Tooling for stress relieving a turbine wheel and shaft

Patent metadata

Field	Value
Publication number	US-10422016-B2
Application number	US-201615235025-A
Country	US
Kind code	B2
Filing date	Aug 11, 2016
Priority date	Aug 11, 2016
Publication date	Sep 24, 2019
Grant date	Sep 24, 2019

Abstract

A tool system for stress relieving a turbocharger turbine wheel longitudinally welded to a hardened rotor shaft. The shaft has a journal bearing region and a turbine-end body forming an A datum surface for receiving an axial bearing. The tool system includes an induction coil and an electronic oscillator, and a tool. The tool forms an opening configured to receive the rotor shaft such that the journal bearing region of the shaft extends into the tool housing while the A datum surface adjoins an end of the tool housing. The induction coil is positioned around the turbine-end body. The housing forms an annular cooling chamber surrounding the journal bearing region of the shaft. The housing forms an inlet passage to provide cooling fluid to the annular chamber, and an outlet passage to remove cooling fluid from the annular chamber.

First claim

What is claimed is:

1. A tool system for stress relieving a weld of a turbocharger turbine wheel longitudinally welded to an end region of a hardened rotor shaft, the hardened rotor shaft having a journal bearing region of the hardened rotor shaft for receiving at least one radial journal bearing, and the hardened rotor shaft having a turbine-end body forming an A datum surface for receiving an axial bearing, comprising:
an electromagnetic induction coil;
an electronic oscillator electronically attached to the electromagnetic induction coil, and being adapted to drive the electromagnetic induction coil with alternating current to create an alternating electromagnetic field; and
a tool, including a tool housing;
wherein the tool forms an opening sized to receive the hardened rotor shaft such that the journal bearing region of the hardened rotor shaft extends into the tool housing while the A datum surface adjoins an end of the tool housing;
wherein the electromagnetic induction coil is sized to be positioned around the turbine-end body such that an electromagnetic field from the electromagnetic induction coil surrounds the turbine-end body of the hardened rotor shaft;
wherein, with the hardened rotor shaft fully received in the opening of the tool, the tool housing forms an annular cooling chamber surrounding the journal bearing region of the hardened rotor shaft;
wherein there is an inlet passage to provide cooling fluid to the annular cooling chamber from a cooling fluid inlet port; and
wherein the tool housing forms an outlet passage to remove cooling fluid from the annular cooling chamber to a cooling fluid outlet port.

2. The tool system of claim 1 , wherein the tool housing forms the inlet passage and the outlet passage.

3. The tool system of claim 2 , wherein the inlet passage is in the form of inlet passage supply tubes extending along an outside edge of the tool housing.

4. The tool system of claim 2 , wherein the outlet passage is within the tool housing.

5. The tool system of claim 1 , wherein within the tool housing is a support structure forming a bore positioned to receive an end region of the hardened rotor shaft opposite the turbine-end body when the A datum surface rests upon the end of the tool housing.

6. A tool for stress relieving a turbocharger turbine wheel longitudinally welded to an end region of a hardened rotor shaft, the hardened rotor shaft having a journal bearing region of the hardened rotor shaft for receiving at least one radial journal bearing, and the hardened rotor shaft having a turbine-end body forming an A datum surface for receiving an axial bearing, comprising:
a tool housing;
wherein the tool housing forms an opening sized to receive the hardened rotor shaft such that the journal bearing region of the hardened rotor shaft extends into the tool housing while the A datum surface adjoins an end of the tool housing;
wherein, with the hardened rotor shaft fully received in the opening of the tool housing, the tool housing forms an annular cooling chamber surrounding the journal bearing region of the hardened rotor shaft;
wherein there is an inlet passage to provide cooling fluid to the annular cooling chamber from a cooling fluid inlet port; and
wherein the tool housing forms an outlet passage to remove cooling fluid from the annular cooling chamber to a cooling fluid outlet port.

7. The tool system of claim 6 , wherein the tool housing forms the inlet passage and the outlet passage.

8. The tool system of claim 7 , wherein the inlet passage is in the form of inlet passage supply tubes extending along an outside edge of the tool housing.

9. The tool system of claim 7 , wherein the outlet passage is within the tool housing.

10. The tool system of claim 6 , wherein within the tool housing is a support structure forming a bore positioned to receive an end region of the hardened rotor shaft opposite the turbine-end body when the A datum surface rests upon the end of the tool housing.

11. A method for stress relieving a turbocharger turbine shaft wheel assembly, including a turbine wheel longitudinally welded via a weld to an end region of a rotor shaft, wherein the rotor shaft is hardened and ground, the rotor shaft having a journal bearing region of the rotor shaft for receiving at least one radial journal bearing, and the rotor shaft having a turbine-end body forming an A datum surface for receiving an axial bearing, comprising:
providing a tool including a tool housing having an end that forms an opening sized to receive the rotor shaft such that the journal bearing region of the rotor shaft extends into the tool housing while the A datum surface adjoins an end of the tool housing, wherein, with the rotor shaft fully received in the opening of the tool housing, the tool housing forms an annular cooling chamber surrounding the journal bearing region of the rotor shaft, wherein there is an inlet passage to provide cooling fluid to the annular cooling chamber from a cooling fluid inlet port, and wherein the tool housing forms an outlet passage to remove cooling fluid from the annular cooling chamber to a cooling fluid outlet port;
positioning an induction coil around the end of the tool housing;
inserting the turbocharger turbine shaft wheel assembly into the opening of the tool housing such that the A datum surface adjoins the end of the tool housing, and such that a cooled-shaft-portion of the rotor shaft is within the annular cooling chamber;
streaming a cooling fluid into the inlet port such that the cooling fluid is driven into the annular cooling chamber; and
driving the induction coil with an electronic oscillator through a range of temperatures adequate to stress relieve the weld.

Assignees

• Garrett Transportation I Inc

Inventors

• Prior Angelo
• Barbone Maurizio

Classifications

• C21D9/50

  for welded joints · CPC title

• F01D5/063

  Welded rotors (welding per se B23K) · CPC title

• C21D1/26

  Methods of annealing · CPC title

• C21D1/10

  by electric induction · CPC title

• B23P15/006

  turbine wheels · CPC title