Engine diagnostics with skip fire control
US-9581098-B2 · Feb 28, 2017 · US
US9784644B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9784644-B2 |
| Application number | US-201514880652-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 12, 2015 |
| Priority date | Oct 16, 2014 |
| Publication date | Oct 10, 2017 |
| Grant date | Oct 10, 2017 |
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A variety of methods and arrangements for detecting misfire and other engine-related errors are described. In one aspect, a window is assigned to a target firing opportunity for a target working chamber. There is an attempt to fire a target working chamber during the target firing opportunity. A change in an engine parameter (e.g., crankshaft angular acceleration) is measured during the window. A model (e.g., a pressure model) is used to help determine an expected change in the engine parameter during the target firing opportunity. Based on a comparison of the expected change and the measured change in the engine parameter, a determination is made as to whether an engine error (e.g., misfire) has occurred.
Opening claim text (preview).
What is claimed is: 1. A method for detecting misfire in an engine, the engine having a plurality of working chambers and being operated in a skip fire manner, the method comprising: assigning a window to a target firing opportunity; attempting to fire a target working chamber during the target firing opportunity; measuring a change in an engine parameter during the target firing opportunity; using a multi-cylinder pressure model to help determine an expected change in the engine parameter during the target firing opportunity wherein the pressure model involves estimating pressure in a skipped working chamber; and based on a comparison between the expected change and the measured change, determining whether the target working chamber misfired. 2. A method as recited in claim 1 wherein the engine parameter is crankshaft acceleration. 3. A method as recited in claim 1 wherein the multi-cylinder pressure model involves modeling pressure within each working chamber during a time period between intake valve closure and exhaust valve opening of the target firing opportunity. 4. A method as recited in claim 1 wherein the pressure model takes into account at least one selected from the group consisting of a rise of temperature in a working chamber due to combustion, fuel mass used to fuel combustion, energy conversion efficiency, ignition timing, residual fraction, leakage rate, fuel properties such as heating value, and total mass of mixture in a working chamber. 5. A method as recited in claim 1 further comprising using the pressure model to determine an expected torque generated by the working chambers of the engine during the target firing opportunity. 6. A method as recited in claim 5 wherein the determination of the expected torque is based on at least one selected from the group consisting of crankcase pressure, crank radius, pin offset, connecting rod length and piston face cross-sectional area. 7. A method as recited in claim 5 wherein: the expected torque, which is determined based on the pressure model, is used to determine an expected crankshaft acceleration; and the determination of the expected crankshaft acceleration is based on at least one selected from the group consisting of engine speed, intake manifold absolute pressure, intake manifold air temperature, air per cylinder, cam phasing, connecting rod length, compression ratio, valve opening window, pin offset, injection timing, spark timing, the moment of inertia of a crankshaft, the moment of inertia of a flywheel, the moment of inertia of a rotating component, a mass of a piston, a mass of a ring and a mass of a linear motion component. 8. A method as recited in claim 1 wherein the determination of the misfire is based at least in part on A, B and A′ wherein A is the expected change in the engine parameter based on the model, A′ is one of an expected change in the engine parameter based on mass air charge and a low-pass filtered mean of A and B is the measured change in the engine parameter. 9. A method as recited in claim 8 wherein the determination of the misfire is based at least in part on A - B A ′ . 10. A method as recited in claim 8 wherein the determination of the misfire further includes: calculating a value Y that is based on A, B and A′; and calculating a value X that is based on an exponentiation of Y; determining whether a misfire has occurred in the target working chamber based at least in part on the value X. 11. A method as recited in claim 1 further comprising: detecting a first offset between the estimated expected change and the measured change in the engine parameter; adjusting the pressure model based on the first offset; and repeating the pressure model usage and measurement operations, thereby providing a second expected change and a second measured change in the engine parameter wherein a second offset between the second expected change and the second measured change is reduced relative to the first offset as a result of the model adjustment. 12. A misfire detection system for determining whether a particular working chamber in an engine has misfired, the engine being operated in a skip fire manner, the misfire detection system comprising: an engine parameter measurement module that is arranged to: assign a window to a target firing opportunity; and measure a change in an engine parameter during the target firing opportunity; and a misfire detection module that is arranged to: use a pressure model to help determine an expected change in the engine parameter during the target firing opportunity wherein the pressure model involves estimating pressure in a skipped working chamber; and determine whether the target working chamber misfired based on a comparison between the expected change and the measured change. 13. A misfire detection system as recited in claim 12 wherein the engine parameter is crankshaft acceleration. 14. A misfire detection system as recited in claim 12 wherein the pressure model involves modeling pressure within a working chamber during a time period between intake valve closure and exhaust valve opening. 15. A misfire detection system as recited in claim 12 wherein the multi-cylinder pressure model takes into account at least one selected from the group consisting of a rise of temperature in a working chamber due to combustion, fuel mass used to fuel combustion, energy conversion efficiency, ignition timing, residual fraction, leakage rate, fuel properties such as heating value, and total mass of mixture in a working chamber. 16. A misfire detection system as recited in claim 12 wherein the misfire detection module is further arranged to determine an expected torque generated by the working chambers of the engine during the firing opportunity. 17. A misfire detection system as recited in claim 16 wherein the determination of the expected torque using the pressure model is based on at least one selected from the group consisting of crankcase pressure, crank radius, pin offset, connection rod length and piston face cross-sectional area. 18. A misfire detection system as recited in claim 16 wherein: the expected torque, which is determined based on the pressure model, is used to determine an expected crankshaft acceleration; and the determination of the expected crankshaft acceleration is based on at least one selected from the group consisting of engine speed, intake manifold absolute pressure, intake manifold air temperature, air per cylinder, cam phasing, connecting rod length, compression ratio, valve opening window, pin offset, injection timing, spark timing, the moment of inertia of a crankshaft, the moment of inertia of a flywheel, the moment of inertia of a rotating component, a mass of a piston, a mass of a ring and a mass of a linear motion component. 19. A misfire detection system as recited in claim 12 wherein the misfire determination is based at least in part on A, B and A′ wherein A is the expected change in the engine parameter based on the model, A′ is one of a low-pass filtered mean of A and an expected change in the engine parameter based on mass air charge, and B is the measured change in the engine parameter. 20. A misfire detection system as recited in
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