Turbocharger bearing assembly
View Patent ↗An assembly can include a turbocharger center housing that includes a through bore that extends between a compressor end and a turbine end of the turbocharger center housing where the through bore includes a sleeve mating surface; and a sleeve positioned at least in part in the through bore of the turbocharger center housing where the sleeve includes an outer mating surface, an inner compressor side bearing lubricant film formation surface disposed at a first radius, an inner turbine side bearing lubricant film formation surface disposed at a second radius, and a surface between the inner compressor side bearing lubricant film formation surface and the inner turbine side bearing lubricant film formation surface that includes a third radius that is less than the first radius and less than the second radius and where outer mating surface of the sleeve contacts the sleeve mating surface of the turbocharger center.
1. An assembly comprising:
a turbocharger center housing that comprises a through bore that extends between a compressor end and a turbine end of the turbocharger center housing and crescent shaped grooves formed into the through bore of the turbocharger center housing wherein the turbocharger center housing comprises at least one lubricant passage that is in fluid communication with the crescent shaped grooves and wherein the through bore comprises a sleeve mating surface; and
a sleeve positioned at least in part in the through bore of the turbocharger center housing wherein the sleeve comprises an outer mating surface, an inner compressor side bearing lubricant film formation surface disposed at a first radius, an inner turbine side bearing lubricant film formation surface disposed at a second radius, and a surface between the inner compressor side bearing lubricant film formation surface and the inner turbine side bearing lubricant film formation surface that comprises a third radius that is less than the first radius and less than the second radius and wherein the outer mating surface of the sleeve contacts the sleeve mating surface of the turbocharger center housing.
2. The assembly of claim 1 wherein the sleeve comprises a flange and an axial extension that extends from the flange.
3. The assembly of claim 1 wherein the sleeve comprises radial grooves.
4. The assembly of claim 3 wherein one of the radial grooves is disposed adjacent to the inner compressor side lubricant film formation surface and wherein another one of the radial grooves is disposed adjacent to the inner turbine side lubricant film formation surface.
5. The assembly of claim 1 further comprising a compressor side bearing that comprises an outer race that comprises an outer surface that forms a radial clearance with respect to the inner compressor side lubricant film formation surface; and a turbine side bearing that comprises an outer race that comprises an outer surface that forms a radial clearance with respect to the inner turbine side lubricant film formation surface.
6. The assembly of claim 5 further comprising a compressor side lubricant passage that extends between the outer mating surface of the sleeve and the inner compressor bearing lubricant film formation surface of the sleeve; and a turbine side lubricant passage that extends between the outer mating surface of the sleeve and the inner turbine bearing lubricant film formation surface of the sleeve.
7. The assembly of claim 1 further comprising a compressor side rolling element bearing received by the sleeve, a turbine side rolling element bearing received by the sleeve and a shaft and turbine wheel assembly (SWA) wherein a first portion of the shaft of the SWA is interference fit to the compressor side rolling element bearing and wherein a second portion of the shaft of the SWA is interference fit to the turbine side rolling element bearing.
8. The assembly of claim 7 further comprising a spring that applies a biasing force to an outer race of the compressor side rolling element bearing and to an outer race of the turbine side rolling element bearing.
9. The assembly of claim 1 wherein the turbocharger center housing comprises lubricant passages in fluid communication with a lubricant inlet port of the turbocharger center housing and wherein the through bore comprises a lubricant outlet in a wall that defines the through bore.
10. The assembly of claim 1 wherein the turbocharger center housing comprises a compressor side crescent shaped groove and a turbine side crescent shaped groove and wherein the sleeve comprises a compressor side groove that is at least in part axially aligned with the compressor side crescent shaped groove and a turbine side groove that is at least in part axially aligned with the turbine side crescent shaped groove.
11. The assembly of claim 10 wherein the compressor side groove of the sleeve comprises an exterior groove and wherein the turbine side groove of the sleeve comprises an exterior groove.
12. The assembly of claim 1 wherein the turbocharger center housing comprises a lubricant gallery that comprises an axial dimension and that comprises an azimuthal span and wherein the turbocharger center housing comprises at least one lubricant passage that is in fluid communication with the lubricant gallery.
13. The assembly of claim 1 wherein the sleeve comprises a compressor side lubricant hole and a turbine side lubricant hole wherein an axial span between the compressor side lubricant hole and the turbine side lubricant hole is less than an axial length of a lubricant gallery recess of the turbocharger center housing that is recessed radially outwardly from the sleeve mating surface.
14. The assembly of claim 1 further comprising a counterbore disposed at an axial location between the compressor end and the turbine end of the through bore of the turbocharger center housing.
15. The assembly of claim 14 wherein an axial clearance exists between a turbine side axial face at an end of the sleeve and a compressor side axial face of the counterbore.
16. The assembly of claim 14 wherein the counterbore comprises an innermost radius that is less than a radius of the turbine side bearing lubricant film formation surface of the sleeve.
17. The assembly of claim 16 further comprising a turbine side rolling element bearing that comprises an outer race that comprises an outer surface disposed at a radius that exceeds the innermost radius of the counterbore.
18. The assembly of claim 14 wherein the counterbore comprises a segmented counterbore wherein each segment spans a respective azimuthal angle.
19. An assembly comprising:
a turbocharger center housing that comprises a through bore that extends between a compressor end and a turbine end of the turbocharger center housing wherein the through bore comprises a sleeve mating surface; and
a sleeve positioned at least in part in the through bore of the turbocharger center housing wherein the sleeve comprises an outer mating surface, an inner compressor side bearing lubricant film formation surface disposed at a first radius, an inner turbine side bearing lubricant film formation surface disposed at a second radius, and a surface between the inner compressor side bearing lubricant film formation surface and the inner turbine side bearing lubricant film formation surface that comprises a third radius that is less than the first radius and less than the second radius and wherein the outer mating surface of the sleeve contacts the sleeve mating surface of the turbocharger center housing,
wherein the turbocharger center housing comprises a compressor side crescent shaped groove and a turbine side crescent shaped groove and wherein the sleeve comprises a compressor side groove that is at least in part axially aligned with the compressor side crescent shaped groove and a turbine side groove that is at least in part axially aligned with the turbine side crescent shaped groove.
20. The assembly of claim 19 wherein the compressor side groove of the sleeve comprises an exterior groove and wherein the turbine side groove of the sleeve comprises an exterior groove.
21. An assembly comprising:
a turbocharger center housing that comprises a through bore that extends between a compressor end and a turbine end of the turbocharger center housing wherein the through bore comprises a sleeve mating surface; and
a sleeve positioned at least in part in the through bore of the turbocharger center housing wherein the sleeve comprises an outer mating surface, an inner compressor side bearing lubricant film formation surface disposed at a first radius, an inner turbine side bearing lubricant film formation surface disposed at a second radius, and a surface between the inner compressor side bearing lubricant film formation surface and the inner turbine side bearing lubricant film formation surface that comprises a third radius that is less than the first radius and less than the second radius, wherein the outer mating surface of the sleeve contacts the sleeve mating surface of the turbocharger center housing, wherein the sleeve comprises a compressor side lubricant hole and a turbine side lubricant hole, and wherein an axial span between the compressor side lubricant hole and the turbine side lubricant hole is less than an axial length of a lubricant gallery recess of the turbocharger center housing that is recessed radially outwardly from the sleeve mating surface.
22. An assembly comprising:
a turbocharger center housing that comprises a through bore that extends between a compressor end and a turbine end of the turbocharger center housing and a counterbore disposed at an axial location between the compressor end and the turbine end of the through bore of the turbocharger center housing wherein the through bore comprises a sleeve mating surface and wherein the counterbore comprises a segmented counterbore wherein each segment spans a respective azimuthal angle; and
a sleeve positioned at least in part in the through bore of the turbocharger center housing wherein the sleeve comprises an outer mating surface, an inner compressor side bearing lubricant film formation surface disposed at a first radius, an inner turbine side bearing lubricant film formation surface disposed at a second radius, and a surface between the inner compressor side bearing lubricant film formation surface and the inner turbine side bearing lubricant film formation surface that comprises a third radius that is less than the first radius and less than the second radius and wherein the outer mating surface of the sleeve contacts the sleeve mating surface of the turbocharger center housing.
23. The assembly of claim 22 wherein an axial clearance exists between a turbine side axial face at an end of the sleeve and a compressor side axial face of the counterbore.
24. The assembly of claim 22 wherein the counterbore comprises an innermost radius that is less than a radius of the turbine side bearing lubricant film formation surface of the sleeve.
25. The assembly of claim 24 further comprising a turbine side rolling element bearing that comprises an outer race that comprises an outer surface disposed at a radius that exceeds the innermost radius of the counterbore.