IP Library Granted Patent US 10,472,988
Granted Patent B2
US 10,472,988 · App. 15/419,320 · Granted Nov 12, 2019

Sheet metal turbine housing and related turbocharger systems

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Quick Facts
Patent No.
US 10,472,988
App. No.
15/419,320
Granted
Nov 12, 2019
Kind
B2
Abstract

Turbine housing assemblies and related turbocharger systems are provided. One exemplary turbine housing assembly includes a bypass valve assembly structure including a guide portion, an inner sheet metal shell including an inner inlet portion and a volute portion providing an outer contour of a volute, wherein an end of the inner inlet portion is surrounded by the guide portion and spaced apart from the bypass valve assembly structure, and an outer sheet metal shell radially surrounding at least a portion of the volute portion and including an outer inlet portion surrounding the inner inlet portion and contacting the guide portion of the bypass valve assembly structure.

Claims (46)

1. A turbine housing assembly comprising:

a bypass valve assembly structure including a guide portion;

an inner sheet metal shell including an inner inlet portion and a volute portion providing an outer contour of a volute, wherein an end of the inner inlet portion is surrounded by the guide portion and spaced apart from the bypass valve assembly structure; and

an outer sheet metal shell radially surrounding at least a portion of the volute portion and including an outer inlet portion surrounding the inner inlet portion and contacting the guide portion of the bypass valve assembly structure, wherein:

the end of the inner inlet portion extends into the bypass valve assembly structure by a first distance;

the end of the outer inlet portion extends into the bypass valve assembly structure by a second distance; and

the first distance is greater than the second distance.

2. The turbine housing assembly of claim 1 , wherein the bypass valve assembly structure includes a flange that is coupled to the outer inlet portion.

3. The turbine housing assembly of claim 1 , wherein the bypass valve assembly structure comprises a cast metal.

4. The turbine housing assembly of claim 1 , wherein the outer inlet portion is welded to the bypass valve assembly structure about a perimeter of the outer inlet portion.

5. The turbine housing assembly of claim 1 , wherein the bypass valve assembly structure includes an opening that extends along a first axis that is oblique to a second axis of an inlet defined by the inner inlet portion.

6. The turbine housing assembly of claim 1 , wherein:

the inner sheet metal shell comprises a first plurality of sheet metal structures joined to one another in a radial plane; and

the outer sheet metal shell comprises a second plurality of sheet metal structures joined to one another in an axial plane transverse to the radial plane.

7. The turbine housing assembly of claim 6 , wherein:

the first plurality of sheet metal structures are coupled about the volute portion; and

portions of the second plurality of sheet metal structures surrounding the volute portion are coupled to one another in an axial direction.

8. The turbine housing assembly of claim 1 , wherein a thickness of the outer sheet metal shell is greater than a thickness of the inner sheet metal shell.

9. A turbine housing assembly comprising:

a cast metal structure having an inlet opening and a bypass opening transverse to the inlet opening;

an inner sheet metal shell including an inner base portion having an end disposed within the inlet opening and a volute portion that defines an outer contour of a volute; and

an outer sheet metal shell that surrounds the volute portion and includes an outer base portion that circumscribes the inner base portion, wherein the outer base portion is joined to the cast metal structure and the end of the inner base portion is freestanding with respect to the cast metal structure, wherein an extension of the end of the inner base portion into the inlet opening is greater than an extension of the outer base portion into the inlet opening.

10. The turbine housing assembly of claim 9 , wherein the cast metal structure includes a flange that surrounds the outer base portion.

11. The turbine housing assembly of claim 10 , wherein the flange is coupled to the outer base portion.

12. The turbine housing assembly of claim 9 , wherein:

the cast metal structure includes a flange that surrounds the outer base portion; and

the flange is coupled to the outer base portion.

13. The turbine housing assembly of claim 9 , wherein the cast metal structure includes:

a first portion contacting the outer base portion; and

a recessed portion providing an air gap between the end of the inner base portion and the recessed portion.

14. The turbine housing assembly of claim 9 , wherein:

the inner sheet metal shell comprises a first plurality of sheet metal structures joined to one another in a radial plane substantially parallel to a rotating plane of a turbine wheel; and

the outer sheet metal shell comprises a second plurality of sheet metal structures joined to one another in an axial plane transverse to the radial plane.

15. The turbine housing assembly of claim 14 , wherein:

the first plurality of sheet metal structures are coupled about the volute portion; and

portions of the second plurality of sheet metal structures that surround the volute portion are coupled to one another in an axial direction aligned with a turbine wheel rotational axis.

16. A turbine housing assembly comprising:

a cast bypass valve assembly structure including a guide portion about an inlet opening and a bypass opening transverse to the inlet opening;

an inner sheet metal shell including an inner inlet portion and a volute portion that defines an outer contour of a volute, wherein an end of the inner inlet portion is disposed within the inlet opening and surrounded by the guide portion; and

an outer sheet metal shell that surrounds the volute portion and includes an outer inlet portion circumscribing the inner inlet portion and contacting the guide portion of the bypass valve assembly structure, wherein the outer inlet portion is joined to the bypass valve assembly structure, an extension of the end of the inner inlet portion into the inlet opening is greater than an extension of the outer inlet portion into the inlet opening, and the end of the inner inlet portion is freestanding with respect to the bypass valve assembly structure.

17. The turbine housing assembly of claim 16 , wherein:

the inner sheet metal shell comprises a first plurality of sheet metal structures joined to one another in a radial plane aligned with a rotating plane of a turbine wheel;

the outer sheet metal shell comprises a second plurality of sheet metal structures joined to one another in an axial plane transverse to the radial plane;

the first plurality of sheet metal structures are coupled about the volute portion;

the bypass valve assembly structure includes a flange that surrounds the outer inlet portion; and

the flange is coupled to the outer inlet portion.

Assignments (8)
CORRECTIVE ASSIGNMENT TO CORRECT THE THE TYPOS IN THE APPLICATION NUMBER PREVIOUSLY RECORDED AT REEL: 056111 FRAME: 0583. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Feb 25, 2022
From: GARRETT TRANSPORTATION I INC.
To: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 059250/0792 →
SECURITY AGREEMENT Recorded May 3, 2021
From: GARRETT TRANSPORTATION I INC.
To: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 056111/0583 →
RELEASE OF SECURITY INTEREST Recorded Apr 30, 2021
From: WILMINGTON SAVINGS FUND SOCIETY, FSB
To: GARRETT TRANSPORTATION I INC.
Reel/Frame 056427/0298 →
ASSIGNMENT AND ASSUMPTION OF SECURITY INTEREST IN PATENTS Recorded Jan 15, 2021
From: JPMORGAN CHASE BANK, N.A., AS RESIGNING ADMINISTRATIVE AND COLLATERAL AGENT
To: WILMINGTON SAVINGS FUND SOCIETY, FSB, AS SUCCESSOR ADMINISTRATIVE AND COLLATERAL AGENT
Reel/Frame 055008/0263 →
SECURITY INTEREST Recorded Oct 1, 2018
From: GARRETT TRANSPORTATION I INC.
To: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 047172/0220 →
CORRECTIVE ASSIGNMENT TO CORRECT THE ASSIGNEE NAME AND EXECUTION DATE PREVIOUSLY RECORDED AT REEL: 046103 FRAME: 0144. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Sep 21, 2018
From: HONEYWELL INTERNATIONAL INC.
To: GARRETT TRANSPORTATION I INC.
Reel/Frame 047119/0864 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 6, 2018
From: HONEYWELL INTERNATIONAL INC.
To: GARRETT TRANSPORTATION I INC.
Reel/Frame 047024/0127 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2017
From: AZUMA, KATSUMI; ISHIHARA, KOUICHIROU
To: HONEYWELL INTERNATIONAL INC
Reel/Frame 041123/0324 →