IP Library Granted Patent US 8,276,551
Granted Patent B2
US 8,276,551 · App. 12/345,775 · Granted Oct 2, 2012

HCCI combustion moding state control for fuel economy and seamless transitions

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Quick Facts
Patent No.
US 8,276,551
App. No.
12/345,775
Granted
Oct 2, 2012
Kind
B2
Abstract

A method and system for controlling an engine includes a homogeneous charge compression ignition (HCCI) operating zone boundary module determining a first HCCI operating boundary and a fuel rate module determining a first fuel rate from an operator input. The system also includes a switch module modifying the first HCCI operating boundary to a modified boundary in response to a measured mass airflow, cam positions and the first HCCI operating boundary. The system also includes a combustion control module operating the engine in a spark ignited mode when a second fuel rate request is outside the modified boundary.

Claims (35)

1. A method comprising:

determining a first maximum fuel rate;

determining a desired fuel rate from an operator input;

modifying the first maximum fuel rate to a second maximum fuel rate in response to a measured mass airflow, a position of a camshaft that actuates at least one of an intake valve and an exhaust valve, and the first maximum fuel rate; and

operating an engine in a spark ignited mode when the desired fuel rate is greater than the second maximum fuel rate.

2. A method as recited in claim 1 further comprising operating the engine in an homogeneous charge compression ignition (HCCI) mode when a the desired fuel rate is less than or equal to the second maximum fuel rate.

3. A method as recited in claim 1 wherein determining the first maximum fuel rate comprises determining the first maximum fuel rate in response to engine speed.

4. A method as recited in claim 1 wherein modifying comprises modifying the first maximum fuel rate to the second maximum fuel rate in response to a relative cam position.

5. A method as recited in claim 1 wherein modifying comprises modifying the first maximum fuel rate to the second maximum fuel rate in response to a relative cam position corresponding to a minimum negative valve overlap.

6. A method as recited in claim 1 wherein modifying comprises modifying the first maximum fuel rate to the second maximum fuel rate in response to a calculated maximum fuel rate determined in response to the measured mass airflow.

7. A method as recited in claim 1 wherein modifying comprises modifying the first maximum fuel rate to the second maximum fuel rate in response to a relative cam position corresponding to a mechanical saturation.

8. A method as recited in claim 1 further comprising determining a calculated maximum fueling rate by dividing the measured mass airflow by stoichiometry and wherein modifying comprises modifying the first maximum fuel rate to the second maximum fuel rate in response to the calculated maximum fueling rate.

9. A method of controlling an engine comprising:

determining a mass airflow for the engine;

determining an engine speed;

determining a first maximum fueling rate in response to the engine speed;

determining a desired fueling rate based on an operator input;

determining a position of a camshaft that actuates at least one of an intake valve and an exhaust valve;

when the position of the camshaft corresponds to a saturated position, modifying the first maximum fueling rate boundary to a second maximum fueling rate based on the mass airflow; and

entering a spark ignition mode when the desired fueling rate is greater than the second maximum fueling rate.

10. A method as recited in claim 9 further comprising operating the engine in an homogeneous charge compression ignition (HCCI) mode when a the desired fueling rate request is less than or equal to the second maximum fueling rate.

11. A method as recited in claim 9 further comprising determining a calculated fueling rate from the mass airflow and wherein modifying the first fueling rate to the second maximum fueling rate comprises modifying the first fueling rate to the second maximum fueling rate based on the calculated fueling rate.

12. A system comprising:

an homogeneous charge compression ignition (HCCI) operating zone boundary module determining a first maximum fuel rate;

a fuel rate module determining a desired fuel rate from an operator input;

a switch module modifying the first maximum fuel rate to a second maximum fuel rate in response to a measured mass airflow, a position of a camshaft that actuates at least one of an intake valve and an exhaust valve, and the first maximum fuel rate; and

a combustion control module operating an engine in a spark ignited mode when the desired fuel rate is greater than the second maximum fuel rate.

13. A system as recited in claim 12 wherein the combustion control module operates the engine in an HCCI mode when the desired fuel rate is less than or equal to the second maximum fuel rate.

14. A system as recited in claim 12 wherein the HCCI operating zone boundary module determines the first maximum fuel rate in response to engine speed.

15. A system as recited in claim 12 wherein the switch module modifies the first maximum fuel rate to the second maximum fuel rate in response to a relative cam position.

16. A system as recited in claim 12 wherein the switch module modifies the first maximum fuel rate to the second maximum fuel rate in response to a relative cam position corresponding to a minimum negative valve overlap.

17. A system as recited in claim 12 wherein the switch module modifies the first maximum fuel rate to the second maximum fuel rate in response to the measured mass airflow.

18. A system as recited in claim 12 wherein the switch module modifies the first maximum fuel rate to the second maximum fuel rate in response to a relative cam position corresponding to a mechanical saturation.

19. A system as recited in claim 12 wherein the switch module modifies the first maximum fuel rate to the second maximum fuel rate in response to a calculated maximum fueling rate that is determined by dividing the measured mass airflow by stoichiometry.

20. A system as recited in claim 12 wherein the engine comprises a direct injection engine.

Assignments (8)
RELEASE OF SECURITY INTEREST Recorded Nov 7, 2014
From: WILMINGTON TRUST COMPANY
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 034185/0789 →
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 025246/0056 →
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 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 22, 2009
From: RAMAPPAN, VIJAY; KANG, JUN-MO
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 022140/0023 →