Anisotropic bearing supports for turbochargers

Patent metadata

Field	Value
Publication number	US-9382812-B2
Application number	US-201414280614-A
Country	US
Kind code	B2
Filing date	May 18, 2014
Priority date	Oct 31, 2007
Publication date	Jul 5, 2016
Grant date	Jul 5, 2016

Abstract

A rotating assembly for a turbocharger can include a center housing that includes a through bore having a central axis; a bearing cartridge positioned in the through bore where the bearing cartridge includes an outer race, an inner race and rolling elements disposed between the inner race and the outer race; an anisotropic member positioned in the through bore between the outer race of the bearing cartridge and a surface of the center housing where the surface defines at least part of the through bore of the center housing; and a shaft rotatably supported in the center housing by the bearing cartridge where the inner race is mounted on the shaft and the shaft is connected at one end to a compressor wheel and at another end to a turbine wheel.

First claim

What is claimed is:

1. A rotating assembly for a turbocharger comprising:
a center housing that comprises a through bore having a central axis;
a bearing cartridge positioned in the through bore wherein the bearing cartridge comprises an outer race, an inner race and rolling elements disposed between the inner race and the outer race;
an anisotropic member positioned in the through bore between the outer race of the bearing cartridge and a surface of the center housing wherein the surface defines at least part of the through bore of the center housing and wherein the anisotropic member comprises a ring and a series of lobes arranged about the ring; and
a shaft rotatably supported in the center housing by the bearing cartridge wherein the inner race is mounted on the shaft and the shaft is connected at one end to a compressor wheel and at another end to a turbine wheel.

2. The rotating assembly of claim 1 wherein the outer race of the bearing cartridge comprises a radial groove and a piston ring seated in the groove that forms a seal between the outer race of the bearing cartridge and a surface of the center housing wherein the surface defines at least part of the through bore.

3. The rotating assembly of claim 1 comprising two anisotropic members positioned in the through bore of the center housing.

4. The rotating assembly of claim 1 further comprising a locating pin for limiting rotation of the outer race of the bearing cartridge in the through bore.

5. The rotating assembly of claim 1 wherein the series of lobes of the anisotropic member impart anisotropic stiffness to the anisotropic member.

6. The rotating assembly of claim 1 wherein the series of lobes comprises lobes positioned at multiple angles about the central axis to generate one or more planes of reflection asymmetry.

7. The rotating assembly of claim 1 wherein the ring of the anisotropic member comprises a split ring.

8. The rotating assembly of claim 1 having an axis perpendicular to the central axis of the through bore of the center housing and wherein the series of lobes of the anisotropic member comprise an alignment with respect to the axis perpendicular to the central axis.

9. The rotating assembly of claim 8 wherein the axis perpendicular to the central axis is aligned with gravity.

10. The rotating assembly of claim 1 wherein the outer race of the bearing cartridge comprises a recessed annular region.

11. The rotating assembly of claim 10 wherein the anisotropic member comprises a position at least partially in the recessed annular region.

12. The rotating assembly of claim 1 wherein the outer race of the bearing cartridge comprises at least one lubricant jet aperture.

13. The rotating assembly of claim 1 wherein the outer race of the bearing cartridge comprises a unitary outer race.

14. The rotating assembly of claim 1 wherein the inner race of the bearing cartridge comprises a multi-piece inner race.

15. The rotating assembly of claim 1 wherein the rolling elements comprise balls.

16. The rotating assembly of claim 1 wherein the rolling elements comprise a set of turbine side rolling elements and a set of compressor side rolling elements.

17. The rotating assembly of claim 1 further comprising at least one seal ring positioned in the through bore between the outer race of the bearing cartridge and a surface of the center housing wherein the surface defines at least part of the through bore of the center housing.

18. The rotating assembly of claim 1 wherein the anisotropic member comprises inner spacers and outer spacers.

19. The rotating assembly of claim 1 wherein the anisotropic member comprises a first segment having a first axial width and a second segment having a second axial width and wherein the first axial width differs from the second axial width.

20. A rotating assembly for a turbocharger comprising:
a center housing that comprises a through bore having a central axis;
a bearing cartridge positioned in the through bore wherein the bearing cartridge comprises an outer race, an inner race and rolling elements disposed between the inner race and the outer race;
two anisotropic members positioned in the through bore between the outer race of the bearing cartridge and a surface of the center housing wherein the surface defines at least part of the through bore of the center housing; and
a shaft rotatably supported in the center housing by the bearing cartridge wherein the inner race is mounted on the shaft and the shaft is connected at one end to a compressor wheel and at another end to a turbine wheel.

21. The rotating assembly of claim 20 wherein each of the two anisotropic members comprises a ring and a series of lobes arranged about the ring.

22. The rotating assembly of claim 20 wherein the outer race of the bearing cartridge comprises two recessed annular regions and wherein each of the two anisotropic members comprises a position at least partially in one of the two recessed annular regions.

23. A rotating assembly for a turbocharger comprising:
a center housing that comprises a through bore having a central axis;
a bearing cartridge positioned in the through bore wherein the bearing cartridge comprises an outer race, an inner race and rolling elements disposed between the inner race and the outer race and wherein the outer race of the bearing cartridge comprises a recessed annular region;
an anisotropic member positioned in the through bore between the outer race of the bearing cartridge and a surface of the center housing wherein the surface defines at least part of the through bore of the center housing and wherein the anisotropic member comprises a position at least partially in the recessed annular region; and
a shaft rotatably supported in the center housing by the bearing cartridge wherein the inner race is mounted on the shaft and the shaft is connected at one end to a compressor wheel and at another end to a turbine wheel.

Assignees

• Honeywell Int Inc

Inventors

• Meacham Walter Lee
• Gjika Kostandin
• Alam Mohsiul
• Larue Gerald D

Classifications

• F16C17/18

  with floating brasses or brushing, rotatable at a reduced speed {(F16C17/03, F16C17/06 take precedence)} · CPC title

• F16C17/02

  for radial load only · CPC title

• F16C27/06

  by means of parts of rubber or like materials (F16C27/08 takes precedence; with sliding surfaces of rubber or synthetic rubber F16C33/22) · CPC title

• F16C35/10

  with sliding-contact bearings · CPC title

• F16C27/02

  Sliding-contact bearings · CPC title