IP Library Granted Patent US 8,118,010
Granted Patent B2
US 8,118,010 · App. 12/574,114 · Granted Feb 21, 2012

Diagnostic systems and methods for fuel injectors in homogenous charge compression ignition engine systems

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Quick Facts
Patent No.
US 8,118,010
App. No.
12/574,114
Granted
Feb 21, 2012
Kind
B2
Abstract

An engine control system for a homogenous charge compression ignition (HCCI) engine includes a fuel injector temperature determination module and a fuel injector control module. The fuel injector temperature determination module determines a temperature of a tip of a fuel injector based on a first temperature model when the HCCI engine is operating in an HCCI combustion mode, and determines the temperature of the tip of the fuel injector based on a second temperature model when the HCCI engine is operating in a spark ignition (SI) combustion mode. The fuel injector control module controls a fuel injector pulse width based on the determined temperature and a predetermined temperature threshold, wherein the fuel injector pulse width increases when the determined temperature is greater than the predetermined temperature threshold.

Claims (34)

1. An engine control system for a homogenous charge compression ignition (HCCI) engine, comprising:

a fuel injector temperature determination module that determines a temperature of a tip of a fuel injector based on a first temperature model when the HCCI engine is operating in an HCCI combustion mode, and that determines the temperature of the tip of the fuel injector based on a second temperature model when the HCCI engine is operating in a spark ignition (SI) combustion mode; and

a fuel injector control module that controls a fuel injector pulse width during an engine on period based on the determined temperature and a predetermined temperature threshold, wherein the fuel injector pulse width increases when the determined temperature is greater than the predetermined temperature threshold.

2. The engine control system of claim 1 , wherein the fuel injector determination module determines the temperature of the tip of the fuel injector based on a third temperature model when the HCCI engine is transitioning between combustion modes.

3. The engine control system of claim 2 , wherein the first temperature model includes a first range of temperatures, wherein the second temperature model includes a second range of temperatures, wherein the third temperature model includes a third range of temperatures, wherein a portions of the first and third ranges of temperatures are less than the second range of temperatures, and wherein a portion of the first range of temperatures is less than the third range of temperatures.

4. The engine control system of claim 2 , wherein the fuel injector temperature determination module determines the temperature of the tip of the fuel injector based on a flow rate of fuel to the fuel injector and one of the first, second, and third temperature models.

5. The engine control system of claim 1 , wherein the fuel injector control module controls the fuel injector pulse width based on the determined temperature and a plurality of temperature thresholds.

6. The engine control system of claim 5 , wherein each of the plurality of temperature thresholds corresponds to one of fuel density and delay in one of opening and closing the fuel injector.

7. The engine control system of claim 5 , wherein the fuel injector control module increases the fuel injector pulse width when the determined temperature is greater than one of the plurality of temperature thresholds.

8. The engine control system of claim 1 , further comprising:

a combustion mode determination module that determines an operation mode of the HCCI engine,

wherein the operation mode is one of the SI combustion mode, the HCCI combustion mode, and a transition between the modes.

9. The engine control system of claim 8 , wherein the combustion mode determination module determines the operation mode of the HCCI engine based on at least one of a position of a throttle, a status of a spark plug, and a pressure in a cylinder of the HCCI engine.

10. The engine control system of claim 1 , wherein the fuel injector control module controls the fuel injector pulse width by generating a pulse-width modulated (PWM) control signal.

11. A method for controlling a homogenous charge compression ignition (HCCI) engine, comprising:

determining a temperature of a tip of a fuel injector based on a first temperature model when the HCCI engine is operating in an HCCI combustion mode;

determining the temperature of the tip of the fuel injector based on a second temperature model when the HCCI engine is operating in a spark ignition (SI) combustion mode; and

controlling a fuel injector pulse width during an engine on period based on the determined temperature and a predetermined temperature threshold, wherein the fuel injector pulse width increases when the determined temperature is greater than the predetermined temperature threshold.

12. The method of claim 11 , further comprising:

determining the temperature of the tip of the fuel injector based on a third temperature model when the HCCI engine is transitioning between combustion modes.

13. The method of claim 12 , wherein the first temperature model includes a first range of temperatures, wherein the second temperature model includes a second range of temperatures, wherein the third temperature model includes a third range of temperatures, wherein a portions of the first and third ranges of temperatures are less than the second range of temperatures, and wherein a portion of the first range of temperatures is less than the third range of temperatures.

14. The method of claim 12 , further comprising:

determining the temperature of the tip of the fuel injector based on a flow rate of fuel to the fuel injector and one of the first, second, and third temperature models.

15. The method of claim 11 , further comprising:

controlling the fuel injector pulse width based on the determined temperature and a plurality of temperature thresholds.

16. The method of claim 15 , wherein each of the plurality of temperature thresholds corresponds to one of fuel density and delay in one of opening and closing the fuel injector.

17. The method of claim 15 , further comprising:

increasing the fuel injector pulse width when the determined temperature is greater than one of the plurality of temperature thresholds.

18. The method of claim 11 , further comprising:

determines an operation mode of the HCCI engine, wherein the operation mode is one of the SI combustion mode, the HCCI combustion mode, and a transition between the modes.

19. The method of claim 18 , further comprising:

determining the operation mode of the HCCI engine based on at least one of a position of a throttle, a status of a spark plug, and a pressure in a cylinder of the HCCI engine.

20. The method of claim 11 , further comprising:

controlling the fuel injector pulse width by generating a pulse-width modulated (PWM) control signal.

Assignments (8)
RELEASE OF SECURITY INTEREST Recorded Nov 7, 2014
From: WILMINGTON TRUST COMPANY
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 034287/0001 →
CHANGE OF NAME Recorded Feb 10, 2011
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 025781/0299 →
SECURITY AGREEMENT Recorded Nov 8, 2010
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: WILMINGTON TRUST COMPANY
Reel/Frame 025324/0555 →
RELEASE OF SECURITY INTEREST Recorded Nov 5, 2010
From: UAW RETIREE MEDICAL BENEFITS TRUST
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025315/0091 →
RELEASE OF SECURITY INTEREST Recorded Nov 4, 2010
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025246/0234 →
SECURITY AGREEMENT Recorded Feb 25, 2010
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UAW RETIREE MEDICAL BENEFITS TRUST
Reel/Frame 023990/0001 →
SECURITY AGREEMENT Recorded Feb 25, 2010
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 023989/0155 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 8, 2009
From: SHIBATA, JONATHAN T.; RAMAPPAN, VIJAY; BAGNASCO, ANDREW P.
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 023346/0389 →