IP Library Granted Patent US 8,820,071
Granted Patent B2
US 8,820,071 · App. 13/186,982 · Granted Sep 2, 2014

Integrated compressor housing and inlet

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Quick Facts
Patent No.
US 8,820,071
App. No.
13/186,982
Granted
Sep 2, 2014
Kind
B2
Abstract

In one exemplary embodiment of the present invention, a compressor housing for a forced induction system of an internal combustion engine is provided. The compressor housing includes a compressor inlet passage in fluid communication with a compressor volute configured to house a compressor wheel, the compressor inlet passage comprising a wall that is shared with the compressor volute. The compressor also includes a compressor outlet in fluid communication with the compressor volute, the compressor outlet being configured to direct a compressed gas to an intake manifold of the internal combustion engine.

Claims (27)

1. A method for forced air induction of an internal combustion engine, the method comprising:

providing a compressor housing fluidly coupled to the internal combustion engine, the compressor housing including a compressor volute portion and a compressor inlet portion fluidly coupled to the compressor volute portion, wherein the compressor volute portion includes an outer wall and the compressor inlet portion includes an inner wall, and wherein a portion of the compressor volute portion outer wall and the compressor inlet portion inner wall together define a passage to fluidly couple the compressor inlet portion and the compressor volute portion;

directing an air flow into the passage defined by the portion of the compressor volute outer wall and the compressor inlet portion inner wall, wherein the passage creates a swirling air flow component into the compressor volute defined by the compressor volute portion; and

directing a compressed air flow from the compressor volute to an intake manifold of the internal combustion engine.

2. The method of claim 1 , wherein directing the air flow comprises receiving the air flow from an air supply conduit.

3. The method of claim 1 , wherein directing the air flow comprises swirling the air flow into the compressor volute.

4. The method of claim 1 , wherein providing the compressor housing further comprises providing the compressor housing with an integrally cast compressor volute portion and compressor inlet portion.

5. A compressor housing for a forced induction system of an internal combustion engine, the compressor housing comprising:

a compressor volute portion defined by a wall comprising an outer surface and an opposed inner surface, the compressor volute wall inner surface defining a compressor volute configured to house a compressor wheel;

a compressor inlet passage in fluid communication with the compressor volute, the compressor inlet passage comprising an inner surface and an opposed outer surface, wherein a portion of the compressor volute wall outer surface comprises a portion of the compressor inlet passage inner surface; and

a compressor outlet in fluid communication with the compressor volute, the compressor outlet being configured to direct a compressed gas to an intake manifold of the internal combustion engine.

6. The compressor housing of claim 5 , wherein the compressor inlet passage is in fluid communication with an air supply conduit.

7. The compressor housing of claim 5 , wherein the compressor inlet passage comprises an offset portion upstream of the compressor wheel to induce a swirl of the air flow into the compressor volute.

8. The compressor housing of claim 7 , wherein the offset portion forms a non-concentric cavity.

9. The compressor housing of claim 5 , wherein the compressor volute portion is integrally cast with the compressor inlet passage.

10. The compressor housing of claim 9 , wherein the compressor housing comprises a cast metal.

11. The compressor housing of claim 5 , wherein the compressor inlet passage extends along an axis that is orthogonal to a rotational axis of the compressor wheel.

12. The compressor housing of claim 5 , further comprising a recirculation duct fluidly coupled between the compressor volute and the compressor inlet passage.

13. A turbocharger for an internal combustion engine, the turbocharger comprising:

a turbine housing; and

a compressor housing comprising:

a compressor volute portion having an outer surface and an opposed inner surface defining a compressor volute configured to house a compressor wheel;

a compressor inlet portion integrated with the compressor volute portion, the compressor inlet portion being configured to direct an air flow to the compressor wheel rotatably disposed within the compressor volute, wherein the compressor inlet portion comprises an inner surface, and wherein a portion of the compressor volute portion outer surface and the compressor inlet portion inner surface together define a passage extending therebetween to direct the air flow to the compressor wheel; and

a compressor outlet in the compressor housing, the compressor outlet configured to direct a compressed air flow from the compressor volute to an intake manifold of the internal combustion engine.

14. The turbocharger of claim 13 , wherein the compressor inlet portion is in fluid communication with an air supply conduit.

15. The turbocharger of claim 13 , wherein the compressor inlet portion comprises an offset portion configured to swirl the air flow in a rotational direction of the compressor wheel rotation.

16. The turbocharger of claim 13 , wherein the compressor housing comprises a cast metal.

Assignments (3)
RELEASE OF SECURITY INTEREST Recorded Nov 7, 2014
From: WILMINGTON TRUST COMPANY
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 034186/0776 →
SECURITY AGREEMENT Recorded Jun 28, 2012
From: GM GLOBAL TECHNOLOGY OPERATIONS LLC
To: WILMINGTON TRUST COMPANY
Reel/Frame 028466/0870 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 20, 2011
From: TKAC, RONALD M.
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 026623/0595 →