IP Library Granted Patent US 8,201,536
Granted Patent B2
US 8,201,536 · App. 12/275,575 · Granted Jun 19, 2012

Intake system with resonator

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Quick Facts
Patent No.
US 8,201,536
App. No.
12/275,575
Granted
Jun 19, 2012
Kind
B2
Abstract

An engine assembly may include an engine block, first and second cylinder heads, and a first and second intake manifolds. The engine block may include a first bank defining a first set of cylinders and a second bank defining a second set of cylinders. The first cylinder head may be fixed to the first bank and the second cylinder head may be fixed to the second bank. The first intake manifold may be fixed to the first cylinder head and may include a first acoustic tuning mechanism in communication with the first intake manifold. The second intake manifold may be fixed to the second cylinder head and may include a second acoustic tuning mechanism in communication with the second intake manifold.

Claims (34)

1. An engine assembly comprising:

an engine block including a first bank defining a first set of cylinders and a second bank defining a second set of cylinders;

a first cylinder head fixed to the first bank and including a first set of intake ports;

a second cylinder head fixed to the second bank and including a second set of intake ports;

a first cylinder head cover defining a first intake manifold fixed to the first cylinder head and including a first air inlet, a first air distribution member defining a cavity in communication with the first air inlet, and a first set of intake manifold ports extending from the first air distribution member and providing communication between the first air distribution member and the first set of intake ports, and a first acoustic tuning mechanism extending from and in communication with the first air distribution member that reduces a first air pressure pulsation within the first air distribution member; and

a second cylinder head cover defining a second intake manifold fixed to the second cylinder head and including a second air inlet, a second air distribution member defining a cavity in communication with the second air inlet, and a second set of intake manifold ports extending from the second air distribution member and providing communication between the second air distribution member and the second set of intake ports, and a second acoustic tuning mechanism extending from and in communication with the second air distribution member that reduces a second air pressure pulsation within the second air distribution member.

2. The engine assembly of claim 1 , wherein the first acoustic tuning mechanism includes a chamber in communication with the first air distribution member.

3. The engine assembly of claim 2 , wherein the first acoustic tuning mechanism includes a conduit providing communication between the chamber and the first air distribution member.

4. The engine assembly of claim 3 , wherein the first acoustic tuning mechanism includes a Helmholtz resonator.

5. The engine assembly of claim 1 , wherein the second set of cylinders is disposed at an angle relative to the first set of cylinders to form a V-configuration, the first cylinder head including a first set of exhaust ports located on an inboard side of the cylinder head proximate a center of the V-configuration.

6. The engine assembly of claim 5 , wherein the first set of cylinders has a first a-periodic firing order corresponding to two revolutions of a crankshaft of the engine that generates the first air pressure pulsation, the second set of cylinders having a second a-periodic firing order that corresponds to the two revolutions of the crankshaft that generates the second air pressure pulsation.

7. The engine assembly of claim 1 , wherein the first set of cylinders has a first a-periodic firing order corresponding to two revolutions of a crankshaft of the engine that generates the first air pressure pulsation.

8. An engine assembly comprising:

an engine block including a first bank defining a first set of cylinders having a first a-periodic firing order corresponding to two revolutions of an engine crankshaft;

a first cylinder head fixed to the first bank and including a first set of intake ports; and

a first cylinder head cover defining a first intake manifold fixed to the first cylinder head and including a first air inlet, a first air distribution member defining a cavity in communication with the first air inlet, and a first set of intake manifold ports extending from the first air distribution member and providing communication between the first air inlet and the first set of intake ports, and a first acoustic tuning mechanism extending from and in communication with the first air distribution member that reduces a first air pressure pulsation created by the first a-periodic firing order of the first set of cylinders.

9. The engine assembly of claim 8 , wherein the first acoustic tuning mechanism includes a chamber in communication with the first air distribution member.

10. The engine assembly of claim 9 , wherein the first acoustic tuning mechanism includes a conduit providing communication between the chamber and the first air distribution member.

11. The engine assembly of claim 10 , wherein the first acoustic tuning mechanism includes a Helmholtz resonator.

12. The engine assembly of claim 8 , wherein the engine block includes a second bank defining a second set of cylinders that are disposed at an angle relative to the first set of cylinders.

13. The engine assembly of claim 12 , wherein the second set of cylinders has a second a-periodic firing order corresponding to the two revolutions of the crankshaft that generates a second air pressure pulsation.

14. The engine assembly of claim 13 , further comprising a second cylinder head and a second cylinder head cover, the second cylinder head being fixed to the second bank and including a second set of intake ports, the second cylinder head cover defining a second intake manifold including a second air inlet, a second air distribution member defining a cavity in communication with the second air inlet and the second set of intake ports, and a second set of intake manifold ports extending from the second air distribution member and providing communication between the second air inlet and the second set of intake ports, and a second acoustic tuning mechanism extending from and in communication with the second air distribution member that reduces a second air pressure pulsation within the second air distribution member.

15. The engine assembly of claim 13 , wherein the first a-periodic firing order is different from the second a-periodic firing order.

16. A method comprising:

determining a first air pressure pulsation in a first intake manifold defined by a first cylinder head cover that is fixed to a first cylinder head that corresponds to a first set of cylinders in an engine, the first cylinder head cover including a first air inlet, a first air distribution member defining a cavity in communication with the first air inlet, and a first set of intake manifold ports extending from the first air distribution member and providing communication between the first air distribution member and a first set of intake ports in the first cylinder head;

determining a second air pressure pulsation in a second intake manifold defined by a second cylinder head cover that is fixed to a second cylinder head that corresponds to a second set of cylinders of the engine, the second cylinder head cover including a second air inlet, a second air distribution member defining a cavity in communication with the second air inlet, and a second set of intake manifold ports extending from the second air distribution member and providing communication between the second air distribution member and a second set of intake ports in the second cylinder head;

selecting a first acoustic tuning mechanism based on the determined first air pressure pulsation;

providing communication between the first intake manifold and the first acoustic tuning mechanism to reduce the first air pressure pulsation;

selecting a second acoustic tuning mechanism based on the determined second air pressure pulsation; and

providing communication between the second intake manifold and the second acoustic tuning mechanism to reduce the second air pressure pulsation.

17. The method of claim 16 , wherein the providing communication between the first intake manifold and the first acoustic tuning mechanism reduces a variation in air flow to each of the cylinders in the first set of cylinders.

18. The method of claim 16 , wherein the determining the first air pressure pulsation includes determining a first frequency of the first air pressure pulsation within the first intake manifold and the determining the second air pressure pulsation includes determining a second frequency of the second air pressure pulsation within the second intake manifold.

19. The method of claim 16 , wherein the determining the first air pressure pulsation includes determining a first amplitude of the first air pressure pulsation within the first intake manifold and the determining the second air pressure pulsation includes determining a second amplitude of the second air pressure pulsation within the second intake manifold.

20. The method of claim 16 , wherein the first set of cylinders is disposed at an angle relative to the second set of cylinders to form a V-configuration.

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 →
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 022201/0405 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 21, 2008
From: HAZELTON, GARY J.; STOJKOVIC, BORIS D.
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 021873/0524 →
Continuity (2)
Provisional Application 61025595 · Feb 1, 2008
Related Publication 20090194056A1 · Aug 6, 2009