Double-walled turbocharger housing, flange and connection thereof

Patent metadata

Field	Value
Publication number	US-9447698-B2
Application number	US-201313889794-A
Country	US
Kind code	B2
Filing date	May 8, 2013
Priority date	May 9, 2012
Publication date	Sep 20, 2016
Grant date	Sep 20, 2016

Abstract

A double-walled turbocharger housing made of sheet metal includes an inner sheet metal shell which conducts hot exhaust gases and a relatively cold outer sheet metal shell which is spaced apart from the inner sheet metal shell via an air gap. The double-walled turbocharger housing is connected to a bearing flange with a circumferential collar via a common welding seam. The bearing flange is provided with a collar on an outside which faces away from the hot exhaust gas. An outer end of the inner sheet metal shell is provided with a collar with which it embraces the outer sheet metal shell. Both sheet metal shells are connected with the collar of the bearing flange via a common welding seam, wherein an air gap is present between the inner sheet metal shell and the outer sheet metal shell up to the outer end of the inner sheet metal shell.

First claim

What is claimed as new and desired to be protected by Letters Patent is set forth in the appended claims and includes equivalents of the elements recited therein:

1. In combination:
a double walled turbocharger housing, comprising an outer sheet metal shell, and an inner sheet metal shell arranged in the outer sheet metal shell and spaced apart from the outer sheet metal shell via an air gap, said inner sheet metal shell having an end provided with a collar and embracing the outer sheet metal shell with the collar, said air gap extending up to the end of the inner sheet metal shell;
a bearing flange having a collar on an outside facing away from hot exhaust gas; and
a welding seam, joining the inner sheet metal shell and the outer sheet metal shell to the collar of the bearing flange.

2. The combination of claim 1 , wherein the turbocharger housing is constructed for connection to a rotor group with adjustable turbine geometry via the bearing flange.

3. The combination of claim 1 , wherein the air gap on the end of the inner sheet metal shell has a width of at least 1 mm.

4. The combination of claim 1 , wherein the collar of the inner sheet metal shell is clamped between the outer sheet metal shell and the collar of the bearing flange.

5. The combination of claim 4 , wherein the collar of the inner sheet metal shell is clamped between the outer sheet metal shell and the collar of the bearing flange by a respective transition fit.

6. The combination of claim 1 , wherein the inner sheet metal shell is configured to protrude outwardly at the end of the inner sheet metal shell in a radial direction, and wherein the collar of the inner sheet metal shell is oriented away from the bearing flange by essentially 90° in relation to the radial direction.

7. The combination of claim 1 , wherein the outer sheet metal shell has a collar which is oriented in a radial direction, and wherein the collar of the outer sheet metal shell rests against an inside of the collar of the inner sheet metal shell.

8. The combination of claim 7 , wherein the collar of the inner sheet metal shell rests against the collar of the bearing flange in the radial direction.

9. The combination of claim 1 , wherein the collar of the inner sheet metal shell is bent outwardly, and wherein an end of the outer sheet metal shell is arranged between the bent collar and a side of the inner sheet metal shell which faces an inside of the double walled turbocharger housing.

10. The combination of claim 1 , wherein at least a section of the inner sheet metal shell is bent around an end of the outer sheet metal shell in a radial direction and/or an axial direction.

11. A method for connecting a turbocharger housing to a bearing flange, comprising:
providing a turbocharger housing, said turbocharger housing having an outer sheet metal shell, and an inner sheet metal shell arranged in the outer sheet metal shell and spaced apart from the outer sheet metal shell via an air gap, said inner sheet metal shell having an end provided with a collar and embracing the outer sheet metal shell with the collar, said air gap extending up to the end of the inner sheet metal shell;
providing a bearing flange having a collar on an outside facing away from hot exhaust gas; and
joining the inner sheet metal shell and the outer sheet metal shell to the collar of the bearing flange with a welding seam.

12. The method of claim 11 , wherein the turbocharger housing is constructed for connection to a rotor group with adjustable turbine geometry via the bearing flange.

13. The method of claim 11 , wherein the air gap on the outer end of the inner sheet metal shell has a width of at least 1 mm.

14. The method of claim 11 , wherein the collar of the inner sheet metal shell is clamped between the outer sheet metal shell and the collar of the bearing flange.

15. The method of claim 14 , wherein the collar of the inner sheet metal shell is clamped between the outer sheet metal shell and the collar of the bearing flange by a respective transition fit.

16. The method of claim 11 , wherein the inner sheet metal shell is configured to protrude outwardly in a radial direction, and wherein the collar of the inner sheet metal shell is oriented away from the bearing flange.

17. The method of claim 11 , wherein the outer sheet metal shell has a collar which is oriented in a radial direction, and wherein the collar of the outer sheet metal shell rests against an inside of the collar of the inner sheet metal shell.

18. The method of claim 17 , wherein the collar of the inner sheet metal shell rests against the collar of the bearing flange in the radial direction.

19. The method of claim 11 , wherein the collar of the inner sheet metal shell is bent outwardly, and wherein an end of the outer sheet metal shell is arranged between the bent collar and a side of the inner sheet metal shell which faces an inside of the double walled turbocharger housing.

20. The method of claim 11 , wherein at least a section of the inner sheet metal shell is bent around an end of the outer sheet metal shell in a radial direction and/or an axial direction.

Assignees

• Benteler Automobiltechnik Gmbh
• Benteler Automobil Technik Gmbh

Inventors

• Grussmann Elmar
• Lesch Arthur

Classifications

• Y10T29/49323

  Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles · CPC title

• F01D25/243

  Flange connections; Bolting arrangements (F01D25/265 takes precedence) · CPC title

• F01D25/06 Primary

  for preventing blade vibration (means on blade-carrying members or blades F01D5/00) · CPC title

• F02C6/12

  Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure · CPC title

• F01D25/26 Primary

  Double casings; Measures against temperature strain in casings · CPC title