Multi-piece piston ring for a turbocharger shaft assembly

Patent metadata

Field	Value
Publication number	US-9267441-B1
Application number	US-201514660114-A
Country	US
Kind code	B1
Filing date	Mar 17, 2015
Priority date	Mar 17, 2015
Publication date	Feb 23, 2016
Grant date	Feb 23, 2016

Abstract

An apparatus includes a bearing housing, a shaft assembly that extends through the bearing housing along a shaft axis, an annular groove formed on the shaft assembly, and a piston ring assembly that is engaged with the bearing housing and extends into the groove of the shaft assembly. The piston ring assembly includes a first ring portion and a second ring portion. The first ring portion has a first contact face that is oriented at a non-perpendicular with respect to the shaft axis, and the second ring portion has a second contact face that is oriented at a non-perpendicular angle with respect to the shaft axis and is engageable with the first contact face.

First claim

The invention claimed is:

1. An apparatus, comprising:
a bearing housing;
a shaft assembly that extends through the bearing housing along a shaft axis;
an annular groove that is formed on the shaft assembly and extends around the shaft axis; and
a piston ring assembly that is engaged with the bearing housing and extends into the annular groove of the shaft assembly, the piston ring assembly including a first ring portion and a second ring portion, the first ring portion having a first contact face that is oriented at a non-perpendicular angle with respect to the shaft axis, and the second ring portion having an outer surface that is engaged with the bearing housing and a second contact face that is oriented at a non-perpendicular angle with respect to the shaft axis and is engageable with the first contact face, wherein the first contact face is oriented such that it faces outward with respect to the shaft axis and the second contact face is oriented such that it faces inward with respect to the shaft axis.

2. The apparatus of claim 1 , wherein the first contact face defines a first angle with respect to the shaft axis, the second contact face defines a second angle with respect to the shaft axis, and the first angle and the second angle are supplementary angles.

3. The apparatus of claim 1 , wherein interaction of the first contact face and the second contact face causes expansion or contraction of an axial length of the piston ring assembly in response to changes in a thrust load applied to the shaft assembly.

4. The apparatus of claim 1 , wherein engagement of the piston ring assembly with the bearing housing restrains rotation of the piston ring assembly with respect to the bearing housing.

5. The apparatus of claim 1 , wherein the first ring portion includes an inner surface that is arranged around the shaft axis at a constant radius for sealing with respect to the shaft assembly.

6. The apparatus of claim 1 , wherein the second ring portion includes an outer surface that is arranged around the shaft axis at a constant radius for sealing with respect to the bearing housing.

7. The apparatus of claim 1 , wherein the shaft assembly includes a turbine wheel.

8. The apparatus of claim 1 , wherein the shaft assembly includes a compressor wheel.

9. The apparatus of claim 1 , wherein the first contact face and the second contact face are each defined as a portion of a conical surface having its axis aligned with the shaft axis.

10. A turbocharger, comprising:
a bearing housing;
a compressor housing;
a turbine housing;
a shaft assembly that extends through the bearing housing along a shaft axis, the shaft assembly including a shaft, a compressor wheel that is disposed in the compressor housing and is connected to the shaft, and a turbine wheel that is disposed in the turbine housing and is connected to the shaft;
an annular groove that is formed on the shaft assembly an extends around the shaft axis; and
a piston ring assembly that is engaged with the bearing housing and extends into the annular groove of the shaft assembly, the piston ring assembly including a first ring portion and a second ring portion, the first ring portion having a first contact face that is oriented at a non-perpendicular angle with respect to the shaft axis, and the second ring portion having an outer surface that is engaged with the bearing housing and a second contact face that is oriented at a non-perpendicular angle with respect to the shaft axis and is engageable with the first contact face, wherein the first contact face is oriented such that it faces outward with respect to the shaft axis and the second contact face is oriented such that it faces inward with respect to the shaft axis.

11. The turbocharger of claim 10 , wherein the first contact face defines a first angle with respect to the shaft axis, the second contact face defines a second angle with respect to the shaft axis, and the first angle and the second angle are supplementary angles.

12. The turbocharger of claim 10 , wherein interaction of the first contact face and the second contact face causes expansion or contraction of an axial length of the piston ring assembly in response to changes in a thrust load applied to the shaft assembly.

13. The turbocharger of claim 10 , wherein engagement of the piston ring assembly with the bearing housing restrains rotation of the piston ring assembly with respect to the bearing housing.

14. The turbocharger of claim 10 , wherein the first ring portion includes an inner surface that is arranged around the shaft axis at a constant radius for sealing with respect to the shaft assembly.

15. The turbocharger of claim 10 , wherein the second ring portion includes an outer surface that is arranged around the shaft axis at a constant radius for sealing with respect to the bearing housing.

16. The turbocharger of claim 10 , wherein the first contact face and the second contact face are each defined as a portion of a conical surface having its axis aligned with the shaft axis.

17. An apparatus, comprising:
a stationary structure that defines a bore;
a rotating structure that is disposed within the bore of the stationary structure, extends along an axis and includes an annular groove that is formed on the rotating structure and extends around the axis; and
a piston ring assembly that is engaged with the stationary structure and extends into the annular groove of the rotating structure, the piston ring assembly including a first ring portion and a second ring portion, the first ring portion having a first contact face that is oriented at a non-perpendicular angle with respect to the axis, and the second ring portion having an outer surface that is engaged with the stationary structure and a second contact face that is oriented at a non-perpendicular angle with respect to the axis and is engageable with the first contact face, wherein the first contact face is oriented such that it faces outward with respect to the axis and the second contact face is oriented such that it faces inward with respect to the axis.

18. The apparatus of claim 17 , wherein the first contact face defines a first angle with respect to the axis, the second contact face defines a second angle with respect to the axis, the first angle and the second angle are supplementary angles, the first contact face is oriented such that is faces outward with respect to the axis, the second contact face is oriented such that is faces outward with respect to the axis, and interaction of the first contact face and the second contact face causes expansion or contraction of an axial length of the piston ring assembly in response to changes in a thrust load applied to the rotating structure.

19. The apparatus of claim 17 , wherein the first contact face and the second contact face are each defined as a portion of a conical surface having its axis aligned with the axis.

Assignees

• Borgwarner Inc

Inventors

• Ellwood Iii Erwin Perry
• Hastings Sean

Classifications

• F05D2220/40

  in turbochargers · CPC title

• F02C7/28 Primary

  Arrangement of seals · CPC title

• F04D29/10

  Shaft sealings · CPC title

• F16J15/3464

  Mounting of the seal · CPC title

• F16J15/346

  the pressing force varying during operation · CPC title