IP Library Granted Patent US 8,499,559
Granted Patent B2
US 8,499,559 · App. 12/294,853 · Granted Aug 6, 2013

Two-stage turbo-charger engine system

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Quick Facts
Patent No.
US 8,499,559
App. No.
12/294,853
Granted
Aug 6, 2013
Kind
B2
Abstract

A turbine housing for a high-pressure turbo-charger of a turbo-charger engine system for an internal combustion engine is provided that includes, but is not limited to a low-pressure charger opening for taking up a low-pressure turbo-charger and a high-pressure charger opening for taking up a high-pressure turbo-charger. A high-pressure exhaust opening is attached to a corresponding flange at an exhaust manifold of the engine and there is a short-cut exhaust opening with a high-pressure turbine by-pass valve area attached to a corresponding flange at the exhaust manifold. An external connection opening is attached to a muffler, a waste gate valve area being provided in the close vicinity of the external connection opening.

Claims (32)

1. A turbine housing of a turbo-charger engine system for an internal combustion engine, the turbine housing comprising:

a low-pressure charger opening attachable to a low-pressure turbo-charger;

a high-pressure charger opening attachable to a high-pressure turbo-charger;

a low-pressure exhaust duct in operable communication between the low-pressure charger opening and high-pressure charger opening;

a high-pressure exhaust opening in operable communication via a high-pressure exhaust duct with the high-pressure charger opening, the high-pressure exhaust opening attachable to a corresponding flange at an exhaust manifold of the internal combustion engine;

a short-cut exhaust opening in operable communication via a short-cut duct with the low-pressure charger opening, the short-cut exhaust opening being attachable to a corresponding flange at an exhaust manifold of the internal combustion engine;

a high-pressure turbine by-pass valve area located in the short-cut duct;

an external connection opening attachable to a muffler, the external connection opening in operable communication with the low-pressure charger opening, the external connection opening further in operable communication with the low-pressure exhaust duct via a low-pressure turbine exhaust bypass duct; and

a waste gate valve area provided in the low-pressure turbine exhaust bypass duct,

wherein a high-pressure exhaust flange and the short-cut exhaust flange are facing essentially in the same direction.

2. The turbine housing according to claim 1 , wherein the low-pressure exhaust duct, the high-pressure exhaust duct, the short-cut duct or the low-pressure turbine exhaust bypass duct are provided as internal channels in the turbine housing.

3. The turbine housing according to claim 1 , wherein the high-pressure exhaust flange and the short-cut exhaust flange lie in essentially parallel planes.

4. The turbine housing according to claim 3 , wherein the high-pressure exhaust flange and the short-cut exhaust flange lie essentially in the same plane.

5. The turbine housing according to claim 1 , wherein the low-pressure charger opening and the high-pressure charger opening lie in essentially parallel planes.

6. The turbine housing according to claim 1 , wherein the waste gate valve area is accessible for at least one machining process from outside of the turbine housing.

7. The turbine housing according to claim 6 , wherein the waste gate valve area is located in a vicinity of the external connection opening such that it is accessible for the at least one machining process through the external connection opening.

8. A high-pressure turbo-charger of a turbo-charger engine system for an internal combustion engine, the high-pressure turbo-charger comprising:

a turbine housing, comprising:

a low-pressure charger opening;

a high-pressure charger opening;

a low-pressure exhaust duct in operable communication between the low-pressure charger opening and high-pressure charger opening;

a high-pressure exhaust opening in operable communication via a high-pressure exhaust duct with the high-pressure charger opening, the high-pressure exhaust opening attachable to a corresponding flange at an exhaust manifold of the internal combustion engine;

a short-cut exhaust opening in operable communication via a short-cut duct with the low-pressure charger opening, the short-cut exhaust opening being attachable to a corresponding flange at an exhaust manifold of the internal combustion engine;

a high-pressure turbine by-pass valve area located in the short-cut duct;

an external connection opening attachable to a muffler, the external connection opening in operable communication with the low-pressure charger opening, the external connection opening further in operable communication with the low-pressure exhaust duct via a low-pressure turbine exhaust bypass duct; and

a waste gate valve area provided in the low-pressure turbine exhaust bypass duct,

wherein the high-pressure exhaust flange and the short-cut exhaust flange are facing essentially in the same direction;

a low-pressure turbo-charger with a low-pressure turbine wheel located in the low-pressure charger opening, the low-pressure turbo-charger in communication with the low-pressure charger opening; and

the high-pressure turbo-charger with a high-pressure turbine wheel located in the high-pressure charger opening, the high-pressure turbo-charger in communication with the high-pressure charger opening, and

the low-pressure turbine wheel and the high-pressure turbine wheel essentially facing towards each other.

9. The high-pressure turbo-charger according to claim 8 , wherein the high-pressure turbine by-pass valve area or the waste gate valve area comprise a movable flap.

10. The high-pressure turbo-charger according to claim 9 , further comprising a pulse-width modulated pneumatic actuator coupled with the movable flap for moving the movable flap between an open and a closed position.

Assignments (12)
RELEASE OF SECURITY INTEREST Recorded Nov 7, 2014
From: WILMINGTON TRUST COMPANY
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 034384/0758 →
CHANGE OF NAME Recorded Feb 10, 2011
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 025781/0245 →
SECURITY AGREEMENT Recorded Nov 8, 2010
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: WILMINGTON TRUST COMPANY
Reel/Frame 025324/0515 →
RELEASE OF SECURITY INTEREST Recorded Nov 5, 2010
From: UAW RETIREE MEDICAL BENEFITS TRUST
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025315/0046 →
RELEASE OF SECURITY INTEREST Recorded Nov 4, 2010
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025245/0909 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 27, 2010
From: AXELSSON, PAL; DRANGEL, HANS; LIND, BJOERN
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025200/0974 →
SECURITY AGREEMENT Recorded Aug 28, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UAW RETIREE MEDICAL BENEFITS TRUST
Reel/Frame 023162/0237 →
SECURITY AGREEMENT Recorded Aug 27, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 023156/0313 →
RELEASE OF SECURITY INTEREST Recorded Aug 21, 2009
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 023126/0914 →
RELEASE OF SECURITY INTEREST Recorded Aug 21, 2009
From: CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECURED PARTIES; CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SECURED PARTIES
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 023155/0769 →
SECURITY AGREEMENT Recorded Apr 16, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECURED PARTIES; CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SECURED PARTIES
Reel/Frame 022554/0538 →
SECURITY AGREEMENT Recorded Feb 4, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 022201/0448 →