US20200063683A1 - System and method for enhancing robustness of engine component diagnostic using compensation learning strategy - Google Patents
System and method for enhancing robustness of engine component diagnostic using compensation learning strategy Download PDFInfo
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- US20200063683A1 US20200063683A1 US16/110,404 US201816110404A US2020063683A1 US 20200063683 A1 US20200063683 A1 US 20200063683A1 US 201816110404 A US201816110404 A US 201816110404A US 2020063683 A1 US2020063683 A1 US 2020063683A1
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/24—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means
- F02D41/2406—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means using essentially read only memories
- F02D41/2425—Particular ways of programming the data
- F02D41/2429—Methods of calibrating or learning
- F02D41/2451—Methods of calibrating or learning characterised by what is learned or calibrated
- F02D41/2464—Characteristics of actuators
- F02D41/2467—Characteristics of actuators for injectors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/04—Introducing corrections for particular operating conditions
- F02D41/06—Introducing corrections for particular operating conditions for engine starting or warming up
- F02D41/062—Introducing corrections for particular operating conditions for engine starting or warming up for starting
- F02D41/064—Introducing corrections for particular operating conditions for engine starting or warming up for starting at cold start
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/18—Circuit arrangements for generating control signals by measuring intake air flow
- F02D41/182—Circuit arrangements for generating control signals by measuring intake air flow for the control of a fuel injection device
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/22—Safety or indicating devices for abnormal conditions
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/24—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means
- F02D41/2406—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means using essentially read only memories
- F02D41/2425—Particular ways of programming the data
- F02D41/2429—Methods of calibrating or learning
- F02D41/2438—Active learning methods
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/24—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means
- F02D41/2406—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means using essentially read only memories
- F02D41/2425—Particular ways of programming the data
- F02D41/2429—Methods of calibrating or learning
- F02D41/2451—Methods of calibrating or learning characterised by what is learned or calibrated
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/24—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means
- F02D41/2406—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means using essentially read only memories
- F02D41/2425—Particular ways of programming the data
- F02D41/2429—Methods of calibrating or learning
- F02D41/2451—Methods of calibrating or learning characterised by what is learned or calibrated
- F02D41/2464—Characteristics of actuators
- F02D41/2467—Characteristics of actuators for injectors
- F02D41/247—Behaviour for small quantities
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/24—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means
- F02D41/2406—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means using essentially read only memories
- F02D41/2425—Particular ways of programming the data
- F02D41/2429—Methods of calibrating or learning
- F02D41/2477—Methods of calibrating or learning characterised by the method used for learning
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/3005—Details not otherwise provided for
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/3011—Controlling fuel injection according to or using specific or several modes of combustion
- F02D41/3017—Controlling fuel injection according to or using specific or several modes of combustion characterised by the mode(s) being used
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/38—Controlling fuel injection of the high pressure type
- F02D41/3809—Common rail control systems
- F02D41/3827—Common rail control systems for diesel engines
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/38—Controlling fuel injection of the high pressure type
- F02D41/3809—Common rail control systems
- F02D41/3836—Controlling the fuel pressure
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/38—Controlling fuel injection of the high pressure type
- F02D41/40—Controlling fuel injection of the high pressure type with means for controlling injection timing or duration
- F02D41/402—Multiple injections
- F02D41/403—Multiple injections with pilot injections
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/38—Controlling fuel injection of the high pressure type
- F02D41/40—Controlling fuel injection of the high pressure type with means for controlling injection timing or duration
- F02D41/402—Multiple injections
- F02D41/405—Multiple injections with post injections
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/22—Safety or indicating devices for abnormal conditions
- F02D2041/224—Diagnosis of the fuel system
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/38—Controlling fuel injection of the high pressure type
- F02D2041/389—Controlling fuel injection of the high pressure type for injecting directly into the cylinder
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2200/00—Input parameters for engine control
- F02D2200/02—Input parameters for engine control the parameters being related to the engine
- F02D2200/06—Fuel or fuel supply system parameters
- F02D2200/0602—Fuel pressure
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2200/00—Input parameters for engine control
- F02D2200/02—Input parameters for engine control the parameters being related to the engine
- F02D2200/06—Fuel or fuel supply system parameters
- F02D2200/0614—Actual fuel mass or fuel injection amount
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/40—Engine management systems
Definitions
- the present disclosure relates to a system and a method for enhancing robustness of an internal combustion engine component diagnostic using compensation learning strategy.
- Modern internal combustion engines typically employ control systems to monitor and regulate engine performance by implementing diagnostic algorithms for various engine components, such as sensors and actuators. Such learning strategies are frequently used to compensate for performance deviations due to part-to-part variation and component aging compared to nominal component behavior.
- such strategies include a learning phase in which the component deviation is measured and stored, and a release phase in which a learning compensation is applied to a control signal or command.
- a learning function may be used to perform a diagnostic observation of a second component parameter that is physically linked to a first component parameter already subject to learning compensation.
- Such use of the learning function for a particular component may result in an influence of the learning compensation of the first component parameter on the diagnostic observation of the second component parameter.
- a removal of the learning compensation of the first component parameter during the diagnostic observation of the second parameter crates an intrusive test that may lead to certain performance targets for the subject component not being met.
- a method using compensation learning strategy for a diagnostic of an internal combustion engine component includes operating the engine component via an actuator command issued by an electronic controller. Specifically, the actuator command is used to establish a first operating parameter representative of a first mode of component operation. The method also includes identifying, via the electronic controller, a drift in the first operating parameter negatively affecting the first mode of operation. The method additionally includes determining, via the electronic controller, a command compensation to the actuator command to counteract the drift in the first operating parameter during the first mode of operation. The method also includes determining, via the electronic controller, a parameter compensation to the first operating parameter using the determined compensation to the actuator command. The method additionally includes applying the determined parameter compensation directly to the first operating parameter.
- the method also includes operating the engine component using the actuator command to establish a second operating parameter representative of a second mode of component operation. Furthermore, the method includes identifying, via the electronic controller, a drift in the second operating parameter negatively affecting the second mode of operation while applying the determined parameter compensation directly to the first operating parameter and without applying the determined command compensation to the actuator command.
- Determining the parameter compensation may include translating the command compensation into a delta reference compensation value to apply directly to the first operating parameter while identifying the drift in the second operating parameter.
- Translating the command compensation into the delta reference compensation value may include using a mathematical relationship programmed into the controller.
- Translating the command compensation into the delta reference compensation value may include accessing an empirically collected look-up table of values of determined compensation to the actuator command versus delta reference compensation values.
- the engine may be a compression ignition engine and the component may be an injector configured to inject fuel into the engine.
- the first operating parameter may be a relatively small injection quantity and the first mode of operation is pilot fuel injection.
- the second operating parameter may be a relatively large injection quantity and the second mode of operation is main combustion fuel injection.
- Identifying the drift in the second operating parameter while applying the determined parameter compensation directly to the first operating parameter and without applying the determined command compensation to the actuator command may include maintaining pre-combustion temperature in the combustion chamber and maintaining combustion stability in the engine.
- the second operating parameter may be a relatively small injection quantity and the second mode of operation may be post-combustion fuel injection.
- the engine may include an exhaust after-treatment (AT) device configured to reduce engine exhaust gas emissions.
- AT exhaust after-treatment
- identifying the drift in the second operating parameter while applying the determined parameter compensation directly to the first operating parameter and without applying the determined command compensation to the actuator command may include at least one of maintaining effective operation of the AT device and maintaining reduction of engine exhaust gas emissions thereby.
- a system using compensation learning strategy for a diagnostic of an internal combustion engine component, such as via an electronic controller performing the above-described method, is also disclosed.
- a vehicle may employ such a system.
- FIG. 1 is a schematic plan view of a vehicle having an internal combustion engine connected to an exhaust system having an after-treatment (AT) system with a number of AT devices for reducing exhaust emissions and including a system using an electronic controller to perform compensation learning strategy for a diagnostic of an engine component.
- AT after-treatment
- FIG. 2 is a close-up schematic illustration of an engine cylinder having a combustion chamber and a representative engine component in the internal combustion engine shown in FIG. 1 .
- FIG. 3 is a flow diagram of a method using compensation learning strategy for a diagnostic of an internal combustion engine component shown in FIGS. 1 and 2 .
- FIG. 1 schematically depicts a motor vehicle 10 .
- the vehicle 10 includes an internal combustion engine 12 configured to propel the vehicle via driven wheels 14 .
- the internal combustion engine 12 may be a compression-ignition or diesel type of an engine.
- internal combustion in a diesel engine 12 occurs when a specific amount of ambient intake airflow 16 is mixed with a metered amount of fuel 18 supplied from a fuel tank 20 and the resultant air-fuel mixture is compressed inside combustion chamber 13 A of the engine's cylinders 13 (shown in FIG. 2 ).
- the engine 12 may include an exhaust manifold 22 configured to collect exhaust gas from the engine's cylinders 13 .
- the engine also includes a turbocharger 24 in fluid communication with cylinders 13 , such as via the exhaust manifold 22 .
- the turbocharger 24 is energized or driven by a flow of exhaust gas, specifically the exhaust gas 26 released by individual cylinders 13 of the engine 12 , such as through the exhaust manifold 22 , following each combustion event.
- the turbocharger 24 is connected to an exhaust system 28 that receives exhaust gas 26 and eventually releases the exhaust gas to the ambient, typically on a side or aft of the vehicle 10 .
- the turbocharger 24 also uses the exhaust gas 26 flow to pressurize the intake airflow 16 .
- the vehicle 10 also includes an engine exhaust after-treatment (AT) system 30 .
- the AT system 30 includes a number of exhaust after-treatment devices configured to methodically remove largely carbonaceous particulate byproducts and emission constituents of engine combustion from the exhaust gas 26 . As shown in FIGS. 1 and 2 , the AT system 30 operates as part of the exhaust system 28 .
- the AT system 30 includes at least one AT device, such as a first AT device 32 arranged downstream of the turbocharger 24 and a second AT device 34 arranged downstream of the first AT device.
- the first AT device 32 may be close-coupled to the turbocharger 24 and arranged inside an engine compartment 11 of the vehicle 10 for close proximity to the engine 12 .
- Such close-coupling of the first AT device 32 to the engine 12 may provide a compact packaging arrangement that minimizes time for activation, i.e., light-off, of the AT system 30 in after-treatment of the exhaust gas 26 following a cold-start of the engine 12 .
- the AT system 30 may also include additional AT devices (not shown) positioned in the exhaust gas flow downstream of the first and second AT devices 32 , 34 .
- the first AT device 32 may be a diesel oxidation catalyst (DOC), while the second AT device 34 may be a selective catalytic reduction (SCR) catalyst and filter.
- the primary function of the DOC is reduction of carbon monoxides (CO) and non-methane hydrocarbons (NMHC).
- the DOC is additionally configured to generate nitrogen dioxide (NO 2 ), which may be used by the SCR arranged remotely downstream of the DOC.
- the primary function of the SCR is to reduce a concentration of nitrogen oxides (NO X ) in the exhaust gas 26 .
- the AT system 30 also includes the exhaust passage 22 A, which may be part of the exhaust manifold 22 , configured to carry the flow of exhaust gas 26 to the turbocharger 24 from the engine's cylinders 13 , and an exhaust passage 36 configured to carry the flow of exhaust gas 26 aft of the turbocharger 24 to the first AT device 32 .
- the intake airflow 16 is supplied to the engine 12 via an intake passage 38 for mixing with the fuel 18 , to generate combustion, thereby operate the engine, and generate a flow of the exhaust gas 26 .
- the engine 12 may include an engine component 40 used to operate the engine component using an actuator command via a control signal issued by an electronic controller to be described in detail below.
- the engine component 40 may be a component employing a learning strategy diagnosing a calibrated zero point and span of control that would benefit from self-calibration without shut-off.
- the engine component 40 may be a fuel injector supplied with the fuel 18 via an injector rail 42 and employed to inject the fuel 18 into the engine's cylinders 13 .
- the engine 12 may include other examples of the engine component 40 , such as sensors and actuators, the remainder of the present disclosure will concentrate on the fuel injector embodiment of the subject component. Accordingly, from hereon, the fuel injector will be labeled with the numeral 40 .
- the internal combustion engine 12 may generally have a multi-cylinder configuration employing at least one such fuel injector 40 per each cylinder 13 .
- An airflow sensor 44 may be arranged in the intake passage 38 and configured to detect an amount of the airflow 16 supplied to the engine 12 during its operation and such data may be used for controlling the amount of fuel 18 injected into the cylinders 13 .
- An exhaust gas passage 46 is configured to receive treated exhaust gas 26 A aft of the second AT device 34 and pass the treated exhaust gas through the rest of the exhaust system 28 and the remainder of the AT system 30 .
- the vehicle 12 also includes a system 48 configured to perform a diagnostic of the component 40 using compensation learning strategy that will be described in detail below.
- the system 48 is further configured to reduce an influence of the learning compensation of one component 40 operating parameter on the diagnostic observation of another component 40 operating parameter, without detrimentally impacting performance of the subject component.
- the vehicle 10 additionally includes an electronic controller 50 configured to regulate the AT system 30 , and, as such, the controller may be part of the AT system.
- the controller 50 is part of the system 48 and may be a stand-alone unit, or be part of an electronic control unit (ECU) that regulates the operation of engine 12 .
- the controller 50 is arranged on the vehicle 10 and includes a processor and a readily accessible non-transitory memory. Instructions for controlling operation of the AT system 30 are programmed or recorded in the memory of the controller 50 , and the processor is configured to execute the instructions from the memory during operation of the vehicle 10 .
- the controller 50 is generally programmed to regulate the injectors 40 for injecting fuel 18 into the cylinders 13 to enable operation of the engine 12 .
- the controller 50 is programmed to operate the injectors 40 during a particular first event, such as during a cold start, using an actuator command 52 , for example, communicated via control signal, to establish a first operating parameter 54 representative of a first mode of component 40 , i.e., injector, operation.
- the first operating parameter is a relatively small injection quantity, for example, in the range of 1-3 mm 3 /stroke for a single injection per engine stroke in an individual cylinder.
- the first mode of operation is pilot fuel injection activated around 10 degrees before top dead center (BTDC) to warm up the combustion chamber 13 A.
- the first mode of injector 40 operation may, for example, be defined by the small injection quantity in the range of 1-3 mm 3 /stroke (of the injector) for a single injection per engine stroke, as described above, and thus configured to support a cold start of the engine 12 .
- the controller 50 is also programmed to identify or diagnose a drift in the first operating parameter 54 negatively affecting, i.e., causing a fault in, the first mode of injector 40 operation.
- the controller 50 is additionally programmed to determine a command compensation 56 to the actuator command 52 to counteract the drift in the first operating parameter 54 during the first mode of injector 40 operation.
- the controller 50 is also programmed to determine a parameter compensation 58 to the first operating parameter 54 using the determined compensation 56 to the actuator command 52 .
- Such determination of parameter compensation 58 may include translating the command compensation 56 into a delta reference compensation 60 value to apply directly to the first operating parameter 54 .
- the controller 50 is additionally programmed to apply the determined parameter compensation 58 directly to the first operating parameter 54 .
- the determined parameter compensation 58 is applied directly to the first operating parameter 54 to counteract the identified drift in the first operating parameter during the first mode of operation of the injector 40 without applying the determined command compensation 56 directly to the actuator command 52 .
- drift in an operating parameter indicates loss of precision in the achievement of the subject parameter, i.e., straying of the parameter from its target value.
- drift in the first operating parameter during the first mode of operation of the injector 40 may indicate an incorrect amount of fuel 18 being injected into the cylinders 13 . Injection of incorrect amount of fuel 18 into the cylinders 13 may be detrimental to the engine's combustion efficiency, and to operation of the AT devices 32 , 34 in removing particulate byproducts and emission constituents of combustion from the exhaust gas 26 .
- the controller 50 is also programmed to operate the injector 40 using the actuator command 52 to establish a second operating parameter 62 representative of a second mode of injector 40 operation.
- the second operating parameter 62 may be a relatively large injection quantity, for example, in the range of 5-150 mm 3 /stroke, cumulative amount of fuel injected per engine cycle, multiple injections per stroke for multiple cylinders.
- the second mode of operation is main combustion fuel injection activated around 2-5 degrees BTDC (with the main injection in a typical diesel engine generally occurring across a full range of 20 degrees BTDC-5 degrees ATDC) to initiate full combustion in the combustion chamber 13 A.
- the second mode of injector 40 operation may, for example, be defined by the large injection quantity in the range of 5-150 mm 3 /stroke, and configured to support operation of the engine 12 over a regular operating temperature range and generate engine torque in response to operator request.
- Other examples of main combustion fuel injection may include particular operating conditions such as engine 12 cranking and fueling during transient maneuvers.
- the second operating parameter 62 may be a relatively small injection quantity, for example, in the range of 1-3 mm 3 /stroke for a single injection per engine stroke in an individual cylinder.
- the second mode of injector 40 operation may be post-combustion fuel injection activated around 100 milliseconds or 10-30 degrees after top dead center (ATDC).
- the post-combustion fuel injection may, for example, be defined by the small injection quantity in the range of 1-3 mm 3 /stroke, and configured to maintain effective operating temperature of the AT devices 32 , 34 following main combustion in cylinders 13 .
- identification of the drift in the second operating parameter 62 while applying the determined parameter compensation 58 directly to the first operating parameter 54 without applying the determined command compensation 56 to the actuator command 52 includes at least one of maintaining pre-combustion temperature in the combustion chambers 13 A and maintaining combustion stability in the engine 12 .
- the controller 50 is programmed to identify or diagnose a drift in the second operating parameter 62 negatively affecting the second mode of injector 40 operation. Identification of the drift in the second operating parameter 62 is intended to take place while the determined parameter compensation is applied directly to the first operating parameter 54 and without applying the determined command compensation 56 to the actuator command 52 . Accordingly, the controller 50 is configured to perform a non-intrusive diagnostic of the second operating parameter 62 drift during the second mode of operation, i.e., the compensated first operating parameter 54 and the first mode of operation are not affected during the second operating parameter 62 diagnostic. Such diagnostic further permits the controller to identify the health and capability of the component, e.g., injector, 40 to support the second mode of injector operation, without detrimentally affecting the injector's ability to support the first mode of operation.
- a non-intrusive diagnostic of the second operating parameter 62 drift during the second mode of operation i.e., the compensated first operating parameter 54 and the first mode of operation are not affected during the second operating parameter 62 diagnostic.
- the controller 50 may be additionally configured to determine and apply compensation to the second operating parameter 62 to counteract the identified drift during the second mode of operation without affecting the first mode of injector 40 operation.
- the controller 50 is configured to maintain effective operation of the AT device(s) 32 , 34 and maintain reduction of engine exhaust gas emissions thereby.
- the determination of the parameter compensation 58 may include translating the command compensation 56 into a delta reference compensation value 64 to be applied directly to the first operating parameter 54 .
- the delta reference compensation value 64 is intended to provide a specific incremental change directly to the first operating parameter 54 , bypassing modification to the actuator command 52 to permit identification of drift in the second operating parameter 62 .
- the controller 50 may be additionally configured to translate the command compensation 56 into the delta reference compensation value 64 via a mathematical relationship 66 .
- the mathematical relationship 66 is intended to be programmed into the controller 50 and be used to calculate the delta reference compensation value 64 in response to the determined value of the command compensation 56 .
- the controller 50 may be programmed to translate the determined value of command compensation 56 into the delta reference compensation value 64 via accessing an empirically derived data look-up table 68 of determined actuator command compensation 56 versus delta reference compensation values 64 .
- the data look-up table 68 includes determined actuator command compensation 56 for operation of the injector 40 being cross-referenced or correlated with empirically derived delta reference compensation values 64 .
- the controller 50 may additionally be programmed to determine a pressure in the injector rail 42 and injection timing of the fuel injectors 40 used to operate the engine 12 .
- the controller 50 may also be programmed to determine a number of injections or pulses of fuel 18 generated by each fuel injector 40 per engine cycle.
- the system 48 uses compensation learning strategy to perform a non-intrusive diagnostic of drift in the performance of engine component 40 during the second mode of operation, such that the compensated operating parameter 54 and the attendant first mode of operation are not affected.
- FIG. 3 depicts a method 100 using compensation learning strategy for a diagnostic of the internal combustion engine component 40 using compensation learning strategy, as described above with respect to FIGS. 1 and 2 .
- the method 100 may be performed via the electronic controller 50 programmed to regulate operation of the engine 12 .
- the method 100 initiates in frame 102 with operating the engine 12 via the engine component, such as the fuel injector 40 .
- the method generally includes supplying predetermined amounts of airflow 16 and fuel 18 to the engine 12 .
- the method proceeds to frame 104 , where the method includes operating the engine component 40 using the actuator command 52 issued by the electronic controller 50 to establish the first operating parameter 54 representative of the first mode of component operation.
- the method advances to frame 106 .
- the method includes identifying, via the electronic controller 50 , drift in the first operating parameter 54 negatively affecting the first mode of operation.
- the method proceeds to frame 108 , where the method includes determining, via the electronic controller 50 , the command compensation 58 to the actuator command 52 to counteract the drift in the first operating parameter 54 during the first mode of operation.
- the method advances to frame 110 .
- the method includes determining, via the electronic controller 50 , the parameter compensation 58 to the first operating parameter 54 using the determined compensation 58 to the actuator command 52 .
- Determining the parameter compensation 58 in frame 110 may include translating the command compensation into the delta reference compensation value 64 to apply directly to the first operating parameter 54 while identifying the drift in the second operating parameter 62 .
- Translating the determined parameter compensation 58 into the delta reference compensation value 64 may include using the mathematical relationship 66 programmed into the controller 50 , as discussed above with respect to FIGS. 1 and 2 .
- translating the determined parameter compensation 58 into the delta reference compensation value 64 may include accessing the look-up table 68 of values of determined parameter compensation 58 to the actuator command 52 versus delta reference compensation values.
- the method moves on to frame 112 .
- the method includes applying the determined parameter compensation 58 directly to the first operating parameter 54 to counteract the drift in the first operating parameter 54 during the first mode of operation without applying the determined command compensation 58 to the actuator command 52 .
- the method may advance to frame 114 .
- the method may include operating the engine component 40 using the actuator command 52 to establish the second operating parameter 62 representative of the second mode of component 40 operation.
- the method moves on to frame 116 .
- the method includes identifying, via the electronic controller 50 , the drift in the second operating parameter 62 negatively affecting the second mode of operation.
- the subject identification of the drift in the second operating parameter 62 takes place while the controller 50 applies the determined parameter compensation 58 directly to the first operating parameter 54 and without applying the determined command compensation 56 to the actuator command 52 .
- the method may advance to frame 118 , where the method includes determining and applying, via the electronic controller 50 , compensation to the second operating parameter 62 of the component 40 to counteract the component's drift during the second mode of operation.
- the method may loop back to frame 104 for continued operation of the engine component 40 using the actuator command 52 to establish the first operating parameter 54 representative of the first mode of component operation.
- the controller 50 may be programmed to continuously monitor operation of the engine 12 , the engine component, e.g., injector, 40 , and the AT system 30 and perform, as part of the method 100 , a non-intrusive diagnostic of drift in the performance of the subject component 40 during the second mode of operation.
- the method 100 being specifically configured to perform the diagnostic such that the compensated operating parameter 54 and the attendant first mode of operation are not affected.
- the method 100 is configured to reduce an influence of the learning compensation one component 40 operating parameter on the diagnostic observation of another component 40 operating parameter, without detrimentally impacting performance of the subject component in achieving a target of the first mode of operation.
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Abstract
Description
- The present disclosure relates to a system and a method for enhancing robustness of an internal combustion engine component diagnostic using compensation learning strategy.
- Modern internal combustion engines typically employ control systems to monitor and regulate engine performance by implementing diagnostic algorithms for various engine components, such as sensors and actuators. Such learning strategies are frequently used to compensate for performance deviations due to part-to-part variation and component aging compared to nominal component behavior.
- Typically, such strategies include a learning phase in which the component deviation is measured and stored, and a release phase in which a learning compensation is applied to a control signal or command. In some instances and for certain components, a learning function may be used to perform a diagnostic observation of a second component parameter that is physically linked to a first component parameter already subject to learning compensation.
- Such use of the learning function for a particular component may result in an influence of the learning compensation of the first component parameter on the diagnostic observation of the second component parameter. However, a removal of the learning compensation of the first component parameter during the diagnostic observation of the second parameter crates an intrusive test that may lead to certain performance targets for the subject component not being met.
- A method using compensation learning strategy for a diagnostic of an internal combustion engine component includes operating the engine component via an actuator command issued by an electronic controller. Specifically, the actuator command is used to establish a first operating parameter representative of a first mode of component operation. The method also includes identifying, via the electronic controller, a drift in the first operating parameter negatively affecting the first mode of operation. The method additionally includes determining, via the electronic controller, a command compensation to the actuator command to counteract the drift in the first operating parameter during the first mode of operation. The method also includes determining, via the electronic controller, a parameter compensation to the first operating parameter using the determined compensation to the actuator command. The method additionally includes applying the determined parameter compensation directly to the first operating parameter. The method also includes operating the engine component using the actuator command to establish a second operating parameter representative of a second mode of component operation. Furthermore, the method includes identifying, via the electronic controller, a drift in the second operating parameter negatively affecting the second mode of operation while applying the determined parameter compensation directly to the first operating parameter and without applying the determined command compensation to the actuator command.
- Determining the parameter compensation may include translating the command compensation into a delta reference compensation value to apply directly to the first operating parameter while identifying the drift in the second operating parameter.
- Translating the command compensation into the delta reference compensation value may include using a mathematical relationship programmed into the controller.
- Translating the command compensation into the delta reference compensation value may include accessing an empirically collected look-up table of values of determined compensation to the actuator command versus delta reference compensation values.
- The engine may be a compression ignition engine and the component may be an injector configured to inject fuel into the engine.
- The first operating parameter may be a relatively small injection quantity and the first mode of operation is pilot fuel injection.
- The second operating parameter may be a relatively large injection quantity and the second mode of operation is main combustion fuel injection.
- Identifying the drift in the second operating parameter while applying the determined parameter compensation directly to the first operating parameter and without applying the determined command compensation to the actuator command may include maintaining pre-combustion temperature in the combustion chamber and maintaining combustion stability in the engine.
- Alternatively, the second operating parameter may be a relatively small injection quantity and the second mode of operation may be post-combustion fuel injection.
- The engine may include an exhaust after-treatment (AT) device configured to reduce engine exhaust gas emissions. In such a case, identifying the drift in the second operating parameter while applying the determined parameter compensation directly to the first operating parameter and without applying the determined command compensation to the actuator command may include at least one of maintaining effective operation of the AT device and maintaining reduction of engine exhaust gas emissions thereby.
- A system using compensation learning strategy for a diagnostic of an internal combustion engine component, such as via an electronic controller performing the above-described method, is also disclosed. A vehicle may employ such a system.
- The above features and advantages, and other features and advantages of the present disclosure, will be readily apparent from the following detailed description of the embodiment(s) and best mode(s) for carrying out the described disclosure when taken in connection with the accompanying drawings and appended claims.
-
FIG. 1 is a schematic plan view of a vehicle having an internal combustion engine connected to an exhaust system having an after-treatment (AT) system with a number of AT devices for reducing exhaust emissions and including a system using an electronic controller to perform compensation learning strategy for a diagnostic of an engine component. -
FIG. 2 is a close-up schematic illustration of an engine cylinder having a combustion chamber and a representative engine component in the internal combustion engine shown inFIG. 1 . -
FIG. 3 is a flow diagram of a method using compensation learning strategy for a diagnostic of an internal combustion engine component shown inFIGS. 1 and 2 . - Referring to the drawings, wherein like reference numbers refer to like components throughout the several views,
FIG. 1 schematically depicts amotor vehicle 10. Thevehicle 10 includes aninternal combustion engine 12 configured to propel the vehicle via drivenwheels 14. Although theinternal combustion engine 12 may be a compression-ignition or diesel type of an engine. Generally, internal combustion in adiesel engine 12 occurs when a specific amount ofambient intake airflow 16 is mixed with a metered amount offuel 18 supplied from afuel tank 20 and the resultant air-fuel mixture is compressed insidecombustion chamber 13A of the engine's cylinders 13 (shown inFIG. 2 ). - As shown, the
engine 12 may include anexhaust manifold 22 configured to collect exhaust gas from the engine'scylinders 13. The engine also includes aturbocharger 24 in fluid communication withcylinders 13, such as via theexhaust manifold 22. Theturbocharger 24 is energized or driven by a flow of exhaust gas, specifically theexhaust gas 26 released byindividual cylinders 13 of theengine 12, such as through theexhaust manifold 22, following each combustion event. Theturbocharger 24 is connected to anexhaust system 28 that receivesexhaust gas 26 and eventually releases the exhaust gas to the ambient, typically on a side or aft of thevehicle 10. Theturbocharger 24 also uses theexhaust gas 26 flow to pressurize theintake airflow 16. - The
vehicle 10 also includes an engine exhaust after-treatment (AT)system 30. TheAT system 30 includes a number of exhaust after-treatment devices configured to methodically remove largely carbonaceous particulate byproducts and emission constituents of engine combustion from theexhaust gas 26. As shown inFIGS. 1 and 2 , the ATsystem 30 operates as part of theexhaust system 28. TheAT system 30 includes at least one AT device, such as afirst AT device 32 arranged downstream of theturbocharger 24 and asecond AT device 34 arranged downstream of the first AT device. Thefirst AT device 32 may be close-coupled to theturbocharger 24 and arranged inside an engine compartment 11 of thevehicle 10 for close proximity to theengine 12. Such close-coupling of thefirst AT device 32 to theengine 12 may provide a compact packaging arrangement that minimizes time for activation, i.e., light-off, of theAT system 30 in after-treatment of theexhaust gas 26 following a cold-start of theengine 12. TheAT system 30 may also include additional AT devices (not shown) positioned in the exhaust gas flow downstream of the first andsecond AT devices - As shown, the
first AT device 32 may be a diesel oxidation catalyst (DOC), while thesecond AT device 34 may be a selective catalytic reduction (SCR) catalyst and filter. The primary function of the DOC is reduction of carbon monoxides (CO) and non-methane hydrocarbons (NMHC). When present, the DOC is additionally configured to generate nitrogen dioxide (NO2), which may be used by the SCR arranged remotely downstream of the DOC. The primary function of the SCR is to reduce a concentration of nitrogen oxides (NOX) in theexhaust gas 26. - The
AT system 30 also includes theexhaust passage 22A, which may be part of theexhaust manifold 22, configured to carry the flow ofexhaust gas 26 to theturbocharger 24 from the engine'scylinders 13, and anexhaust passage 36 configured to carry the flow ofexhaust gas 26 aft of theturbocharger 24 to thefirst AT device 32. Theintake airflow 16 is supplied to theengine 12 via anintake passage 38 for mixing with thefuel 18, to generate combustion, thereby operate the engine, and generate a flow of theexhaust gas 26. Theengine 12 may include anengine component 40 used to operate the engine component using an actuator command via a control signal issued by an electronic controller to be described in detail below. - The
engine component 40 may be a component employing a learning strategy diagnosing a calibrated zero point and span of control that would benefit from self-calibration without shut-off. Specifically, theengine component 40 may be a fuel injector supplied with thefuel 18 via aninjector rail 42 and employed to inject thefuel 18 into the engine'scylinders 13. Although theengine 12 may include other examples of theengine component 40, such as sensors and actuators, the remainder of the present disclosure will concentrate on the fuel injector embodiment of the subject component. Accordingly, from hereon, the fuel injector will be labeled with thenumeral 40. Theinternal combustion engine 12 may generally have a multi-cylinder configuration employing at least onesuch fuel injector 40 per eachcylinder 13. - An
airflow sensor 44 may be arranged in theintake passage 38 and configured to detect an amount of theairflow 16 supplied to theengine 12 during its operation and such data may be used for controlling the amount offuel 18 injected into thecylinders 13. Anexhaust gas passage 46 is configured to receive treatedexhaust gas 26A aft of thesecond AT device 34 and pass the treated exhaust gas through the rest of theexhaust system 28 and the remainder of theAT system 30. - The
vehicle 12 also includes asystem 48 configured to perform a diagnostic of thecomponent 40 using compensation learning strategy that will be described in detail below. Thesystem 48 is further configured to reduce an influence of the learning compensation of onecomponent 40 operating parameter on the diagnostic observation of anothercomponent 40 operating parameter, without detrimentally impacting performance of the subject component. Thevehicle 10 additionally includes anelectronic controller 50 configured to regulate theAT system 30, and, as such, the controller may be part of the AT system. Thecontroller 50 is part of thesystem 48 and may be a stand-alone unit, or be part of an electronic control unit (ECU) that regulates the operation ofengine 12. Thecontroller 50 is arranged on thevehicle 10 and includes a processor and a readily accessible non-transitory memory. Instructions for controlling operation of theAT system 30 are programmed or recorded in the memory of thecontroller 50, and the processor is configured to execute the instructions from the memory during operation of thevehicle 10. - The
controller 50 is generally programmed to regulate theinjectors 40 for injectingfuel 18 into thecylinders 13 to enable operation of theengine 12. Specifically, thecontroller 50 is programmed to operate theinjectors 40 during a particular first event, such as during a cold start, using anactuator command 52, for example, communicated via control signal, to establish afirst operating parameter 54 representative of a first mode ofcomponent 40, i.e., injector, operation. The first operating parameter is a relatively small injection quantity, for example, in the range of 1-3 mm3/stroke for a single injection per engine stroke in an individual cylinder. The first mode of operation is pilot fuel injection activated around 10 degrees before top dead center (BTDC) to warm up thecombustion chamber 13A. In such an embodiment, the first mode ofinjector 40 operation may, for example, be defined by the small injection quantity in the range of 1-3 mm3/stroke (of the injector) for a single injection per engine stroke, as described above, and thus configured to support a cold start of theengine 12. - The
controller 50 is also programmed to identify or diagnose a drift in thefirst operating parameter 54 negatively affecting, i.e., causing a fault in, the first mode ofinjector 40 operation. Thecontroller 50 is additionally programmed to determine acommand compensation 56 to theactuator command 52 to counteract the drift in thefirst operating parameter 54 during the first mode ofinjector 40 operation. Thecontroller 50 is also programmed to determine aparameter compensation 58 to thefirst operating parameter 54 using the determinedcompensation 56 to theactuator command 52. Such determination ofparameter compensation 58 may include translating thecommand compensation 56 into adelta reference compensation 60 value to apply directly to thefirst operating parameter 54. - The
controller 50 is additionally programmed to apply thedetermined parameter compensation 58 directly to thefirst operating parameter 54. Specifically, thedetermined parameter compensation 58 is applied directly to thefirst operating parameter 54 to counteract the identified drift in the first operating parameter during the first mode of operation of theinjector 40 without applying thedetermined command compensation 56 directly to theactuator command 52. Generally, drift in an operating parameter indicates loss of precision in the achievement of the subject parameter, i.e., straying of the parameter from its target value. In the case of drift in the first operating parameter during the first mode of operation of theinjector 40 may indicate an incorrect amount offuel 18 being injected into thecylinders 13. Injection of incorrect amount offuel 18 into thecylinders 13 may be detrimental to the engine's combustion efficiency, and to operation of theAT devices exhaust gas 26. - The
controller 50 is also programmed to operate theinjector 40 using theactuator command 52 to establish asecond operating parameter 62 representative of a second mode ofinjector 40 operation. Thesecond operating parameter 62 may be a relatively large injection quantity, for example, in the range of 5-150 mm3/stroke, cumulative amount of fuel injected per engine cycle, multiple injections per stroke for multiple cylinders. The second mode of operation is main combustion fuel injection activated around 2-5 degrees BTDC (with the main injection in a typical diesel engine generally occurring across a full range of 20 degrees BTDC-5 degrees ATDC) to initiate full combustion in thecombustion chamber 13A. In such an embodiment, the second mode ofinjector 40 operation may, for example, be defined by the large injection quantity in the range of 5-150 mm3/stroke, and configured to support operation of theengine 12 over a regular operating temperature range and generate engine torque in response to operator request. Other examples of main combustion fuel injection may include particular operating conditions such asengine 12 cranking and fueling during transient maneuvers. - Alternatively, the
second operating parameter 62 may be a relatively small injection quantity, for example, in the range of 1-3 mm3/stroke for a single injection per engine stroke in an individual cylinder. In such an embodiment, the second mode ofinjector 40 operation may be post-combustion fuel injection activated around 100 milliseconds or 10-30 degrees after top dead center (ATDC). The post-combustion fuel injection may, for example, be defined by the small injection quantity in the range of 1-3 mm3/stroke, and configured to maintain effective operating temperature of theAT devices cylinders 13. As a result, identification of the drift in thesecond operating parameter 62 while applying thedetermined parameter compensation 58 directly to thefirst operating parameter 54 without applying thedetermined command compensation 56 to theactuator command 52 includes at least one of maintaining pre-combustion temperature in thecombustion chambers 13A and maintaining combustion stability in theengine 12. - Furthermore, the
controller 50 is programmed to identify or diagnose a drift in thesecond operating parameter 62 negatively affecting the second mode ofinjector 40 operation. Identification of the drift in thesecond operating parameter 62 is intended to take place while the determined parameter compensation is applied directly to thefirst operating parameter 54 and without applying thedetermined command compensation 56 to theactuator command 52. Accordingly, thecontroller 50 is configured to perform a non-intrusive diagnostic of thesecond operating parameter 62 drift during the second mode of operation, i.e., the compensated first operatingparameter 54 and the first mode of operation are not affected during thesecond operating parameter 62 diagnostic. Such diagnostic further permits the controller to identify the health and capability of the component, e.g., injector, 40 to support the second mode of injector operation, without detrimentally affecting the injector's ability to support the first mode of operation. - The
controller 50 may be additionally configured to determine and apply compensation to thesecond operating parameter 62 to counteract the identified drift during the second mode of operation without affecting the first mode ofinjector 40 operation. By identification of the drift in thesecond operating parameter 62 while applying thedetermined parameter compensation 58 directly to thefirst operating parameter 54 and without applying thedetermined command compensation 56 to theactuator command 52, thecontroller 50 is configured to maintain effective operation of the AT device(s) 32, 34 and maintain reduction of engine exhaust gas emissions thereby. - The determination of the
parameter compensation 58 may include translating thecommand compensation 56 into a deltareference compensation value 64 to be applied directly to thefirst operating parameter 54. The deltareference compensation value 64 is intended to provide a specific incremental change directly to thefirst operating parameter 54, bypassing modification to theactuator command 52 to permit identification of drift in thesecond operating parameter 62. Thecontroller 50 may be additionally configured to translate thecommand compensation 56 into the deltareference compensation value 64 via amathematical relationship 66. Themathematical relationship 66 is intended to be programmed into thecontroller 50 and be used to calculate the deltareference compensation value 64 in response to the determined value of thecommand compensation 56. Alternatively, thecontroller 50 may be programmed to translate the determined value ofcommand compensation 56 into the deltareference compensation value 64 via accessing an empirically derived data look-up table 68 of determinedactuator command compensation 56 versus delta reference compensation values 64. In other words, the data look-up table 68 includes determinedactuator command compensation 56 for operation of theinjector 40 being cross-referenced or correlated with empirically derived delta reference compensation values 64. - The
controller 50 may additionally be programmed to determine a pressure in theinjector rail 42 and injection timing of thefuel injectors 40 used to operate theengine 12. Thecontroller 50 may also be programmed to determine a number of injections or pulses offuel 18 generated by eachfuel injector 40 per engine cycle. Overall, thesystem 48 uses compensation learning strategy to perform a non-intrusive diagnostic of drift in the performance ofengine component 40 during the second mode of operation, such that the compensated operatingparameter 54 and the attendant first mode of operation are not affected. -
FIG. 3 depicts amethod 100 using compensation learning strategy for a diagnostic of the internalcombustion engine component 40 using compensation learning strategy, as described above with respect toFIGS. 1 and 2 . Themethod 100 may be performed via theelectronic controller 50 programmed to regulate operation of theengine 12. Themethod 100 initiates inframe 102 with operating theengine 12 via the engine component, such as thefuel injector 40. Throughout the method, and starting withframe 102, the method generally includes supplying predetermined amounts ofairflow 16 andfuel 18 to theengine 12. Followingframe 102, the method proceeds to frame 104, where the method includes operating theengine component 40 using theactuator command 52 issued by theelectronic controller 50 to establish thefirst operating parameter 54 representative of the first mode of component operation. - After
frame 104, the method advances to frame 106. Inframe 106, the method includes identifying, via theelectronic controller 50, drift in thefirst operating parameter 54 negatively affecting the first mode of operation. Followingframe 106 the method proceeds to frame 108, where the method includes determining, via theelectronic controller 50, thecommand compensation 58 to theactuator command 52 to counteract the drift in thefirst operating parameter 54 during the first mode of operation. Afterframe 108, the method advances to frame 110. In frame 110 the method includes determining, via theelectronic controller 50, theparameter compensation 58 to thefirst operating parameter 54 using the determinedcompensation 58 to theactuator command 52. - Determining the
parameter compensation 58 in frame 110 may include translating the command compensation into the deltareference compensation value 64 to apply directly to thefirst operating parameter 54 while identifying the drift in thesecond operating parameter 62. Translating thedetermined parameter compensation 58 into the deltareference compensation value 64 may include using themathematical relationship 66 programmed into thecontroller 50, as discussed above with respect toFIGS. 1 and 2 . Alternatively, translating thedetermined parameter compensation 58 into the deltareference compensation value 64 may include accessing the look-up table 68 of values ofdetermined parameter compensation 58 to theactuator command 52 versus delta reference compensation values. - Following frame 110, the method moves on to frame 112. In
frame 112 the method includes applying thedetermined parameter compensation 58 directly to thefirst operating parameter 54 to counteract the drift in thefirst operating parameter 54 during the first mode of operation without applying thedetermined command compensation 58 to theactuator command 52. Afterframe 112, the method may advance to frame 114. Inframe 114 the method may include operating theengine component 40 using theactuator command 52 to establish thesecond operating parameter 62 representative of the second mode ofcomponent 40 operation. - Following
frame 114, the method moves on to frame 116. Inframe 116 the method includes identifying, via theelectronic controller 50, the drift in thesecond operating parameter 62 negatively affecting the second mode of operation. The subject identification of the drift in thesecond operating parameter 62 takes place while thecontroller 50 applies thedetermined parameter compensation 58 directly to thefirst operating parameter 54 and without applying thedetermined command compensation 56 to theactuator command 52. Followingframe 116, the method may advance to frame 118, where the method includes determining and applying, via theelectronic controller 50, compensation to thesecond operating parameter 62 of thecomponent 40 to counteract the component's drift during the second mode of operation. Following eitherframe frame 104 for continued operation of theengine component 40 using theactuator command 52 to establish thefirst operating parameter 54 representative of the first mode of component operation. - Accordingly, the
controller 50 may be programmed to continuously monitor operation of theengine 12, the engine component, e.g., injector, 40, and theAT system 30 and perform, as part of themethod 100, a non-intrusive diagnostic of drift in the performance of thesubject component 40 during the second mode of operation. Themethod 100 being specifically configured to perform the diagnostic such that the compensated operatingparameter 54 and the attendant first mode of operation are not affected. In other words, themethod 100 is configured to reduce an influence of the learning compensation onecomponent 40 operating parameter on the diagnostic observation of anothercomponent 40 operating parameter, without detrimentally impacting performance of the subject component in achieving a target of the first mode of operation. - The detailed description and the drawings or figures are supportive and descriptive of the disclosure, but the scope of the disclosure is defined solely by the claims. While some of the best modes and other embodiments for carrying out the claimed disclosure have been described in detail, various alternative designs and embodiments exist for practicing the disclosure defined in the appended claims. Furthermore, the embodiments shown in the drawings or the characteristics of various embodiments mentioned in the present description are not necessarily to be understood as embodiments independent of each other. Rather, it is possible that each of the characteristics described in one of the examples of an embodiment may be combined with one or a plurality of other desired characteristics from other embodiments, resulting in other embodiments not described in words or by reference to the drawings. Accordingly, such other embodiments fall within the framework of the scope of the appended claims.
Claims (20)
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US16/110,404 US10578045B1 (en) | 2018-08-23 | 2018-08-23 | System and method for enhancing robustness of engine component diagnostic using compensation learning strategy |
DE102019113860.4A DE102019113860A1 (en) | 2018-08-23 | 2019-05-23 | System and method for improving the robustness of engine component diagnostics using a compensation learning strategy |
CN201910445560.0A CN110857666B (en) | 2018-08-23 | 2019-05-27 | System and method for enhancing engine component diagnostic robustness using compensation learning strategy |
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US11687071B2 (en) | 2021-08-19 | 2023-06-27 | Garrett Transportation I Inc. | Methods of health degradation estimation and fault isolation for system health monitoring |
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EP1526267A3 (en) * | 2003-10-21 | 2010-07-28 | Continental Automotive GmbH | Method and device for compensating the drift of an injector for an internal combustion engine with direct injection |
GB2475521B (en) * | 2009-11-20 | 2016-05-04 | Gm Global Tech Operations Llc | Method for the determination of the actual quantity of fuel injected in an internal combustion engine |
US8412407B2 (en) * | 2010-09-16 | 2013-04-02 | GM Global Technology Operations LLC | Calibration control systems and methods |
DE102010041999A1 (en) * | 2010-10-05 | 2012-04-05 | Robert Bosch Gmbh | Method for correcting actual position of sensor parameter e.g. charge pressure sensor, for detecting pressure of gaseous or liquid medium in air system of motor car, involves correcting parameter by pressurizing with compensation parameter |
FR2975136B1 (en) * | 2011-05-13 | 2014-11-21 | Continental Automotive France | METHOD FOR DETERMINING THE FUEL QUANTITY EXCEEDING AN INJECTOR |
FR2990998B1 (en) * | 2012-05-23 | 2016-02-26 | Continental Automotive France | METHOD FOR CONTROLLING AT LEAST ONE PIEZOELECTRIC FUEL INJECTOR ACTUATOR OF AN INTERNAL COMBUSTION ENGINE |
DE102012222899A1 (en) * | 2012-12-12 | 2014-06-12 | Robert Bosch Gmbh | Method for determining the fuel quality in an internal combustion engine, in particular of a motor vehicle |
CN104919163B (en) * | 2013-01-08 | 2017-08-25 | 沃尔沃卡车集团 | For determining the method and apparatus of fuel mass and possessing the vehicle of the device |
KR101566741B1 (en) * | 2014-04-09 | 2015-11-06 | 현대자동차 주식회사 | Method for compensating post injectiion timing |
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US11687071B2 (en) | 2021-08-19 | 2023-06-27 | Garrett Transportation I Inc. | Methods of health degradation estimation and fault isolation for system health monitoring |
US12117824B2 (en) | 2021-08-19 | 2024-10-15 | Garrett Transportation I Inc. | Methods of health degradation estimation and fault isolation for system health monitoring |
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