Welded shaft and turbine wheel assembly

Patent metadata

Field	Value
Publication number	US-10047607-B2
Application number	US-201314097330-A
Country	US
Kind code	B2
Filing date	Dec 5, 2013
Priority date	Dec 5, 2013
Publication date	Aug 14, 2018
Grant date	Aug 14, 2018

Abstract

A component for a turbocharger can include a shaft made of a first material where the shaft includes a turbine wheel end and a shaft axis; a turbine wheel made of a second material where the turbine wheel includes a shaft end and a turbine wheel axis; a weld joint formed by solidification of at least a portion of a weld pool that includes the first material and the second material, where the weld joint joins the turbine wheel end of the shaft and the shaft end of the turbine wheel and where the weld joint includes an inner radial border and an outer radial border; a reservoir disposed radially inwardly of the inner radial border of the weld joint; and a solidified portion of the weld pool disposed in the reservoir. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.

First claim

What is claimed is:

1. A component for a turbocharger comprising:
a shaft made of a first material wherein the shaft comprises a turbine wheel end and a shaft axis, wherein the turbine wheel end comprises an outer edge, an annular reservoir with a cross-sectional profile and a first axial depth, a central cavity with a second axial depth that exceeds the first axial depth, a first annular face that extends between the outer edge and the annular reservoir and a second annular face that extends from the central cavity to the annular reservoir wherein an axial position of the first annular face differs from an axial position of the second annular face;
a turbine wheel made of a second material wherein the turbine wheel comprises a shaft end and a turbine wheel axis, wherein the shaft end comprises an outer edge, a central cavity and an annular face that extends from the central cavity to the outer edge, wherein in an unwelded and contacting state of the annular face of the shaft end of the turbine wheel and the first annular face of the turbine wheel end of the shaft, an axial gap exists that extends diametrically across an inner perimeter of the first annular face of the turbine wheel end of the shaft wherein the axial gap is defined in part by the annular face of the shaft end of the turbine wheel and the second annular face of the turbine wheel end of the shaft;
a weld joint formed by solidification of at least a portion of a weld pool, wherein the weld joint comprises the first material of at least a portion of the first annular face of the shaft and the second material of at least a portion of the annular face of the turbine wheel, wherein the weld joint joins the turbine wheel end of the shaft and the shaft end of the turbine wheel, wherein a portion of the axial gap exists between the second annular face of the shaft and the annular face of the turbine wheel to define, in part, a reservoir overflow volume, and wherein the weld joint determines the axial and radial welded positions of the shaft and the turbine wheel without positional interference between surfaces that are located radially inwardly from the annular reservoir; and
a solidified portion of the weld pool disposed in the annular reservoir.

2. The component of claim 1 wherein the shaft axis and the turbine wheel axis align.

3. The component of claim 1 wherein the first material and the second material differ.

4. The component of claim 1 wherein the annular reservoir comprises a maximum axial depth in range from approximately 50 microns to approximately 500 microns.

5. The component of claim 1 wherein the annular reservoir comprises a maximum axial depth less than approximately 1 mm.

6. The component of claim 1 wherein the annular reservoir comprises a closed side and an open side wherein the open side opens to the axial gap that opens to the central cavity of the shaft.

7. The component of claim 6 wherein the central cavity of the shaft comprises a volume that exceeds a volume of the annular reservoir.

8. The component of claim 1 wherein the weld pool comprises a filler material.

9. The component of claim 8 wherein the filler material comprises nickel.

10. An assembly for a turbocharger comprising:
a shaft that comprises a shaft axis and a turbine wheel end, wherein the turbine wheel end comprises an outer edge, an annular reservoir with a cross-sectional profile and a first axial depth, a central cavity with a second axial depth that exceeds the first axial depth, a first annular face that extends between the outer edge and the annular reservoir and a second annular face that extends from the central cavity to the annular reservoir wherein an axial position of the first annular face differs from an axial position of the second annular face; and
a turbine wheel that comprises a turbine wheel axis and a shaft end, wherein the shaft end comprises an outer edge, a central cavity and an annular face that extends from the central cavity to the outer edge,
wherein in an unwelded and contacting state of the annular face of the shaft end of the turbine wheel and the first annular face of the turbine wheel end of the shaft, an axial gap exists that extends diametrically across an inner perimeter of the first annular face of the turbine wheel end of the shaft wherein the axial gap is defined in part by the annular face of the shaft end of the turbine wheel and the second annular face of the turbine wheel end of the shaft,
wherein, upon welding, a weld joint forms at the outer edges of the shaft and the turbine wheel, extends radially inwardly and determines the axial and radial welded positions of the shaft and the turbine wheel without positional interference between surfaces that are located radially inwardly from the annular reservoir, and wherein a portion of the axial gap formed between the second annular face of the shaft and the annular face of the turbine wheel defines, in part, a reservoir overflow volume.

11. The assembly of claim 10 wherein the cross-sectional profile of the annular reservoir comprises one or more of a curved cross-sectional profile and a linear cross-sectional profile.

12. The component of claim 1 wherein the cross-sectional profile of the annular reservoir comprises a curved cross-sectional profile.

13. The component of claim 1 wherein the cross-sectional profile of the annular reservoir comprises a linear cross-sectional profile.

14. The component of claim 1 wherein the cross-sectional profile of the annular reservoir comprises one or more of a curved cross-sectional profile and a linear cross-sectional profile.

Assignees

• Honeywell Int Inc

Inventors

• Thirion Michel Maurice
• Zollinger Brent
• Vazeille Nicolas
• Wilson Marc
• Horlaville Didier
• Armand Dominique
• Minculescu Andrei

Classifications

• F05D2230/234

  Laser welding · CPC title

• F01D5/063

  Welded rotors (welding per se B23K) · CPC title

• F01D5/025 Primary

  Fixing blade carrying members on shafts (attachment of a member on a shaft in general F16D1/06; for non-positive displacement pumps F04D29/00) · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F16D1/027

  non-disconnectable, e.g. involving gluing, welding or the like · CPC title