Turbocharger spring assembly
View Patent ↗A turbocharger bearing assembly can include a spacer that includes an axial through bore, a compressor side surface and a turbine side surface; a compressor side rolling element bearing that includes an outer race surface that faces the compressor side surface of the spacer; a turbine side rolling element bearing that includes an outer race surface that faces the turbine side surface of the spacer; and a spring seated between a first end cap disposed at least in part in the axial through bore of the spacer and a second end cap disposed at least in part in the axial through bore of the spacer where the spring biases an axially facing surface of the first end cap against the outer race surface of the compressor side rolling element bearing and where the spring biases an axially facing surface of the second end cap against the outer race surface of the turbine side rolling element bearing.
1. A turbocharger bearing assembly comprising:
a spacer that comprises an inner surface at an inner diameter that defines an axial through bore, an outer surface at an outer diameter, a compressor side surface and a turbine side surface;
a compressor side rolling element bearing that comprises an outer race surface that faces the compressor side surface of the spacer wherein the outer race comprises an outer diameter that exceeds the inner diameter of the spacer;
a turbine side rolling element bearing that comprises an outer race surface that faces the turbine side surface of the spacer wherein the outer race comprises an outer diameter that exceeds the inner diameter of the spacer; and
a spring seated between a first end cap disposed at least in part in the axial through bore of the spacer and a second end cap disposed at least in part in the axial through bore of the spacer wherein the spring biases an axially facing surface of the first end cap against the outer race surface of the compressor side rolling element bearing, wherein the spring biases an axially facing surface of the second end cap against the outer race surface of the turbine side rolling element bearing, wherein the first and second end caps comprise an end cap outer diameter that is less than the inner diameter of the spacer and wherein the spring comprises an outer diameter that is less than the end cap outer diameter to avoid direct contact between the spring and the spacer.
2. The turbocharger bearing assembly of claim 1 wherein the outer race surface of the compressor side rolling element bearing comprises an outer race opening having an outer race opening diameter and wherein the axially facing surface of the first end cap comprises an end cap opening having an end cap opening diameter that is less than the outer race opening diameter.
3. The turbocharger bearing assembly of claim 2 wherein the first end cap comprises an outwardly axially facing annular beveled surface disposed about the end cap opening.
4. The turbocharger bearing assembly of claim 3 wherein the outwardly axially facing annular beveled surface directs lubricant toward the axially facing surface of the first end cap.
5. The turbocharger bearing assembly of claim 1 wherein the outer race surface of the turbine side rolling element bearing comprises an outer race opening having an outer race opening diameter and wherein the axially facing surface of the second end cap comprises an end cap opening having an end cap opening diameter that is less than the outer race opening diameter.
6. The turbocharger bearing assembly of claim 5 wherein the second end cap comprises an outwardly axially facing annular beveled surface disposed about the end cap opening.
7. The turbocharger bearing assembly of claim 1 wherein at least one of the first end cap and the second end cap comprises at least one lubricant channel.
8. The turbocharger bearing assembly of claim 1 wherein at least one of the first end cap and the second end cap comprises a polymeric material.
9. The turbocharger bearing assembly of claim 1 wherein the first end cap comprises a recess and wherein the spring comprises an end feature seated at least partially in the recess of the first end cap.
10. The turbocharger bearing assembly of claim 1 wherein the second end cap comprises a recess and wherein the spring comprises an end feature seated at least partially in the recess of the second end cap.
11. The turbocharger bearing assembly of claim 1 wherein a sum of an annular dimension of the compressor side surface of the spacer and an annular dimension of the axially facing surface of the first end cap exceed an annular dimension of the outer race surface of the compressor side rolling element bearing.
12. The turbocharger bearing assembly of claim 1 wherein a sum of an annular dimension of the turbine side surface of the spacer and an annular dimension of the axially facing surface of the second end cap exceed an annular dimension of the outer race surface of the turbine side rolling element bearing.
13. The turbocharger bearing assembly of claim 1 wherein at least one of the first end cap and the second end cap comprises a cylindrical wall portion and a flange portion.
14. The turbocharger bearing assembly of claim 13 wherein the cylindrical wall portion comprises an inner diameter that receives an outer diameter of the spring.
15. A turbocharger bearing assembly comprising:
a spacer that comprises an axial through bore, a compressor side surface and a turbine side surface;
a compressor side rolling element bearing that comprises an outer race surface that faces the compressor side surface of the spacer;
a turbine side rolling element bearing that comprises an outer race surface that faces the turbine side surface of the spacer; and
a spring seated between a first end cap disposed at least in part in the axial through bore of the spacer and a second end cap disposed at least in part in the axial through bore of the spacer wherein the spring biases an axially facing surface of the first end cap against the outer race surface of the compressor side rolling element bearing, wherein the spring biases an axially facing surface of the second end cap against the outer race surface of the turbine side rolling element bearing, wherein at least one of the first end cap and the second end cap comprises a cylindrical wall portion and a flange portion, and wherein the spring comprises an inner diameter that receives an outer diameter of the cylindrical wall portion.
16. A turbocharger bearing assembly comprising:
a spacer that comprises an axial through bore, a compressor side surface and a turbine side surface;
a compressor side rolling element bearing that comprises an outer race surface that faces the compressor side surface of the spacer;
a turbine side rolling element bearing that comprises an outer race surface that faces the turbine side surface of the spacer; and
a spring seated between a first end cap disposed at least in part in the axial through bore of the spacer and a second end cap disposed at least in part in the axial through bore of the spacer wherein the spring biases an axially facing surface of the first end cap against the outer race surface of the compressor side rolling element bearing, wherein the spring biases an axially facing surface of the second end cap against the outer race surface of the turbine side rolling element bearing and wherein the first end cap and the compressor side rolling element bearing form tiered lubricant drainage bevels and/or the second end cap and the turbine side rolling element bearing form tiered lubricant drainage bevels.