Turbocharger rotating assembly
View Patent ↗A system can include a shaft and turbine wheel assembly that includes a seal portion; a bearing assembly that includes an outer race and rolling elements that rotatably support the shaft and turbine wheel assembly; a sleeve that includes an outer diameter and a through bore that includes a first inner diameter that accommodates an outer diameter of the outer race of the bearing assembly and a second, smaller inner diameter that accommodates an outer diameter of the seal portion of the shaft and turbine wheel assembly; and a center housing that includes a compressor side, a turbine side and a bore that includes a turbine side bore diameter that accommodates the outer diameter of the sleeve.
1. A system comprising:
a shaft and turbine wheel assembly that comprises a seal portion;
a bearing assembly that comprises an outer race and rolling elements that rotatably support the shaft and turbine wheel assembly;
a sleeve that comprises an outer diameter and a through bore that comprises a first inner diameter that accommodates an outer diameter of the outer race of the bearing assembly and a second, smaller inner diameter that accommodates an outer diameter of the seal portion of the shaft and turbine wheel assembly; and
a center housing that comprises a compressor side, a turbine side and a bore that comprises a turbine side bore diameter that accommodates the outer diameter of the sleeve wherein the bore of the center housing comprises a compressor side bore diameter that is less than the turbine side bore diameter.
2. The system of claim 1 wherein the through bore of the sleeve comprises a counter bore disposed between a bearing assembly portion of the through bore that comprises the first inner diameter and another portion of the through bore that comprises the second, smaller inner diameter that accommodates the outer diameter of the seal portion of the shaft and turbine wheel assembly.
3. The system of claim 1 wherein the outer diameter of the outer race of the bearing assembly exceeds the outer diameter of the seal portion of the shaft and turbine wheel assembly.
4. The system of claim 1 wherein the bearing assembly comprises a set of compressor side rolling elements and a set of turbine side rolling elements.
5. The system of claim 4 wherein the sets of rolling elements contact the outer race.
6. The system of claim 4 wherein the bearing assembly comprises an inner race and wherein the rolling elements contact the inner race.
7. The system of claim 6 wherein a shaft portion of the shaft and turbine wheel assembly is press-fit to the inner race.
8. The system of claim 1 wherein the seal portion of the shaft and turbine wheel assembly comprises at least one annular groove.
9. The system of claim 8 comprising a seal component disposed in at least one of the at least one annular groove.
10. The system of claim 1 further comprising a compressor wheel attached to the shaft and turbine wheel assembly.
11. The system of claim 10 further comprising a compressor housing operatively coupled to the compressor side of the center housing.
12. The system of claim 1 further comprising a turbine housing operatively coupled to the turbine side of the center housing.
13. The system of claim 1 wherein the bore of the center housing comprises a counter bore that axially locates the sleeve.