Turbocharger shaft and wheel assembly
View Patent ↗A unit for a turbocharger can include a turbine wheel portion that includes a turbine wheel material and a turbine wheel axis; a shaft portion that includes a shaft material and a shaft axis; a first weld that includes a first average axial position over a first azimuthal span and first weld composition formed of a greater proportion of the turbine wheel material than the shaft material; and a second weld that includes a second average axial position over a second azimuthal span and second weld composition formed of a greater proportion of the turbine wheel material than the shaft material, where a sum of the first azimuthal span and the second azimuthal span is approximately 360 degrees, where the first average axial position differs from the second average axial position, and where the first weld composition differs from the second weld composition.
1. A unit for a turbocharger, the unit comprising:
a turbine wheel portion that comprises a turbine wheel material and a turbine wheel axis;
a shaft portion that comprises a shaft material and a shaft axis;
a first weld that comprises a first average axial position over a first azimuthal span and a first weld composition formed of a greater proportion of the turbine wheel material than the shaft material; and
a second weld that comprises a second average axial position over a second azimuthal span and a second weld composition formed of a greater proportion of the turbine wheel material than the shaft material,
wherein a sum of the first azimuthal span and the second azimuthal span is approximately 360 degrees,
wherein the first average axial position differs from the second average axial position, and
wherein the first weld composition differs from the second weld composition.
2. The unit of claim 1 wherein the first weld comprises a first axial width of a shank portion of 0.4 mm or less and wherein the second weld comprises a second axial width of a shank portion of 0.4 mm or less.
3. The unit of claim 1 comprising a run-out of less than 200 microns.
4. The unit of claim 1 wherein the turbine wheel material comprises nickel.
5. The unit of claim 1 wherein the turbine wheel portion comprises a bore.
6. The unit of claim 1 wherein the shaft portion comprises a spigot.
7. The unit of claim 1 wherein the shaft portion comprises a piloting spigot and the turbine wheel portion comprises a piloting bore.
8. The unit of claim 7 wherein a radial clearance exists between the piloting spigot and the piloting bore.
9. The unit of claim 1 wherein the shaft portion is without a piloting spigot and the turbine wheel portion is without a piloting bore.
10. The unit of claim 1 wherein the first azimuthal span is approximately 180 degrees and wherein the second azimuthal span is approximately 180 degrees.
11. A turbocharger comprising:
a compressor housing;
a center housing;
a turbine housing; and
a unit that comprises
a turbine wheel portion that comprises a turbine wheel material and a turbine wheel axis;
a shaft portion that comprises a shaft material and a shaft axis;
a first weld that comprises a first average axial position over a first azimuthal span and a first weld composition formed of a greater proportion of the turbine wheel material than the shaft material; and
a second weld that comprises a second average axial position over a second azimuthal span and a second weld composition formed of a greater proportion of the turbine wheel material than the shaft material,
wherein a sum of the first azimuthal span and the second azimuthal span is approximately 360 degrees,
wherein the first average axial position differs from the second average axial position, and
wherein the first weld composition differs from the second weld composition.
12. The turbocharger of claim 11 wherein the first weld comprises a first axial width of a shank portion of 0.4 mm or less and wherein the second weld comprises a second axial width of a shank portion of 0.4 mm or less.
13. The turbocharger of claim 11 wherein the unit comprises a run-out of less than 200 microns.
14. The turbocharger of claim 11 wherein the turbine wheel material comprises nickel.
15. The turbocharger of claim 11 wherein the turbine wheel portion comprises a bore.
16. The turbocharger of claim 11 wherein the shaft portion comprises a spigot.
17. The turbocharger of claim 11 wherein the shaft portion comprises a piloting spigot and the turbine wheel portion comprises a piloting bore.
18. The turbocharger of claim 17 wherein a radial clearance exists between the piloting spigot and the piloting bore.
19. The turbocharger of claim 11 wherein the shaft portion is without a piloting spigot and the turbine wheel portion is without a piloting bore.
20. The turbocharger of claim 11 wherein the first azimuthal span is approximately 180 degrees and wherein the second azimuthal span is approximately 180 degrees.