Granted Patent B2

US 10,495,097 · App. 15/375,650 · Granted Dec 3, 2019

Abstract

Claims (19)

1. A compressor assembly comprising:

a shaft sleeve that comprises a bore that extends between a first end and a second end and that comprises an outer shoulder;

a shaft received by the bore of the shaft sleeve wherein the shaft comprises a compressor end;

a compressor wheel disposed on the shaft; and

a thrust collar disposed on the shaft and seated between the outer shoulder of the shaft sleeve and the compressor wheel wherein the thrust collar comprises a stem portion and a cap portion that comprises a sacrificial portion, wherein the cap portion comprises a sensor surface, wherein the sacrificial portion is on a compressor wheel side of the thrust collar and the sensor surface is on a shaft sleeve side of the thrust collar, wherein the sacrificial portion of the thrust collar comprises at least one balance cut, and wherein the cap portion of the thrust collar comprises a sensor notch that forms a notch in the sensor surface and extends through the sacrificial portion.

2. The compressor assembly of claim 1 wherein the thrust collar comprises an annular groove about an exterior of the stem portion.

3. The compressor assembly of claim 1 wherein the sacrificial portion comprises a triangular cross-sectional shape.

4. The compressor assembly of claim 1 wherein the sacrificial portion extends to an outermost perimeter of the thrust collar.

5. The compressor assembly of claim 1 wherein the sacrificial portion extends axially to an apex.

6. The compressor assembly of claim 1 comprising a plane disposed at an axial position wherein the sacrificial portion is disposed axially to one side of the plane, wherein the sacrificial portion is disposed axially to the side of the plane that is toward the compressor end of the shaft.

7. The compressor assembly of claim 1 wherein the balance cut is inset radially from an outermost perimeter of the cap portion of the thrust collar.

8. The compressor assembly of claim 1 comprising a speed sensor wherein the speed sensor is on the shaft sleeve side of the thrust collar.

9. The compressor assembly of claim 1 wherein the shaft sleeve is operatively coupled to a rotor of an electric motor.

10. A method comprising:

providing a rotating group of a turbocharger that comprises a compressor assembly that comprises a shaft sleeve that comprises a bore that extends between a first end and a second end and that comprises an outer shoulder, a shaft received by the bore of the shaft sleeve wherein the shaft comprises a compressor end, a compressor wheel disposed on the shaft, and a thrust collar disposed on the shaft and seated between the outer shoulder of the shaft sleeve and the compressor wheel wherein the thrust collar comprises a stem portion and a cap portion that comprises a sacrificial portion, wherein the cap portion comprises a sensor surface, wherein the sacrificial portion is on a compressor wheel side of the thrust collar and the sensor surface is on a shaft sleeve side of the thrust collar, and wherein the cap portion of the thrust collar comprises a sensor notch that forms a notch in the sensor surface and extends through the sacrificial portion;

measuring unbalance of the rotating group of the turbocharger; and

based at least in part on the unbalance, removing an amount of material from the sacrificial portion of the thrust collar to form at least one balance cut.

11. The method of claim 10 comprising rotating the rotating group via an electric motor operatively coupled to the turbocharger.

12. The method of claim 11 wherein the turbocharger comprises the electric motor wherein the electric motor is disposed between the compressor wheel and a turbine wheel of the turbocharger.

Assignments (8)