Granted Patent B2

US 8,858,173 · App. 13/100,968 · Granted Oct 14, 2014

Abstract

Claims (29)

1. A spacer configured to space two turbocharger bearings, the spacer comprising:

an annular body that defines a central through bore and that comprises an axial end face, an opposing axial end face, a lubricant passage configured to direct lubricant to the axial end face, and a lubricant passage configured to direct lubricant to the opposing axial end face wherein at least one of the axial end faces comprises a lubricant well.

2. The spacer of claim 1 wherein the annular body comprises at least one lubricant inlet located on an outer surface and disposed between the axial end faces.

3. The spacer of claim 1 wherein each of the lubricant passages comprises a portion of a radially displaced through bore.

4. The spacer of claim 3 wherein the radially displaced through bore comprises an axis disposed substantially parallel to an axis of the central through bore.

5. The spacer of claim 3 wherein the annular body comprises a lubricant inlet in fluid communication with the radially displaced through bore.

6. The spacer of claim 1 wherein the lubricant well comprises an annular channel configured to receive lubricant from a respective one of the lubricant passages.

7. The spacer of claim 1 wherein the lubricant well comprises an isolated well.

8. The spacer of claim 1 wherein the annular body comprises an opening located on an outer surface, the opening configured to drain lubricant.

9. The spacer of claim 1 further comprising a spring.

10. The spacer of claim 9 wherein the spring comprises an uncompressed axial length that exceeds an axial length of the spacer.

11. The spacer of claim 9 wherein the spring comprises a wave spring.

12. A turbocharger bearing assembly comprising:

a compressor side bearing;

a turbine side bearing; and

a spacer configured to axially space the compressor side bearing and the turbine side bearing wherein the spacer comprises a spring disposed in a central through bore and lubricant passages to direct lubricant to spacer-bearing interfaces wherein each of the spacer-bearing interfaces comprises a respective lubricant well.

13. The turbocharger bearing assembly of claim 12 wherein the spring comprises an uncompressed axial length that exceeds an axial length of the spacer.

14. The turbocharger bearing assembly of claim 12 wherein the lubricant passages direct lubricant to the lubricant wells.

15. A method comprising:

providing turbocharger bearings and a spacer with a spring;

applying a load to the bearings via the spring;

rotating a turbocharger shaft supported by the bearings while providing lubricant;

forming a lubricant film between the spacer and one of the bearings; and

damping axial vibration via the lubricant film.

16. The method of claim 15 wherein the lubricant film comprises a film disposed between a compressor side bearing and the spacer.

17. The method of claim 15 wherein the lubricant film comprises a film disposed between a turbine side bearing and the spacer.

18. The method of claim 15 further comprising forming an additional lubricant film between the spacer and another one of the bearings.

19. A spacer configured to space two turbocharger bearings, the spacer comprising:

an annular body that defines a central through bore and that comprises an axial end face, an opposing axial end face, a lubricant passage configured to direct lubricant to the axial end face, and a lubricant passage configured to direct lubricant to the opposing axial end face wherein each of the lubricant passages comprises a portion of a radially displaced through bore and wherein the radially displaced through bore comprises an axis disposed substantially parallel to an axis of the central through bore.

Assignments (6)