Sheet metal turbine housing with cellular structure reinforcement

Patent metadata

Field	Value
Publication number	US-9945258-B2
Application number	US-201414511987-A
Country	US
Kind code	B2
Filing date	Oct 10, 2014
Priority date	Oct 10, 2014
Publication date	Apr 17, 2018
Grant date	Apr 17, 2018

Abstract

Systems are provided for a reinforcement element coupled to a sheet metal turbine housing that imparts desirable thermal-protective and structurally strengthening characteristics to the housing layers. In one example, a system may include a turbine comprising a housing surrounding a turbine rotor, the housing having an outer layer surrounding an inner layer at a distance to form an intermediate space between the inner and outer layers. Moreover, disposed in the intermediate space is a reinforcement element coupled to the inner and outer layers, providing strength and consistent rigidity without a significant increase in weight to the housing.

First claim

The invention claimed is:

1. A turbine comprising:
a housing surrounding a rotor of a turbocharger, the housing having:
an inner sheet metal layer being innermost of the housing and defining a boundary of a scroll portion;
an outer sheet metal layer being outermost of the housing, the outer sheet metal layer surrounding the inner sheet metal layer at a distance to form an intermediate space between the inner and outer sheet metal layers; and
a sheet metal reinforcement element disposed within the intermediate space and welded or bolted to the inner sheet metal layer and the outer sheet metal layer such that a threshold length between the inner sheet metal layer and the rotor is maintained.

2. The turbine of claim 1 , wherein the sheet metal reinforcement element is one of a plurality of sheet metal reinforcement elements and comprises a body of corrugated or bellowed layers of a sheet metal forming a pattern.

3. The turbine of claim 2 , wherein the pattern is a honeycomb-like shape such that a cross-section of the sheet metal reinforcement element is a plurality of hexagons.

4. The turbine of claim 2 , wherein the pattern is a bellowing wave, such that a cross-section of the sheet metal reinforcement element is a sine wave.

5. The turbine of claim 2 , wherein the pattern is a plurality of squares or triangles aligned in series and wherein a thickness of the sheet metal reinforcement element is between 1 and 5 mm.

6. The turbine of claim 1 , wherein the sheet metal reinforcement element is in face-sharing contact with a first surface of the outer sheet metal layer facing toward the rotor and a second surface of the inner sheet metal layer facing away from the rotor.

7. The turbine of claim 1 , wherein the scroll portion is provided in a space about the rotor and configured to receive exhaust gases from an exhaust manifold and drive the rotor.

8. The turbine of claim 7 , wherein the sheet metal reinforcement element is coupled to the outer and inner sheet metal layers at a region proximal to the scroll portion.

9. The turbine of claim 1 , wherein the sheet metal reinforcement element is one of a plurality of sheet metal reinforcement elements, and wherein the plurality of sheet metal reinforcement elements is spaced at symmetrical intervals intermittently along the housing.

10. The turbine of claim 1 , wherein the sheet metal reinforcement element is disposed in the intermediate space along an entirety of the housing.

11. A turbine of a turbocharger, comprising:
a housing having an inner sheet metal layer being innermost of the housing and defining a scroll portion, an outer sheet metal layer being outermost of the housing, and an intermediate space formed therebetween; and
a reinforcement element disposed in the intermediate space and coupled to each of the inner sheet metal layer and the outer sheet metal layer, the reinforcement element comprising a body of corrugated or bellowed layers consisting of a sheet metal, the sheet metal forming a pattern having a cross-section of one of a hexagon, sine wave, square, or triangle.

12. The turbine of the turbocharger of claim 11 , wherein the reinforcement element is in face sharing contact with a first surface of the outer sheet metal layer facing a turbine rotor and a second surface of the inner sheet metal layer facing away from the turbine rotor.

13. The turbine of the turbocharger of claim 11 further comprising additional reinforcement elements that are spaced at even intervals along an entirety of the housing.

14. The turbine of the turbocharger of claim 11 , further comprising a plurality of reinforcement elements.

15. The turbine of the turbocharger of claim 11 , wherein the scroll portion is provided in a space about a turbine rotor and configured to receive exhaust gases from an exhaust manifold and drive the turbine rotor.

16. The turbine of the turbocharger of claim 11 , wherein the reinforcement element and the inner sheet metal layer are joined via welding, and a threshold distance between the inner sheet metal layer and a rotor is maintained.

17. A turbocharger including a turbine, comprising:
a housing having an outer sheet metal layer being outermost of the housing, an inner sheet metal layer being innermost of the housing and defining a scroll portion, and an intermediate space formed therebetween; and
a sheet metal reinforcement element disposed in the intermediate space, the sheet metal reinforcement element having a cross-section of a hexagon and an outer face of the sheet metal reinforcement element coupled via spot welding to the outer sheet metal layer and, the sheet metal reinforcement element maintaining a distance between the inner and outer sheet metal layers.

18. The turbocharger including the turbine of claim 17 , wherein the sheet metal reinforcement element is one of a plurality of sheet metal reinforcement elements, and wherein the plurality of sheet metal reinforcement elements is spaced at symmetrical intervals intermittently along the housing.

19. The turbocharger including the turbine of claim 17 , wherein the inner sheet metal layer and the outer sheet metal layer are connected at one or more locations along the housing via welding or bolting.

20. The turbocharger including the turbine of claim 17 , wherein the scroll portion is provided in a space about a turbine rotor and configured to receive exhaust gases from an exhaust manifold and drive the turbine rotor.

Assignees

• Ford Global Tech Llc

Inventors

• Sun Harold Huimin
• Hu Leon
• Hanna David R

Classifications

• F01D25/26 Primary

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

• F05D2250/283

  honeycomb · CPC title

• F05D2260/231

  Preventing heat transfer · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F05D2250/61

  corrugated · CPC title