IP Library Granted Patent US 9,133,745
Granted Patent B2
US 9,133,745 · App. 14/015,240 · Granted Sep 15, 2015

Split/dual plane integrated exhaust manifold for dual scroll turbo charger

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Quick Facts
Patent No.
US 9,133,745
App. No.
14/015,240
Granted
Sep 15, 2015
Kind
B2
Abstract

An integrated exhaust manifold for use with an internal combustion engine and dual scroll turbocharger. The integrated exhaust manifold includes a first exhaust passageway fluidly connected between a first pair of piston cylinders and the dual scroll turbocharger for transporting exhaust gas from the first pair of piston cylinders to a first input of dual scroll turbocharger. The integrated exhaust manifold includes a second exhaust passageway fluidly connected between a second pair of piston cylinders and the dual scroll turbocharger for transporting exhaust gas from the second pair of piston cylinders to a second input of the dual scroll turbocharger. The second exhaust passageway is fluidly independent from the first exhaust passageway and the first and second exhaust passageways are positioned to define a septum area therebetween. A cooling system having a septum cooling jacket is use to cool the septum area between the first and second exhaust passageways.

Claims (19)

1. An internal combustion engine comprising:

a plurality of piston cylinders each operable to combust a chemical mixture and output an exhaust gas;

a dual scroll turbocharger having first and second inputs;

an integrated exhaust manifold having an integrally formed cylinder head and exhaust system, said integrated exhaust manifold having a first exhaust passageway fluidly coupled between a first and a second of the plurality of piston cylinders and the dual scroll turbocharger, the first exhaust passageway transporting the exhaust gas from the first and second piston cylinders to the first input of the dual scroll turbocharger, wherein the first exhaust passageway comprises:

a first exhaust valve section being positioned immediately downstream of an exhaust valve of the first piston cylinder;

a second exhaust valve section being positioned immediately downstream of an exhaust valve of the second piston cylinder;

a first branch passageway being fluidly coupled with the first exhaust valve section and the second exhaust valve section to receive the exhaust gases of the first piston cylinder and the second piston cylinder therein, said first branch passageway terminating at a first exhaust output opening directly from an exterior surface of the integrated exhaust manifold;

the integrated exhaust manifold further having a second exhaust passageway fluidly coupled between a third and a fourth of the plurality of piston cylinders and the dual scroll turbocharger, the second exhaust passageway transporting the exhaust gas from the third and fourth piston cylinders to the second input of the dual scroll turbocharger, the second exhaust passageway comprises:

a third exhaust valve section being positioned immediately downstream of an exhaust valve of the third piston cylinder;

a fourth exhaust valve section being positioned immediately downstream of an exhaust valve of the fourth piston cylinder; and

a second branch passageway being fluidly coupled with the third exhaust valve section and the fourth exhaust valve section to receive the exhaust gases of the third piston cylinder and the fourth piston cylinder therein,

the second exhaust passageway being fluidly independent from the first exhaust passageway, the first exhaust passageway and the second exhaust passageway positioned to define a septum area therebetween, said second branch passageway terminating at a second exhaust output opening directly from the exterior surface of the integrated exhaust manifold, wherein the first exhaust output and the second exhaust output each include a half circle cross section with an arcuate outer edge and a substantially flat inner edge such that the substantially flat inner edge of said first exhaust output and the substantially flat inner edge of said second exhaust output are positioned directly along opposite side edges of the septum area to form the septum area therebetween; and

a cooling system having an upper head cooling jacket, a lower head cooling jacket and a septum cooling jacket, the septum cooling jacket receiving a liquid coolant and routing the liquid coolant through at least a portion of the septum area between the first exhaust passageway and the second exhaust passageway, and a coolant output line extending from an upper surface of the upper head cooling jacket.

2. The internal combustion engine according to claim 1 wherein the first branch passageway is positioned at a first elevation and the second branch passageway is positioned at a second elevation, the second elevation being different than the first elevation such that the second branch passageway is offset relative to the first branch passageway.

3. The internal combustion engine according to claim 1 wherein the combination of the third and fourth piston cylinders are positioned between the first and the second piston cylinders such that the first exhaust valve section and the second exhaust valve section are positioned outboard from the third exhaust valve section and the fourth exhaust valve section.

4. The internal combustion engine according to claim 1 wherein the cooling system further comprises:

an upper cooling jacket; and

a lower cooling jacket,

wherein the upper cooling jacket is positioned above the first exhaust passageway and the second exhaust passageway, the lower cooling jacket is positioned below the first exhaust passageway and the second exhaust passageway.

Assignments (3)
RELEASE OF SECURITY INTEREST Recorded Nov 7, 2014
From: WILMINGTON TRUST COMPANY
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 034189/0065 →
SECURITY INTEREST Recorded Jun 12, 2014
From: GM GLOBAL TECHNOLOGY OPERATIONS LLC
To: WILMINGTON TRUST COMPANY
Reel/Frame 033135/0440 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 30, 2013
From: ZAHDEH, AKRAM R.; BOSMAN, COLIN BLACKLOCK; EASTMAN, KENNETH M.; MCALPINE, ROBERT S.
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 031119/0770 →