Method of joining by electron beam or laser welding a turbocharger turbine wheel to a shaft; corresponding turbocharger turbine wheel

Patent metadata

Field	Value
Publication number	US-10603740-B2
Application number	US-201615549286-A
Country	US
Kind code	B2
Filing date	Jan 22, 2016
Priority date	Feb 9, 2015
Publication date	Mar 31, 2020
Grant date	Mar 31, 2020

Abstract

A turbocharger wheel (4) and shaft (1) assembly exhibits a frustoconical geometry of welding zone contact surfaces extending to the outer circumference of the shaft (1). This frustoconical geometry not only allows continuous centering of the parts (1, 4) during joining, it also eliminates the problem of stress propagation along a plane. The location of the electron beam is shifted so that only the radially outer segment of the frustoconical contact surface is joined by welding, leaving a radially inner unmelted and unfused zone for maintaining firm contact of the oblique surfaces.

First claim

Now that the invention has been described, we claim:

1. A method for joining a turbocharger turbine wheel to a shaft, the method comprising:
providing on one end of the shaft, the shaft having a shaft axis, the shaft having an outer diameter, a frustoconical contact surface extending to the outer diameter of the shaft,
providing on the turbine wheel a complementary mating contact surface,
contacting the contact surfaces of the turbine wheel and shaft along a contact zone having a depth (x+y) from the shaft outer diameter, the contact zone comprising a radially outer section (x) and a radially inner section (y),
electron beam or laser beam welding the turbine wheel and shaft, wherein the turbine wheel is joined to the shaft by melting and fusing the radially outer section of the contact zone (x), and wherein the radially inner section of the contact zone (y) is not melted.

2. A method for joining a turbocharger turbine wheel to a shaft, the method comprising:
providing on one end of the shaft, the shaft having a shaft axis, the shaft having an outer diameter, a frustoconical contact surface extending to the outer diameter of the shaft,
providing on the turbine wheel a complementary mating contact surface,
contacting the contact surfaces of the turbine wheel and shaft along a contact zone having a depth from the shaft outer diameter of (x+y), the contact zone comprising a radially outer section (x) and a radially inner section (y), and
electron beam or laser beam welding the turbine wheel and shaft, wherein the turbine wheel is joined to the shaft by melting and fusing the radially outer section (x) of the contact zone, and wherein the radially inner section of the contact zone (y) is not melted, wherein the radially outer section (x) of the contact zone extends from the shaft outer diameter to ⅓ to ¾ of the contact zone depth (x+y).

3. The method according to claim 2 , wherein
the radially outer section (x) of the contact zone extends from the shaft outer diameter to ½ to ⅔ of the contact zone depth (x+y).

4. The method according to claim 1 , wherein the contact surfaces are at an angle of from 5° to 45° relative to a plane perpendicular of the shaft axis.

5. The method according to claim 1 , wherein the contact surfaces are at an angle of from 10° to 30° relative to a plane perpendicular to the shaft axis.

6. The method according to claim 1 , wherein the contact surfaces are at an angle of from 15° to 25° relative to a plane perpendicular to the shaft axis.

7. The method according to claim 1 , wherein the turbine wheel has a turbine wheel axis, wherein an angle between the frustoconical contact surface and the shaft axis is less than 85° and an angle of the complementary frustoconical contact surface of the turbine wheel axis is greater than 95°.

8. The method according to claim 1 , wherein the turbine wheel has a turbine wheel axis, wherein an angle between the frustoconical contact surface and the shaft axis is greater than 95° and an angle of the complementary frustoconical contact surface of the turbine wheel axis is less than 85°.

9. The method according to claim 1 , wherein the electron beam or laser beam welding forms a weld having a depth and a width at the welded wheel and shaft surface, wherein the depth of the weld is from 2 to 3 times the width of the weld at the welded wheel and shaft surface.

10. A turbocharger turbine wheel and shaft assembly, produced by the method according to claim 1 .

Assignees

• Borgwarner Inc

Inventors

• Koch Silvio
• Eisinger Stefan

Classifications

• F01D5/025

  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

• B23K2101/003

  Pistons · CPC title

• F05D2230/233

  Electron beam welding · CPC title

• B23K2101/006

  Vehicles · CPC title

• B23K33/008

  for automotive applications · CPC title