System for controlling an operating condition of an internal combustion engine

• US 6,619,261 B1
• Filed: 03/21/2002
• Issued: 09/16/2003
• Est. Priority Date: 03/21/2002
• Status: Active Grant

• Current Assignee: Cummins Incorporated
• Original Assignee: Cummins Incorporated
• Inventors: Vittorio, David A., Wright, John F., Wang, Yue Yun
• Primary Examiner(s): Denion, Thomas
• Assistant Examiner(s): TRIEU, THAI BA
• Application Number:
  US10/103,427
• Publication Number:
  US 20030177766A1
• Time in Patent Office: 544 Days
• Field of Search: 606/02, 606/01, 606/00, 606/03, 605/99, 723/435, 723/676
• US Class Current: 123/435
• CPC Class Codes: F02B 29/0406 Layout of the intake air cooling or coolant circuit
• CPC Class Codes: F02B 29/0493 Controlling the air charge temperature
• CPC Class Codes: F02D 35/024 using an estimation
• CPC Class Codes: F02D 41/0065 Specific aspects of external EGR control constructional details of EGR system F02M26/00
• CPC Class Codes: F02D 41/1447 with determination means using an estimation
• CPC Class Codes: F02D 41/145 with determination means using an estimation
• CPC Class Codes: F02M 26/05 High pressure loops, i.e. wherein recirculated exhaust gas is taken out from the exhaust system upstream of the turbine and reintroduced into the intake system downstream of the compressor
• CPC Class Codes: F02M 26/10 having means to increase the pressure difference between the exhaust and intake system, e.g. venturis, variable geometry turbines, check valves using pressure pulsations or throttles in the air intake or exhaust system
• CPC Class Codes: F02M 26/23 Layout, e.g. schematics
• CPC Class Codes: F02M 26/33 controlling the temperature of the recirculated gases
• CPC Class Codes: F02M 26/47 the characteristics being temperatures, pressures or flow rates
• CPC Class Codes: F02M 26/61 in response to exhaust pressure

Abstract

A system for controlling an operating condition of an internal combustion engine includes a control mechanism responsive to a final control command to establish an engine control parameter, and a control computer configured to estimate a current value of the operating condition as a function of the final control command. The control computer determines an error value as a difference between an operating condition limit and the current value of the operating condition, and determines an operating condition parameter as function of the error value and of the current value of the operating condition. The control computer further determines a control command limit as a function of the operating condition parameter, and determines the final control command as a function of the control command limit and a default control command to thereby limit the operating condition to the operating condition limit.

Claims

1. System for controlling an operating condition of an internal combustion engine, the system comprising:

a control mechanism responsive to a final control command to establish an engine control parameter;

means for estimating a current value of the operating condition as a function of the final control command;

means for determining an error value as a difference between an operating condition limit and the current value of the operating condition;

means for determining an operating condition parameter as function of the error value and of the current value of the operating condition;

means for determining a control command limit as a function of the operating condition parameter; and

means for determining the final control command as a function of the control command limit and a default control command to thereby limit the operating condition to the operating condition limit.

2. The system of claim 1 further including a memory unit having the operating condition limit stored therein.

3. The system of claim 1 wherein the final control command is a final fuel command and the control mechanism is a fuel system responsive to the final fuel command to supply fuel to the engine.

4. The system of claim 3 wherein the operating condition is engine exhaust temperature, and the operating condition limit is an engine exhaust gas temperature limit.

5. The system of claim 3 wherein the operating condition is turbocharger turbine temperature, and the operating condition limit is a turbocharger turbine temperature limit.

6. The system of claim 3 wherein the operating condition is peak cylinder pressure, and the operating condition limit is a peak cylinder pressure limit.

7. The system of claim 5 wherein said means for estimating a current value of the operating condition as a function of the final control command includes:

means for estimating engine exhaust temperature as a function of the final fuel command; and

means for determining turbocharger turbine temperature as a function of the engine exhaust temperature.

8. The system of claim 7 wherein said means for determining an operating condition parameter as function of the error value and of the current value of the operating condition includes:

a gain unit producing a modified error value as a product of said error value and a gain value; and

a summation unit producing said operating condition parameter as a sum of said modified error value and the current value of the turbocharger turbine temperature.

9. The system of claim 1 further including a turbocharger having a variable geometry (VG) turbine;

and wherein the final control command is a final VG position command and the control mechanism is a VG control mechanism responsive to the final VG position command to establish a corresponding swallowing capacity of the turbine.

10. The system of claim 9 wherein the operating condition is rotational speed of the turbocharger, and the operating condition limit is a turbocharger speed limit.

11. System for controlling an operating condition of an internal combustion engine, the system comprising:

a control mechanism responsive to a final control command to establish an engine control parameter; and

a control computer configured to estimate a current value of the operating condition as a function of the final control command, said control computer determining an error value as a difference between an operating condition limit and the current value of the operating condition and determining an operating condition parameter as function of the error value and of the current value of the operating condition, said control computer determining a control command limit as a function of the operating condition parameter and determining the final control command as a function of the control command limit and a default control command to thereby limit the operating condition to the operating condition limit.

12. The system of claim 11 wherein the final control command is a final fuel command and the control mechanism is a fuel system responsive to the final fuel command to supply fuel to the engine.

13. The system of claim 12 wherein the operating condition is engine exhaust temperature, and the operating condition limit is an engine exhaust gas temperature limit.

14. The system of claim 12 wherein the operating condition is turbocharger turbine temperature, and the operating condition limit is a turbocharger turbine temperature limit.

15. The system of claim 12 wherein the operating condition is peak cylinder pressure, and the operating condition limit is a peak cylinder pressure limit.

16. The system of claim 12 wherein said control computer is operable to estimate a current value of the operating condition as a function of the final control command by estimating engine exhaust temperature as a function of the final fuel command, and determining turbocharger turbine temperature as a function of the engine exhaust temperature.

17. The system of claim 16 wherein said control computer is operable to determine the operating condition parameter as function of the error value and of the current value of the operating condition by determining a modified error value as a product of said error value and a gain value, and producing said operating condition parameter as a sum of said modified error value and the current value of the turbocharger turbine temperature.

18. The system of claim 11 further including a turbocharger having a variable geometry (VG) turbine;

and wherein the final control command is a final VG position command and the control mechanism is a VG control mechanism responsive to the final VG position command to establish a corresponding swallowing capacity of the turbine.

19. The system of claim 18 wherein the operating condition is rotational speed of the turbocharger, and the operating condition limit is a turbocharger speed limit.

20. A method of controlling an operating condition of an internal combustion engine, the method comprising the steps of:

estimating a current value of the operating condition as a function of a final control mechanism command;

determining an error value as a difference between an operating condition limit and the current value of the operating condition;

determining an operating condition parameter as a function of the error value and of the operating condition limit;

determining a control mechanism limit value as a function of the operating condition parameter; and

determining the final control mechanism command as a minimum of a default control mechanism command and the control mechanism limit value to thereby limit the operating condition to the operating condition limit.

21. The method of claim 20 wherein the final control mechanism command is a final fueling command for fueling the engine.

22. The method of claim 21 wherein the operating condition is engine exhaust temperature, and the operating condition limit is an engine exhaust temperature limit.

23. The method of claim 21 wherein the operating condition is turbocharger turbine temperature, and the operating condition limit is a turbocharger turbine temperature limit.

24. The method of claim 21 wherein the operating condition is peak cylinder pressure, and the operating condition limit is a peak cylinder pressure limit.

25. The method of claim 20 wherein the final control mechanism command is a variable geometry turbocharger position command for establishing a turbocharger swallowing capacity.

26. The method of claim 25 wherein the operating condition is turbocharger rotational speed, and the operating condition limit is a turbocharger speed limit.