IP Library Granted Patent US 7,735,478
Granted Patent B1
US 7,735,478 · App. 12/276,915 · Granted Jun 15, 2010

Method of calculating mass fraction burnt in an internal combustion engine based on rassweiler-withrow method for real-time applications

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Quick Facts
Patent No.
US 7,735,478
App. No.
12/276,915
Granted
Jun 15, 2010
Kind
B1
Abstract

A system and method for determining mass fraction burned in an internal combustion engine includes a plurality of engine sensors and a control module determining a ratio of specific heat from a combination of one or more from the group of exhaust gas temperature, injected fuel quantity, air quantity inside a cylinder, mass air flow, air fuel ratio, manifold pressure and a residual gas amount determined from the plurality of engine sensors. The control module includes a mass fraction burned module determining a mass fraction burned in response to a cylinder volume, and the ratio of specific heat. The control module controls an engine parameter based on mass fraction burned.

Claims (29)

1. A method of controlling an engine, the method comprising:

determining a ratio of specific heat by determining a mixture temperature, air fuel ratio, and a representation of an amount of residual gasses in a cylinder from a combination of one or more from the group of exhaust gas temperature, injected fuel quantity, air quantity inside a cylinder, mass air flow, air fuel ratio, manifold pressure, and a residual gas amount;

determining a mass fraction burned in response to a cylinder volume, the mixture temperature, air fuel ratio, manifold pressure, and the ratio of specific heat; and

controlling engine parameters based on mass fraction burned.

2. A method as recited in claim 1 wherein determining a mixture temperature, air fuel ratio, and a representation of an amount of residual gasses comprises forming a polynomial in a polynomial block of a gamma module.

3. A method as recited in claim 1 wherein determining a mass fraction burned in response to a cylinder volume, the mixture temperature, air fuel ratio, manifold pressure, and the ratio of specific heat comprises determining a mass fraction burned in response to a cylinder volume, a change in cylinder volume, the mixture temperature, air fuel ratio, intake manifold pressure, and the ratio of specific heat.

4. A method as recited in claim 1 wherein determining a mass fraction burned in response to a cylinder volume, the mixture temperature, air fuel ratio, manifold pressure, and the ratio of specific heat comprises determining a mass fraction burned in response to a cylinder volume, a change in cylinder volume, the mixture temperature, air fuel ratio, a cylinder pressure, and the ratio of specific heat.

5. A method as recited in claim 1 wherein controlling an engine parameter comprises controlling dilution.

6. A method as recited in claim 5 wherein controlling dilution comprises controlling an exhaust gas recirculation valve.

7. A method as recited in claim 1 wherein determining a mass fraction burned comprises determining a mass fraction burned in response to a Taylor series expansion.

8. A method of controlling an engine comprising:

forming a table output from a two-dimensional table from two inputs selected from the group of exhaust gas temperature, injected fuel quantity, air quantity inside a cylinder, mass air flow, air fuel ratio, manifold pressure, a residual gas amount, and a correction factor selected from the group not one of the two inputs selected to form the two-dimensional table;

determining a mass fraction burned in response to a cylinder volume, the table output and the correction factor; and

controlling engine parameters based on mass fraction burned.

9. A method as recited in claim 8 wherein determining a mass fraction burned in response to a cylinder volume, the table output and the correction factor comprises determining a mass fraction burned in response to a cylinder volume, a change in cylinder volume, the table output, and the correction factor.

10. A method as recited in claim 8 wherein determining a mass fraction burned comprises adding the table output and the correction factor together.

11. A method as recited in claim 8 wherein determining a mass fraction burned comprises multiplying the table output and the correction factor together.

12. A method as recited in claim 8 wherein controlling an engine parameter comprises controlling dilution.

13. A method as recited in claim 12 wherein controlling dilution comprises controlling an exhaust gas recirculation valve.

14. A method as recited in claim 8 wherein determining a mass fraction burned comprises determining a mass fraction burned in response to a Taylor series expansion.

15. A system comprising:

a plurality of engine sensors; and

a control module determining a ratio of specific heat from a combination of one or more from the group of exhaust gas temperature, injected fuel quantity, air quantity inside a cylinder, mass air flow, air fuel ratio, manifold pressure, and a residual gas amount determined from the plurality of engine sensors,

said control module comprising a mass fraction burned module determining a mass fraction burned in response to a cylinder volume, and the ratio of specific heat, said control module controlling an engine parameter based on mass fraction burned.

16. A system as recited in claim 15 wherein said control module comprising a two-dimensional table having a table output from two inputs selected from the group of exhaust gas temperature, injected fuel quantity, air quantity inside a cylinder, mass air flow, air fuel ratio, manifold pressure, and a residual gas amount, said control module forming a correction factor selected from the group not one of the two inputs selected from the group.

17. A method as recited in claim 16 wherein the control module determines the ratio of specific heat by adding the correction factor and the table output.

18. A method as recited in claim 16 wherein the control module determines the ratio of specific heat by multiplying the correction factor and the table output.

19. A method as recited in claim 16 wherein the control module forms a polynomial representative of mixture temperature, air fuel ratio, and an amount of residual gasses in a cylinder from the at least two from the group.

20. A method as recited in claim 16 wherein the controller controls dilution of input gasses.

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 24, 2008
From: DAGCI, OGUZ H.; BUSLEPP, KENNETH J.
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 021883/0363 →