WO2018059485A1 - 汽油发动机过量空气系数燃烧控制方法及燃烧控制系统 - Google Patents
汽油发动机过量空气系数燃烧控制方法及燃烧控制系统 Download PDFInfo
- Publication number
- WO2018059485A1 WO2018059485A1 PCT/CN2017/103980 CN2017103980W WO2018059485A1 WO 2018059485 A1 WO2018059485 A1 WO 2018059485A1 CN 2017103980 W CN2017103980 W CN 2017103980W WO 2018059485 A1 WO2018059485 A1 WO 2018059485A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- engine
- excess air
- exhaust gas
- combustion
- load state
- Prior art date
Links
Classifications
-
- 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
-
- 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
-
- 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
- F02D41/0002—Controlling intake air
-
- 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
- F02D41/0025—Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
- F02D41/0047—Controlling exhaust gas recirculation [EGR]
- F02D41/005—Controlling exhaust gas recirculation [EGR] according to engine operating conditions
- F02D41/0057—Specific combustion modes
-
- 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
- F02D41/3035—Controlling fuel injection according to or using specific or several modes of combustion characterised by the mode(s) being used a mode being the premixed charge compression-ignition mode
- F02D41/3041—Controlling fuel injection according to or using specific or several modes of combustion characterised by the mode(s) being used a mode being the premixed charge compression-ignition mode with means for triggering compression ignition, e.g. spark plug
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
- F02N11/00—Starting of engines by means of electric motors
- F02N11/08—Circuits or control means specially adapted for starting of engines
- F02N11/087—Details of the switching means in starting circuits, e.g. relays or electronic switches
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02P—IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
- F02P5/00—Advancing or retarding ignition; Control therefor
- F02P5/04—Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions
- F02P5/045—Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions combined with electronic control of other engine functions, e.g. fuel injection
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D11/00—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated
- F02D11/06—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated characterised by non-mechanical control linkages, e.g. fluid control linkages or by control linkages with power drive or assistance
- F02D11/10—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated characterised by non-mechanical control linkages, e.g. fluid control linkages or by control linkages with power drive or assistance of the electric type
- F02D11/105—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated characterised by non-mechanical control linkages, e.g. fluid control linkages or by control linkages with power drive or assistance of the electric type characterised by the function converting demand to actuation, e.g. a map indicating relations between an accelerator pedal position and throttle valve opening or target engine torque
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D13/00—Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing
- F02D13/02—Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing during engine operation
- F02D13/0269—Controlling the valves to perform a Miller-Atkinson cycle
-
- 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
- F02D41/0002—Controlling intake air
- F02D2041/001—Controlling intake air for engines with variable valve actuation
-
- 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
- F02D2200/04—Engine intake system parameters
- F02D2200/0402—Engine intake system parameters the parameter being determined by using a model of the engine intake or its components
-
- 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
- F02D2200/04—Engine intake system parameters
- F02D2200/0414—Air temperature
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
- F02N11/00—Starting of engines by means of electric motors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
- F02N11/00—Starting of engines by means of electric motors
- F02N11/006—Starting of engines by means of electric motors using a plurality of electric motors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
- F02N11/00—Starting of engines by means of electric motors
- F02N11/04—Starting of engines by means of electric motors the motors being associated with current generators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
- F02N11/00—Starting of engines by means of electric motors
- F02N11/08—Circuits or control means specially adapted for starting of engines
- F02N11/0803—Circuits or control means specially adapted for starting of engines characterised by means for initiating engine start or stop
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
- F02N11/00—Starting of engines by means of electric motors
- F02N11/08—Circuits or control means specially adapted for starting of engines
- F02N11/0862—Circuits or control means specially adapted for starting of engines characterised by the electrical power supply means, e.g. battery
- F02N11/0866—Circuits or control means specially adapted for starting of engines characterised by the electrical power supply means, e.g. battery comprising several power sources, e.g. battery and capacitor or two batteries
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
- F02N11/00—Starting of engines by means of electric motors
- F02N11/08—Circuits or control means specially adapted for starting of engines
- F02N2011/0881—Components of the circuit not provided for by previous groups
- F02N2011/0888—DC/DC converters
-
- 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
- Y02T10/12—Improving ICE efficiencies
-
- 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 invention relates to the field of engine technology, and in particular, to a gasoline engine excess air coefficient combustion control method and a combustion control system.
- Homogeneous Charging Compression Ignition (HCCl) control technology achieves low temperature lean combustion by controlling intake air temperature and adopting premixing and compression ignition method, effectively improving the effective thermal efficiency of the engine and reducing Pollutant emissions.
- HCCl Homogeneous Charging Compression Ignition
- the combustion start point and heat release rate of the control technology cannot be controlled; the increase of the engine load also causes the combustion pressure increase rate to rise sharply, and an uncontrollable and abnormal combustion process similar to knocking occurs.
- the object of the present invention is to provide a gasoline engine excess air coefficient combustion control method and a combustion control system for the deficiencies of the prior art. For different operating conditions of the gasoline engine, different excess air coefficients are used to obtain gasoline. The engine improves the overall efficiency of thermal efficiency, power and pollutant emissions over the full range of operating conditions.
- the present invention provides a gasoline engine excess air coefficient combustion control method, including the steps of:
- the engine adopts a lean combustion mode with an excess air ratio of 1.6 to 2.0;
- the engine adopts a combustion mode with an excess air ratio of 1;
- the engine uses a combustion mode with an excess air ratio of 0.8 0.9.
- the partial load state is 0 to 50% of the engine power running state
- the heavy load state is 50% to 90% of the engine power running state
- the full load state is the state of the engine power running.
- the engine adopts a lean combustion mode with an excess air coefficient of 1.6 to 2.0, and the combustion mode is as follows: precise control of fuel supply amount and variable by using a fuel injection system
- the gas distribution system precisely controls the amount of fresh air intake, so that a lean mixture with an excess air ratio of 1.6 to 2.0 is formed in the cylinder and is ignited; meanwhile, the engine uses a Miller cycle combined with exhaust gas recirculation to reduce the combustion temperature in the engine cylinder.
- the combustion temperature in the engine cylinder is below 1900K.
- the exhaust gas recirculation is used to control the exhaust gas recirculation flow rate and the exhaust gas recirculation temperature after combustion, so that the mixture gas temperature of the lean mixture having an excess air ratio of 1.6 to 2.0 in the cylinder is equal to the critical auto-ignition temperature.
- the lean mixture having an excess air ratio of 1.6 to 2.0 is ignited with an ignition energy greater than 400 MJ.
- the engine adopts a combustion mode with an excess air coefficient of 1, the combustion mode is as follows: precise control of fuel supply amount and variable matching by using a fuel injection system
- the gas system precisely controls the amount of fresh air intake, so that an excess air ratio of 1 is formed in the cylinder and is ignited.
- the engine uses exhaust gas recirculation to adjust the exhaust gas return flow and exhaust gas recirculation temperature for combustion adaptation.
- the engine adopts a combustion mode with an excess air coefficient of 0.8 to 0.9, and the combustion mode is as follows: precise control by the fuel injection system
- the fuel supply amount and the variable gas distribution system precisely control the fresh air intake amount, so that a rich mixture with an excess air coefficient of 0.8 to 0.9 is formed in the cylinder and ignited; meanwhile, the engine uses exhaust gas recirculation to adjust the exhaust gas return flow and exhaust gas.
- the combustion temperature is adapted to the reflux temperature.
- the gasoline engine excess air coefficient combustion control method further comprises: using exhaust gas recirculation to control the exhaust gas return flow after combustion, wherein the exhaust gas return flow rate in the three combustion modes is: excess air coefficient is 1.6 ⁇ 2.0
- the gasoline engine excess air coefficient combustion control method further comprises: using exhaust gas recirculation to control the exhaust gas recirculation temperature after combustion, wherein the exhaust gas reflow temperature in the three combustion modes is: an excess air coefficient of 1.6 to 2.0
- the exhaust gas to be discharged generated by the combustion of the engine is finally discharged after being catalytically converted.
- the present invention also provides a gasoline engine excess air coefficient combustion control system, the combustion control system including a cylinder block structure, a variable gas distribution system, a fuel injection system, a high energy ignition system, an exhaust gas recirculation system, and a condition monitoring system. a system and an engine electronic control unit, the cylinder block structure including a cylinder, the variable air distribution system for controlling an intake air amount of fresh air entering the cylinder, the fuel injection system for controlling injection into the cylinder
- the amount of fuel, the high-energy ignition system includes a high-energy spark plug and is used for discharge ignition, and the exhaust gas recirculation system is used to control exhaust gas recirculation flow rate and exhaust gas recirculation temperature, wherein:
- the engine electronic control unit is electrically connected to the condition monitoring system, the variable gas distribution system, the fuel injection system, the high energy ignition system, and the exhaust gas recirculation system;
- condition monitoring system is configured to monitor an operating condition of the engine and transmit the monitoring result to the engine electronic control unit;
- the engine electronic control unit determines the current load state of the engine according to the operating condition of the engine, wherein the load state of the engine is divided into: a partial load state, a heavy load state, and a full load state;
- the engine electronic control unit selects a suitable excess air coefficient combustion mode according to the current load state of the engine, where
- the engine electronic control unit controls the engine to adopt a lean combustion mode with an excess air ratio of 1.6 to 2.0;
- the engine electronic control unit controls the engine to adopt a combustion mode with an excess air ratio of 1;
- the engine electronic control unit controls the engine to adopt a combustion mode with an excess air ratio of 0.8 to 0.9.
- condition monitoring system includes an engine speed monitoring sensor and a power monitoring device.
- the exhaust gas recirculation system includes an exhaust gas recirculation pipe, an exhaust gas recirculation control valve, an exhaust gas recirculation intercooler, an exhaust gas recirculation bypass pipe, and a wastegate valve, and the exhaust gas recirculation pipe
- An exhaust end of the road is connected to the intake pipe, and an inlet end of the exhaust gas recirculation line is in communication with the exhaust pipe, and the exhaust gas recirculation control valve and the exhaust gas recirculation intercooler are connected in series
- the exhaust gas recirculation bypass line is connected in parallel with the exhaust gas recirculation intercooler
- the waste gas bypass valve is disposed in the exhaust gas recirculation bypass line.
- the exhaust gas recirculation system is used for controlling the exhaust gas return flow after combustion, wherein the exhaust gas return flow rate in the three combustion modes is: a lean combustion mode with an excess air ratio of 1.6 to 2.0 > excess air A combustion mode with a coefficient of 1 > a combustion mode with an excess air ratio of 0.8 to 0.9.
- the exhaust gas recirculation system is used to control the exhaust gas recirculation temperature after combustion, wherein the exhaust gas recirculation temperature in the three combustion modes is: a lean combustion mode with an excess air ratio of 1.6 to 2.0 > excess air A combustion mode with a coefficient of 1 > a combustion mode with an excess air ratio of 0.8 to 0.9.
- the ignition energy of the high-energy spark plug can ignite a rich mixture with an excess air ratio of 0.8-0.9 and a mixture with an excess air ratio of 1, and can also ignite a lean mixture with an excess air ratio of 1.6-2.0. gas.
- 1 is a schematic structural view of a gasoline engine excess air coefficient combustion control system of the present invention.
- 2 is a block diagram of a gasoline engine excess air coefficient combustion control system of the present invention.
- FIG. 3 is a flow chart of a gasoline engine excess air coefficient combustion control method of the present invention.
- FIG. 1 is a schematic structural view of a gasoline engine excess air coefficient combustion control system of the present invention
- FIG. 2 is a block diagram of a gasoline engine excess air coefficient combustion control system of the present invention, as shown in FIG. 1 and FIG.
- the inventive gasoline engine excess air coefficient combustion control system 100 includes a cylinder block structure 10, a variable gas distribution system 20, a fuel injection system 30, a high energy ignition system 40, an exhaust gas recirculation system 50, a catalytic converter 60, and a condition monitoring system. 70 and engine electronic control unit 80.
- the cylinder block structure 10 includes a cylinder 11 and a cylinder head 12.
- the cylinder head 12 is disposed above the hollow cylinder 11, and the cylinder 11 includes a hollow cylinder 111, a piston 112 inserted in the cylinder 111 and movable along the axis of the cylinder 111, and a connecting rod 113 hingedly coupled to the piston 112. .
- the space formed by the bottom surface of the cylinder head 12, the top surface of the piston 112 of the cylinder 11, and the cylinder 111 of the cylinder 11 is the combustion chamber 13.
- the Miller Cycle technique is employed, so the combustion chamber 13 is metered. Le cycle combustion chamber.
- the variable gas distribution system 20 is used to precisely control the amount of air required for combustion provided to the cylinder 11.
- the variable gas distribution system 20 includes an intake pipe 21, an exhaust pipe 22, an intake valve 23, an exhaust valve 24, a throttle valve 25, and a variable valve positive dam device 26.
- the intake valve 23 and the exhaust valve 24 are disposed on the cylinder head 12, and the intake pipe 21 and the exhaust pipe 22 are disposed outside the cylinder head 12 and fixedly coupled to the cylinder head 12, and the intake pipe 21 communicates with the cylinder 11 through the intake valve 23.
- the exhaust pipe 22 is in communication with the cylinder 11 through the exhaust valve 24.
- This embodiment uses the Miller cycle technology, so the intake valve 23 uses a Miller cycle small lift intake valve.
- the variable valve positive damper device 26 uses Variable Valve Timing (VVT) technology to adjust the amount of intake (exhaust) according to the operation of the engine, that is, the intake valve 2 3 (intake valve 24) ⁇ Between turns and angles, the amount of air entering is optimized to improve combustion efficiency.
- the variable valve positive pressure device 26 includes a variable intake valve driver 261 and a variable exhaust valve actuator 262 that is disposed at an upper end of the intake valve 23 to control opening and closing of the intake valve 23.
- a variable exhaust valve actuator 262 is disposed at an upper end of the exhaust valve 24 to control the opening and closing of the exhaust valve 24.
- Throttle The refrigerant valve 25 is disposed on the intake pipe 21, and the throttle valve 25 controls the intake air amount of the intake pipe 21.
- variable intake valve actuator 2 61, the variable exhaust valve actuator 262, and the throttle valve 25 are electrically controlled drive components, specifically, the engine electronic control unit 80 and the variable intake valve drive 261, the variable exhaust valve actuator 262
- the throttle 25 is electrically connected and controls these components to operate.
- the cylinder block structure 10 is matched with the variable gas distribution system 20 by using Miller cycle technology, and the Miller cycle can realize a combustion cycle in which the expansion ratio is greater than the effective compression ratio, thereby improving the thermal efficiency of the engine, and simultaneously achieving the reduction of the maximum combustion temperature. effect.
- the fuel injection system 30 is for controlling the amount of fuel injected into the cylinder 11, and the fuel injection system 30 employs Gasoline Direct Injection (GDI) technology.
- the fuel injection system 30 includes a fuel tank 31, an oil delivery pipe 32, a low pressure oil delivery pump 33, a high pressure oil delivery pump 34, and a high pressure fuel injector 35.
- the two ends of the oil delivery pipe 32 are respectively connected to the oil tank 31 and the high pressure fuel injector 35, and the low pressure oil pump 33 and the fuel tank.
- the high-pressure oil pump 34 pressurizes the fuel to deliver it
- the high-pressure oil pump 34 is disposed on the oil delivery pipe 32
- the high-pressure oil pump 34 further pressurizes the fuel in the oil pipe 32
- the high-pressure fuel injector 35 is disposed on the cylinder head 12 is used for directly injecting fuel into the cylinder 11, and the fuel injector of the high pressure injector 35 is located in the cylinder 11 (combustion chamber 13).
- the fuel in the oil delivery pipe 32 is injected into the cylinder 11 through the injector of the high pressure injector 35.
- the high pressure injector 35 is an electrically controlled drive unit.
- the engine electronic control unit 80 is electrically coupled to the high pressure injector 35 and controls the fuel injection operation.
- the fuel injection system 30 cooperates with the variable valve system 20 to achieve precise control of the fuel amount and intake air amount of the cylinder 11, thereby achieving variable control of the excess air ratio of the engine.
- the high energy ignition system 40 includes a high energy spark plug 41 and a high energy discharge power source (not shown) that supplies electrical energy to the high energy spark plug 41.
- the high energy spark plug 41 is disposed on the cylinder head 12, and the ignition end of the high energy spark plug 41 is located in the combustion chamber 21.
- the high-energy spark plug 41 can generate up to 400 MJ of ignition energy, which not only ignites a rich mixture with an excess air ratio of 0.8 to 0.9 and a mixture of excess air ratio of 1, but also ignites a lean mixture having an excess air ratio of 1.6 to 2.0.
- the high energy spark plug 41 is an electrically controlled drive component. Specifically, the firing electrical control unit 80 is electrically coupled to the high energy spark plug 41 and controlled for discharge ignition.
- An Exhaust Gas Recirculation (EGR) system 50 includes an exhaust gas recirculation line 51, an exhaust gas recirculation control valve 52, an exhaust gas recirculation intercooler 53, an exhaust gas recirculation bypass line 54, and a wastegate bypass Valve 55.
- An exhaust end of the exhaust gas recirculation line 51 communicates with an intake pipe 21 located behind the throttle valve 25, and an intake end of the exhaust gas recirculation line 51 communicates with the exhaust pipe 22.
- Exhaust gas recirculation control valve 52 and exhaust gas re The circulating intercooler 53 is disposed in series in the exhaust gas recirculation line 51.
- the exhaust gas recirculation bypass line 54 is connected in parallel with the exhaust gas recirculation intercooler 53, the waste gas bypass valve 55 is disposed in the exhaust gas recirculation bypass line 54, and the waste gas bypass valve 55 is used to control the exhaust gas recirculation line 51.
- the ratio of the exhaust gas of the intercooler 53 to the exhaust gas recirculation that does not pass is precisely controlled to precisely control the reflux exhaust gas temperature.
- the exhaust gas recirculation control valve 52 and the wastegate valve 55 are electrically controlled driving components. Specifically, the engine electronic control unit 80 is electrically connected to the exhaust gas recirculation control valve 52 and the wastegate valve 55 and controls the opening and closing of these valves. .
- This embodiment utilizes an exhaust gas recirculation technique to control the amount of reflux gas and the temperature of the reflux gas. Specifically, a part of the exhaust gas discharged from the cylinder 11 enters the exhaust gas recirculation line 51 through the exhaust pipe 22, and the amount of exhaust gas entering the exhaust gas recirculation line 51 is controlled by the exhaust gas recirculation control valve 52, in the exhaust gas recirculation line 51.
- the exhaust gas is divided into two parts, one part is cooled and cooled by the exhaust gas recirculation intercooler 53, and the other part is bypassed by the exhaust gas recirculation bypass line 54 and then enters the exhaust gas recirculation line 51, and flows through the exhaust gas.
- the cooled and cooled exhaust gas of the recirculation intercooler 53 is mixed, then returned to the intake pipe 21, and mixed with fresh air to re-enter the cylinder 11.
- the ratio of the exhaust gas passing through the exhaust gas recirculation intercooler 53 and the exhaust gas passing through the exhaust gas recirculation bypass line 54 is adjusted by the opening and closing of the wastegate valve 55 in the exhaust gas return bypass line 54. Further, the temperature of the exhaust gas which is returned to the intake pipe 21 is precisely controlled.
- the function of the exhaust gas recirculation system 50 is to control the exhaust gas recirculation flow rate and the exhaust gas recirculation temperature to achieve control of the exhaust gas recirculation flow rate and the exhaust gas recirculation temperature demand under different operating conditions.
- the exhaust gas recirculation system 50 controls the exhaust gas recirculation temperature and the exhaust gas recirculation flow rate, thereby controlling the temperature of the mixture of the in-cylinder mixture in the inter-ship window.
- the amount of waste gas return flow directly affects the maximum combustion temperature after the mixture is ignited and burned. The larger the exhaust gas return flow rate, the lower the maximum combustion temperature.
- the catalytic converter 60 is disposed in the exhaust pipe 22, and the catalytic converter 60 may be filled with a catalyst such as platinum or palladium, and the nitrogen oxides and hydrocarbons discharged into the exhaust pipe 22 after the cylinder 11 is burned. Exhaust gas such as carbon monoxide is catalytically converted into exhaust gas that meets environmental requirements and can be discharged.
- the catalytic converter 60 is different according to the combustion temperature and the air coefficient (such as low-temperature lean combustion, generating carbon and hydrogen, carbon monoxide, etc., high-temperature combustion, generating nitrogen oxides, hydrocarbons, carbon monoxide and other exhaust gases), respectively Polluted waste gas is converted into exhaust gas.
- the engine electronic control unit 80 is electrically coupled to the condition monitoring system 70, the variable valve system 20, the fuel injection system 30, the high energy ignition system 40, and the exhaust gas recirculation system 50.
- Condition monitoring system 70 is used Monitoring the operating conditions of the engine, such as engine speed and engine power, the condition monitoring system may include an engine speed monitoring sensor (not shown) and a power monitoring device (not shown) for monitoring engine speed and engine power, etc. And transmitting the monitored monitoring result to the engine electronic control unit 80. Then, the engine electronic control unit 80 controls the variable valve system 20, the fuel injection system 30, the high energy ignition system 40, and the exhaust gas recirculation system 50 to operate based on these monitoring results.
- gasoline engine excess air coefficient combustion control method of the present invention includes the following steps:
- S1 monitoring an operating condition of the engine
- S2 determining a current load state of the engine according to an operating condition of the engine
- S3 selecting a suitable excess air coefficient combustion mode according to a current load state of the engine
- S4 The exhaust gas to be discharged generated by combustion of the engine is discharged after being catalytically converted.
- step S1 the operating conditions of the engine are monitored, for example, by monitoring engine operating parameters including engine speed and engine power to obtain operating conditions of the engine.
- step S2 based on the obtained operating conditions of the engine, the current load state of the engine is determined, wherein the load state of the engine is divided into: a partial load state, a heavy load state, and a full load state, in this embodiment, a part
- the load state is 0 ⁇ 50% of engine power running state
- the heavy load state is 50 ⁇ 3 ⁇ 4 ⁇ 90 ⁇ 3 ⁇ 4 engine power running state
- the full load state is 90% ⁇ 100% engine power running state.
- step S3 according to the obtained current load state of the engine, the selected excess air coefficient combustion mode is selected.
- the engine when the current load state of the engine is a partial load state, the engine adopts an excess air coefficient. It is a lean combustion mode of 1.6 ⁇ 2.0; when the current load state of the engine is a heavy load state, the engine adopts a combustion mode with an excess air ratio of 1; when the current load state of the engine is a full load state, the engine adopts an excess air ratio of Burning mode of 0.8 ⁇ 0.9.
- the engine When the current load state of the engine is a partial load state, the engine employs a combustion mode with an excess air ratio of 1.6 to 2.0, which is to accurately control the intake air amount using the variable gas distribution system 20 and utilize the fuel injection system 30.
- the fuel quantity is precisely controlled, and a lean mixture having an excess air ratio of 1.6 to 2.0 is formed in the cylinder 11 and ignited by the ignition energy of the high-energy ignition system 40; meanwhile, the engine uses a Miller cycle combined with exhaust gas recirculation (exhaust gas recirculation system) 50)
- the combustion temperature in the engine cylinder 11 is lowered, and the combustion temperature in the engine cylinder 11 is controlled to be 1900K or less.
- exhaust gas recirculation control is also utilized After the combustion, the exhaust gas return flow rate and the exhaust gas recirculation temperature, so that the exhaust gas temperature of the lean mixture with an excess air ratio of 1.6 to 2.0 in the cylinder is equal to the critical auto-ignition temperature in the window of the ignition, and the combustion start point can be controlled to improve combustion, etc. Capacity. Further, the lean mixture with an excess air ratio of 1.6 to 2.0 is ignited with an ignition energy greater than 400 MJ, that is, the ignition energy of the high energy ignition system 40 can reach 400 MJ or more.
- the engine adopts a combustion mode with an excess air ratio of 1, which is a precise control of the intake air amount by the variable valve system 20 and precise control by the fuel injection system 30.
- the amount of fuel is such that a mixture of excess air ratio 1 is formed in the cylinder 11; meanwhile, the engine uses exhaust gas recirculation (exhaust gas recirculation system 50) to regulate the exhaust gas recirculation flow rate and the exhaust gas recirculation temperature so as to be compared with the combustion mode in the current combustion mode. Adapted to suppress the severity of the burn.
- the engine adopts a combustion mode with an excess air ratio of 0.8 0.9, which is a precise control of the intake air amount by the variable valve system 20 and accurate by the fuel injection system 30. Control the amount of fuel to form a rich mixture with an excess air ratio of 0.8 to 0.9 in the cylinder; meanwhile, the engine uses exhaust gas recirculation (exhaust gas recirculation system 50) to adjust the exhaust gas return flow and exhaust gas recirculation temperature so that it is in the current combustion mode.
- the combustion is adapted to ensure the effective output of the engine power
- the engine uses exhaust gas recirculation to control the exhaust gas return flow after combustion, wherein the magnitude of the exhaust gas return flow in the three combustion modes is: a lean combustion mode with an excess air ratio of 1.6 to 2.0 > an excess air ratio of 1
- the combustion mode > the combustion mode with an excess air ratio of 0.8 to 0.9.
- the engine uses the exhaust gas recirculation to control the exhaust gas recirculation temperature after combustion, wherein the exhaust gas recirculation temperature in the three combustion modes is: a lean combustion mode with an excess air ratio of 1.6 to 2.0 > an excess air coefficient of 1
- the combustion mode > the combustion mode with an excess air ratio of 0.8 to 0.9.
- step S4 the exhaust gas to be discharged generated by the combustion of the engine is discharged after being catalytically converted.
- the engine adopts a combustion mode with an excess air ratio of 1.6 to 2.0, and the exhaust gas to be discharged generated by the combustion of the engine contains hydrocarbon and carbon monoxide, and is discharged after being catalytically converted by the catalytic converter 60;
- the engine adopts a combustion mode with an excess air ratio of 1, and the exhaust gas to be discharged by the combustion of the engine contains hydrocarbon, carbon monoxide and nitrogen oxides, after catalytic conversion by the catalytic converter 60.
- the engine adopts a combustion mode with an excess air ratio of 0.8 to 0.9, and the exhaust gas to be discharged by the combustion of the engine contains hydrocarbon, carbon monoxide and nitrogen oxides, and is discharged after being catalytically converted by the catalytic converter 60.
- the gasoline engine excess air coefficient combustion control method of the present invention adopts an exhaust gas recirculation technology, a Miller cycle technology in which a combustion cycle expansion ratio is greater than an effective compression ratio, and an in-cylinder direct injection technology capable of controlling a fuel injection amount in a cylinder.
- a variable valve system technology that controls the amount of intake air in the cylinder and a high-energy ignition system control the combustion start point technique to control engine combustion, and a catalytic converter is used to treat the combustion exhaust gas.
- Exhaust gas recirculation technology Recycles waste gas to control exhaust gas recirculation and exhaust gas recirculation to control combustion.
- the technical solution of the embodiments of the present invention has the beneficial effects of: the above-described gasoline engine excess air coefficient combustion control method and combustion control system, and different excess air coefficients are adopted for different operating conditions of the gasoline engine.
- the combustion mode achieves a comprehensive improvement in the effective thermal efficiency, power and pollutant emissions of the gasoline engine over the full operating range.
- the gasoline engine excess air coefficient combustion control method and the combustion control system according to the embodiments of the present invention use different excess air coefficient combustion modes for different operating conditions of the gasoline engine to obtain an effective effect of the gasoline engine in the full working condition range. Comprehensive improvement in thermal efficiency, power and pollutant emissions.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Abstract
一种汽油发动机过量空气系数燃烧控制方法和燃烧控制系统,其中该汽油发动机过量空气系数燃烧控制方法包括步骤:监测发动机的运行工况;根据发动机的运行工况判断发动机当前的负荷状态,其中发动机的负荷状态分为:部分负荷状态、大负荷状态及满负荷状态;根据发动机当前的负荷状态选择相适配的过量空气系数燃烧模式,其中当发动机当前的负荷状态为部分负荷状态时,发动机采用过量空气系数为1.6~2.0的稀薄燃烧模式;当发动机当前的负荷状态为大负荷状态时,发动机采用过量空气系数为1的燃烧模式;当发动机当前的负荷状态为满负荷状态时,发动机采用过量空气系数为0.8~0.9的燃烧模式。
Description
汽油发动机过量空气系数燃烧控制方法及燃烧控制系统 技术领域
[0001] 本发明涉及发动机技术领域, 尤其涉及汽油发动机过量空气系数燃烧控制方法 及燃烧控制系统。
背景技术
[0002] 均质充量压缩燃烧 (Homogeneous Charging Compression Ignition, HCCl) 控制 技术通过控制进气温度, 并采用预混合、 压缩着火的燃烧方式实现了低温稀薄 燃烧, 有效提升了发动机有效热效率, 并降低了污染物排放。 然而, 由于进气 温度难以精确控制, 且随着发动机负荷的增加, 压缩着火对进气温度的敏感程 度大幅增加, 细微的温度控制差异将会导致压缩着火吋出现较大的变动, 最终 导致 HCCI控制技术的燃烧始点和放热率无法获得控制; 同吋发动机负荷的增加 , 还会使燃烧压力升高率急剧上升, 出现类似爆震的不可控、 不正常的燃烧过 程。
技术问题
[0003] 现有汽油发动机燃烧控制技术中, 汽油与空气通常以化学计量空燃比进行混合 后燃烧, 过量空气系数不会随着发动机工况 (负荷情况) 的变化而改变, 难以 发挥稀薄燃烧有效提升发动机热效率的优势。 问题的解决方案
技术解决方案
[0004] 本发明的目的在于针对现有技术的不足之处, 提供一种汽油发动机过量空气系 数燃烧控制方法及燃烧控制系统, 针对汽油发动机不同的工况, 采用不同的过 量空气系数, 获得汽油发动机在全工况范围内有效热效率、 动力性和污染物排 放的综合改善的效果。
[0005] 本发明提供一种汽油发动机过量空气系数燃烧控制方法, 包括步骤:
[0006] 监测发动机的运行工况;
[0007] 根据发动机的运行工况判断发动机当前的负荷状态, 其中发动机的负荷状态分
为: 部分负荷状态、 大负荷状态及满负荷状态;
[0008] 根据发动机当前的负荷状态选择相适配的过量空气系数燃烧模式, 其中,
[0009] 当发动机当前的负荷状态为部分负荷状态吋, 发动机采用过量空气系数为 1.6~ 2.0的稀薄燃烧模式;
[0010] 当发动机当前的负荷状态为大负荷状态吋, 发动机采用过量空气系数为 1的燃 烧模式;
[0011] 当发动机当前的负荷状态为满负荷状态吋, 发动机采用过量空气系数为 0.8 0.9 的燃烧模式。
[0012] 进一步地, 部分负荷状态为 0~50%发动机功率运行的状态, 大负荷状态为 50%~ 90%发动机功率运行的状态, 满负荷状态为 ^ ΙΟΟ^发动机功率运行的状态。
[0013] 进一步地, 当发动机当前的负荷状态为部分负荷状态吋, 发动机采用过量空气 系数为 1.6~2.0的稀薄燃烧模式, 所述燃烧模式如下: 利用燃油喷射系统精确控 制燃油供给量和可变配气系统精确控制新鲜空气进气量, 使气缸内形成过量空 气系数为 1.6~2.0的稀薄混合气并进行点火; 同吋, 发动机采用米勒循环结合废 气再循环降低发动机气缸内的燃烧温度, 使发动机气缸内的燃烧温度处于 1900K 以下。
[0014] 进一步地, 利用废气再循环控制燃烧后的废气回流量和废气回流温度, 使气缸 内过量空气系数为 1.6~2.0的稀薄混合气在点火吋间窗口的混合气温度等于临界 自燃温度。
[0015] 进一步地, 所述过量空气系数为 1.6~2.0的稀薄混合气采用大于 400MJ的点火能 量进行点火。
[0016] 进一步地, 当所述发动机当前的负荷状态为大负荷状态吋, 发动机采用过量空 气系数为 1的燃烧模式, 所述燃烧模式如下: 利用燃油喷射系统精确控制燃油供 给量和可变配气系统精确控制新鲜空气进气量, 使气缸内形成过量空气系数为 1 的混合气并进行点火; 同吋, 发动机利用废气再循环调节废气回流量和废气回 流温度进行燃烧适配。
[0017] 进一步地, 当所述发动机当前的负荷状态为满负荷状态吋, 发动机采用过量空 气系数为 0.8~0.9的燃烧模式, 所述燃烧模式如下: 利用燃油喷射系统精确控制
燃油供给量和可变配气系统精确控制新鲜空气进气量, 使气缸内形成过量空气 系数为 0.8~0.9的浓混合气并进行点火; 同吋, 发动机利用废气再循环调节废气 回流量和废气回流温度进行燃烧适配。
[0018] 进一步地, 该汽油发动机过量空气系数燃烧控制方法还包括利用废气再循环控 制燃烧后的废气回流量, 其中三种燃烧模式下的废气回流量的大小为: 过量空 气系数为 1.6~2.0的稀薄燃烧模式>过量空气系数为 1的燃烧模式 >过量空气系数为 0.8 0.9的燃烧模式。
[0019] 进一步地, 该汽油发动机过量空气系数燃烧控制方法还包括利用废气再循环控 制燃烧后的废气回流温度, 其中三种燃烧模式下的废气回流温度的大小为: 过 量空气系数为 1.6~2.0的稀薄燃烧模式>过量空气系数为 1的燃烧模式 >过量空气系 数为 0.8~0.9的燃烧模式。
[0020] 进一步地, 所述发动机燃烧产生的待排放废气最后经催化转化后排出。
[0021] 本发明还提供一种汽油发动机过量空气系数燃烧控制系统, 所述燃烧控制系统 包括气缸体结构、 可变配气系统、 燃油喷射系统、 高能点火系统、 废气再循环 系统、 工况监测系统和发动机电控单元, 所述气缸体结构包括气缸, 所述可变 配气系统用于控制新鲜空气进入所述气缸的进气量, 所述燃油喷射系统用于控 制喷射进入所述气缸的燃油量, 所述高能点火系统包括高能火花塞并用于放电 点火, 所述废气再循环系统用于控制废气回流量和废气回流温度, 其中:
[0022] 所述发动机电控单元与所述工况监测系统、 所述可变配气系统、 所述燃油喷射 系统、 所述高能点火系统和所述废气再循环系统电连接;
[0023] 所述工况监测系统用于监测发动机的运行工况并将监测结果传递给所述发动机 电控单元;
[0024] 所述发动机电控单元根据发动机的运行工况判断发动机当前的负荷状态, 其中 发动机的负荷状态分为: 部分负荷状态、 大负荷状态及满负荷状态;
[0025] 所述发动机电控单元根据发动机当前的负荷状态选择相适配的过量空气系数燃 烧模式, 其中,
[0026] 当发动机当前的负荷状态为部分负荷状态吋, 所述发动机电控单元控制发动机 采用过量空气系数为 1.6~2.0的稀薄燃烧模式;
[0027] 当发动机当前的负荷状态为大负荷状态吋, 所述发动机电控单元控制发动机采 用过量空气系数为 1的燃烧模式;
[0028] 当发动机当前的负荷状态为满负荷状态吋, 所述发动机电控单元控制发动机采 用过量空气系数为 0.8~0.9的燃烧模式。
[0029] 进一步地, 所述工况监测系统包括发动机转速监测传感器和功率监测装置。
[0030] 进一步地, 所述废气再循环系统包括废气再循环管路、 废气再循环控制阀、 废 气再循环中冷器、 废气回流旁通管路及废气旁通阀, 所述废气再循环管路的出 气端与进气管相连通, 所述废气再循环管路的入气端与排气管相连通, 所述废 气再循环控制阀和所述废气再循环中冷器串接设置于所述废气再循环管路中, 所述废气回流旁通管路与所述废气再循环中冷器并联, 所述废气旁通阀设置于 所述废气回流旁通管路中。
[0031] 进一步地, 所述废气再循环系统用于控制燃烧后的废气回流量, 其中三种燃烧 模式下的废气回流量的大小为: 过量空气系数为 1.6~2.0的稀薄燃烧模式>过量空 气系数为 1的燃烧模式 >过量空气系数为 0.8~0.9的燃烧模式。
[0032] 进一步地, 所述废气再循环系统用于控制燃烧后的废气回流温度, 其中三种燃 烧模式下的废气回流温度的大小为: 过量空气系数为 1.6~2.0的稀薄燃烧模式>过 量空气系数为 1的燃烧模式 >过量空气系数为 0.8~0.9的燃烧模式。
[0033] 进一步地, 所述高能火花塞的点火能量可点燃过量空气系数为 0.8~0.9的浓混合 气及过量空气系数为 1的混合气, 且还可点燃过量空气系数为 1.6~2.0的稀薄混合 气。
发明的有益效果
有益效果
[0034] 上述汽油发动机过量空气系数燃烧控制方法和燃烧控制系统, 针对汽油发动机 不同的工况, 采用不同的过量空气系数燃烧模式, 获得汽油发动机在全工况范 围内的有效热效率、 动力性和污染物排放的综合改善效果。
对附图的简要说明
附图说明
[0035] 图 1是本发明的汽油发动机过量空气系数燃烧控制系统的结构示意图。
[0036] 图 2是本发明的汽油发动机过量空气系数燃烧控制系统的模块示意图。
[0037] 图 3是本发明的汽油发动机过量空气系数燃烧控制方法的流程图。
本发明的实施方式
[0038] 为更进一步阐述本发明为达成预定发明目的所采取的技术手段及功效, 以下结 合附图及较佳实施例, 对本发明的具体实施方式、 结构、 特征及其功效, 详细 说明如后。
[0039] 图 1是本发明的汽油发动机过量空气系数燃烧控制系统的结构示意图, 图 2是本 发明的汽油发动机过量空气系数燃烧控制系统的模块示意图, 请参图 1与图 2所 示, 本发明的汽油发动机过量空气系数燃烧控制系统 100, 包括气缸体结构 10、 可变配气系统 20、 燃油喷射系统 30、 高能点火系统 40、 废气再循环系统 50、 催 化转化器 60、 工况监测系统 70和发动机电控单元 80。
[0040] 气缸体结构 10包括气缸 11和缸盖 12。 缸盖 12设于中空的气缸 11的上方, 气缸 11 包括中空的缸体 111、 插设于缸体 111中且可沿缸体 111轴线移动的活塞 112、 以 及与活塞 112铰接连接的连杆 113。 由缸盖 12的底面、 气缸 11的活塞 112顶面、 及 气缸 11的缸体 111所形成的空间为燃烧室 13, 本实施例采用米勒循环 (Miller Cycle) 技术, 故燃烧室 13为米勒循环燃烧室。
[0041] 可变配气系统 20用于精确控制向气缸 11提供的燃烧所需空气量。 可变配气系统 20包括进气管 21、 排气管 22、 进气门 23、 排气门 24、 节气门 25及可变气门正吋 装置 26。 进气门 23和排气门 24设置在缸盖 12上, 进气管 21和排气管 22设置于缸 盖 12外侧且与缸盖 12固定连接, 进气管 21通过进气门 23与气缸 11连通, 排气管 2 2通过排气门 24与气缸 11连通。 本实施例采用米勒循环技术, 因此进气门 23采用 米勒循环小升程进气门。 可变气门正吋装置 26采用可变气门正吋 (Variable Valve Timing, VVT)技术, 根据发动机的运行情况调整进气 (排气) 的量, 即进气门 2 3 (进气门 24) 幵合吋间和角度, 使进入的空气量达到最佳, 以提高燃烧效率。 可变气门正吋装置 26包括可变进气门驱动器 261和可变排气门驱动器 262, 可变 进气门驱动器 261设置于进气门 23的上端以控制进气门 23的幵启与关闭, 可变排 气门驱动器 262设置于排气门 24的上端以可控制排气门 24的幵启与关闭。 节气门
25设置于进气管 21上, 节气门 25可控制进气管 21的进气量。 可变进气门驱动器 2 61、 可变排气门驱动器 262和节气门 25为电控驱动部件, 具体地, 发动机电控单 元 80与可变进气门驱动器 261、 可变排气门驱动器 262和节气门 25电连接并控制 这些部件进行工作。
[0042] 气缸体结构 10与可变配气系统 20相配合采用米勒循环技术, 米勒循环能够实现 膨胀比大于有效压缩比的燃烧循环, 提高发动机热效率, 同吋可以实现降低最 高燃烧温度的效果。
[0043] 燃油喷射系统 30用于控制向气缸 11内喷射的燃油量, 燃油喷射系统 30采用缸内 直喷 (Gasoline Direct Injection, GDI) 技术。 燃油喷射系统 30包括油箱 31、 输油 管 32、 低压输油泵 33、 高压输油泵 34及高压喷油器 35, 输油管 32的两端分别与 油箱 31和高压喷油器 35连接, 低压输油泵 33与油箱 31相连, 高压输油泵 34对燃 油加压而将其输送, 高压输油泵 34设置于输油管 32上, 高压输油泵 34对输油管 3 2中的燃油进一步加压, 高压喷油器 35设于缸盖 12上用于往气缸 11内直接喷射燃 油, 高压喷油器 35的喷油嘴位于气缸 11 (燃烧室 13) 内, 输油管 32中燃油经高 压喷油器 35的喷油嘴喷射至气缸 11内。 高压喷油器 35为电控驱动部件, 具体地 , 发动机电控单元 80与高压喷油器 35电连接并控制其进行喷油工作。
[0044] 燃油喷射系统 30与可变配气系统 20配合实现对气缸 11燃油量和进气量的精确控 制, 进而实现了发动机过量空气系数的可变控制。
[0045] 高能点火系统 40包括高能火花塞 41和高能放电电源 (图未示) , 高能放电电源 为高能火花塞 41提供电能。 高能火花塞 41设于缸盖 12上, 高能火花塞 41的打火 端位于燃烧室 21内。 高能火花塞 41可产生高达 400MJ的点火能量, 其不仅可点燃 过量空气系数为 0.8~0.9的浓混合气及过量空气系数为 1的混合气, 还可点燃过量 空气系数为 1.6~2.0的稀薄混合气。 高能火花塞 41为电控驱动部件, 具体地, 发 动机电控单元 80与高能火花塞 41电连接并控制其进行放电点火。
[0046] 废气再循环 (Exhaust Gas Recirculation, EGR) 系统 50包括废气再循环管路 51 、 废气再循环控制阀 52、 废气再循环中冷器 53、 废气回流旁通管路 54、 及废气 旁通阀 55。 废气再循环管路 51的出气端与位于节气门 25后的进气管 21相连通, 废气再循环管路 51的入气端与排气管 22相连通。 废气再循环控制阀 52和废气再
循环中冷器 53串接设置于废气再循环管路 51中。 废气回流旁通管路 54与废气再 循环中冷器 53并联, 废气旁通阀 55设置于废气回流旁通管路 54中, 废气旁通阀 5 5用于控制废气再循环管路 51中经过与不经过的废气再循环中冷器 53的废气比例 以精确控制回流废气温度。 废气再循环控制阀 52和废气旁通阀 55为电控驱动部 件, 具体地, 发动机电控单元 80与废气再循环控制阀 52和废气旁通阀 55电连接 并控制这些阀的幵启与关闭。
[0047] 本实施例利用废气再循环技术来控制回流废气量和回流废气温度。 具体地, 从 气缸 11排出的一部分废气经排气管 22进入废气再循环管路 51, 通过废气再循环 控制阀 52控制进入废气再循环管路 51的废气量, 废气再循环管路 51中的废气分 为两部分, 一部分经由废气再循环中冷器 53冷却降温, 另一部分则经由废气回 流旁通管路 54绕过废气再循环中冷器 53再进入废气再循环管路 51, 与经由废气 再循环中冷器 53的冷却降温的废气相混合, 之后回流至进气管 21, 再与新鲜空 气混合重新进入气缸 11中。 其中, 经由废气再循环中冷器 53的废气和经由废气 回流旁通管路 54的废气的比例是通过废气回流旁通管路 54中的废气旁通阀 55的 幵启与关闭来进行调整, 进而精确控制回流至进气管 21的废气温度。
[0048] 废气再循环系统 50的作用是控制废气回流量和废气回流温度, 实现不同工况对 废气回流量和废气回流温度需求的控制。 通过废气再循环系统 50控制废气回流 温度和废气回流量, 进而控制气缸内混合气在点火吋间窗口的混合气温度。 废 气回流量大小, 直接影响混合气点火燃烧后的最高燃烧温度, 废气回流量越大 , 最高燃烧温度越低。
[0049] 催化转化器 60设置于排气管 22中, 催化转化器 60中可填充有铂或钯等催化剂, 可将气缸 11燃烧后排入排气管 22中的含氮氧化物、 碳氢及一氧化碳等废气催化 转化成符合环保要求可排放的废气再进行排放。 催化转化器 60根据燃烧温度及 空气系数的不同所产生的污染废气 (如低温稀薄燃烧吋产生碳氢和一氧化碳等 废气, 高温燃烧吋产生氮氧化物、 碳氢和一氧化碳等废气) 不同, 分别将污染 废气转化为可排放废气。
[0050] 如图 2所示, 发动机电控单元 80与工况监测系统 70、 可变配气系统 20、 燃油喷 射系统 30、 高能点火系统 40和废气再循环系统 50电连接。 工况监测系统 70用于
监测发动机的运行工况, 如发动机转速和发动机功率等, 工况监测系统可以包 括发动机转速监测传感器 (图未示) 和功率监测装置 (图未示) 等, 用于监测 发动机转速和发动机功率等, 并将监测得到的监测结果传递给发动机电控单元 8 0。 然后, 发动机电控单元 80根据这些监测结果, 控制可变配气系统 20、 燃油喷 射系统 30、 高能点火系统 40和废气再循环系统 50进行工作。
[0051] 图 3是本发明的汽油发动机过量空气系数燃烧控制方法的流程图, 请参图 3所示 , 本发明的汽油发动机过量空气系数燃烧控制方法, 包括步骤:
[0052] S1 : 监测发动机的运行工况;
[0053] S2: 根据发动机的运行工况判断发动机当前的负荷状态;
[0054] S3: 根据发动机当前的负荷状态选择相适配的过量空气系数燃烧模式;
[0055] S4: 发动机燃烧产生的待排放废气经催化转化后排出。
[0056] 在步骤 S1中, 监测发动机的运行工况, 例如是监测包括发动机转速和发动机功 率在内的发动机运行参数, 来获得发动机的运行工况。
[0057] 在步骤 S2中, 根据获得的发动机的运行工况, 判断发动机当前的负荷状态, 其 中发动机的负荷状态分为: 部分负荷状态、 大负荷状态及满负荷状态, 本实施 例中, 部分负荷状态为 0~50%发动机功率运行的状态, 大负荷状态为 50<¾~90<¾ 发动机功率运行的状态, 满负荷状态为 90%~ 100%发动机功率运行的状态。
[0058] 在步骤 S3中, 根据获得的发动机当前的负荷状态, 选择相适配的过量空气系数 燃烧模式, 本实施例中, 当发动机当前的负荷状态为部分负荷状态吋, 发动机 采用过量空气系数为 1.6~2.0的稀薄燃烧模式; 当发动机当前的负荷状态为大负 荷状态吋, 发动机采用过量空气系数为 1的燃烧模式; 当发动机当前的负荷状态 为满负荷状态吋, 发动机采用过量空气系数为 0.8~0.9的燃烧模式。
[0059] 当发动机当前的负荷状态为部分负荷状态吋, 发动机采用过量空气系数为 1.6~ 2.0的燃烧模式, 该燃烧模式是利用可变配气系统 20精确控制进气量和利用燃油 喷射系统 30精确控制燃油量, 使气缸 11内形成过量空气系数为 1.6~2.0的稀薄混 合气并利用高能点火系统 40的点火能量进行点火; 同吋, 发动机采用米勒循环 结合废气再循环 (废气再循环系统 50) 降低发动机气缸 11内的燃烧温度, 控制 发动机气缸 11内的燃烧温度处于 1900K以下。 进一步地, 还利用废气再循环控制
燃烧后的废气回流量和废气回流温度, 使气缸内过量空气系数为 1.6~2.0的稀薄 混合气在点火吋间窗口的混合气温度等于临界自燃温度, 实现燃烧始点可控的 同吋提高燃烧等容度。 进一步地, 过量空气系数为 1.6~2.0的稀薄混合气采用大 于 400MJ的点火能量进行点火, 即高能点火系统 40的点火能量可达到 400MJ以上
[0060] 当发动机当前的负荷状态为大负荷状态吋, 发动机采用过量空气系数为 1的燃 烧模式, 该燃烧模式是利用可变配气系统 20精确控制进气量和利用燃油喷射系 统 30精确控制燃油量, 使气缸 11内形成过量空气系数为 1的混合气; 同吋, 发动 机利用废气再循环 (废气再循环系统 50) 调节废气回流量和废气回流温度, 使 得与当前燃烧模式下的燃烧相适配, 以对燃烧的粗暴程度进行抑制。
[0061] 当发动机当前的负荷状态为满负荷状态吋, 发动机采用过量空气系数为 0.8 0.9 的燃烧模式, 该燃烧模式是利用可变配气系统 20精确控制进气量和利用燃油喷 射系统 30精确控制燃油量, 使气缸内形成过量空气系数为 0.8~0.9的浓混合气; 同吋, 发动机利用废气再循环 (废气再循环系统 50) 调节废气回流量和废气回 流温度, 使得与当前燃烧模式下的燃烧相适配, 以确保发动机动力的有效输出
[0062] 具体地, 发动机利用废气再循环控制燃烧后的废气回流量, 其中三种燃烧模式 下的废气回流量的大小为: 过量空气系数为 1.6~2.0的稀薄燃烧模式>过量空气系 数为 1的燃烧模式 >过量空气系数为 0.8~0.9的燃烧模式。
[0063] 具体地, 发动机利用废气再循环控制燃烧后的废气回流温度, 其中三种燃烧模 式下的废气回流温度的大小为: 过量空气系数为 1.6~2.0的稀薄燃烧模式>过量空 气系数为 1的燃烧模式 >过量空气系数为 0.8~0.9的燃烧模式。
[0064] 在步骤 S4中, 发动机燃烧产生的待排放废气经催化转化后排出。 当发动机当前 的负荷状态为部分负荷状态吋, 发动机采用过量空气系数为 1.6~2.0的燃烧模式 , 发动机燃烧产生的待排放废气含有碳氢和一氧化碳, 通过催化转化器 60的催 化转化后再排出; 当发动机当前的负荷状态为大负荷状态吋, 发动机采用过量 空气系数为 1的燃烧模式, 发动机燃烧产生的待排放废气含有碳氢、 一氧化碳及 氮氧化物, 通过催化转化器 60的催化转化后再排出; 当发动机当前的负荷状态
为满负荷状态吋, 发动机采用过量空气系数为 0.8~0.9的燃烧模式, 发动机燃烧 产生的待排放废气含有碳氢、 一氧化碳及氮氧化物, 通过催化转化器 60的催化 转化后再排出。
[0065] 本发明的汽油发动机过量空气系数燃烧控制方法, 采用废气再循环技术、 燃烧 循环膨胀比大于有效压缩比的米勒循环技术、 可控制气缸内喷油量的缸内直喷 技术、 可控制气缸内进气量的可变配气系统技术以及高能点火系统控制燃烧始 点技术来控制发动机燃烧, 并采用催化转化器处理燃烧废气。 废气再循环技术 实现废气再利用, 可控制废气回流量和废气回流温度, 以对燃烧进行控制。
[0066] 如上所述, 本发明实施例的技术方案带来的有益效果是: 上述汽油发动机过量 空气系数燃烧控制方法和燃烧控制系统, 针对汽油发动机不同的运行工况, 采 用不同的过量空气系数燃烧模式, 获得汽油发动机在全工况范围内的有效热效 率、 动力性和污染物排放的综合改善效果。
[0067] 以上所述仅为本发明的较佳实施例, 并不用以限制本发明, 凡在本发明的精神 和原则之内, 所作的任何修改、 等同替换、 改进等, 均应包含在本发明的保护 范围之内。
工业实用性
[0068] 本发明实施例的汽油发动机过量空气系数燃烧控制方法和燃烧控制系统, 针对 汽油发动机不同的运行工况, 采用不同的过量空气系数燃烧模式, 获得汽油发 动机在全工况范围内的有效热效率、 动力性和污染物排放的综合改善效果。
Claims
[权利要求 1] 一种汽油发动机过量空气系数燃烧控制方法, 其特征在于, 包括步骤 监测发动机的运行工况;
根据发动机的运行工况判断发动机当前的负荷状态, 其中发动机的负 荷状态分为: 部分负荷状态、 大负荷状态及满负荷状态;
根据发动机当前的负荷状态选择相适配的过量空气系数燃烧模式, 其 中,
当发动机当前的负荷状态为部分负荷状态吋, 发动机采用过量空气系 数为 1.6~2.0的稀薄燃烧模式;
当发动机当前的负荷状态为大负荷状态吋, 发动机采用过量空气系数 为 1的燃烧模式;
当发动机当前的负荷状态为满负荷状态吋, 发动机采用过量空气系数 为 0.8~0.9的燃烧模式。
[权利要求 2] 如权利要求 1所述的汽油发动机过量空气系数燃烧控制方法, 其特征 在于, 部分负荷状态为 0~50%发动机功率运行的状态, 大负荷状态为 SOy^ ^发动机功率运行的状态, 满负荷状态为 90%~ 100%发动机功 率运行的状态。
[权利要求 3] 如权利要求 1所述的汽油发动机过量空气系数燃烧控制方法, 其特征 在于, 当发动机当前的负荷状态为部分负荷状态吋, 发动机采用过量 空气系数为 1.6~2.0的稀薄燃烧模式, 所述燃烧模式如下: 利用燃油喷 射系统精确控制燃油供给量和可变配气系统精确控制新鲜空气进气量 , 使气缸内形成过量空气系数为 1.6~2.0的稀薄混合气并进行点火; 同 吋, 发动机采用米勒循环结合废气再循环降低发动机气缸内的燃烧温 度, 使发动机气缸内的燃烧温度处于 1900K以下。
[权利要求 4] 如权利要求 3所述的汽油发动机过量空气系数燃烧控制方法, 其特征 在于, 利用废气再循环控制燃烧后的废气回流量和废气回流温度, 使 气缸内过量空气系数为 1.6~2.0的稀薄混合气在点火吋间窗口的混合气
温度等于临界自燃温度。
[权利要求 5] 如权利要求 3所述的汽油发动机过量空气系数燃烧控制方法, 其特征 在于, 所述过量空气系数为 1.6~2.0的稀薄混合气采用大于 400MJ的点 火能量进行点火。
[权利要求 6] 如权利要求 1所述的汽油发动机过量空气系数燃烧控制方法, 其特征 在于, 当所述发动机当前的负荷状态为大负荷状态吋, 发动机采用过 量空气系数为 1的燃烧模式, 所述燃烧模式如下: 利用燃油喷射系统 精确控制燃油供给量和可变配气系统精确控制新鲜空气进气量, 使气 缸内形成过量空气系数为 1的混合气并进行点火; 同吋, 发动机利用 废气再循环调节废气回流量和废气回流温度进行燃烧适配。
[权利要求 7] 如权利要求 1所述的汽油发动机过量空气系数燃烧控制方法, 其特征 在于, 当所述发动机当前的负荷状态为满负荷状态吋, 发动机采用过 量空气系数为 0.8~0.9的燃烧模式, 所述燃烧模式如下: 利用燃油喷射 系统精确控制燃油供给量和可变配气系统精确控制新鲜空气进气量, 使气缸内形成过量空气系数为 0.8~0.9的浓混合气并进行点火; 同吋, 发动机利用废气再循环调节废气回流量和废气回流温度进行燃烧适配
[权利要求 8] 如权利要求 1所述的汽油发动机过量空气系数燃烧控制方法, 其特征 在于, 该汽油发动机过量空气系数燃烧控制方法还包括利用废气再循 环控制燃烧后的废气回流量, 其中三种燃烧模式下的废气回流量的大 小为: 过量空气系数为 1.6~2.0的稀薄燃烧模式>过量空气系数为 1的 燃烧模式>过量空气系数为 0.8~0.9的燃烧模式。
[权利要求 9] 如权利要求 1所述的汽油发动机过量空气系数燃烧控制方法, 其特征 在于, 该汽油发动机过量空气系数燃烧控制方法还包括利用废气再循 环控制燃烧后的废气回流温度, 其中三种燃烧模式下的废气回流温度 的大小为: 过量空气系数为 1.6~2.0的稀薄燃烧模式>过量空气系数为
1的燃烧模式 >过量空气系数为 0.8~0.9的燃烧模式。
[权利要求 10] 如权利要求 1~9任一项所述的汽油发动机过量空气系数燃烧控制方法
, 其特征在于, 所述发动机燃烧产生的待排放废气最后经催化转化后 排出。
[权利要求 11] 一种汽油发动机过量空气系数燃烧控制系统, 其特征在于, 所述燃烧 控制系统包括气缸体结构、 可变配气系统、 燃油喷射系统、 高能点火 系统、 废气再循环系统、 工况监测系统和发动机电控单元, 所述气缸 体结构包括气缸, 所述可变配气系统用于控制新鲜空气进入所述气缸 的进气量, 所述燃油喷射系统用于控制喷射进入所述气缸的燃油量, 所述高能点火系统包括高能火花塞并用于放电点火, 所述废气再循环 系统用于控制废气回流量和废气回流温度;
所述发动机电控单元与所述工况监测系统、 所述可变配气系统、 所述 燃油喷射系统、 所述高能点火系统和所述废气再循环系统电连接; 所述工况监测系统用于监测发动机的运行工况并将监测结果传递给所 述发动机电控单元;
所述发动机电控单元根据发动机的运行工况判断发动机当前的负荷状 态, 其中发动机的负荷状态分为: 部分负荷状态、 大负荷状态及满负 荷状态;
所述发动机电控单元根据发动机当前的负荷状态选择相适配的过量空 气系数燃烧模式, 其中,
当发动机当前的负荷状态为部分负荷状态吋, 所述发动机电控单元控 制发动机采用过量空气系数为 1.6~2.0的稀薄燃烧模式;
当发动机当前的负荷状态为大负荷状态吋, 所述发动机电控单元控制 发动机采用过量空气系数为 1的燃烧模式;
当发动机当前的负荷状态为满负荷状态吋, 所述发动机电控单元控制 发动机采用过量空气系数为 0.8~0.9的燃烧模式。
[权利要求 12] 如权利要求 11所述的汽油发动机过量空气系数燃烧控制系统, 其特征 在于, 所述工况监测系统包括发动机转速监测传感器和功率监测装置
[权利要求 13] 如权利要求 11所述的汽油发动机过量空气系数燃烧控制系统, 其特征
在于, 所述废气再循环系统包括废气再循环管路、 废气再循环控制阀 、 废气再循环中冷器、 废气回流旁通管路及废气旁通阀, 所述废气再 循环管路的出气端与进气管相连通, 所述废气再循环管路的入气端与 排气管相连通, 所述废气再循环控制阀和所述废气再循环中冷器串接 设置于所述废气再循环管路中, 所述废气回流旁通管路与所述废气再 循环中冷器并联, 所述废气旁通阀设置于所述废气回流旁通管路中。
[权利要求 14] 如权利要求 11所述的汽油发动机过量空气系数燃烧控制系统, 其特征 在于, 所述废气再循环系统用于控制燃烧后的废气回流量, 其中三种 燃烧模式下的废气回流量的大小为: 过量空气系数为 1.6~2.0的稀薄燃 烧模式 >过量空气系数为 1的燃烧模式 >过量空气系数为 0.8~0.9的燃烧 模式。
[权利要求 15] 如权利要求 11所述的汽油发动机过量空气系数燃烧控制系统, 其特征 在于, 所述废气再循环系统用于控制燃烧后的废气回流温度, 其中三 种燃烧模式下的废气回流温度的大小为: 过量空气系数为 1.6~2.0的稀 薄燃烧模式 >过量空气系数为 1的燃烧模式 >过量空气系数为 0.8~0.9的 燃烧模式。
[权利要求 16] 如权利要求 11所述的汽油发动机过量空气系数燃烧控制系统, 其特征 在于, 所述高能火花塞的点火能量可点燃过量空气系数为 0.8~0.9的浓 混合气及过量空气系数为 1的混合气, 且还可点燃过量空气系数为 1.6 ~2.0的稀薄混合气。
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US16/304,700 US20190170077A1 (en) | 2016-09-30 | 2017-09-28 | Combustion control method and combustion control system with variable excess air coefficient for gasoline engine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610880511.6A CN106285985A (zh) | 2016-09-30 | 2016-09-30 | 汽油发动机过量空气系数燃烧控制方法及燃烧控制系统 |
CN201610880511.6 | 2016-09-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2018059485A1 true WO2018059485A1 (zh) | 2018-04-05 |
Family
ID=57717900
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/CN2017/103980 WO2018059485A1 (zh) | 2016-09-30 | 2017-09-28 | 汽油发动机过量空气系数燃烧控制方法及燃烧控制系统 |
Country Status (3)
Country | Link |
---|---|
US (1) | US20190170077A1 (zh) |
CN (1) | CN106285985A (zh) |
WO (1) | WO2018059485A1 (zh) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111779584A (zh) * | 2019-04-03 | 2020-10-16 | 广州汽车集团股份有限公司 | 一种燃料燃烧系统及发动机燃烧控制方法 |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106285985A (zh) * | 2016-09-30 | 2017-01-04 | 广州汽车集团股份有限公司 | 汽油发动机过量空气系数燃烧控制方法及燃烧控制系统 |
CN111379634B (zh) * | 2018-12-27 | 2021-03-12 | 广州汽车集团股份有限公司 | 稀薄燃烧发动机及汽车 |
EP3942170B1 (en) * | 2019-03-20 | 2023-07-26 | Volvo Penta Corporation | A method and a control system for controlling an internal combustion engine |
CN110284999A (zh) * | 2019-06-26 | 2019-09-27 | 浙江吉利控股集团有限公司 | 一种稀薄燃烧系统及车辆 |
CN113715796B (zh) * | 2021-07-23 | 2023-07-25 | 东风汽车集团股份有限公司 | 车辆的控制方法、装置、混动车辆和混动车辆的存储介质 |
CN114483341A (zh) * | 2022-01-12 | 2022-05-13 | 清华大学 | 掺氢天然气发动机中的燃烧控制方法 |
CN116466568B (zh) * | 2023-03-07 | 2024-03-22 | 浙江中智达科技有限公司 | 一种零手动操作控制系统、控制逻辑切换方法及装置 |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20020100454A1 (en) * | 2001-02-01 | 2002-08-01 | Nissan Motor Co., Ltd. | Air-fuel ratio control system for internal combustion engine |
US20050022778A1 (en) * | 2003-07-30 | 2005-02-03 | Nissan Motor Co., Ltd. | Engine fuel injection control system |
US20070089721A1 (en) * | 2005-10-21 | 2007-04-26 | Denso Corporation | Fuel vapor treatment apparatus |
CN102619636A (zh) * | 2012-04-01 | 2012-08-01 | 重庆长安汽车股份有限公司 | 一种汽油机节能减排燃烧方法 |
CN104500247A (zh) * | 2014-12-05 | 2015-04-08 | 清华大学 | 直喷压燃发动机全工况平面燃烧控制方法 |
CN105422327A (zh) * | 2015-12-11 | 2016-03-23 | 吉林大学 | 复合喷射双燃料内燃机可变egr进气系统及方法 |
CN105673199A (zh) * | 2016-03-01 | 2016-06-15 | 上海交通大学 | 带egr的进气掺氢富氧汽油发动机及燃烧的控制方法 |
CN106285985A (zh) * | 2016-09-30 | 2017-01-04 | 广州汽车集团股份有限公司 | 汽油发动机过量空气系数燃烧控制方法及燃烧控制系统 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE9402651L (sv) * | 1994-08-08 | 1996-02-09 | Mecel Ab | Metod för kvasi-återkopplad lean-burn reglering med smalbandig lambda sensor |
EP0983433B1 (en) * | 1998-02-23 | 2007-05-16 | Cummins Inc. | Premixed charge compression ignition engine with optimal combustion control |
JP4677935B2 (ja) * | 2006-03-14 | 2011-04-27 | 日産自動車株式会社 | NOx排出低減装置 |
CN100467844C (zh) * | 2006-11-24 | 2009-03-11 | 联合汽车电子有限公司 | 小型发动机动态闭环控制方法 |
JP4367547B2 (ja) * | 2007-11-06 | 2009-11-18 | トヨタ自動車株式会社 | 火花点火式内燃機関 |
CN100572775C (zh) * | 2008-01-02 | 2009-12-23 | 武汉理工大学 | 富氢混合气燃料发动机可燃混合气浓度控制方法及其控制装置 |
US8156730B2 (en) * | 2008-04-29 | 2012-04-17 | Cummins, Inc. | Engine performance management during a diesel particulate filter regeneration event |
CN101619670B (zh) * | 2009-01-20 | 2011-12-28 | 清华大学 | 一种汽油机火花点火激发均质压燃燃烧及控制方法 |
JP5040951B2 (ja) * | 2009-03-31 | 2012-10-03 | マツダ株式会社 | 直噴エンジンの制御方法および直噴エンジン |
CN102080598B (zh) * | 2010-12-20 | 2012-06-27 | 北京工业大学 | 一种采用二甲醚和高辛烷值燃料内燃机的控制方法 |
JP6123634B2 (ja) * | 2013-10-29 | 2017-05-10 | マツダ株式会社 | 圧縮着火式エンジンの制御装置 |
WO2018096590A1 (ja) * | 2016-11-22 | 2018-05-31 | マツダ株式会社 | 圧縮自己着火式エンジンの制御装置 |
-
2016
- 2016-09-30 CN CN201610880511.6A patent/CN106285985A/zh active Pending
-
2017
- 2017-09-28 US US16/304,700 patent/US20190170077A1/en not_active Abandoned
- 2017-09-28 WO PCT/CN2017/103980 patent/WO2018059485A1/zh active Application Filing
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20020100454A1 (en) * | 2001-02-01 | 2002-08-01 | Nissan Motor Co., Ltd. | Air-fuel ratio control system for internal combustion engine |
US20050022778A1 (en) * | 2003-07-30 | 2005-02-03 | Nissan Motor Co., Ltd. | Engine fuel injection control system |
US20070089721A1 (en) * | 2005-10-21 | 2007-04-26 | Denso Corporation | Fuel vapor treatment apparatus |
CN102619636A (zh) * | 2012-04-01 | 2012-08-01 | 重庆长安汽车股份有限公司 | 一种汽油机节能减排燃烧方法 |
CN104500247A (zh) * | 2014-12-05 | 2015-04-08 | 清华大学 | 直喷压燃发动机全工况平面燃烧控制方法 |
CN105422327A (zh) * | 2015-12-11 | 2016-03-23 | 吉林大学 | 复合喷射双燃料内燃机可变egr进气系统及方法 |
CN105673199A (zh) * | 2016-03-01 | 2016-06-15 | 上海交通大学 | 带egr的进气掺氢富氧汽油发动机及燃烧的控制方法 |
CN106285985A (zh) * | 2016-09-30 | 2017-01-04 | 广州汽车集团股份有限公司 | 汽油发动机过量空气系数燃烧控制方法及燃烧控制系统 |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111779584A (zh) * | 2019-04-03 | 2020-10-16 | 广州汽车集团股份有限公司 | 一种燃料燃烧系统及发动机燃烧控制方法 |
CN111779584B (zh) * | 2019-04-03 | 2022-05-17 | 广州汽车集团股份有限公司 | 一种燃料燃烧系统及发动机燃烧控制方法 |
Also Published As
Publication number | Publication date |
---|---|
US20190170077A1 (en) | 2019-06-06 |
CN106285985A (zh) | 2017-01-04 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Zheng et al. | Effect of equivalence ratio on combustion and emissions of a dual-fuel natural gas engine ignited with diesel | |
WO2018059485A1 (zh) | 汽油发动机过量空气系数燃烧控制方法及燃烧控制系统 | |
Zeng et al. | Combustion characteristics of a direct-injection natural gas engine under various fuel injection timings | |
JP5136721B2 (ja) | 内燃機関の燃料噴射制御装置 | |
US8555852B2 (en) | Gaseous-fuelled stoichiometric compression ignition internal combustion engine | |
KR101693895B1 (ko) | 복합 착화방식의 디젤-가솔린 혼합연소엔진과 그 제어방법 및 복합 착화방식의 디젤-가솔린 혼합연소시스템 | |
US9482166B2 (en) | Method of controlling a direct-injection gaseous-fuelled internal combustion engine system with a selective catalytic reduction converter | |
US7900600B2 (en) | Homogeneous charge compressed ignition engine operating method | |
CN101215996A (zh) | 一种燃料现场混合压燃内燃机及控制方法 | |
US11578684B2 (en) | Method for operating an engine | |
US10961943B1 (en) | Method and system for controlling combustion of natural gas engine | |
KR20130069081A (ko) | 가솔린/디젤 연료 혼합 압축 착화 연소 엔진의 이지알 제어 시스템 및 그 방법 | |
WO2014084023A1 (ja) | 天然ガスエンジン及び天然ガスエンジンの運転方法 | |
JP2018040264A (ja) | 内燃機関の制御装置 | |
JP2018040263A (ja) | 内燃機関の制御装置 | |
WO2024109963A2 (zh) | 一种可控温电热塞辅助压燃式甲醇发动机及其控制方法 | |
CN102226426A (zh) | 基于活化热氛围的双燃料复合均质压燃燃烧系统 | |
Hu et al. | Experimental Research on Performance Development of Direct Injection Hydrogen Internal Combustion Engine with High Injection Pressure | |
JP2004510910A (ja) | 内燃機関作動方法および内燃機関作動用コンピュータプログラムならびに内燃機関 | |
JP5115660B2 (ja) | 内燃機関の燃料噴射制御装置 | |
JP6398543B2 (ja) | 天然ガスエンジン及び天然ガスエンジンの運転方法 | |
Babu et al. | Experimental investigation on performance and emission characteristics of dual fuel split injection of ethanol and diesel in CI engine | |
JP2004278428A (ja) | ディーゼルエンジン及びその運転方法 | |
US20100288225A1 (en) | Clean air reciprocating internal combustion engine | |
Dinesh et al. | Experimental investigation on HCCI engine with gasoline injection |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 17854935 Country of ref document: EP Kind code of ref document: A1 |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
122 | Ep: pct application non-entry in european phase |
Ref document number: 17854935 Country of ref document: EP Kind code of ref document: A1 |