WO2002097255A1 - Moteur thermique a allumage par compression - Google Patents
Moteur thermique a allumage par compression Download PDFInfo
- Publication number
- WO2002097255A1 WO2002097255A1 PCT/JP2001/004271 JP0104271W WO02097255A1 WO 2002097255 A1 WO2002097255 A1 WO 2002097255A1 JP 0104271 W JP0104271 W JP 0104271W WO 02097255 A1 WO02097255 A1 WO 02097255A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- internal combustion
- combustion engine
- type internal
- ignition
- compression ignition
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 289
- 230000006835 compression Effects 0.000 title claims abstract description 207
- 238000007906 compression Methods 0.000 title claims abstract description 207
- 239000000446 fuel Substances 0.000 claims abstract description 267
- 238000002347 injection Methods 0.000 claims abstract description 225
- 239000007924 injection Substances 0.000 claims abstract description 225
- 101710154918 Trigger factor Proteins 0.000 claims abstract description 61
- 239000000203 mixture Substances 0.000 claims abstract description 24
- 239000007921 spray Substances 0.000 claims description 18
- 238000001514 detection method Methods 0.000 claims description 16
- 230000007246 mechanism Effects 0.000 claims description 9
- 239000012530 fluid Substances 0.000 claims description 5
- 210000000056 organ Anatomy 0.000 claims 2
- 238000010586 diagram Methods 0.000 description 36
- 238000000034 method Methods 0.000 description 33
- 239000007789 gas Substances 0.000 description 27
- 230000008569 process Effects 0.000 description 16
- 239000003054 catalyst Substances 0.000 description 11
- 230000000694 effects Effects 0.000 description 6
- 239000000498 cooling water Substances 0.000 description 4
- 238000009792 diffusion process Methods 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 3
- 239000013626 chemical specie Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 230000000994 depressogenic effect Effects 0.000 description 2
- 238000011049 filling Methods 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 238000000746 purification Methods 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- 235000009781 Myrtillocactus geometrizans Nutrition 0.000 description 1
- 240000009125 Myrtillocactus geometrizans Species 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- 239000003570 air Substances 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 238000009841 combustion method Methods 0.000 description 1
- 238000006356 dehydrogenation reaction Methods 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 230000020169 heat generation Effects 0.000 description 1
- 239000008240 homogeneous mixture Substances 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000004043 responsiveness Effects 0.000 description 1
- 239000004071 soot Substances 0.000 description 1
- 238000001694 spray drying Methods 0.000 description 1
- 230000007480 spreading Effects 0.000 description 1
- 230000001629 suppression Effects 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M67/00—Apparatus in which fuel-injection is effected by means of high-pressure gas, the gas carrying the fuel into working cylinders of the engine, e.g. air-injection type
- F02M67/02—Apparatus in which fuel-injection is effected by means of high-pressure gas, the gas carrying the fuel into working cylinders of the engine, e.g. air-injection type the gas being compressed air, e.g. compressed in pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N11/00—Monitoring or diagnostic devices for exhaust-gas treatment apparatus, e.g. for catalytic activity
- F01N11/002—Monitoring or diagnostic devices for exhaust-gas treatment apparatus, e.g. for catalytic activity the diagnostic devices measuring or estimating temperature or pressure in, or downstream of the exhaust apparatus
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B77/00—Component parts, details or accessories, not otherwise provided for
- F02B77/08—Safety, indicating, or supervising devices
- F02B77/085—Safety, indicating, or supervising devices with sensors measuring combustion processes, e.g. knocking, pressure, ionization, combustion flame
-
- 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
- F02D13/0203—Variable control of intake and exhaust valves
- F02D13/0207—Variable control of intake and exhaust valves changing valve lift or valve lift and timing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D35/00—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for
- F02D35/02—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions
- F02D35/027—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions using knock sensors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D37/00—Non-electrical conjoint control of two or more functions of engines, not otherwise provided for
- F02D37/02—Non-electrical conjoint control of two or more functions of engines, not otherwise provided for one of the functions being ignition
-
- 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
- F02D41/30—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
-
- 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
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/32—Controlling fuel injection of the low pressure type
- F02D41/34—Controlling fuel injection of the low pressure type with means for controlling injection timing or duration
- F02D41/345—Controlling injection timing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F1/00—Cylinders; Cylinder heads
- F02F1/24—Cylinder heads
- F02F1/42—Shape or arrangement of intake or exhaust channels in cylinder heads
- F02F1/4214—Shape or arrangement of intake or exhaust channels in cylinder heads specially adapted for four or more valves per cylinder
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/162—Means to impart a whirling motion to fuel upstream or near discharging orifices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1853—Orifice plates
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M67/00—Apparatus in which fuel-injection is effected by means of high-pressure gas, the gas carrying the fuel into working cylinders of the engine, e.g. air-injection type
- F02M67/06—Apparatus in which fuel-injection is effected by means of high-pressure gas, the gas carrying the fuel into working cylinders of the engine, e.g. air-injection type the gas being other than air, e.g. steam, combustion gas
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/08—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
- F01N3/10—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
- F01N3/18—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by methods of operation; Control
- F01N3/20—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by methods of operation; Control specially adapted for catalytic conversion ; Methods of operation or control of catalytic converters
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B1/00—Engines characterised by fuel-air mixture compression
- F02B1/12—Engines characterised by fuel-air mixture compression with compression ignition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/12—Other methods of operation
- F02B2075/125—Direct injection in the combustion chamber for spark ignition engines, i.e. not in pre-combustion chamber
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B7/00—Engines characterised by the fuel-air charge being ignited by compression ignition of an additional fuel
-
- 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
- F02D2041/3088—Controlling fuel injection for air assisted injectors
-
- 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
- F02D2200/50—Input parameters for engine control said parameters being related to the vehicle or its components
- F02D2200/501—Vehicle speed
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2250/00—Engine control related to specific problems or objectives
- F02D2250/18—Control of the engine output torque
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D35/00—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for
- F02D35/02—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions
- F02D35/021—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions using an ionic current sensor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M51/00—Fuel-injection apparatus characterised by being operated electrically
- F02M51/06—Injectors peculiar thereto with means directly operating the valve needle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M51/00—Fuel-injection apparatus characterised by being operated electrically
- F02M51/06—Injectors peculiar thereto with means directly operating the valve needle
- F02M51/061—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
-
- 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
-
- 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 a compression ignition type internal combustion engine in which a premixed gas supplied into a combustion chamber is self-ignited by piston compression, and more particularly to a compression ignition type internal combustion engine in a wide engine operation region.
- the present invention relates to a compression ignition type internal combustion engine capable of appropriately controlling a self ignition timing.
- a compression ignition type internal combustion engine adopting a combustion method in which a premixed gas supplied into a combustion chamber is self-ignited by piston compression is disclosed in, for example, JP-A-10-56413. Things are known.
- the compression ignition type internal combustion engine is capable of operating in an ultra-lean region (air-fuel ratio of 80 or more) that cannot be achieved with conventional gasoline and diesel engines, and achieves flame temperature reduction and ignition combustion with a homogeneous mixture. A large, simultaneous reduction of NOx and soot is possible.
- the conventional compression ignition type internal combustion engine has the following problems.
- the pressure and temperature of the mixture of fuel and air rise due to piston compression after the intake valve is closed.
- the ignition timing will fluctuate and misfires will occur, making normal engine operation difficult.
- the self-ignition of the air-fuel mixture is affected not only by the temperature and pressure in the combustion chamber, but also by the air-fuel ratio of the air-fuel mixture. Therefore, the ignition timing differs depending on the state of fuel diffusion in the combustion chamber. Fluctuations and torque fluctuations between cylinders have become problems.
- a control piston as an auxiliary compression means is provided in the combustion chamber, and this is actuated near the top dead center to make the combustion chamber work.
- a compression ignition type internal combustion engine is known in which the volume is reduced and the temperature of the mixture is transiently increased to control the ignition timing of the mixture.
- the control of the pressure and temperature in the combustion chamber can be controlled by adding a control piston to make the volume of the combustion chamber variable.
- the system was complicated due to a drastic change in the shape of the engine, the vehicle mountability deteriorated, and the cost increased.
- An object of the present invention is to provide a compression ignition type internal combustion engine that can be controlled to an appropriate self-ignition timing in an engine operation region where a load and a rotation speed are wide without largely changing a combustion chamber shape.
- the present invention provides a combustion chamber to which air and fuel are supplied, an intake valve that opens and closes a passage between an intake port communicating with the combustion chamber and the combustion chamber, An exhaust port that communicates with the exhaust chamber, and an exhaust valve that opens and closes a passage of the combustion chamber.
- the piston compression operation after the intake valve is closed raises the temperature and pressure in the combustion chamber to self-ignite the air-fuel mixture.
- the ignition trigger factor is set according to the operating conditions of the compression ignition type internal combustion engine so that the air-fuel mixture during piston compression or expansion can be ignited.
- Ignition trigger factor injection means for injecting directly into the combustion chamber at any time while the valve is closed, and at least one of the injection timing, injection amount, and injection pressure of the ignition trigger factor according to the operating conditions. Is also provided with control means for controlling one.
- FIG. 1 is a block diagram showing a configuration of a compression ignition type internal combustion engine according to a first embodiment of the present invention.
- FIG. 2 is a plan view showing a configuration near a combustion chamber of the compression ignition type internal combustion engine according to the first embodiment of the present invention.
- FIG. 3 is a flowchart showing an ignition control method for the compression ignition type internal combustion engine according to the first embodiment of the present invention.
- FIG. 4 is an operation explanatory diagram of the compression ignition type internal combustion engine according to the first embodiment of the present invention. '
- FIG. 5 is an operation explanatory diagram of another example of the compression ignition type internal combustion engine according to the first embodiment of the present invention.
- FIG. 6 is a block diagram showing a configuration of a compression ignition type internal combustion engine of a second example used for compression ignition control according to the first embodiment of the present invention.
- FIG. 7 is a block diagram showing a configuration of a compression ignition type internal combustion engine of a third example used for compression ignition control according to the first embodiment of the present invention.
- FIG. 8 is a block diagram illustrating a configuration of a compression ignition type internal combustion engine of a fourth example used for compression ignition control according to the first embodiment of the present invention.
- FIG. 9 is a block diagram showing a configuration of a compression ignition type internal combustion engine according to the second embodiment of the present invention.
- FIG. 10 is a plan view showing a configuration near a combustion chamber of a compression ignition type internal combustion engine according to a second embodiment of the present invention.
- FIG. 11 is an explanatory diagram of a configuration of a fuel injection valve used for a compression ignition type internal combustion engine according to a second embodiment of the present invention.
- FIG. 12 shows an ignition control method for a compression ignition type internal combustion engine according to a second embodiment of the present invention. It is a flowchart which shows.
- FIG. 13 is an explanatory diagram of an operation of the compression ignition type internal combustion engine according to the second embodiment of the present invention.
- FIG. 14 is an explanatory diagram of the relationship between the fuel pressure and the air-fuel ratio of the rich spot when a predetermined time has elapsed under a constant atmospheric pressure in the compression ignition type internal combustion engine according to the second embodiment of the present invention.
- FIG. 15 is a flowchart showing a second ignition control method for the compression ignition type internal combustion engine according to the second embodiment of the present invention.
- FIG. 16 is an explanatory diagram of a second configuration of the fuel injection valve used for the compression ignition type internal combustion engine according to the second embodiment of the present invention.
- FIG. 17 is an explanatory diagram of a third configuration of the fuel injection valve used in the compression ignition type internal combustion engine according to the second embodiment of the present invention.
- FIG. 18 is an explanatory diagram of a fourth configuration of the fuel injection valve used in the compression ignition type internal combustion engine according to the second embodiment of the present invention.
- FIG. 19 is an explanatory diagram of a fifth configuration of the fuel injection valve used in the compression ignition type internal combustion engine according to the second embodiment of the present invention.
- FIG. 20 is a block diagram showing the configuration of the compression ignition type internal combustion engine according to the third embodiment of the present invention.
- FIG. 21 is a flowchart showing an ignition control method for a compression ignition type internal combustion engine according to the third embodiment of the present invention.
- FIG. 22 is an explanatory diagram of the operation of the compression ignition type internal combustion engine according to the third embodiment of the present invention.
- FIG. 23 is a characteristic diagram of another example of the fuel injection valve used for the compression ignition type internal combustion engine in each embodiment of the present invention.
- BEST MODE FOR CARRYING OUT THE INVENTION The configuration and operation of a compression ignition type internal combustion engine according to a first embodiment of the present invention will be described below with reference to FIGS. First, the configuration of the compression ignition type internal combustion engine according to the present embodiment will be described with reference to FIGS.
- FIG. 1 is a block diagram showing a configuration of a compression ignition type internal combustion engine according to a first embodiment of the present invention
- FIG. 2 is a combustion diagram of a compression ignition type internal combustion engine according to the first embodiment of the present invention. It is a top view showing composition of a room neighborhood.
- an intake port 6 and an exhaust port 14 communicate with a combustion chamber 16 surrounded by a cylinder block 9, a piston 17 and a cylinder head 10.
- an intake valve 19a is provided to open and close the passage with the combustion chamber 16.
- An exhaust valve 19b is provided at the connection between the combustion chamber 16 and the exhaust port 14 to open and close the passage with the combustion chamber 16.
- the intake port 6 is branched into two and connected to the combustion chamber 16, and an intake valve 19a is provided at each connection.
- the exhaust port 14 is branched into two and connected to the combustion chamber 16, and an exhaust valve 19b is provided at each connection portion.
- the reciprocating motion of the piston 17 is transmitted to the crankshaft 21 via the connecting rod 20 to rotate the crankshaft 21.
- a spark plug 13 is disposed in the combustion chamber 16.
- spark ignition combustion is instructed from the engine control unit (ECU) 1
- spark discharge from the spark plug 13 is performed.
- the ignition plug 13 can also function as an ion current detector for detecting the combustion state. In that case, the combustion state in the combustion chamber 16 And monitor the ignition timing.
- the ignition plug 13 is not used and any operating region is to be ignited by compression ignition combustion, that is, only by piston compression, the ignition plug 13 need not be provided.
- the spark plug 13 is provided in the upper center of the combustion chamber 16 as shown in FIG. 2, but is not particularly limited to this location.
- the ECU 1 includes output values of an accelerator opening degree detecting device 2a and a brake pedal force detecting device 2b as driver intention detecting means for detecting an intention of a driver for driving a vehicle equipped with the compression ignition type internal combustion engine of the present embodiment. Also, an output value of a vehicle speed detecting device 2c as a vehicle running state detecting means for detecting a vehicle running state, and an air flow sensor 5 for detecting engine operating conditions, an engine cooling water temperature sensor 24, an air-fuel ratio sensor 22, catalyst Output values from the post-catalyst exhaust temperature sensor 23, the crank angle sensor 4, and the knock sensor 25, which are installed behind 12, are sequentially captured. At this time, it is desirable that the air flow sensor 5 has a function of measuring the intake air temperature, and this output value is also taken into the ECU 1 at the same time.
- the target torque of the engine is estimated from the output value of the accelerator opening detection device 2a and the vehicle speed.
- the differential value of the vehicle speed sensor attached to the vehicle is used as a means for grasping the acceleration of the vehicle equipped with the compression ignition type internal combustion engine. It may be used.
- the output value of the brake depression force detector 2b uses the ON / OFF signal that determines whether the driver has depressed the brake pedal, but it is also possible to install a brake depression force sensor behind the brake pedal and use that output value. It is also possible to provide a hydraulic pressure sensor in the hydraulic piping of the rake, so that the driver's braking force can be grasped.
- the fuel injection valve 11 is installed so that fuel can be directly injected into the combustion chamber 16.
- the fuel injection valve 11 is installed between the branched intake ports 6 as shown in FIG.
- the fuel injection valve 11 is located near the inner surface of the combustion chamber 16 near the intake valve 19a, but it does not specify the location, and any fuel that can be injected into the combustion chamber 16 is not specified. Good thing in place.
- the fuel injection valve 11 is an air-assisted injector capable of injecting two fluids, air and fuel, and is capable of injecting only fuel, injecting only air, and simultaneously injecting fuel and air.
- a fuel system and an air system are introduced into the fuel injection valve 11, which is an air-assist injection.
- the air pump 26 is configured to be able to constantly supply air pressure of 5 MPa or more to the fuel injection valve 11.
- the pressure regulator 28 is provided in a bypass passage 30 that bypasses the air pump 26, and controls the air pressure fed to the fuel injection valve 11. The pressure is controlled according to engine operating conditions and cylinder pressure.
- the solenoid valve 27 opens and closes in response to a control signal from the ECU 1 to control the amount of air fed to the fuel injection valve 11. With these configurations, any air pressure, air amount and fuel pressure, and fuel amount can be supplied to the fuel injector 11 and eventually the combustion chamber 16 according to the operating conditions of the engine. Will be able to pay.
- FIG. 3 is a flowchart showing an ignition control method for the compression ignition type internal combustion engine according to the first embodiment of the present invention
- FIG. 4 is an operation explanatory diagram of the compression ignition type internal combustion engine according to the first embodiment of the present invention. It is.
- step S101 the ECU 1 reads the accelerator opening based on the output value of the accelerator opening detecting device 2a, and reads the accelerator opening based on the output value of the brake pedal force detecting device 2b.
- the driver's intention of the vehicle equipped with the compression ignition type internal combustion engine is read.
- step S102 the ECU 1 reads the output value of the vehicle speed detecting device 2c to detect the vehicle running conditions.
- Air flow sensor 5 engine cooling water temperature sensor 24, air-fuel ratio sensor 22, post-catalyst exhaust temperature sensor 23 installed behind catalyst 12, crank angle sensor 4, knock sensor 25, etc.
- the ECU 1 calculates the target torque of the engine based on the vehicle running conditions and the engine operating conditions.
- step S103 the ECU 1 determines whether or not operation by compression ignition is possible based on the driver intention read in step S101 and the engine target torque calculated in step S102. Is determined.
- step S104 If it is determined in step S103 that operation is not possible, the process proceeds to step S104. If the engine is a spark ignition engine, for example, spark ignition combustion, or if the engine is a diesel engine without a spark plug, Controls each parameter of the engine to perform spray combustion. ,
- step S105 If it is determined in step S103 that operation by compression ignition is possible, control is performed in the compression ignition combustion mode in steps S105 and subsequent steps.
- step S 105 the ECU 1 reads the intake air amount according to the current engine operation condition from the map stored in the ECU 1 in advance. Recall and determine the fuel injection amount and fuel injection timing.
- step S106 the ECU 1 determines whether the ignition trigger Determine the injection quantity, injection pressure and injection timing.
- the ignition trigger factor will be described with reference to FIG.
- the horizontal axis shows the exhaust process EXH, the intake process INT, the compression stroke COM, and the expansion process EXP of the internal combustion engine
- the vertical axis shows the combustion chamber pressure P and the fuel injection timing, respectively.
- INJ (Fu) indicates the timing of pressurized air injection INJ (Air).
- the fuel injection timing TF1 is near the intake bottom dead center BDCin, which is determined in step S105.
- the compressed air is injected from the fuel injection valve near the compression top dead center TDCcom. The injection timing, injection amount, and injection pressure of the compressed air are determined in step S106.
- the outlet B1 fresh air is supplied into the combustion chamber 16 during the intake stroke.
- fuel is injected from the fuel injection valve at the fuel injection timing INKFu) near the intake bottom dead center BDCin.
- the injected fuel diffuses into the combustion chamber 16 as shown in a blowout B3 to form a premixed gas.
- the configuration is such that self ignition does not occur by the top dead center at this premixed air temperature, air-fuel ratio, and engine compression ratio.
- Pressurized air is injected from the fuel injection valve at the pressurized air injection timing INJ (Air) near the compression top dead center TDCcom, as shown in Blowout B4, to the premixture that has been compressed by the piston. .
- INJ Air
- This pressurized air is the ignition trigger factor.
- the pressure P in the combustion chamber 16 rises rapidly as shown by the solid line P1, and reaches the temperature and pressure conditions under which the premixed gas can ignite, leading to ignition.
- the pressure of the injected compressed air is adjusted by the air pump 26 and the regulator 28 so that the pressure of the compressed air is larger than the pressure in the combustion chamber 16, and the compressed air to be injected is adjusted. Is determined by the signal from the ECU 1.
- the ECU 1 executes fuel injection control and air amount control to operate the parameters so as to satisfy the determined fuel injection condition and air amount condition.
- step S108 the ECU1 adjusts the air pressure and injects air into the combustion chamber.
- step S110 the ECU 1 requests the generated torque at this time. Whether the torque has been reached is estimated from the current accelerator opening. If the estimated value has not reached the target torque, the process proceeds to step S109, and if it has, the process proceeds to step S110.
- step S109 the ECU 1 determines whether the ignition timing is normal.
- the ignition timing is detected by detecting the ion current generated between the electrodes of the ignition plug or by using the output value of the knock sensor 25.
- the compression sensor that monitors the pressure history in the combustion chamber 16 is used for the compression ignition type internal combustion engine. It may be provided to make a determination based on the output signal.
- step S108 If the ignition timing is not normal, the process returns to step S108, and feedback control is performed on the injection amount, injection pressure, and injection timing of the ignition trigger factor so that the ignition timing becomes normal.
- step S107 If the ignition timing is normal and the target torque has not been reached, the flow returns to step S107, and the fuel injection amount, the injection timing, and the intake air amount are fed-pack controlled to achieve the target torque.
- step S111 it is determined whether ECU1 is the target air-fuel ratio.
- the air-fuel ratio detecting means at this time is the air-fuel ratio sensor 22 shown in FIG. 1, and the output value determines the air-fuel ratio during engine operation.
- step S107 If it is not the target air-fuel ratio, the flow returns to step S107, and the intake air amount and the fuel injection amount are feedback-controlled.
- the control ends.
- the exhaust gas purification efficiency of the catalyst 12 shown in FIG. 1 can be controlled to an optimum value.
- injection control of the ignition trigger factor may be a method of performing feedback control such as the ignition timing as shown in the figure, but it is also possible to operate only by control based on a map recorded in ECU1.
- pressurized air is injected near the compression top dead center to increase the degree of filling in the combustion chamber, thereby increasing the temperature and pressure of the air-fuel mixture during compression of the piston.
- compression ignition becomes possible even when the ignition trigger is used and the air-fuel ratio is set to be low. Therefore, it is possible to control the appropriate self-ignition timing in an engine operating region where the load and the number of revolutions are wide without significantly changing the shape of the combustion chamber.
- the configuration of the compression ignition type internal combustion engine according to the present embodiment is the same as that shown in FIG.
- the configuration near the combustion chamber of the compression ignition type internal combustion engine according to the present embodiment is the same as that shown in FIG.
- FIG. 5 is an operation explanatory diagram of another example of the compression ignition type internal combustion engine according to the first embodiment of the present invention.
- the same reference numerals as those in FIG. 4 indicate the same parts.
- the ignition trigger factor not only the pressurized air described with reference to FIG. 4 but also the pressurized air and the fuel are simultaneously injected as shown by a blowout B 4 ′.
- Pressurized air is injected from the fuel injection valve at the pressurized air injection timing INJ (Air) near the compression top dead center TDCcom as shown in the outlet B 4 ′ to the premixture compressed by the piston.
- fuel is injected from the fuel injection valve at the fuel injection timing INJ (Fu).
- This pressurized air and fuel are ignition trigger factors.
- the pressure P in the combustion chamber 16 rises rapidly as shown by the solid line P1, and reaches the temperature and pressure conditions under which the premixed gas can be ignited, causing ignition. Will be reached.
- step S106 ECU1 determines the injection amount, injection pressure, and injection timing of air and fuel, which are ignition trigger factors. Then, when the piston is near the compression top dead center and it is time to inject the ignition trigger factor, in step S108, the ECU 1 injects air and fuel into the combustion chamber. Then, in the determination of step S110, the generated torque has not reached the target torque. If the ignition timing is not normal in the determination of step S109, the process returns to step S108, and Feedback control is performed on the injection amount, injection pressure, and injection timing of the ignition trigger factor so that the ignition timing becomes normal.
- the injection control of the compressed air is performed near the compression top dead center, so that the same ignition control effect as that of FIG. 3 can be obtained. Also air injection
- the air-fuel ratio in the spray can be controlled, making it possible to control not only the ignition timing but also the combustion speed after ignition, making it possible to optimize the engine Realizes torque generation.
- FIG. 6 is a block diagram showing a configuration of a compression ignition type internal combustion engine of a second example used for compression ignition control according to the first embodiment of the present invention.
- the same reference numerals as those in FIG. 1 indicate the same parts.
- a fuel injection valve 50 for injecting fuel and an air injection valve 51 for injecting air are separately provided. Even in such a configuration, optimal ignition control can be performed in the same manner as in the embodiment shown in FIGS.
- the arrangement of the fuel injection valve 50 and the air injection valve 51 is not limited to the location shown in the drawing, and the same effects as described above can be obtained in an arbitrary arrangement.
- FIG. 7 is a block diagram showing a configuration of a compression ignition type internal combustion engine of a third example used for compression ignition control according to the first embodiment of the present invention.
- the same reference numerals as those in FIG. 1 indicate the same parts.
- the fuel injection valve 52 for injecting fuel and the air injection valve 51 which is an ignition trigger factor are separated, and the fuel injection valve 52 is disposed inside the intake port 6. Even in such a configuration, optimal ignition control can be performed in the same manner as in the embodiment shown in FIGS.
- FIG. 8 is a fourth example used for compression ignition control according to the first embodiment of the present invention.
- FIG. 2 is a block diagram illustrating a configuration of a compression ignition type internal combustion engine. The same reference numerals as those in FIG. 1 indicate the same parts.
- a fuel system and an ignition trigger gas cylinder 54 are connected to a fuel injection valve 53 for injecting fuel.
- the ignition trigger factor can be a gas other than air, for example, hydrogen, carbon dioxide, nitrogen, etc.
- the gas in the mounted gas cylinder 54 can be changed according to the characteristics of the engine and the mode of use. It is also possible to use them in consideration of ignitability. Even with such a configuration, optimal ignition control can be performed in the same manner as in the embodiment shown in FIGS.
- the arrangement of the fuel injection valve 53 is not limited to the location shown in the figure, and the same effect as described above can be obtained with an arbitrary arrangement on the side and top surfaces of the combustion chamber 16.
- the ignition trigger factor by injecting gas, such as air, into the combustion chamber when it is desired to ignite, the pressure in the combustion chamber is increased, and the optimum ignition timing can be obtained under a wide range of operating conditions, and by controlling these for each cylinder, ignition control can be easily performed for each cylinder and each cycle.
- gas such as air
- the combustion trigger is generated by accumulating the burned gas in the sub-chamber connected to the combustion chamber using the combustion pressure of the previous cycle and injecting it in the next cycle. It is needless to say that the configuration of the present embodiment is also within the scope of the present embodiment.
- a combustion chamber pressure detecting means such as a pressure sensor for detecting the pressure in the combustion chamber is provided, and the injection pressure of the ignition trigger factor is controlled according to the detection result of the pressure in the combustion chamber and the engine operating conditions. Can also.
- means for detecting an operation state of the ignition trigger factor injection means for detecting the pressure of the compressed air and means for detecting an operation state of the compression ignition type internal combustion engine, and an operation state of the ignition trigger factor injection means.
- the engine operation by self-ignition combustion is judged to be inappropriate or impossible based on at least one of the detection result of the means for detecting the combustion state and the detection result of the means for detecting the operating state of the compression ignition type internal combustion engine. Can be controlled to prohibit engine operation by self-ignition combustion.
- the fuel in order to increase the temperature and pressure of the air-fuel mixture during compression of the piston, the fuel is injected near the compression top dead center, or pressurized air and fuel are injected. It is characterized by doing.
- the fluid to be injected is compressed air or compressed air.
- the gas is not limited to fuel, and gases other than air can be used.
- FIG. 9 is a block diagram showing a configuration of a compression ignition type internal combustion engine according to the second embodiment of the present invention.
- FIG. 10 is a combustion diagram of the compression ignition type internal combustion engine according to the second embodiment of the present invention. It is a top view showing composition of a room neighborhood. 1 and 2 denote the same parts.
- the fuel injection valve 59 used in the present embodiment has a plurality of injection holes in the nozzle portion.
- the fuel 57 is adjusted in fuel pressure by a fuel pump 58, and is injected into a combustion chamber 16 by a fuel injection service 59.
- the ECU 1 controls the fuel pressure using the fuel pump 58 in accordance with the engine operating conditions.
- FIG. 11 is an explanatory diagram of a configuration of a fuel injection valve used for a compression ignition type internal combustion engine according to a second embodiment of the present invention.
- FIG. 11 (A) is a front view showing the overall configuration of the fuel injection valve used in the present embodiment
- FIG. 11 (B) is a cross-sectional view of a main part of the fuel injection valve used in the present embodiment.
- FIG. 11 (C) is a bottom view of the fuel injection valve used in the present embodiment.
- a plurality of fuel sprays are injected from the tip of the fuel injection valve 69.
- a nozzle 75 is provided at the tip of the fuel injection valve. ing. At the tip of the nozzle 75, a main injection hole 78 is formed. Inside the nozzle 75, a plunger 74 and a swirler 73 are arranged. A pole 76 is attached to the tip of the plunger 74. Between the stirrer 73 and the nozzle 75, a fuel passage 71 and a swirler single passage 72 are formed. When the nozzle 75 moves up and down, the pole 76 opens and closes the main injection hole 78, and the fuel supplied through the fuel passage 71 and the swirler one-way passage 72 is ejected from the main injection hole 78. An atomizer 79 is provided at the tip of the nozzle 75.
- the atomizer 79 is provided with a plurality of sub injection holes 77. Fuel injected from the main injection holes 78 is injected into the combustion chamber 16 from the plurality of sub injection holes 77.
- a ball having another shape such as a conical shape can be used.
- injection holes are arranged linearly, but the arrangement and number are not limited to this.
- a plurality of injection holes are provided and each injection hole is sprayed with fuel. Any configuration may be used so long as they are arranged so as to interfere with each other, and it is clear that all such configurations are within the scope of the present embodiment.
- FIG. 12 is a flowchart showing an ignition control method for a compression ignition type internal combustion engine according to the second embodiment of the present invention
- FIG. 13 is a diagram illustrating the operation of the compression ignition type internal combustion engine according to the second embodiment of the present invention.
- FIG. 14 is an explanatory diagram of the relationship between the fuel pressure and the air-fuel ratio of the rich spot when a predetermined time has elapsed under a constant atmospheric pressure in the compression ignition internal combustion engine according to the second embodiment of the present invention. .
- step S112 the ECU 1 reads the engine operating conditions.
- step S113 the ECU 1 determines a target torque of the engine.
- step S114 the ECU 1 determines the intake air amount, the fuel injection amount, and the fuel injection timing based on the result in step S113.
- step S115 the ECU 1 determines the fuel pressure and the fuel injection period based on the result in step S113.
- step S116 the ECU 1 controls the fuel pump 58 to The fuel pressure of the fuel pump 58 is controlled to a predetermined fuel pressure.
- step S117 the ECU 1 executes air amount control and fuel injection.
- the spray 70 a injected from the respective injection holes of the fuel injection valve 69 shown in FIG. 11 interferes in the combustion chamber, and the fuel-rich portion 7 O b ( Hereinafter, this is referred to as “rich spot”.
- the rich spot 7 Ob has a large particle size due to the collision (1000 ⁇ ) of the spray 70a, so the fuel diffusion is slower than in other parts of the spray 70a.
- the vaporization of the fuel progresses, and a lean air-fuel mixture 66a is formed in a relatively wide area in the combustion chamber 16 as shown by a blowout B3.
- the air-fuel mixture When the air-fuel mixture reaches the top dead center due to the compression of the piston, it ignites from a region where the air-fuel ratio is relatively large, that is, the vicinity of the rich spot 7 Ob, as indicated by a blowout B3.
- the ignition of the rich spot 70b sharply raises the temperature and pressure in the combustion chamber 16 and, as a result, ignition occurs even in the lean region 66a.
- the time difference between the ignition timing in the vicinity of the rich spot 70b and the ignition timing in the lean region 66a is very small, it is no problem even if the ignitions are substantially simultaneous.
- the point is that the rich spot 70 b due to the spray interference is used as an ignition trigger.
- the air-fuel ratio of the rich spot 70b can be controlled by changing the particle size according to the fuel pressure.However, at the time of ignition, the air-fuel ratio in the vicinity should be near the stoichiometric air-fuel ratio or richer than it. Is desirable.
- the air-fuel ratio of the rich spot is increased, that is, lean, indicating that the compression ignition timing is delayed.
- the air-fuel ratio in the spray and the fuel The compression ignition timing can be controlled by controlling the diffusion speed.
- step S118 in FIG. 12 the ECU 1 determines whether the target torque has been reached.
- the process returns to steps S1 16 and S117, and the ECU 1 performs feedback control of the fuel pressure, the air amount, and the fuel injection of the fuel pump 58.
- step S119 the ECU 1 determines whether or not the target air-fuel ratio has been reached.
- the process returns to steps S116 and S117, and the ECU 1 controls the fuel pressure, the air amount, and the fuel injection of the fuel pump 58 by feed-pack control.
- the ignition timing is controlled by the fuel pressure control and the required torque from the ECU 1 is achieved, a smooth engine operation state can be achieved and maintained. Furthermore, by controlling the total air-fuel ratio appropriately in accordance with the state of the catalyst, it becomes possible to realize low-emission operation.
- FIG. 15 is a flowchart showing a second ignition control method for the compression ignition type internal combustion engine according to the second embodiment of the present invention. Note that the same step numbers as those in FIG. 12 indicate the same processing contents.
- step S114 fuel is injected several times in one cycle. That is, in step S114, the ECU 1 determines the injection ratio, the number of injections, the injection timing, and the like. If fuel is injected multiple times at different times during one cycle, for example, twice during the compression stroke, the fuel injected earlier will ignite more fuel than the fuel injected during the compression stroke.
- the air-fuel ratio tends to be relatively long, so a relatively homogeneous air-fuel mixture is likely to be formed in a wide area within the combustion chamber (the air-fuel ratio in this area depends on the fuel injection amount, but is almost always set to lean). In other words, the rich region and the lean region can be more clearly separated by multiple injections.
- FIGS. 16 to 19 another configuration of the fuel injection valve used in the compression ignition type internal combustion engine according to the present embodiment will be described with reference to FIGS. 16 to 19.
- FIG. 16 is an explanatory diagram of a second configuration of the fuel injection valve used for the compression ignition type internal combustion engine according to the second embodiment of the present invention.
- FIG. 16 (A) is a sectional view of a main part of the fuel injection valve used in the present embodiment
- FIG. 16 (B) is a bottom view of the fuel injection valve used in the present embodiment.
- the fuel injection valve 69 A has a large number of injection holes 77 on the nozzle face 80. Spreading fuel over a wide area in the fuel chamber 16 avoids excessively rich spots during ignition and suppresses NOX generation even if spray drying is performed or a rich Z-lean region occurs. be able to.
- FIG. 17 is an explanatory diagram of a third configuration of the fuel injection valve used in the compression ignition type internal combustion engine according to the second embodiment of the present invention.
- FIG. 17 (A) is a cross-sectional view of a main part of the fuel injection valve used in the present embodiment
- FIG. 17 (B) is a bottom view of the fuel injection valve used in the present embodiment.
- a top surface 81 of a nozzle having a plurality of injection holes 77 has an inclination toward the center.
- the injected fuel is directed to a certain space in the combustion chamber 16. In this pattern, some or all of the injected spray, as well as the spray from the adjacent injection holes, collide (dry) at some point in the combustion chamber.
- FIG. 18 is an explanatory diagram of a fourth configuration of the fuel injection valve used in the compression ignition type internal combustion engine according to the second embodiment of the present invention.
- FIG. 18 (A) is a sectional view of a principal part of the fuel injection valve used in the present embodiment
- FIG. 18 (B) is a bottom view of the fuel injection valve used in the present embodiment.
- the fuel injection valve 69C has a plurality of slit-shaped injection holes 77A.
- the spray injected from each injection hole has a fan shape centered on the vicinity of the injection hole, and therefore, spray interference occurs in the space in the combustion chamber after injection.
- FIG. 19 is an explanatory diagram of a fifth configuration of the fuel injection valve used in the compression ignition type internal combustion engine according to the second embodiment of the present invention.
- FIG. 19 (A) is a sectional view of a main part of the fuel injection valve used in the present embodiment
- FIG. 19 (B) is a bottom view of the fuel injection valve used in the present embodiment.
- the fuel injection valve 69D has a pattern in which slit-shaped nozzles are crossed and overlapped inside a nozzle plate 83 having injection holes of the pattern shown in FIG. Since it has the property of amplifying turbulence upstream of the nozzle hole, it has a more atomizing effect than the example in Fig. 18.
- this embodiment is also applicable to a fuel injection valve having a plurality of injection holes and exhibiting the same effects as the present embodiment. It goes without saying that it is within the range.
- a plurality of injection holes are provided in the nozzle portion of the fuel injection valve used, and the injected fuel sprays interfere with each other in the combustion chamber. Because the fuel droplets are difficult to diffuse at the interference part between the sprays, the air-fuel ratio distribution in the spray and the fuel diffusion rate are controlled by controlling the fuel pressure of the injected fuel according to the engine operating conditions, and this is ignited. As a trigger, the compression ignition timing can be controlled appropriately.
- FIG. 20 is a block diagram showing the configuration of the compression ignition type internal combustion engine according to the third embodiment of the present invention.
- the same reference numerals as those in FIG. 1 indicate the same parts.
- an intake port 6 and an exhaust port 14 communicate with a combustion chamber 16 surrounded by a cylinder block 9, a piston 17 and a cylinder head 10.
- an intake valve 19a is provided to open and close the passage with the combustion chamber 16.
- An exhaust valve 19b is provided at the connection between the combustion chamber 16 and the exhaust port 14 to open and close the passage with the combustion chamber 16.
- the intake port 6 is branched into two and connected to the combustion chamber 16, and an intake valve 19 a is provided at each connection portion.
- the exhaust port 14 is branched into two and connected to the combustion chamber 16, and an exhaust valve 19b is provided at each connection portion.
- a spark plug 13 is disposed in the combustion chamber 16.
- ECU engine control unit
- a spark discharge from the spark plug 13 is performed.
- the ignition plug 13 can also function as an ion current detector for detecting the combustion state. In that case, the combustion state in the combustion chamber 16 And monitor the ignition timing.
- the ignition plug 13 is not used and any operating region is to be ignited by compression ignition combustion, that is, only by piston compression, the ignition plug 13 need not be provided.
- the ignition plug 13 is provided at the upper center of the combustion chamber 16, but is not particularly limited to this location.
- the ECU 1 includes output values of an accelerator opening degree detecting device 2a and a brake pedal force detecting device 2b as driver intention detecting means for detecting an intention of a driver for driving a vehicle equipped with the compression ignition type internal combustion engine of the present embodiment. Also, an output value of a vehicle speed detecting device 2c as a vehicle running state detecting means for detecting a vehicle running state, and an air flow sensor 5 for detecting engine operating conditions, an engine cooling water temperature sensor 24, an air-fuel ratio sensor 22, Output values from the after-catalyst exhaust temperature sensor 23, the crank angle sensor 4, and the knock sensor 25, which are installed behind the catalyst 12, are sequentially taken. At this time, the airflow sensor 5 desirably has a function of measuring the intake air temperature, and this output value is also taken into the ECU1 at the same time.
- the target torque of the engine is calculated based on the output value of the accelerator opening detection device 2a.
- the differential value of the vehicle speed sensor attached to the vehicle is used as a means for grasping the acceleration of the vehicle equipped with the compression ignition type internal combustion engine. May be used.
- the output value of the brake depression force detection device 2b uses the ON'OFF signal that determines whether the driver has depressed the brake pedal, but a brake depression sensor is installed behind the brake pedal and the output value is used. It is also possible to grasp the driver's brake pressing force by providing a hydraulic pressure sensor in the hydraulic pressure piping of the brake.
- the fuel injection valve 11 is installed so that fuel can be directly injected into the combustion chamber 16.
- the fuel injection valve 11 is provided between the branched intake ports 6.
- Fuel injection valve The arrangement of 11 is in the vicinity of the inner surface of the combustion chamber 16 near the intake valve 19a, but does not particularly define the location, and may be any location that can be injected into the combustion chamber 16.
- the intake valve 19a and the exhaust valve 19b have variable valve mechanisms 15a and 15b, respectively.
- the ECU 1 controls the variable valve mechanisms 15a and 15b according to the engine operating state, driver intention, vehicle running state, and the like, and controls the valve timing or valve lift amount of the intake valve 19a or the exhaust valve 19b. At least one of them is controlled.
- FIG. 21 is a flowchart showing an ignition control method for a compression ignition type internal combustion engine according to the third embodiment of the present invention
- FIG. 22 is a diagram illustrating the operation of the compression ignition type internal combustion engine according to the third embodiment of the present invention.
- step S101 the ECU 1 reads the accelerator opening based on the output value of the accelerator opening detecting device 2a, and calculates the brake pedal force based on the output value of the brake pedal detecting device 2b. By reading, the driver's intention of the vehicle equipped with the compression ignition type internal combustion engine is read.
- step S102 the ECU 1 reads the output value of the vehicle speed detecting device 2c to detect the vehicle running conditions. Also read the output values of the air flow sensor 5, engine cooling water temperature sensor 24, air-fuel ratio sensor 22, post-catalyst exhaust temperature sensor 23 installed behind the catalyst 12, crank angle sensor 4, knock sensor 25, etc. Thus, the engine operating conditions are detected. Then, the ECU 1 calculates an engine load based on the vehicle running conditions and the engine operating conditions.
- step S103 the ECU 1 determines whether or not operation by compression ignition is possible based on the driver intention read in step S101 and the engine load calculated in step S102.
- step S104 If it is determined in step S103 that the engine cannot be operated, the process proceeds to step S104. If the engine is, for example, a spark ignition engine, spark ignition combustion is performed. If the engine is a diesel engine having no spark plug, spray combustion is performed. Each parameter of the institution to do Control the meter.
- step S105A If it is determined in step S103 that operation by compression ignition is possible, control is performed in the compression ignition combustion mode in steps S105 and subsequent steps.
- step S105A the ECU 1 obtains the amount of intake air according to the current engine operation condition from the map stored in advance in the ECU 1. Recall and determine the variable valve operation amount, total fuel injection amount, fuel injection ratio and fuel injection timing.
- the ignition trigger factor in the present embodiment will be described with reference to FIG.
- the horizontal axis shows the exhaust process EXH, the intake process compression stroke COM, and the expansion stroke EXP in the internal combustion engine
- the vertical axis shows the combustion chamber pressure P and the fuel injection timing INJ, respectively.
- the exhaust valve 19 b is closed early during the exhaust stroke so that the burned gas up to the previous cycle remains.
- the auxiliary fuel is injected into the residual gas as an ignition trigger.
- blowout B A the residual gas at any time during the exhaust stroke
- the auxiliary fuel 8 9 b is injected into 8 9 a. At this time, the injection amount of auxiliary fuel should be kept at most 50% of the fuel amount injected per cycle.
- the auxiliary fuel 89 b stays in the high-temperature residual gas as shown in the blowout BB, and is compressed by the piston with both the intake and exhaust valves closed. It is modified to a component containing a lot of active species. At this time, the sub-fuel amount is at most 50% or less of the total injection amount, so that self-ignition does not occur.
- the remaining fuel 92a is injected as the main fuel.
- the injection timing is not particularly specified in the present embodiment, the timing is changed depending on the engine lot rotation condition, the set air-fuel ratio, and the like.
- the injected main fuel 92 a is distributed in the combustion chamber 16, and the auxiliary fuel 89 b is reformed to promote ignition by activated chemical species such as OH radicals, as shown in the blowout B 4. However, self-ignition occurs near the top dead center of compression. Reformed auxiliary fuel 8 9 It goes without saying that b also ignites and contributes to heat generation in the combustion chamber 16.
- the auxiliary fuel injected with the intake and exhaust valves closed during the exhaust stroke is the ignition trigger factor
- the valve timing of the intake valve 19a and the exhaust valve 19b is Alternatively, the compression ignition timing is controlled by at least one of the valve lift amount and the injection amount of the auxiliary fuel which is the ignition trigger factor.
- the auxiliary fuel 89b and the main fuel 92a are the same fuel injected from the same fuel injection valve, but two are different fuels or a plurality of fuels are injected. Single or multiple fuels may be injected from the firing valve.
- step S107A of FIG. 21 the ECU 1 controls the intake air amount control device 7 and the variable valve mechanism 15a, so that the conditions determined in step S105A are satisfied. Control 1 5b.
- a throttle is used as the intake air control device, but a supercharger may be provided upstream of the throttle to control the intake air amount.
- step S110 the ECU 1 determines whether or not the generated torque at this time has reached the required torque. If not, the process proceeds to step S109, and if it has, the process proceeds to step S110.
- step S109 the ECU 1 determines whether the ignition timing is normal.
- the ignition timing is detected by detecting the ion current generated between the electrodes of the ignition plug or by using the output value of the knock sensor 25.
- the compression sensor that monitors the pressure history in the combustion chamber 16 is used for the compression ignition type internal combustion engine. It may be provided to make a determination based on the output signal.
- the flow returns to step S108, and the fuel injection control and the injection timing of the auxiliary fuel, which are the ignition trigger factors, are controlled so as to make the ignition timing normal. For example, if the ignition timing is more advanced than the target ignition timing, Control so that the injection amount of the ignition trigger factor is reduced or the injection timing of the ignition trigger factor is retarded. If the ignition timing is later than the target ignition timing, control is performed so that the injection amount of the ignition trigger factor is increased or the injection timing of the ignition trigger factor is advanced.
- step S107 If the ignition timing is normal and the generated torque has not reached the target torque, the process returns to step S107, and the intake air amount, fuel injection amount, and injection timing are fed back so that the target torque is generated. Control.
- step S111 it is determined whether ECU1 is the target air-fuel ratio.
- the air-fuel ratio detecting means at this time is the air-fuel ratio sensor 22 shown in FIG. 1, and the output value determines the air-fuel ratio during engine operation.
- step S107 If it is not the target air-fuel ratio, the flow returns to step S107, and the intake air amount and the fuel injection amount are feedback-controlled.
- the control ends.
- the exhaust gas purification efficiency of the catalyst 12 shown in FIG. 1 can be controlled to an optimum value.
- the variable valve mechanism that makes at least one of the intake valve and the exhaust valve variable is provided.
- both the intake valve and the exhaust valve are used.
- the variable valve mechanism is controlled so that both are closed, high-temperature burned gas remains, and a part of the fuel is injected into the remaining gas, and this fuel itself is used as an ignition trigger factor. This is because part of the fuel injected into the high-temperature gas is further compressed, and although it does not lead to ignition, a gas containing a large amount of active chemical species such as OH radicals that promote ignition is generated. It controls the concentration of active chemical species that promotes ignition by controlling the ratio of fuel injected into the main gas and fuel injected into the residual gas, and the ignition timing Can be controlled.
- the ignition timing can be controlled to an optimum value by controlling the fuel injection timing, the number of injections, and the injection ratio using the fuel injection valve. And provide a low-cost engine with good responsiveness to ignition control. You. At this time, by judging the operating state (ignition timing, combustion pressure, etc.) of each cylinder, it is possible to control the fuel injection timing, number of injections, and injection ratio for each cylinder.
- the internal EGR amount is controlled by a variable valve mechanism, and the fuel injection timing, the number of injections, and the injection ratio are controlled by using a fuel injection valve, and the auxiliary fuel is used as an ignition trigger factor. Since the ignition timing can be controlled to an optimum value, it is not necessary to remodel the system or add complicated devices, and it is possible to provide an internal combustion engine with low cost, good control response, and low exhaust and low fuel consumption.
- the present invention is characterized in that in an operating state in which compression ignition combustion is performed, an ignition trigger factor is injected when the intake / exhaust valve is closed to optimally control the ignition timing. Therefore, a method and a method for controlling the compression ignition timing by means for injecting the ignition trigger factor other than the method described in the above embodiment are within the scope of the present invention.
- the ignition trigger factor injection device is used.
- FIG. 23 is a characteristic diagram of another example of the fuel injection valve used for the compression ignition type internal combustion engine in each embodiment of the present invention.
- the vertical axis indicates the fuel injection amount IN J vol
- the horizontal axis indicates the injection pulse width Winj.
- the injection amount of the secondary fuel and the main fuel is controlled by controlling the voltage value and the injection pulse width supplied to the injection valve using a piezoelectric element or a magnetostrictive element as the injection valve that injects the ignition trigger factor. To control.
- a dotted line X indicates the relationship between the injection pulse width and the injection amount in the conventional injection valve.
- the conventional injection valve is of a type in which a core valve in the injection valve is attracted by an electromagnet.
- the injection pulse width is narrow, that is, where the injection amount is small, there is an invalid injection pulse width t inv, and it is difficult to accurately control fluid injection in this region.
- the minimum injection quantity that can be injected once is about 4 mcc.
- the piezoelectric element or the magnetostrictive element is deformed in accordance with the supplied voltage value, thereby increasing the lift of the core valve. Since the amount can be controlled, it is possible to obtain a characteristic in which there is almost no invalid injection pulse width as shown by a solid line Y in FIG. In other words, in the low engine load region such as idle conditions, an injection amount of 4 mcc or less may be required during sub-injection.In such a case, an injection valve using a piezoelectric element or a magnetostrictive element must be used. As a result, control accuracy can be improved even in a low engine load region.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
Claims
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/478,352 US6966295B2 (en) | 2001-05-22 | 2001-05-22 | Compression ignition internal combustion engine |
EP01932196.7A EP1389679B1 (en) | 2001-05-22 | 2001-05-22 | Compression ignition internal combustion engine |
JP2003500402A JP3964387B2 (ja) | 2001-05-22 | 2001-05-22 | 圧縮着火式内燃機関の制御装置 |
PCT/JP2001/004271 WO2002097255A1 (fr) | 2001-05-22 | 2001-05-22 | Moteur thermique a allumage par compression |
US10/812,983 US7055495B2 (en) | 2001-05-22 | 2004-03-31 | Compression ignition internal combustion engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/JP2001/004271 WO2002097255A1 (fr) | 2001-05-22 | 2001-05-22 | Moteur thermique a allumage par compression |
Related Child Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10478352 A-371-Of-International | 2001-05-22 | ||
US10/478,352 A-371-Of-International US6966295B2 (en) | 2001-05-22 | 2001-05-22 | Compression ignition internal combustion engine |
US10/812,983 Continuation US7055495B2 (en) | 2001-05-22 | 2004-03-31 | Compression ignition internal combustion engine |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2002097255A1 true WO2002097255A1 (fr) | 2002-12-05 |
Family
ID=11737336
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2001/004271 WO2002097255A1 (fr) | 2001-05-22 | 2001-05-22 | Moteur thermique a allumage par compression |
Country Status (4)
Country | Link |
---|---|
US (2) | US6966295B2 (ja) |
EP (1) | EP1389679B1 (ja) |
JP (1) | JP3964387B2 (ja) |
WO (1) | WO2002097255A1 (ja) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005047683A1 (de) * | 2003-10-29 | 2005-05-26 | Daimlerchrysler Ag | Verfahren zum betrieb einer brennkraftmaschine |
JP2007040234A (ja) * | 2005-08-04 | 2007-02-15 | Honda Motor Co Ltd | 圧縮着火内燃機関の制御装置 |
WO2007022602A1 (en) * | 2005-08-26 | 2007-03-01 | Orbital Australia Pty Ltd | Engine control strategy |
JP2007177755A (ja) * | 2005-12-28 | 2007-07-12 | Honda Motor Co Ltd | 自己着火式エンジン |
JP2012007556A (ja) * | 2010-06-25 | 2012-01-12 | Aisin Seiki Co Ltd | 予混合圧縮着火式内燃機関 |
Families Citing this family (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002206446A (ja) * | 2001-01-10 | 2002-07-26 | Hitachi Ltd | 内燃機関及び内燃機関の燃料噴射制御装置 |
JP4005941B2 (ja) | 2003-06-03 | 2007-11-14 | 株式会社日立製作所 | 筒内噴射エンジンの燃焼制御装置及び燃焼制御方法 |
JP4206882B2 (ja) * | 2003-09-24 | 2009-01-14 | いすゞ自動車株式会社 | 予混合圧縮自己着火式内燃機関 |
US7047909B1 (en) * | 2005-01-21 | 2006-05-23 | Delphi Technologies, Inc. | Methods of operating a compression ignition engine and a vehicle system |
JP4483684B2 (ja) * | 2005-04-28 | 2010-06-16 | 株式会社デンソー | 筒内噴射式内燃機関の燃料噴射制御装置 |
EP1744040B1 (en) * | 2005-07-14 | 2011-09-07 | Honda Motor Co., Ltd. | Control system for internal combustion engine |
EP1744039B1 (en) * | 2005-07-14 | 2014-10-22 | Honda Motor Co., Ltd. | Control system for internal combustion engine |
JP4243598B2 (ja) * | 2005-08-25 | 2009-03-25 | 本田技研工業株式会社 | 内燃機関の制御装置 |
JP4243601B2 (ja) * | 2005-07-14 | 2009-03-25 | 本田技研工業株式会社 | 内燃機関の制御装置 |
JP4414377B2 (ja) * | 2005-07-15 | 2010-02-10 | 本田技研工業株式会社 | 内燃機関の制御装置 |
EP1744041B1 (en) * | 2005-07-14 | 2013-05-22 | Honda Motor Co., Ltd. | Control system for internal combustion engine |
DE102006004235B4 (de) * | 2006-01-30 | 2013-04-18 | Continental Automotive Gmbh | Verfahren und Vorrichtung zum Betreiben einer Brennkraftmaschine |
DE102006004234B4 (de) * | 2006-01-30 | 2010-04-15 | Continental Automotive Gmbh | Verfahren und Vorrichtung zum Betreiben einer Brennkraftmaschine, Brennkraftmaschine und Zumessbaueinheit |
DE102006004236A1 (de) * | 2006-01-30 | 2007-08-09 | Siemens Ag | Verfahren und Vorrichtung zum Betreiben einer Brennkraftmaschine |
JP2007224908A (ja) * | 2006-02-20 | 2007-09-06 | Robert Bosch Gmbh | 内燃機関の運転方法 |
US9010293B2 (en) | 2006-04-07 | 2015-04-21 | David A. Blank | Combustion control via homogeneous combustion radical ignition (HCRI) or partial HCRI in cyclic IC engines |
US20130306045A1 (en) * | 2006-04-07 | 2013-11-21 | David A. Blank | Combustion Control via Homogeneous Combustion Radical Ignition (HCRI) or Partial HCRI in Cyclic IC Engines |
US7322339B1 (en) * | 2006-09-11 | 2008-01-29 | Gm Global Technology Operations, Inc. | Apparent torque reserve at idle for direct injected engines |
US7676319B2 (en) * | 2006-12-28 | 2010-03-09 | Hitachi, Ltd. | Intake air amount control apparatus for engine and control method thereof |
JP2008291720A (ja) * | 2007-05-23 | 2008-12-04 | Honda Motor Co Ltd | 内燃機関の制御装置 |
EP2171233A4 (en) * | 2007-06-22 | 2015-10-14 | Orbital Australia Pty Ltd | CONTROL OF CONTROLLED AUTOIGNITION COMBUSTION PROCESS (CAI) |
JP4836088B2 (ja) | 2007-11-08 | 2011-12-14 | 日立オートモティブシステムズ株式会社 | 圧縮自己着火式内燃機関の制御装置および制御方法 |
JP4793382B2 (ja) * | 2007-12-07 | 2011-10-12 | トヨタ自動車株式会社 | 内燃機関の燃料噴射制御装置 |
US8431043B2 (en) * | 2008-02-15 | 2013-04-30 | Cummins Inc. | System and method for on-board waste heat recovery |
US7823563B2 (en) * | 2008-05-08 | 2010-11-02 | Ford Global Technologies, Llc | Cylinder-by-cylinder balancing of combustion timing in HCCI engines |
JP4740286B2 (ja) * | 2008-05-30 | 2011-08-03 | 日立オートモティブシステムズ株式会社 | 火花点火式内燃機関の制御装置 |
US8464750B1 (en) | 2010-06-30 | 2013-06-18 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Magnetostrictive pressure regulating system |
DE102011002936A1 (de) | 2011-01-20 | 2012-07-26 | Ford Global Technologies, Llc | Partikelsensor, Abgassystem und Verfahren zum Bestimmen von Partikeln im Abgas |
JP2013024100A (ja) * | 2011-07-20 | 2013-02-04 | Yamaha Motor Co Ltd | 内燃機関およびそれを備えた鞍乗型車両 |
JP2013024098A (ja) | 2011-07-20 | 2013-02-04 | Yamaha Motor Co Ltd | 内燃機関およびそれを備えた鞍乗型車両 |
JP2013024099A (ja) * | 2011-07-20 | 2013-02-04 | Yamaha Motor Co Ltd | 内燃機関およびそれを備えた鞍乗型車両 |
JP6123175B2 (ja) * | 2012-06-29 | 2017-05-10 | マツダ株式会社 | 直噴エンジンの燃料噴射装置 |
US20190338730A1 (en) * | 2016-10-31 | 2019-11-07 | Cummins Inc. | In-cylinder air injection via dual-fuel injector |
US20220018321A1 (en) * | 2016-10-31 | 2022-01-20 | Cummins Inc. | In-cylinder air injection via dual-fuel injector |
BR112021022895A2 (pt) | 2019-05-15 | 2022-01-18 | Clearflame Engines Inc | Partida a frio para combustíveis de alta octanagem em uma arquitetura de motor a diesel |
RU194935U1 (ru) * | 2019-10-15 | 2019-12-30 | Денис Викторович Шабалин | Система кратковременного форсирования силовой установки танка с устройством корректировки угла начала впрыска топлива |
CN110632430A (zh) * | 2019-10-17 | 2019-12-31 | 潍柴西港新能源动力有限公司 | 一种模拟节气门抗回火能力的测试***及其测试方法 |
AU2021225956A1 (en) | 2020-02-26 | 2022-08-25 | Clearflame Engines, Inc. | Fuel agnostic compression ignition engine |
MX2023000435A (es) | 2020-07-09 | 2023-04-12 | Clearflame Engines Inc | Sistemas y métodos de desactivación de cilindro en motores de mezclado controlado de alta temperatura. |
US11230989B1 (en) * | 2021-03-04 | 2022-01-25 | International Engine Intellectual Property Company, Llc | System and method for disablement of diesel engine fuel injectors during cranking |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4947922B1 (ja) * | 1970-03-17 | 1974-12-18 | ||
JPS6456964A (en) * | 1987-08-25 | 1989-03-03 | Hino Motors Ltd | Air nozzle for blowing air |
JPH0953485A (ja) * | 1995-08-11 | 1997-02-25 | Mitsubishi Heavy Ind Ltd | 内燃機関の二流体噴射装置 |
JPH10196424A (ja) | 1996-12-28 | 1998-07-28 | Toyota Central Res & Dev Lab Inc | 混合気の圧縮着火式燃焼方法および混合気の圧縮着火式ピストン内燃機関 |
JPH10238374A (ja) * | 1997-02-21 | 1998-09-08 | Daihatsu Motor Co Ltd | 予混合着火内燃機関とその着火時期制御方法 |
JPH10252476A (ja) * | 1997-03-06 | 1998-09-22 | Yanmar Diesel Engine Co Ltd | 直噴式ディーゼル機関の燃焼方法 |
JPH11107820A (ja) * | 1997-09-30 | 1999-04-20 | Nissan Motor Co Ltd | ディーゼルエンジンの燃焼制御装置 |
DE19810935A1 (de) | 1998-03-13 | 1999-09-16 | Daimler Chrysler Ag | Verfahren zum Betrieb einer im Viertakt arbeitenden Hubkolben-Brennkraftmaschine |
JP2000064876A (ja) * | 1998-06-18 | 2000-02-29 | Avl List Gmbh | 内燃機関の運転方法及びこの方法を実施する内燃機関 |
JP2000179369A (ja) * | 1998-12-11 | 2000-06-27 | Tokyo Gas Co Ltd | 予混合圧縮自着火機関及びその運転制御方法 |
JP2000192828A (ja) * | 1998-12-25 | 2000-07-11 | Nissan Motor Co Ltd | 内燃機関の燃焼制御装置 |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4947922A (ja) | 1972-05-23 | 1974-05-09 | ||
JP2747988B2 (ja) | 1995-05-17 | 1998-05-06 | 茂己 小林 | 内燃機関の燃焼制御方法及び装置 |
JPH1056413A (ja) | 1996-08-12 | 1998-02-24 | Nissan Motor Co Ltd | 放送受信機 |
JPH1056412A (ja) | 1996-08-12 | 1998-02-24 | Denso Corp | 携帯電話機 |
DE19801245C2 (de) | 1998-01-15 | 2000-12-14 | Andresen Peter L | Anordnung zur Beladung eines Brennraumes über eine mehrfach öffnende Ventilkombination |
JPH11336600A (ja) * | 1998-05-22 | 1999-12-07 | Nissan Motor Co Ltd | 火花点火式内燃機関 |
JP2000282848A (ja) * | 1999-03-30 | 2000-10-10 | Nissan Motor Co Ltd | 内燃機関の排気浄化装置 |
DE60010176T2 (de) * | 1999-05-12 | 2004-08-26 | Nissan Motor Co., Ltd., Yokohama | Selbstgezündete Brennkraftmaschine |
JP3835142B2 (ja) * | 1999-09-07 | 2006-10-18 | 日産自動車株式会社 | 自己着火・火花点火式内燃機関の制御装置 |
JP4253426B2 (ja) * | 1999-09-14 | 2009-04-15 | 日産自動車株式会社 | 圧縮自己着火式ガソリン機関 |
US6390057B2 (en) * | 1999-12-14 | 2002-05-21 | Nissan Motor Co., Ltd. | Compression self-ignition gasoline engine |
JP3815163B2 (ja) * | 2000-01-25 | 2006-08-30 | 日産自動車株式会社 | 圧縮自己着火式内燃機関 |
US6401688B2 (en) * | 2000-01-27 | 2002-06-11 | Nissan Motor Co., Ltd. | Auto-ignition combustion management in internal combustion engine |
JP2001248484A (ja) * | 2000-02-29 | 2001-09-14 | Hitachi Ltd | 筒内噴射エンジン及びその制御装置,制御方法 |
JP4016568B2 (ja) * | 2000-03-30 | 2007-12-05 | 日産自動車株式会社 | ガソリン自己着火式内燃機関 |
JP3760725B2 (ja) * | 2000-05-16 | 2006-03-29 | 日産自動車株式会社 | 圧縮自己着火式ガソリン機関 |
JP2001323828A (ja) * | 2000-05-16 | 2001-11-22 | Nissan Motor Co Ltd | 圧縮自己着火式ガソリン機関 |
JP3804403B2 (ja) * | 2000-05-23 | 2006-08-02 | トヨタ自動車株式会社 | 内燃機関の燃料供給量制御装置 |
JP3980477B2 (ja) * | 2000-08-17 | 2007-09-26 | 株式会社日立製作所 | 圧縮着火式内燃機関 |
JP3800020B2 (ja) * | 2001-03-13 | 2006-07-19 | 日産自動車株式会社 | 圧縮自己着火式エンジン |
JP3927395B2 (ja) * | 2001-09-28 | 2007-06-06 | 株式会社日立製作所 | 圧縮着火エンジンの制御装置 |
-
2001
- 2001-05-22 WO PCT/JP2001/004271 patent/WO2002097255A1/ja active Application Filing
- 2001-05-22 EP EP01932196.7A patent/EP1389679B1/en not_active Expired - Lifetime
- 2001-05-22 US US10/478,352 patent/US6966295B2/en not_active Expired - Lifetime
- 2001-05-22 JP JP2003500402A patent/JP3964387B2/ja not_active Expired - Fee Related
-
2004
- 2004-03-31 US US10/812,983 patent/US7055495B2/en not_active Expired - Fee Related
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4947922B1 (ja) * | 1970-03-17 | 1974-12-18 | ||
JPS6456964A (en) * | 1987-08-25 | 1989-03-03 | Hino Motors Ltd | Air nozzle for blowing air |
JPH0953485A (ja) * | 1995-08-11 | 1997-02-25 | Mitsubishi Heavy Ind Ltd | 内燃機関の二流体噴射装置 |
JPH10196424A (ja) | 1996-12-28 | 1998-07-28 | Toyota Central Res & Dev Lab Inc | 混合気の圧縮着火式燃焼方法および混合気の圧縮着火式ピストン内燃機関 |
JPH10238374A (ja) * | 1997-02-21 | 1998-09-08 | Daihatsu Motor Co Ltd | 予混合着火内燃機関とその着火時期制御方法 |
JPH10252476A (ja) * | 1997-03-06 | 1998-09-22 | Yanmar Diesel Engine Co Ltd | 直噴式ディーゼル機関の燃焼方法 |
JPH11107820A (ja) * | 1997-09-30 | 1999-04-20 | Nissan Motor Co Ltd | ディーゼルエンジンの燃焼制御装置 |
DE19810935A1 (de) | 1998-03-13 | 1999-09-16 | Daimler Chrysler Ag | Verfahren zum Betrieb einer im Viertakt arbeitenden Hubkolben-Brennkraftmaschine |
JP2000064876A (ja) * | 1998-06-18 | 2000-02-29 | Avl List Gmbh | 内燃機関の運転方法及びこの方法を実施する内燃機関 |
JP2000179369A (ja) * | 1998-12-11 | 2000-06-27 | Tokyo Gas Co Ltd | 予混合圧縮自着火機関及びその運転制御方法 |
JP2000192828A (ja) * | 1998-12-25 | 2000-07-11 | Nissan Motor Co Ltd | 内燃機関の燃焼制御装置 |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005047683A1 (de) * | 2003-10-29 | 2005-05-26 | Daimlerchrysler Ag | Verfahren zum betrieb einer brennkraftmaschine |
US7263982B2 (en) | 2003-10-29 | 2007-09-04 | Diamler Chrysler Ag | Method for operating and internal combustion engine |
JP2007040234A (ja) * | 2005-08-04 | 2007-02-15 | Honda Motor Co Ltd | 圧縮着火内燃機関の制御装置 |
JP4551292B2 (ja) * | 2005-08-04 | 2010-09-22 | 本田技研工業株式会社 | 圧縮着火内燃機関の制御装置 |
WO2007022602A1 (en) * | 2005-08-26 | 2007-03-01 | Orbital Australia Pty Ltd | Engine control strategy |
JP2007177755A (ja) * | 2005-12-28 | 2007-07-12 | Honda Motor Co Ltd | 自己着火式エンジン |
JP4493593B2 (ja) * | 2005-12-28 | 2010-06-30 | 本田技研工業株式会社 | 自己着火式エンジン |
JP2012007556A (ja) * | 2010-06-25 | 2012-01-12 | Aisin Seiki Co Ltd | 予混合圧縮着火式内燃機関 |
Also Published As
Publication number | Publication date |
---|---|
EP1389679A4 (en) | 2005-04-13 |
US6966295B2 (en) | 2005-11-22 |
JP3964387B2 (ja) | 2007-08-22 |
US20040154581A1 (en) | 2004-08-12 |
US7055495B2 (en) | 2006-06-06 |
EP1389679B1 (en) | 2017-11-29 |
US20040177830A1 (en) | 2004-09-16 |
EP1389679A1 (en) | 2004-02-18 |
JPWO2002097255A1 (ja) | 2004-09-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP3964387B2 (ja) | 圧縮着火式内燃機関の制御装置 | |
US6240724B1 (en) | Control device for direct injection engine | |
US7219650B2 (en) | Control apparatus of fuel injection type internal combustion engine | |
RU2411386C2 (ru) | Двигатель внутреннего сгорания на газовом топливе и способ управления двигателем внутреннего сгорания на газовом топливе | |
US5967113A (en) | Exhaust-gas temperature raising system for an in-cylinder injection type internal combustion engine | |
US6932048B2 (en) | Combustion control device and method for engine | |
US7690369B2 (en) | Fuel pressure controlling device of engine | |
US20080257304A1 (en) | Internal combustion engine and combustion method of the same | |
CN101415927B (zh) | 用于运行内燃机的方法 | |
KR20030022040A (ko) | 불꽃 점화식 직접 분사 엔진의 제어 장치 | |
JP4126971B2 (ja) | 混合気を圧縮自着火させて運転する内燃機関、および内燃機関の制御方法 | |
JP4297288B2 (ja) | 予混合圧縮着火エンジンの着火時期制御方法 | |
CN102734031B (zh) | 用于稳健的自燃和火焰传播的hcci燃料喷射器 | |
US20010027643A1 (en) | Cylinder injection type internal combustion engine and combustion control method at starting thereof | |
JP4117799B2 (ja) | 予混合圧縮着火エンジンの着火時期制御方法 | |
JP2001152853A (ja) | 予混合圧縮着火内燃機関の制御装置 | |
JP2007192235A (ja) | 火花点火内燃機関の制御装置及び方法 | |
JP3635670B2 (ja) | 火花点火内燃機関の制御装置及び方法 | |
JP3685103B2 (ja) | 筒内直噴式エンジン | |
JP2003106195A (ja) | 火花点火式直噴エンジンの制御装置 | |
JP2003106186A (ja) | 火花点火式直噴エンジンの制御装置 | |
JP2000110646A (ja) | ディーゼルエンジン | |
JP2002038995A (ja) | ディーゼルエンジンの燃料噴射装置 | |
JP5262991B2 (ja) | 火花点火式直噴エンジンの吸気制御装置 | |
JP3030226B2 (ja) | 自動車用リーンバーンエンジン |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AK | Designated states |
Kind code of ref document: A1 Designated state(s): JP KR US |
|
AL | Designated countries for regional patents |
Kind code of ref document: A1 Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE TR |
|
DFPE | Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101) | ||
121 | Ep: the epo has been informed by wipo that ep was designated in this application | ||
WWE | Wipo information: entry into national phase |
Ref document number: 2003500402 Country of ref document: JP |
|
REEP | Request for entry into the european phase |
Ref document number: 2001932196 Country of ref document: EP |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2001932196 Country of ref document: EP Ref document number: 10478352 Country of ref document: US |
|
WWP | Wipo information: published in national office |
Ref document number: 2001932196 Country of ref document: EP |