Turbine exhaust housing

Patent metadata

Field	Value
Publication number	US-10196914-B2
Application number	US-201615168157-A
Country	US
Kind code	B2
Filing date	May 30, 2016
Priority date	May 11, 2012
Publication date	Feb 5, 2019
Grant date	Feb 5, 2019

Abstract

A turbine assembly can include a turbine wheel, a shroud component, a turbine housing and a seal that includes a wall and a lower lip that that extends radially outwardly from the wall where the seal is disposed, at least in part, between an outer surface of the shroud component and an inner surface of the turbine housing and where the lower lip is in contact with the turbine housing.

First claim

What is claimed is:

1. A turbine assembly comprising:
a turbine wheel that comprises a base, a nose, blades, and a rotational axis that extends from the base to the nose;
a shroud component that comprises an axis aligned with the rotational axis of the turbine wheel, an inner shroud surface, a lower axial face, an upper axial face and an outer surface that extends between the lower axial face and the upper axial face;
a turbine housing that comprises an axis aligned with the rotational axis of the turbine wheel, a lower axial face, an upper axial face and an inner surface that extends between the lower axial face and the upper axial face; and
a seal that comprises
an axis aligned with the rotational axis of the turbine wheel,
a wall disposed between the outer surface of the shroud component and the inner surface of the turbine housing, and
a lower lip extending radially outwardly from the wall, the lower lip disposed, at least in part, between the lower axial face of the shroud component and the lower axial face of the turbine housing and in contact with the lower axial face of the turbine housing.

2. The turbine assembly of claim 1 wherein the seal comprises an upper lip that extends from the wall wherein the upper lip is disposed between the upper axial face of the shroud component and the upper axial face of the turbine housing.

3. The turbine assembly of claim 2 wherein the upper lip of the seal extends radially inwardly from the wall at approximately a right angle.

4. The turbine assembly of claim 1 wherein the seal comprises an upper, inwardly hooked portion that extends from the wall.

5. The turbine assembly of claim 1 wherein the wall of the seal contacts the inner surface of the turbine housing.

6. The turbine assembly of claim 1 wherein the wall of the seal comprises a diameter that exceeds a diameter of the inner surface of the turbine housing to provides for an interference fit between the seal and the turbine housing.

7. The turbine assembly of claim 1 wherein the seal contacts the shroud component and contacts the turbine housing.

8. The turbine assembly of claim 1 wherein the turbine housing defines, at least in part, a volute and wherein the lower axial face of the shroud component extends radially outwardly into the volute.

9. The turbine assembly of claim 1 wherein the outer surface of the shroud component comprises a ridge.

10. The turbine assembly of claim 9 wherein the seal contacts the ridge.

11. A method comprising:
providing a center housing, a variable geometry cartridge, a turbine housing and a seal that comprises a wall and a lower lip;
positioning the variable geometry cartridge with respect to the center housing; and
attaching the turbine housing to the center housing with the seal disposed between the variable geometry cartridge and the turbine housing to form a turbocharger wherein the lower lip of the seal contacts a surface of the turbine housing.

12. The method of claim 11 further comprising operating the turbocharger and expanding or contracting the seal between the variable geometry cartridge and the turbine housing.

13. A turbocharger assembly comprising:
a compressor wheel disposed in a compressor housing;
a center housing that comprises a bore and a bearing system disposed in the bore, the compressor housing attached to the center housing;
a shaft and turbine wheel assembly that comprises a shaft portion, a turbine wheel portion, and a rotational axis wherein the compressor wheel is attached to the shaft portion and the shaft portion is rotatably supported by the bearing system disposed in the bore of the center housing;
a variable geometry cartridge positioned with respect to the center housing wherein the variable geometry cartridge comprises a shroud component that comprises an axis aligned with the rotational axis of the turbine wheel, an inner shroud surface, a lower axial face, an upper axial face and an outer surface that extends between the lower axial face and the upper axial face;
a turbine housing attached to the center housing wherein the turbine housing comprises an axis aligned with the rotational axis of the turbine wheel, a lower axial face, an upper axial face and an inner surface that extends between the lower axial face and the upper axial face; and
a seal that comprises
an axis aligned with the rotational axis of the turbine wheel,
a wall disposed between the outer surface of the shroud component and the inner surface of the turbine housing, and
a lower lip extending radially outwardly from the wall, the lower lip disposed, at least in part, between the lower axial face of the shroud component and the lower axial face of the turbine housing and in contact with the lower axial face of the turbine housing.

Assignees

• Garrett Transportation I Inc

Inventors

• Gerard Arnaud
• Tingaud Aurelien
• Solanki Shankar Pandurangasa
• Javvadi Mohan

Classifications

• F02C7/28

  Arrangement of seals · CPC title

• F02B37/24

  by using pumps or turbines with adjustable guide vanes · CPC title

• Y10T29/49323

  Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles · CPC title

• F02B33/40

  of non-positive-displacement type · CPC title

• F01D11/003

  by packing rings; Mechanical seals · CPC title