounds the shaft.

6. The power turbine unit according to claim 1 , wherein the buffer gas duct is thermally insulated from the housing.

7. The power turbine unit according to claim 6 , wherein the thermal insulation is partly formed by an air gap between the buffer gas duct and the housing.

8. The power turbine unit according to claim 6 , wherein the thermal insulation is at least partly formed by an insulation material having a low thermal conductivity being arranged between the buffer gas duct and the housing.

9. The power turbine unit according to claim 6 , wherein the thermal insulation is partly realised by providing at least one of the at least one fasteners in at least one axial end region of the buffer gas duct, and specifically only in one axial end region of the buffer gas duct.

10. The power turbine unit according to claim 6 , wherein the thermal insulation is partly realised by providing insulation material between at least part of at least one of the at least one fasteners and the inner and/or outer buffer gas duct walls.

11. The power turbine unit according to claim 1 , wherein the at least one fastener is engaged in a hole in the housing.

12. The power turbine unit according to claim 1 , wherein the at least one fastener is engaged in a hole or recess in the inner and/or outer buffer gas duct walls.

13. The power turbine unit according to claim 1 , wherein the outer buffer gas duct wall have a first section forming part of the exhaust duct, and a second section extending radially inwardly towards the shaft.

14. The power turbine unit according to claim 1 , wherein the sealing arrangement comprises a first sealing section and a second sealing section, the first sealing section being axially displaced from the second sealing section,
and the buffer gas duct is arranged to supply exhaust gas to an annular cavity that is axially delimited by the first and second sealing sections.

15. The power turbine unit according to claim 14 , wherein the second sealing section is defined partly by the outer buffer gas duct wall.

16. The power turbine unit according to claim 14 , wherein the second sealing section is defined partly by at least one radial projection arranged on the shaft.

17. The power turbine unit according to claim 1 , wherein at least one exhaust gas inlet is provided in the exhaust duct for conveying exhaust gas from the exhaust duct into the buffer gas duct.

18. The power turbine unit according to claim 17 , wherein at least one exhaust gas inlet is formed as a NACA inlet.

19. The power turbine unit according to claim 16 , wherein the exhaust duct is a diffuser duct, and the at least one inlet is arranged in a downstream region of the diffuser duct, where the exhaust gas static pressure is configured to be higher than in an upstream region of the diffuser duct.

20. The power turbine unit according to claim 17 , wherein the at least one inlet is arranged downstream of the turbine wheel in the exhaust duct.

21. Internal combustion engine comprising a turbo charger and a power turbine unit, the power turbine unit comprising
a turbine housing,
an exhaust duct,
a turbine wheel with blades positioned in the exhaust duct,
a shaft rigidly connected to the turbine wheel and rotatably supported in the housing, and
an oil sealing system comprising a sealing arrangement positioned in the vicinity of the turbine wheel for preventing oil from escaping from the turbine housing along the shaft to the exhaust duct, wherein
the oil sealing system comprises a buffer gas duct that is arranged to supply exhaust gas from the exhaust duct to the sealing arrangement for pressurizing the sealing arrangement, and
the buffer gas duct is formed partly by an outer buffer gas duct wall and an inner buffer gas duct wall, each of which being separate from the housing, wherein the power turbine unit is arranged downstream of the turbo charger and connected to an engine crankshaft via fluid coupling and a gear train.

Assignees

• Volvo Truck Corp

Inventors

• Giselmo Kent
• Ekstrand Magnus
• Sundin Lars
• Krausche Sebastian

Classifications

• F01D25/22

  using working-fluid or other gaseous fluid as lubricant · CPC title

• F01D25/30

  Exhaust heads, chambers, or the like · CPC title

• F02C6/12

  Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure · CPC title

• F01D11/04 Primary

  using sealing fluid, e.g. steam · CPC title