Method And Apparatus For Using An Accelerometer Signal To Detect Misfiring In An Internal Combustion Engine

• US 20100286891A1
• Filed: 05/26/2010
• Published: 11/11/2010
• Est. Priority Date: 11/29/2007
• Status: Active Grant

• Current Assignee: Westport Fuel Systems Canada Inc. (Westport Fuel Systems, Inc.)
• Original Assignee: Westport Power Inc. (Westport Fuel Systems, Inc.)
• Inventors: Huang, Jian, Mumford, David, Cheung, Duran
• Granted Patent: US 8,108,131 B2
• Time in Patent Office: Days
• US Class Current: 701/102
• CPC Class Codes: F02D 2200/1012 Engine speed gradient
• CPC Class Codes: F02D 2200/1015 Engines misfires
• CPC Class Codes: F02D 35/027 using knock sensors
• CPC Class Codes: F02D 41/1498 measuring engine roughness
• CPC Class Codes: G01M 15/11 by detecting misfire

Abstract

The method comprises operating an engine and collecting a real-time accelerometer signal from an accelerometer sensor. The real-time accelerometer signal is digitized and filtered to isolate data in a frequency range associated with combustion to produce a filtered signal data set. The filtered signal data set is integrated to produce an integrated signal data set, and misfire is detected by comparing the integrated signal data set with a predetermined reference data set associated with the same operating point. The apparatus is a control system for an engine that comprises an accelerometer sensor mounted to the engine; a look-up table in which is stored predetermined reference data sets, in association with predetermined operating conditions; and an electronic controller programmed to carry out the foregoing method.

Claims

1. A method of using a real-time accelerometer signal to detect misfire in an internal combustion engine, said method comprising:

(a) operating said engine at an operating point, and collecting said real-time accelerometer signal from an accelerometer sensor that comprises data characteristic of a combustion parameter;

(b) digitizing and filtering said real-time accelerometer signal to isolate data in a frequency range associated with said combustion parameter to produce a filtered signal data set;

(c) integrating said filtered signal data set to produce an integrated signal data set; and

(d) comparing said integrated signal data set with a predetermined reference data set associated with said operating point, to determine when misfire occurs.

2. The method of claim 1 further comprising converting said filtered signal data set to absolute values prior to integrating it.

3. The method of claim 1 further comprising subtracting a motoring component from said filtered signal data set before integrating it.

4. The method of claim 1 further comprising comparing shapes of a plot of said integrated signal data set with that of said predetermined reference data set and detecting misfire when a predefined characteristic feature of a shape associated with said predetermined reference data set is absent from said integrated signal data set.

5. The method of claim 1 further comprising retrieving said predetermined reference data set from a look-up table.

6. The method of claim 1 further comprising collecting said predetermined reference data set from a calibration engine of the same model and specification as said engine, and storing said predetermined reference data set in a look-up table.

7. The method of claim 6, wherein said predetermined reference data set was collected from said calibration engine when it was firing, and when comparing said integrated data set to said predetermined reference data set, misfire is detected when a plot of said integrated signal data set does not include a slope within a predetermined range defined in relation to a characteristic slope associated with said predetermined reference data set.

8. The method of claim 6 wherein said predetermined reference data set comprises a threshold limit associated with each operating point in said look-up table and misfire is detected when said integrated signal data set comprises data that is below said threshold limit.

9. The method of claim 1 further comprising counting detected misfires, and when more than a predetermined number of misfires are counted, commanding said engine to operate with reduced power output until it can be diagnosed to determine why said misfires have occurred.

10. The method of claim 1 further comprising counting detected misfires, and when more than a predetermined number of misfires are counted, sending a warning to an operator of said engine so that said engine can be diagnosed to determine why said misfires have occurred.

11. The method of claim 1 further comprising counting detected misfires, and when more than a predetermined number of misfires are counted, limiting how many times that the engine can be re-started to prevent said engine from being operated for a prolonged time without being diagnosed to determine why said misfires have occurred.

12. The method of claim 1 further comprising rejecting a determination that misfire has occurred if a secondary indicator of firing indicates that said engine did fire.

13. The method of claim 1 wherein said operating point is defined by engine speed and load.

14. A control system for an internal combustion engine, said control system comprising:

an accelerometer sensor mounted to said internal combustion engine at a location where said accelerometer sensor can detect oscillations that correlate to a combustion parameter;

a look-up table in which is stored a predetermined reference data set, in association with a predetermined operating condition;

an electronic controller programmed to receive a real-time accelerometer signal from said accelerometer sensor when said engine is operating at said predetermined operating condition, to digitize and filter said real-time accelerometer signal to isolate data in a frequency range associated with said combustion parameter to produce a filtered signal data set, to integrate said filtered signal data set to produce an integrated signal data set, and to compare said integrated signal data set to said predetermined reference data set to determine when misfire occurs; and

a signal wire for transmitting said signal from said accelerometer sensor to said electronic controller.

15. The control system of claim 14 wherein said electronic controller is the electronic control unit for said engine.

16. The control system of claim 14 wherein said predetermined reference data set is derived from filtered and integrated accelerometer sensor data that was collected from a calibration engine when it was firing.

17. The control system of claim 14 further comprising a hardware filter between said accelerometer sensor and said electronic controller to pre-process said real-time accelerometer signal.

18. The control system of claim 14 wherein said real-time accelerometer signal is a voltage signal and said electronic controller is programmed to convert said voltage signal to absolute values before integrating it.

19. The control system of claim 14 wherein said electronic controller is programmed to compare shapes of a plot of said integrated signal data set from said real-time accelerometer signal with that of said predetermined reference data set and detecting misfire when a predefined characteristic feature of a shape associated with said reference data set is absent from said integrated signal data set.

20. The control system of claim 14 wherein said predetermined reference data set comprises a characteristic slope associated with a plot of a filtered and integrated data set collected from a calibration engine when it was firing, and said electronic controller is programmed to compute slopes of a plot of said integrated signal data set, and to detect firing when said computed slopes include a slope within a predetermined range defined in relation to said characteristic slope.

21. The control system of claim 14 wherein said predetermined reference data set comprises for each operating point, a threshold limit selected between integrated data associated with firing and integrated data associated with misfiring.

22. The control system of claim 14 wherein said electronic controller is programmed to count detected misfires, and when more than a predetermined number of misfires are counted, said electronic controller is programmed to command said engine to operate with reduced power output until said engine can be diagnosed to determine why said misfires have occurred.

23. The control system of claim 14 wherein said electronic controller is programmed to count detected misfires, and when more than a predetermined number of misfires are counted, said electronic controller is programmed to send a warning to an operator of said engine so that said engine can be diagnosed to determine why said misfires have occurred.

24. The control system of claim 14 wherein said electronic controller is programmed to count detected misfires, and when more than a predetermined number of misfires are counted, said electronic controller is programmed to limit how many times said engine can be re-started to prevent said engine from being operated for a prolonged time without being diagnosed to determine why said misfires have occurred.

25. The control system of claim 14 wherein said electronic controller is programmed to reject a determination that misfire has occurred if a secondary indicator of firing indicates that said engine did fire.