IP Library Granted Patent US 8,307,649
Granted Patent B2
US 8,307,649 · App. 12/020,948 · Granted Nov 13, 2012

Arrangement of a two stage turbocharger system for an internal combustion engine

Assignee: GM Global Technology Operations LLC
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Quick Facts
Patent No.
US 8,307,649
App. No.
12/020,948
Granted
Nov 13, 2012
Kind
B2
Abstract

Arrangement of a two stage turbocharger system for an internal combustion engine including an intake manifold and an exhaust manifold, including a low-pressure turbocharger, a high-pressure turbocharger and a bypass duct in flow communication with an outlet of the low-pressure compressor, an inlet of the high-pressure compressor, an outlet of the high-pressure compressor and an inlet of the intake manifold. The bypass duct includes a first bypass valve for opening and closing the bypass duct. The first bypass valve and the high-pressure compressor are accommodated within a common housing.

Claims (25)

1. An arrangement of a two stage turbocharger system for an internal combustion engine comprising an intake manifold and an exhaust manifold, comprising:

a low-pressure turbocharger comprising a low-pressure turbine and a low-pressure compressor;

a high-pressure turbocharger comprising a high-pressure turbine and a high-pressure compressor;

a bypass duct in flow communication with an outlet of the low-pressure compressor and with an inlet of the high-pressure compressor and with an outlet of the high-pressure compressor and with an inlet of the intake manifold, the bypass duct comprising a bypass valve for opening and closing the bypass duct;

a common housing, wherein the bypass valve and the high-pressure compressor are each integrated within the common housing; and

a pipe, wherein the outlet of the low-pressure compressor is coupled to a first end of the pipe by a first free-floating interface and the inlet of the high-pressure compressor is coupled to a second end of the pipe by a second free floating interface, wherein the first free-floating interface is orthogonal to the second free-floating interface.

2. The arrangement according to claim 1 , wherein air is directed from the outlet of the low-pressure compressor to the inlet of the high-pressure compressor and from the outlet of the high-pressure compressor to the inlet of the intake manifold when the bypass valve is in a closed position.

3. The arrangement according to claim 1 , wherein the air is directed from the outlet of the low-pressure compressor to the inlet of the intake manifold when the bypass valve is in an open position.

4. The arrangement according to claim 3 , wherein substantially no air is directed through the high-pressure compressor when the bypass valve is in the open position.

5. The arrangement according to claim 1 , wherein the common housing further comprises the bypass duct, the bypass duct comprising:

an inlet being in flow communication with the outlet of the low-pressure compressor;

an outlet being in flow communication with the inlet of the intake manifold; and

the bypass valve being positioned between the inlet and the outlet,

wherein the inlet of the high-pressure compressor is in flow communication with the bypass duct upstream of the bypass valve and the outlet of the high-pressure compressor is in flow communication with the bypass duct downstream of the bypass valve.

6. The arrangement according to claim 5 , wherein the inlet of the bypass duct is generally orthogonal to the inlet of the high-pressure compressor.

7. The arrangement according to claim 5 , wherein the inlet of the bypass duct is generally orthogonal to the outlet of the high-pressure compressor.

8. The arrangement according to claim 5 , wherein the common housing further comprises an additional outlet, the additional outlet being the outlet of the high-pressure compressor.

9. The arrangement according to claim 8 , wherein the additional outlet is in flow communication with the first outlet within the common housing.

10. The arrangement according to claim 8 , wherein the additional outlet is separate from the outlet within the common housing.

11. The arrangement according to claim 1 , wherein the bypass valve is pneumatically actuated or electrically actuated or hydraulically actuated.

12. The arrangement according to claim 1 , wherein the bypass valve is controllable in response to parameters comprising at least one of engine speed and engine load.

13. The arrangement according to claim 1 , wherein the common housing, the bypass duct, and the inlet of the high-pressure compressor are provided as a single piece.

14. The arrangement according to claim 1 , wherein the common housing comprises aluminium.

15. The arrangement according to claim 1 , wherein the first free floating interface and the second free floating interface are adapted to accommodate movement between the pipe and the outlet of the low-pressure compressor and the inlet of the high-pressure compressor in at least first and second orthogonal directions, and wherein the first free floating interface is configured to accommodate rotational movement in a plane defined by the first and second orthogonal directions.

16. The arrangement according to claim 1 , wherein the pipe is rigid.

Assignments (12)
RELEASE OF SECURITY INTEREST Recorded Nov 7, 2014
From: WILMINGTON TRUST COMPANY
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 034185/0587 →
CHANGE OF NAME Recorded Feb 10, 2011
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 025781/0211 →
SECURITY AGREEMENT Recorded Nov 8, 2010
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: WILMINGTON TRUST COMPANY
Reel/Frame 025324/0475 →
RELEASE OF SECURITY INTEREST Recorded Nov 5, 2010
From: UAW RETIREE MEDICAL BENEFITS TRUST
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025315/0001 →
RELEASE OF SECURITY INTEREST Recorded Nov 4, 2010
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025245/0780 →
SECURITY AGREEMENT Recorded Aug 28, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UAW RETIREE MEDICAL BENEFITS TRUST
Reel/Frame 023162/0187 →
SECURITY AGREEMENT Recorded Aug 27, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 023156/0215 →
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 023155/0880 →
RELEASE OF SECURITY INTEREST Recorded Aug 20, 2009
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 023124/0670 →
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 022554/0479 →
SECURITY AGREEMENT Recorded Feb 4, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 022201/0448 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 4, 2008
From: AXELSSON, PAL; DRANGEL, HANS; LIND, BJORN
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 020458/0206 →
Priority Claims (1)
EP 0710850 · Jan 31, 2007 · regional
Continuity (1)
Related Publication 20080178591A1 · Jul 31, 2008