Method for detection of abnormal combustion for internal combustion engines

• US 8,677,975 B2
• Filed: 09/18/2009
• Issued: 03/25/2014
• Est. Priority Date: 09/18/2008
• Status: Expired due to Fees

• Current Assignee: IFP Energies Nouvelles
• Original Assignee: IFP Energies Nouvelles
• Inventors: Auclair, Dominique, Duval, Laurent, Pagot, Alexandre, Zaccardi, Jean-Marc
• Primary Examiner(s): Cronin, Stephen K
• Assistant Examiner(s): VILAKAZI, SIZO BINDA
• Application Number:
  US12/562,339
• Publication Number:
  US 20100077992A1
• Time in Patent Office: 1,649 Days
• Field of Search: 123/434, 123/435, 123/479, 123/585, 123/630, 123/406.21, 123/406.29, 123/406.47, 123/436, 123/406.34, 73/350.9, 701/111
• US Class Current: 123/435
• CPC Class Codes: F02D 19/12 peculiar to engines working with non-fuel substances or with anti-knock agents, e.g. with anti-knock fuel
• CPC Class Codes: F02D 35/023 by determining the cylinder pressure
• CPC Class Codes: F02D 35/024 using an estimation
• CPC Class Codes: F02D 41/0025 Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
• CPC Class Codes: F02D 41/402 Multiple injections

Abstract

A method for detection of abnormal combustion for internal combustion engines is disclosed. A physical model is chosen that describes, as a function of the angle α of rotation of the engine crankshaft, the development of pressure in the cylinder during combustion without any pre-ignition phenomenon. The cylinder pressure P_e(α) is estimated using this model and the intake pressure is measured. The beginning of abnormal combustion is detected by comparing a first value of a variable calculated using the measurement of the cylinder pressure, to a second value of the variable calculated using the estimation of the cylinder pressure. The amplitude of the pre-ignition is determined by repeating these steps for a defined number of crankshaft angles. Then the progress of the abnormal combustion detected in the combustion chamber is controlled as a function of the amplitude of the pre-ignition phenomenon.

Claims

1. A method for controlling combustion of a supercharged internal combustion engine with controlled ignition, in which abnormal combustion is detected in a combustion chamber of at least one cylinder of the engine by a continuous measurement of pressure inside the at least one cylinder, comprising:

a) using a computer to estimate cylinder pressure with a physical model describing, as a function of an angle of rotation of a crankshaft of the engine, development of pressure in the at least one cylinder during one combustion without any pre-ignition;

b) estimating a cylinder pressure, starting from the model and the measurement of intake pressure to the at least one cylinder;

c) detecting a start of the abnormal combustion by comparing at least one first value of a variable calculated using measurement of the pressure in the at least one cylinder and at least one second value of the variable calculated using an estimation of the pressure in the at least one cylinder;

d) determining an amplitude of pre-ignition by repeating steps b) and c) for a number of crankshaft angles; and

e) controlling progress of the abnormal combustion detected in the combustion chamber according to the amplitude of the pre-ignition.

2. A method according to claim 1, wherein:

the physical model describes a variation in pressure in the at least one cylinder as a function of the intake pressure and volume of the at least one cylinder.

3. A method according to claim 1, wherein:

progress of the abnormal combustion is controlled by introducing into the combustion chamber an agent containing one of fuel, water, or carbon dioxide.

4. A method according to claim 2, wherein:

progress of the abnormal combustion is controlled by introducing into the combustion chamber an agent containing one of fuel, water, or carbon dioxide.

5. A method according to claim 1, wherein:

progress of the abnormal combustion is controlled by causing pressure to drop in the at least one cylinder.

6. A method according to claim 2, wherein:

progress of the abnormal combustion is controlled by causing pressure to drop in the at least one cylinder.

7. A method according to claim 1, wherein:

progress of the abnormal combustion is controlled by opening at least one additional valve causing pressure to drop in the at least one chamber.

8. A method according to claim 2, wherein:

progress of the abnormal combustion is controlled by opening at least one additional valve causing pressure to drop in the at least one chamber.

9. A method according to claim 1, wherein:

progress of the abnormal combustion is controlled by opening at least one additional valve causing pressure to drop in the at least one chamber.

10. A method according to claim 2, wherein:

progress of the abnormal combustion is controlled by opening at least one additional valve causing pressure to drop in the at least one chamber.

11. A method according to claim 1, wherein:

the variable is a cylinder pressure gradient and in which a start of abnormal combustion is detected by analyzing a sign of the gradient.

12. A method according to claim 2, wherein:

the variable is a cylinder pressure gradient and in which a start of abnormal combustion is detected by analyzing a sign of the gradient.

13. A method according to claim 3, wherein:

the variable is a cylinder pressure gradient and in which a start of abnormal combustion is detected by analyzing a sign of the gradient.

14. A method according to claim 4, wherein:

the variable is a cylinder pressure gradient and in which a start of abnormal combustion is detected by analyzing a sign of the gradient.

15. A method according to claim 5, wherein:

the variable is a cylinder pressure gradient and in which a start of abnormal combustion is detected by analyzing a sign of the gradient.

16. A method according to claim 6, wherein:

the variable is a cylinder pressure gradient and in which a start of abnormal combustion is detected by analyzing a sign of the gradient.

17. A method according to claim 7, wherein:

the variable is a cylinder pressure gradient and in which a start of abnormal combustion is detected by analyzing a sign of the gradient.

18. A method according to claim 8, wherein:

the variable is a cylinder pressure gradient and in which a start of abnormal combustion is detected by analyzing a sign of the gradient.

19. A method according to claim 9, wherein:

the variable is a cylinder pressure gradient and in which a start of abnormal combustion is detected by analyzing a sign of the gradient.

20. A method according to claim 10, wherein:

the variable is a cylinder pressure gradient and in which a start of abnormal combustion is detected by analyzing a sign of the gradient.

21. A method according to claim 1, wherein:

the variable is chosen from among the following variables;

cylinder pressure gradient, energy release, temperature of cool gas, and a logarithm of the cylinder pressure.

22. A method according to claim 2, wherein:

the variable is chosen from among the following variables;

cylinder pressure gradient, energy release, temperature of cool gas, and a logarithm of the cylinder pressure.

23. A method according to claim 3, wherein:

the variable is chosen from among the following variables;

cylinder pressure gradient, energy release, temperature of cool gas, and a logarithm of the cylinder pressure.

24. A method according to claim 4, wherein:

the variable is chosen from among the following variables;

cylinder pressure gradient, energy release, temperature of cool gas, and a logarithm of the cylinder pressure.

25. A method according to claim 5, wherein:

the variable is chosen from among the following variables;

cylinder pressure gradient, energy release, temperature of cool gas, and a logarithm of the cylinder pressure.

26. A method according to claim 6, wherein:

the variable is chosen from among the following variables;

cylinder pressure gradient, energy release, temperature of cool gas, and a logarithm of the cylinder pressure.

27. A method according to claim 7, wherein:

the variable is chosen from among the following variables;

cylinder pressure gradient, energy release, temperature of cool gas, and a logarithm of the cylinder pressure.

28. A method according to claim 8, wherein:

the variable is chosen from among the following variables;

cylinder pressure gradient, energy release, temperature of cool gas, and a logarithm of the cylinder pressure.

29. A method according to claim 9, wherein:

the variable is chosen from among the following variables;

cylinder pressure gradient, energy release, temperature of cool gas, and a logarithm of the cylinder pressure.

30. A method according to claim 10, wherein:

the variable is chosen from among the following variables;

cylinder pressure gradient, energy release, temperature of cool gas, and a logarithm of the cylinder pressure.

31. A method according to claim 11, wherein:

the variable is chosen from among the following variables;

cylinder pressure gradient, energy release, temperature of cool gas, and a logarithm of the cylinder pressure.

32. A method according to claim 1, wherein:

the measured and the estimated variables are compared.

33. A method according to claim 32, wherein:

the measured and the estimated variables are compared using thresholds.