Turbocharger assembly

Patent metadata

Field	Value
Publication number	US-10677253-B2
Application number	US-201615375597-A
Country	US
Kind code	B2
Filing date	Dec 12, 2016
Priority date	Dec 12, 2016
Publication date	Jun 9, 2020
Grant date	Jun 9, 2020

Abstract

A turbocharger assembly can include a shaft sleeve that includes a bore that extends between a first end and a second end; a shaft received by the bore of the shaft sleeve where the shaft includes a compressor end and a turbine wheel that defines a turbine end; and a balance collar disposed on the shaft and seated axially between the end of the shaft sleeve and the turbine wheel wherein the balance collar includes a stem portion and a flared portion that includes a sacrificial portion.

First claim

What is claimed is:

1. A turbocharger assembly, comprising:
a shaft sleeve that comprises a bore that extends between a first end and a second end;
a shaft received by the bore of the shaft sleeve, wherein the shaft comprises a compressor end and a turbine wheel that defines a turbine end; and
a balance collar disposed on the shaft and seated axially between the second end of the shaft sleeve and the turbine wheel, wherein the balance collar comprises a stem portion and a flared portion that comprises a sacrificial portion, wherein the balance collar comprises a stepped bore that comprises an annular axial face, wherein an axial face surface of a hub portion of the shaft seats against the annular axial face, wherein the stem portion of the balance collar is loaded by an axial load between the second end of the shaft sleeve and the axial face surface of the hub portion of the shaft, wherein the sacrificial portion is disposed over an axial length of the balance collar that is not axially loaded and that does not overlap axially with the stem portion of the balance collar, and wherein the sacrificial portion of the balance collar comprises at least one balance cut.

2. The turbocharger assembly of claim 1 , wherein the sacrificial portion is disposed at a radial distance greater than an outermost radius of the stem portion of the balance collar.

3. The turbocharger assembly of claim 1 , wherein the at least one balance cut comprises a balance cut defined at least in part by a chord of a circle, wherein the circle has a radius defined by an outermost perimeter of the balance collar.

4. The turbocharger assembly of claim 1 , wherein the sacrificial portion comprises a sloped annular end surface.

5. The turbocharger assembly of claim 1 , wherein the shaft sleeve is operatively coupled to a rotor of an electric motor.

6. The turbocharger assembly of claim 1 , comprising a bearing assembly seated with respect to the shaft sleeve.

7. The turbocharger assembly of claim 6 , wherein the bearing assembly comprises an inner race, an outer race and rolling elements disposed between the inner race and the outer race, wherein a lubricant gap exists between the inner race and the outer race.

8. The turbocharger assembly of claim 7 , comprising a seal ring disposed radially about the shaft and axially between a lubricated bearing space and an exhaust turbine space, wherein an outer lock nut axially locates the outer race and wherein a surface of the outer lock nut and a surface of the stem portion of the balance collar define a radial gap for flow of lubricant, from the lubricant gap, axially outwardly to the flared portion of the balance collar to contact the balance collar and to be flung substantially radially outwardly away from the balance collar as it rotates such that the lubricant more readily flows toward a lubricant exit with reduced risk of the lubricant migrating toward the seal ring.

9. The turbocharger assembly of claim 8 , wherein at least a portion of the flared portion of the balance collar axially overlaps with the radial gap.

10. The turbocharger assembly of claim 7 , comprising a seal ring disposed radially about the shaft and axially between a lubricated bearing space and an exhaust turbine space, wherein an outer lock nut axially locates the outer race, an inner lock nut axially locates the inner race and wherein a surface of the outer lock nut and a surface of the inner lock nut define a radial gap for flow of lubricant, from the lubricant gap, axially outwardly to the flared portion of the balance collar to contact the balance collar and to be flung substantially radially outwardly away from the balance collar as it rotates such that the lubricant more readily flows toward a lubricant exit with reduced risk of the lubricant migrating toward the seal ring.

11. The turbocharger assembly of claim 10 , wherein at least a portion of the flared portion of the balance collar axially overlaps with the radial gap.

12. The turbocharger assembly of claim 7 , comprising a seal ring disposed radially about the shaft and axially between a lubricated bearing space and an exhaust turbine space, wherein the lubricant gap directs lubricant axially outwardly to the flared portion of the balance collar to contact the balance collar and to be flung substantially radially outwardly away from the balance collar as it rotates such that the lubricant more readily flows toward a lubricant exit with reduced risk of the lubricant migrating toward the seal ring.

13. The turbocharger assembly of claim 12 , wherein at least a portion of the flared portion of the balance collar axially overlaps with the lubricant gap.

14. The turbocharger assembly of claim 13 , wherein the sacrificial portion of the balance collar comprises a balance cut that does not axially overlap with the lubricant gap.

Assignees

• Garrett Transportation I Inc

Inventors

• Merritt Shawn W
• Tabacchi Luca

Classifications

• F02B37/10

  at least one pump being alternatively {or simultaneously} driven by exhaust and other drive, {e.g. by pressurised fluid from a reservoir or an engine-driven pump} · CPC title

• F04D29/053

  Shafts · CPC title

• F04D29/051 Primary

  Axial thrust balancing · CPC title

• F01D5/027 Primary

  Arrangements for balancing (for balancing rotating bodies in general F16F15/32; for compensating imbalance G01M1/36) · CPC title

• F04D29/662

  Balancing of rotors (compensating imbalance G01M1/36) · CPC title