Exhaust turbine assembly

Patent metadata

Field	Value
Publication number	US-10087940-B2
Application number	US-201414566522-A
Country	US
Kind code	B2
Filing date	Dec 10, 2014
Priority date	Dec 10, 2014
Publication date	Oct 2, 2018
Grant date	Oct 2, 2018

Abstract

An assembly can include a turbine wheel; a turbine housing that includes a lower turbine housing surface that extends from an exhaust volute to a cylindrical surface that defines an upper portion of a turbine wheel space; a shroud component that includes a contoured surface disposed between an inner end of an upper shroud component surface and an inner end of a lower shroud component surface where the contoured surface defines a lower portion of a turbine wheel space; and a seal mechanism where the turbine housing and the shroud component form an axial gap between a lower axial position of the cylindrical surface and an upper axial position of the contoured surface where the axial gap is axially positioned between an axial position of an inducer portion of the turbine wheel and an axial position of an exducer portion of the turbine wheel.

First claim

What is claimed is:

1. An assembly comprising:
a turbine wheel that comprises a base, a nose, a rotational axis extending from a lower position at the base to an upper position at the nose, an inducer portion and an exducer portion;
a turbine housing that at least in part defines an exhaust volute and that comprises a lower turbine housing surface that extends from the exhaust volute to a cylindrical surface that defines an upper portion of a turbine wheel space for the turbine wheel;
a shroud component that comprises an upper shroud component surface, a lower shroud component surface and a contoured surface disposed between an inner end of the upper shroud component surface and an inner end of the lower shroud component surface wherein the contoured surface defines a lower portion of the turbine wheel space for the turbine wheel; and
a seal mechanism wherein the turbine housing receives the shroud component and forms an axial gap between a lower axial position of the cylindrical surface and an upper axial position of the contoured surface, wherein the turbine housing and the shroud component receive at least a portion of the turbine wheel, wherein the axial gap is axially positioned between an axial position of the inducer portion of the turbine wheel and an axial position of the exducer portion of the turbine wheel and wherein the seal mechanism hinders flow of exhaust from the exhaust volute to the turbine wheel space via the axial gap, wherein the seal mechanism comprises a seal that contacts the lower turbine housing surface of the turbine housing and the upper shroud component surface of the shroud component to form seal interfaces and wherein the lower turbine housing surface of the turbine housing comprises an annular step having an axial step height and wherein the seal comprises an axial height defined by the axial gap and the axial step height.

2. A turbine assembly for a turbocharger comprising:
a turbine wheel that comprises a base, a nose, and a rotational axis extending from a lower position at the base to an upper position at the nose;
a turbine housing that comprises a lower turbine housing surface that extends to a cylindrical surface that defines an upper portion of a turbine wheel space for the turbine wheel;
a shroud component that comprises a lower shroud component surface, an upper shroud component surface, and a contoured surface that extends between the lower shroud component surface and the upper shroud component surface and that defines a lower portion of the turbine wheel space, wherein the turbine housing receives the shroud component and forms an axial gap between a lower axial position of the cylindrical surface and an upper axial position of the contoured surface; and
a seal that comprises a lower edge, a sloped annular portion that extends from the lower edge, a lower bend that extends from the sloped annular portion, a cylindrical portion that extends from the lower bend, and an upper bend that extends from the cylindrical portion to an upper edge, wherein the seal contacts the lower turbine housing surface of the turbine housing and contacts the upper shroud component surface of the shroud component to axially overlap at least a portion of the cylindrical portion of the seal and the axial gap, and wherein the turbine housing defines in part a volute wherein, in absence of the seal, a line-of-sight of exists between the volute and the axial gap.

3. The turbine assembly of claim 1 wherein the lower edge of the seal comprises a radius and wherein the upper shroud component surface comprises a ridge disposed at a radius that exceeds the radius of the lower edge of the seal.

4. The turbine assembly of claim 3 wherein the upper shroud component surface comprises a well that extends radially inwardly from the ridge and wherein the lower edge of the seal is disposed within the well.

5. The turbine assembly of claim 1 wherein the upper shroud component surface comprises an annular axial face, wherein the lower turbine housing surface comprises an annular axial face and wherein the axial gap exists between the annular axial faces.

6. The turbine assembly of claim 1 wherein the upper shroud component surface comprises an annular ridge, an annular well, an annular shoulder and an annular axial face.

7. The turbine assembly of claim 1 wherein the lower turbine housing surface comprises an annular ridge, an annular well, an annular shoulder and an annular axial face.

8. The turbine assembly of claim 1 wherein the upper shroud component surface comprises a shroud component annular ridge, a shroud component annular well, a shroud component annular shoulder and a shroud component annular axial face and wherein the lower turbine housing surface comprises a turbine housing annular ridge, a turbine housing annular well, a turbine housing annular shoulder and a turbine housing annular axial face.

9. The turbine assembly of claim 1 wherein an axial clearance exists between the upper shroud component surface and the lower turbine housing surface.

10. The turbine assembly of claim 1 wherein the turbine wheel comprises an inducer portion and an exducer portion wherein the axial gap is axially disposed between the inducer portion and the exducer portion of the turbine wheel.

11. A turbine assembly for a turbocharger comprising:
a turbine wheel that comprises a base, a nose, and a rotational axis extending from a lower position at the base to an upper position at the nose;
a turbine housing that comprises a lower turbine housing surface that extends to a cylindrical surface that defines an upper portion of a turbine wheel space for the turbine wheel;
a shroud component that comprises a lower shroud component surface, an upper shroud component surface, and a contoured surface that extends between the lower shroud component surface and the upper shroud component surface and that defines a lower portion of the turbine wheel space, wherein the turbine housing receives the shroud component and forms an axial gap between a lower axial position of the cylindrical surface and an upper axial position of the contoured surface; and
a seal that comprises a lower edge, a sloped annular portion that extends from the lower edge, a lower bend that extends from the sloped annular portion, a cylindrical portion that extends from the lower bend, and an upper bend that extends from the cylindrical portion to an upper edge, wherein the seal contacts the lower turbine housing surface of the turbine housing and contacts the upper shroud component surface of the shroud component to axially overlap at least a portion of the cylindrical portion of the seal and the axial gap, and wherein the lower edge of the seal comprises a radius and wherein the upper shroud component surface comprises a ridge disposed at a radius that exceeds the radius of the lower edge of the seal.

12. The turbine assembly of claim 11 wherein the upper shroud component surface comprises a well that extends radially inwardly from the ridge and wherein the lower edge of the seal is disposed within the well.

Assignees

• Honeywell Int Inc

Inventors

• Gerard Arnaud
• Solanki Shankar Pandurangasa
• Eumont Vincent
• Morand Nicolas
• Abel Francis
• Barthelet Pierre

Classifications

• F01D11/003 Primary

  by packing rings; Mechanical seals · CPC title

• F04D29/083

  especially adapted for elastic fluid pumps · CPC title

• F01D25/24

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title

• F04D25/045

  the pump wheel carrying the fluid driving means, e.g. turbine blades · CPC title

• F04D17/10 Primary

  for compressing or evacuating · CPC title