WO2005017348A1 - 火花点火機関及びその燃焼制御方法 - Google Patents
火花点火機関及びその燃焼制御方法 Download PDFInfo
- Publication number
- WO2005017348A1 WO2005017348A1 PCT/JP2003/010374 JP0310374W WO2005017348A1 WO 2005017348 A1 WO2005017348 A1 WO 2005017348A1 JP 0310374 W JP0310374 W JP 0310374W WO 2005017348 A1 WO2005017348 A1 WO 2005017348A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- fuel
- fuel injection
- engine
- temperature
- combustion chamber
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 179
- 238000000034 method Methods 0.000 title claims abstract description 42
- 230000006835 compression Effects 0.000 claims abstract description 49
- 238000007906 compression Methods 0.000 claims abstract description 49
- 239000000446 fuel Substances 0.000 claims description 412
- 238000002347 injection Methods 0.000 claims description 233
- 239000007924 injection Substances 0.000 claims description 233
- 239000007921 spray Substances 0.000 claims description 72
- 230000035515 penetration Effects 0.000 claims description 36
- 239000000470 constituent Substances 0.000 claims description 8
- 238000011144 upstream manufacturing Methods 0.000 claims description 6
- 230000000979 retarding effect Effects 0.000 claims description 4
- 238000013517 stratification Methods 0.000 claims description 4
- 230000001934 delay Effects 0.000 claims description 3
- 241000239290 Araneae Species 0.000 claims 1
- 238000005485 electric heating Methods 0.000 claims 1
- 239000007789 gas Substances 0.000 abstract description 57
- 230000003197 catalytic effect Effects 0.000 abstract description 29
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 abstract description 19
- 229910002091 carbon monoxide Inorganic materials 0.000 abstract description 19
- 238000002156 mixing Methods 0.000 abstract description 10
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 abstract description 7
- 239000001301 oxygen Substances 0.000 abstract description 7
- 229910052760 oxygen Inorganic materials 0.000 abstract description 7
- 239000000203 mixture Substances 0.000 description 52
- 238000010586 diagram Methods 0.000 description 25
- 238000007254 oxidation reaction Methods 0.000 description 19
- 230000008569 process Effects 0.000 description 19
- 230000007423 decrease Effects 0.000 description 17
- 238000012360 testing method Methods 0.000 description 15
- 239000000498 cooling water Substances 0.000 description 13
- 239000000779 smoke Substances 0.000 description 13
- 235000014676 Phragmites communis Nutrition 0.000 description 12
- 238000005457 optimization Methods 0.000 description 12
- 230000001276 controlling effect Effects 0.000 description 11
- 230000000694 effects Effects 0.000 description 11
- 239000003595 mist Substances 0.000 description 11
- 239000007788 liquid Substances 0.000 description 9
- 238000000746 purification Methods 0.000 description 8
- 239000003054 catalyst Substances 0.000 description 7
- 239000004071 soot Substances 0.000 description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 7
- 238000005094 computer simulation Methods 0.000 description 6
- 238000009826 distribution Methods 0.000 description 6
- 239000000463 material Substances 0.000 description 6
- 230000015572 biosynthetic process Effects 0.000 description 5
- 238000005259 measurement Methods 0.000 description 5
- 238000012545 processing Methods 0.000 description 5
- 230000004913 activation Effects 0.000 description 4
- 230000008859 change Effects 0.000 description 4
- 230000003111 delayed effect Effects 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 238000001179 sorption measurement Methods 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 3
- 239000002826 coolant Substances 0.000 description 3
- 238000009834 vaporization Methods 0.000 description 3
- 230000008016 vaporization Effects 0.000 description 3
- 239000013598 vector Substances 0.000 description 3
- 239000004215 Carbon black (E152) Substances 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000003213 activating effect Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 239000002828 fuel tank Substances 0.000 description 2
- 230000014509 gene expression Effects 0.000 description 2
- 229930195733 hydrocarbon Natural products 0.000 description 2
- 150000002430 hydrocarbons Chemical class 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 230000001737 promoting effect Effects 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- 238000010792 warming Methods 0.000 description 2
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 241001272720 Medialuna californiensis Species 0.000 description 1
- 206010027336 Menstruation delayed Diseases 0.000 description 1
- 235000006508 Nelumbo nucifera Nutrition 0.000 description 1
- 240000002853 Nelumbo nucifera Species 0.000 description 1
- 235000006510 Nelumbo pentapetala Nutrition 0.000 description 1
- 239000006096 absorbing agent Substances 0.000 description 1
- 238000000889 atomisation Methods 0.000 description 1
- 244000309464 bull Species 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000002596 correlated effect Effects 0.000 description 1
- 230000000875 corresponding effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000020169 heat generation Effects 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910001120 nichrome Inorganic materials 0.000 description 1
- 239000012299 nitrogen atmosphere Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 230000002195 synergetic effect Effects 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 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
- 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
- F02M61/188—Spherical or partly spherical shaped valve member ends
-
- 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
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
- F01N13/14—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00 having thermal insulation
- F01N13/141—Double-walled exhaust pipes or housings
-
- 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
- F01N3/2006—Periodically heating or cooling catalytic reactors, e.g. at cold starting or overheating
-
- 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
- F01N3/24—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 constructional aspects of converting apparatus
- F01N3/28—Construction of catalytic reactors
- F01N3/2892—Exhaust flow directors or the like, e.g. upstream of catalytic device
-
- 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
- F02B17/00—Engines characterised by means for effecting stratification of charge in cylinders
- F02B17/005—Engines characterised by means for effecting stratification of charge in cylinders having direct injection in the 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
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/08—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
- F02B23/10—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder
- F02B23/104—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder the injector being placed on a side position of the cylinder
-
- 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
- F02B31/00—Modifying induction systems for imparting a rotation to the charge in the cylinder
- F02B31/08—Modifying induction systems for imparting a rotation to the charge in the cylinder having multiple air inlets
- F02B31/085—Modifying induction systems for imparting a rotation to the charge in the cylinder having multiple air inlets having two inlet valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/021—Introducing corrections for particular conditions exterior to the engine
- F02D41/0235—Introducing corrections for particular conditions exterior to the engine in relation with the state of the exhaust gas treating apparatus
- F02D41/024—Introducing corrections for particular conditions exterior to the engine in relation with the state of the exhaust gas treating apparatus to increase temperature of the exhaust gas treating apparatus
- F02D41/025—Introducing corrections for particular conditions exterior to the engine in relation with the state of the exhaust gas treating apparatus to increase temperature of the exhaust gas treating apparatus by changing the composition of the exhaust gas, e.g. for exothermic reaction on exhaust gas treating apparatus
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/021—Introducing corrections for particular conditions exterior to the engine
- F02D41/0235—Introducing corrections for particular conditions exterior to the engine in relation with the state of the exhaust gas treating apparatus
- F02D41/024—Introducing corrections for particular conditions exterior to the engine in relation with the state of the exhaust gas treating apparatus to increase temperature of the exhaust gas treating apparatus
- F02D41/0255—Introducing corrections for particular conditions exterior to the engine in relation with the state of the exhaust gas treating apparatus to increase temperature of the exhaust gas treating apparatus to accelerate the warming-up of the exhaust gas treating apparatus at engine start
-
- 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
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/10091—Air intakes; Induction systems characterised by details of intake ducts: shapes; connections; arrangements
- F02M35/10118—Air intakes; Induction systems characterised by details of intake ducts: shapes; connections; arrangements with variable cross-sections of intake ducts along their length; Venturis; Diffusers
-
- 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
-
- 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
- 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
- F02P5/145—Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions using electrical means
- F02P5/15—Digital data processing
- F02P5/1502—Digital data processing using one central computing unit
- F02P5/1506—Digital data processing using one central computing unit with particular means during starting
-
- 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
- F01N2260/00—Exhaust treating devices having provisions not otherwise provided for
- F01N2260/14—Exhaust treating devices having provisions not otherwise provided for for modifying or adapting flow area or back-pressure
-
- 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
- F01N2430/00—Influencing exhaust purification, e.g. starting of catalytic reaction, filter regeneration, or the like, by controlling engine operating characteristics
- F01N2430/08—Influencing exhaust purification, e.g. starting of catalytic reaction, filter regeneration, or the like, by controlling engine operating characteristics by modifying ignition or injection timing
- F01N2430/085—Influencing exhaust purification, e.g. starting of catalytic reaction, filter regeneration, or the like, by controlling engine operating characteristics by modifying ignition or injection timing at least a part of the injection taking place during expansion or exhaust stroke
-
- 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
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/08—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
- F02B23/10—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder
- F02B2023/106—Tumble flow, i.e. the axis of rotation of the main charge flow motion is horizontal
-
- 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
- F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
- F02B2275/48—Tumble motion in gas movement in cylinder
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/04—Introducing corrections for particular operating conditions
- F02D41/06—Introducing corrections for particular operating conditions for engine starting or warming up
- F02D41/068—Introducing corrections for particular operating conditions for engine starting or warming up for warming-up
-
- 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
- F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
- F02M69/04—Injectors peculiar thereto
- F02M69/042—Positioning of injectors with respect to engine, e.g. in the air intake conduit
- F02M69/044—Positioning of injectors with respect to engine, e.g. in the air intake conduit for injecting into the intake conduit downstream of an air throttle valve
-
- 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 spark ignition engine and a combustion control method thereof, and in particular, can effectively reduce HC (unburned hydrocarbon) emission to the outside during engine operation when the engine temperature is low, and the like.
- the present invention relates to a spark ignition engine capable of quickly activating an exhaust purification catalyst and a combustion control method thereof. Background technology,
- the present invention can effectively reduce the amount of HC emitted to the outside during engine operation with a low engine temperature, can activate the exhaust purification catalyst quickly, It is another object of the present invention to provide a spark ignition engine and a combustion control method for the same that can suppress generation of soot, fluctuations in rotation, fluctuations in torque, and the like. Disclosure of the invention
- a spark ignition engine includes: combustion control means for controlling the ignition timing of a spark plug; and turbulence generation means for causing a turbulence in an exhaust flow in an exhaust passage.
- the combustion control means sets the ignition timing immediately before or after the top dead center of the compression stroke when the engine temperature is lower than a predetermined temperature.
- HC can be effectively reduced at the same time as the exhaust gas temperature rises.
- the catalytic converter for exhaust gas purification can be activated at an early stage.
- the fuel injection valve includes a fuel injection valve for directly injecting fuel into a combustion chamber, and the combustion control means supplies the fuel to the fuel injection valve in a compression stroke when an engine temperature is lower than a predetermined temperature. Injection is performed.
- the fuel is injected in the compression stroke, and the fuel is stratified in the combustion chamber.
- a relatively lean air-fuel mixture is formed on the outer peripheral portion of the combustion chamber formed and away from the spark plug. For this reason, the air-fuel mixture does not completely burn in the combustion chamber in the expansion stroke and the exhaust stroke, and in the exhaust stroke, a large amount of HC, carbon monoxide (CO), hydrogen (H2), oxygen ( 02) Exhaust including exhaust is discharged.
- turbulence generating means is provided in the exhaust passage, mixing of HC, CO, H2, and O2 discharged into the exhaust passage is promoted, and oxidation reaction (combustion) of HC is performed. Go fast.
- another preferred embodiment of the spark ignition engine according to the present invention is an ignition timing control means for controlling an ignition timing by an ignition plug, a fuel injection valve for directly injecting fuel into a combustion chamber, and a fuel injection by the fuel injection valve.
- Fuel injection control means for controlling timing, wherein the penetration of fuel injected from the fuel injection valve in the direction of the spark plug is made longer than the penetration in the direction of the piston, and the engine temperature becomes lower than the predetermined temperature.
- the fuel injection control means causes the fuel injection valve to perform fuel injection in the latter half of the compression stroke so as to be close to the stoichiometric air-fuel ratio. Is set immediately before or after the top dead center of the compression stroke.
- an ignition timing control means for controlling an ignition timing by a spark plug, a fuel injection valve for directly injecting fuel into a combustion chamber, and a fuel injection by the fuel injection valve.
- Fuel to control timing Means and a vertical vortex generating means for generating a vertical vortex in the combustion chamber, wherein when the engine temperature is lower than a predetermined temperature, the vertical vortex generating means generates a vertical vortex in the combustion chamber.
- the fuel injection control means causes the fuel injection valve to perform fuel injection in the latter half of the compression stroke so as to be close to the stoichiometric air-fuel ratio, and the ignition timing control means changes the ignition timing to the compression stroke. It is set immediately before or after the top dead center.
- the generation of the forward longitudinal vortex in the combustion chamber further reduces the adhesion of the fuel to the piston and facilitates the collection of a rich air-fuel mixture around the spark plug.
- the generation of soot can be suppressed, and the ignition timing can be further retarded, whereby the exhaust gas temperature can be further increased and HC can be further reduced.
- a spark ignition engine includes an ignition timing control means for controlling an ignition timing by a spark plug, a fuel injection valve for directly injecting fuel into a combustion chamber, and a fuel injection timing by the fuel injection valve. And a vertical vortex generating means for generating a forward vertical vortex in the combustion chamber, wherein the penetration of the fuel fog injected from the fuel injection valve in the direction of the spark plug is in the direction of the piston.
- the vertical vortex generating means When the engine temperature is lower than a predetermined temperature, the vertical vortex generating means generates a forward vertical vortex in the combustion chamber, and the fuel injection control means performs the fuel injection control.
- the valve is caused to perform fuel injection at least in the latter half of the compression stroke so as to be close to the stoichiometric air-fuel ratio, and the ignition timing control means sets the ignition timing immediately before or after the top dead center of the compression stroke.
- the apparatus comprises: a vertical vortex adjusting means for adjusting the strength of a forward vertical vortex generated in the combustion chamber; and a fluctuation detecting means for detecting a magnitude of rotation fluctuation or torque fluctuation of the engine.
- the vertical vortex adjusting means adjusts the strength of the vertical vortex so that the magnitude of rotation fluctuation or torque fluctuation becomes equal to or less than a predetermined value, and the ignition timing control means retards the ignition timing as much as possible. Let me do it.
- the strength of the vertical vortex in the combustion chamber is determined by the rotation fluctuation or torque fluctuation of the engine. By controlling it to be less than the value, it is possible to further retard the ignition timing.
- the temperature of the exhaust gas can be increased and the HC can be reduced more efficiently.
- an ignition timing control means for controlling an ignition timing by a spark plug, a fuel injection valve for directly injecting fuel into a combustion chamber, and a fuel injection control for controlling a fuel injection timing by the fuel injection valve Means, fuel pressure adjusting means for adjusting the pressure of fuel supplied to the fuel injection valve, and fluctuation detecting means for detecting the magnitude of engine rotational fluctuation or torque fluctuation, wherein the engine temperature is lower than a predetermined temperature.
- the fuel injection control means causes the fuel injection valve to perform fuel injection at least in the second half of the compression stroke so as to be close to the stoichiometric air-fuel ratio, and the magnitude of the rotation fluctuation or the torque fluctuation is a predetermined value.
- the fuel pressure adjusting means adjusts the fuel pressure
- the ignition timing control means delays the ignition timing as much as possible.
- a turbulence generator is provided as described above.
- the turbulence generating means is preferably disposed in the exhaust passage to forcibly generate turbulence in the exhaust flow and increase the turbulence as much as possible. It may be composed of a plurality of rods or plate-like bodies arranged side by side, or may be composed of a lattice-like body or a web-like body. In this case, preferably, the interval between the constituent members is smaller on the inner wall surface side than in the center of the exhaust passage.
- FIG. 1 is a schematic configuration diagram showing a first embodiment of a spark ignition engine according to the present invention.
- FIG. 2 is a perspective view showing the periphery of a combustion chamber of the engine shown in FIG.
- FIG. 3 is an exhaust passage sectional view showing a turbulence generator used in the first embodiment.
- FIG. 4 is a sectional view taken along line AA of FIG.
- FIG. 5 is a diagram showing an example of a cross-sectional shape of a constituent member of the turbulence generator shown in FIG. 3.
- FIG. 6 is a side view showing an example of a fuel injection valve used in the first embodiment.
- FIG. 7 is an enlarged view of a main part of the fuel injection valve shown in FIG.
- FIG. 8 is an enlarged bottom view of the fuel injection valve shown in FIG.
- FIG. 9 is a side view showing the shape of the fuel fog in the fuel injection valve shown in FIG.
- FIG. 10 is a sectional view taken along line AA of FIG.
- FIG. 11 is a side view showing another example of the fuel injection valve used in the first embodiment.
- FIG. 12 is an enlarged view of a main part of the fuel injection valve shown in FIG.
- FIG. 13 is an enlarged bottom view of the fuel injection valve shown in FIG.
- FIG. 14 is a side view showing the shape of the fuel spray in the fuel injection valve shown in FIG.
- FIG. 15 is a sectional view taken along line AA of FIG.
- FIG. 16 is a side view showing another example of the fuel injection valve used in the first embodiment.
- FIG. 17 is an enlarged view of a main part of the fuel injection valve shown in FIG.
- FIG. 18 is a diagram showing the flow of fuel in the AA cross section of FIG.
- FIG. 19 is a diagram showing a fuel swirl velocity distribution in a cross section BB of FIG.
- FIG. 20 is a side view showing the shape of the fuel spray in the fuel injection valve shown in FIG.
- FIG. 21 is a sectional view taken along line AA of FIG.
- FIG. 22 is a flowchart of combustion control immediately after engine start according to the first embodiment. is there.
- FIG. 23 is a diagram showing the air flow in the intake stroke during the warm-up operation in the first embodiment.
- FIG. 24 is a diagram illustrating the air flow and the fuel spray during the compression stroke (middle period) during the warm-up operation in the first embodiment.
- FIG. 25 is a diagram illustrating the behavior of the air-fuel mixture during the compression stroke (late period) during the warm-up operation in the first embodiment.
- FIG. 26 is a diagram showing the behavior of the air-fuel mixture at the ignition timing during the warm-up operation in the first embodiment.
- FIG. 27 is a diagram showing the exhaust gas flow in the exhaust stroke during the warm-up operation in the first embodiment.
- FIG. 28 is a diagram provided for explaining the turbulence of the exhaust flow in the exhaust passage provided with the turbulence generator.
- FIG. 29 is a diagram illustrating a relationship between the opening degree of the tumble generating valve and the engine rotation fluctuation rate during the warm-up operation in the first embodiment.
- FIG. 30 is a diagram provided for describing the definition of the opening degree of the tumble generation valve.
- FIG. 31 is a diagram showing the behavior of the air-fuel mixture at the latter stage of the compression stroke in the combustion chamber when the opening of the tumble generation valve is excessively small and the forward tumble flow in the combustion chamber is too strong during the warm-up operation.
- FIG. 32 is a diagram showing the mixture behavior at the ignition timing in the combustion chamber when the opening of the tumble generating valve is excessively small and the forward tumble flow in the combustion chamber is too strong during the engine operation.
- FIG. 33 is a diagram showing the behavior of the air-fuel mixture at the latter stage of the compression stroke in the combustion chamber when the forward tumble flow in the combustion chamber is too weak when the opening of the tumble generation valve is excessively large during the engine operation.
- FIG. 34 is a diagram showing the mixture behavior at the ignition timing in the combustion chamber when the opening of the tumble generating valve is excessively large and the forward tumble flow in the combustion chamber is too weak during the warm-up operation.
- FIG. 35 shows the procedure of ignition timing control during engine operation in the first embodiment. It is a flowchart.
- FIG. 36 is a flowchart of the control for optimizing the opening of the tumble generating valve during the engine operation in the first embodiment.
- FIG. 37 is a flowchart illustrating another procedure of the ignition timing control during the warm-up operation in the first embodiment.
- FIG. 38 is a flowchart of the fuel pressure optimization control during the warm-up operation in the first embodiment.
- FIG. 39 is a schematic configuration diagram of a second embodiment of the spark ignition engine according to the present invention.
- FIG. 40 is a schematic plan view showing the configuration around the combustion chamber of the engine shown in FIG. 39.
- FIG. 41 is a flowchart of the combustion control immediately after starting the engine in the second embodiment.
- FIG. 42 is a diagram showing the behavior of air and fuel in the combustion chamber during the intake stroke of the second embodiment.
- FIG. 43 is a diagram showing the behavior of air and fuel in the combustion chamber during the compression stroke of the second embodiment.
- FIG. 44 is a diagram showing the behavior of air and fuel in the combustion chamber at the ignition timing according to the second embodiment.
- FIG. 45 is a diagram showing the exhaust behavior in the exhaust stroke of the second embodiment.
- FIG. 46 is a diagram showing an example of a turbulence generator used in the engine of the present invention.
- FIG. 47 is a diagram showing another example of the turbulence generator used in the engine of the present invention.
- FIG. 48 is a view showing another example of the turbulence generator used in the engine of the present invention.
- FIG. 49 is a view showing another example of the turbulence generator used in the engine of the present invention.
- FIG. 50 is a view showing another example of the turbulence generator used in the engine of the present invention.
- FIG. 51 is a sectional view taken along line AA of FIG.
- FIG. 52 is a view showing another example of the turbulence generator used in the engine of the present invention.
- FIG. 53 is a sectional view taken along line AA of FIG. 52.
- FIG. 54 is a view showing another example of the turbulence generator used in the engine of the present invention.
- FIG. 55 is a view showing another example of the turbulence generator used in the engine of the present invention.
- FIG. 56 is a cross-sectional view showing a portion of the exhaust passage where a turbulence generator is arranged.
- FIG. 57 is a cross-sectional view showing an exhaust passage having a double pipe structure.
- FIG. 58 is a cross-sectional view showing another example of the turbulence generator used in the engine of the present invention.
- FIG. 59 is a side view of the turbulence generator shown in FIG.
- FIG. 60 is a view showing an example in which a turbulence generator used in the engine of the present invention is integrated with a gasket.
- FIG. 61 is a view showing a gasket used in the engine of the present invention.
- Fig. 62 shows a plate-like structure incorporating a turbulence generator.
- FIG. 63 is a view showing a state in which the plate-like structure of FIG. 62 is inserted and attached between the gaskets of FIG. 61.
- FIG. 64 is a cross-sectional view of the exhaust passage used to explain the definition of the width of the constituent member of the turbulence generator.
- FIG. 65 is a computer simulation result in an exhaust passage provided with a turbulence generator, and is a vector diagram of exhaust flow velocity.
- FIG. 66 is a computer simulation result in an exhaust passage provided with a turbulence generator, and is a contour map of HC concentration when no combustion is performed.
- FIG. 67 is a computer simulation result in an exhaust passage provided with a turbulence generator, and is a contour map of HC concentration during combustion.
- Figure 68 shows the measurement results of the HC concentration in the exhaust passage by the on-board test.
- Figure 69 is a vertical tomographic photograph of the fuel spray used in the bench test of the direct injection spark ignition engine.
- FIG. 70 shows the actual measurement results of the HC concentration during the warm-up operation in the in-cylinder injection spark ignition engine according to the present invention, and shows the time interval from the fuel injection timing to the ignition timing and the HC concentration. It is a figure which shows a correlation.
- FIG. 71 is a result of actual measurement of smoke concentration in the in-cylinder injection type spark ignition engine according to the present invention at the time of engine operation. The time interval between the fuel injection timing and the ignition timing and the smoke concentration are shown. It is a figure which shows a correlation.
- FIG. 1 is an overall configuration diagram of a first embodiment of a direct injection type spark ignition engine according to the present invention
- FIG. 2 is a perspective view showing the vicinity of a combustion chamber of the engine shown in FIG.
- the in-cylinder injection spark ignition engine 1A shown in FIGS. 1 and 2 has a combustion chamber 25 formed by a cylinder head 26, a cylinder block 17, and a piston 7 slidably fitted into a cylinder block 17. Is defined.
- the crown surface of the piston 7 is provided with a concave groove 18 having an arc-shaped bottom surface (cylindrical surface) 18a and a crescent or half-moon side surface 18b.
- two intake passages 15 (the intake port 15a thereof) and two exhaust passages 16 (the exhaust port 16a thereof) are opened.
- the intake port 15a and the exhaust port 16a of each of the intake passage 15 and the exhaust passage 16 are provided with an intake valve 13 and an exhaust valve 14, respectively, for opening and closing them.
- the fuel injection valve 5 is provided on the intake port 15a side of the combustion chamber 25, and fuel is directly injected and supplied from the fuel injection valve 5 into the combustion chamber 25.
- the fuel injection valve 5 is arranged between the two intake ports 15a, and is mounted to be inclined with respect to the central axis of the combustion chamber 25.
- the angle formed by the central axis of the combustion chamber 25 and the central axis of the fuel injection valve 5 is, for example, 50 ° force or 70 °.
- the fuel injection valve 5 is connected to a fuel tank 27, a fuel pump 23, and a power by a fuel pipe 24, respectively.
- the fuel pump 23 pressurizes the fuel supplied from the fuel tank 27 in order to inject sufficiently atomized fuel from the fuel injection valve 5 even when the pressure in the combustion chamber 25 is high.
- the fuel pressure at this time is, for example, 3 to 12 MPa, and the Sauter mean diameter of the fuel spray injected from the fuel injection valve 5 is, for example, 15 to 30 ⁇ .
- the pressure of the fuel pressurized by the fuel pump 23 can be arbitrarily adjusted within a range of, for example, 3 to 12 MPa by a fuel pressure control signal 43 from an engine control unit (ECU) 6.
- ECU engine control unit
- a spark plug 4 is provided at the center of the ceiling of the combustion chamber 25, and its electrode 4E Project into the combustion chamber 25.
- a creeping electrode type or a semi-creeping type is preferable because of its high stain resistance.
- the spark plug structure of the creepage electrode and the semi-creepage electrode is already widely known, and the detailed description thereof is omitted here.
- the ignition plug 4 is supplied with electric energy by an ignition coil (not shown), is discharged by the electrode 4E, and ignites the air-fuel mixture. At this time, the ignition plug 4 must be supplied with electric energy as high as possible. However, it is desirable from the viewpoint of stable ignition of a rich air-fuel mixture and the high fouling resistance of the electrode 4E.
- the electric energy supplied to the spark plug 4 is, for example, 70 to: L OmJ.
- the electric energy supplied from the ignition coil to the ignition plug 4 may be divided into a plurality of times. For example, the electric energy of a total of 100 mJ is divided into two times, the first time discharges 30 mJ of electric energy, and the second time discharges the remaining 70 mJ of electric energy.
- the first and second discharge time intervals are, for example, lms.
- a catalytic converter is provided downstream of the exhaust passage 16.
- a three-way catalytic converter, an N ⁇ x adsorption catalytic converter, an HC adsorption catalytic converter, or the like can be used.
- a plurality of different types of catalytic converters may be used in combination.
- a single catalytic converter that combines the functions of a plurality of these catalytic converters may be used.
- the exhaust passage 16 has, for example, a double-pipe structure, a thin wall, or the like so that the exhaust gas temperature does not decrease due to heat conduction to the wall surface of the exhaust passage 16.
- the exhaust passage having the double-pipe structure has a structure in which a tube wall 16 ⁇ is further provided outside the inner tube 16i (exhaust passage) with the air layer LY interposed therebetween, and the air layer L Due to ⁇ , the heat insulating effect is high, and the exhaust temperature is not easily reduced.
- the air layer between the double tubes a vacuum layer, the convective heat conduction of air is eliminated, so that the heat insulating effect is further enhanced.
- the exhaust passage having a reduced thickness has a lower heat capacity than the ordinary exhaust passage so that the temperature of the exhaust passage can be easily increased by the heat of the exhaust. In any However, by raising the temperature of the exhaust passage, a decrease in the exhaust gas temperature can be suppressed.
- a throttle valve is provided upstream of the intake passage 15, and the amount of air charged into the combustion chamber 25 is controlled by the degree of opening of the throttle valve.
- the throttle valve is an electronically controlled throttle valve, and the opening of the throttle valve is adjusted by a throttle valve opening signal 36 from the ECU 6.
- a tumbler valve 12 for opening and closing the lower half of the intake passage 15 for generating a forward longitudinal vortex 19 (hereinafter referred to as a forward tumble flow) in the combustion chamber 25 during the intake stroke.
- the tumble generating valve 12 is rotated by a drive motor 21 directly connected to the valve shaft 22, and the opening thereof is determined by a tumble generating valve opening signal supplied from the ECU 6 to the drive motor 21. Adjusted by 35.
- the tumble generating valve 12 is in a fully closed state (a state in which the lower half of the intake passage 15 is completely closed)
- the strongest forward turbulent flow is generated in the combustion chamber 25, and the tumbling generating valve 12 is opened from the fully closed state.
- the forward tumble flow in the combustion chamber 25 becomes the weakest.
- the ECU 6 outputs a pulse signal at every constant crank angle (for example, every 30 ° CA), a rotation angle signal 38 from the rotation angle sensor 37, and a pulse signal at every 720 ° CA. And a reference position signal 41 are input.
- the ECU 6 detects the engine speed Ne and the reference crank position from the rotation angle signal 38 and the reference position signal 41.
- a turbulence generator 50 is provided in the exhaust passage 16 (in the exhaust manifold) to generate turbulence in the exhaust air flow and increase the turbulence. It is desirable that the turbulence generator 50 be mounted at a position where the temperature of exhaust gas discharged from the combustion chamber 25 is sufficiently high during a warm-up operation to be described later. It is less than 500mm in the downstream direction from 16a). Further, the exhaust temperature at the mounting position of the turbulence generator 50 during the warm-up operation described later is generally 600 ° C. or higher.
- FIG. 3 shows a cross section of an exhaust passage 16 portion provided with a turbulence generator 50A.
- FIG. 4 shows an AA cross section of FIG.
- the illustrated turbulence generator 50A is composed of a plurality of rod-shaped members 50a arranged in parallel at equal intervals so as to be perpendicular (interrupted) to the exhaust flow direction.
- the cross-sectional shape of the rod-shaped material 50a may be any of a circle, a square, a rectangle, a triangle, etc., as shown in FIGS. ) May be used in combination.
- the turbulence generator 50A Since the turbulence generator 50A is exposed to high-temperature exhaust gas, it is preferable that the turbulence generator 50A be formed of a material having a melting point of 1500 ° C or more, such as pure iron, carbon steel, stainless steel, and ceramic.
- the fuel injection valve 5 (5A, 5B, 5C) used in the present embodiment and the spray of fuel injected from the fuel injection valve 5 will be described.
- FIG. 7 An example (5A) of the fuel injection valve 5 whose entirety is shown in FIG. 6 is shown in FIG. 7 in which a cross section of a main part (a region X surrounded by a broken line in FIG. 6) is shown.
- a tip portion 28 is provided at the tip side, and the tip portion 28 has a conical valve 29, a plunger 30 connected to the conical valve 29, and a spur that gives a turning force to the spray. 31, an injection port 32, an axial groove 33, and a radial groove 34.
- the nozzle 32 provided at the tip of the nozzle 28 has a notch 32a in a part thereof which is not symmetrical. In the illustrated example, the notch 32a is provided in a range of 180 °.
- the direction of arrow IGN-P is on the spark plug 4 side
- the direction of arrow PSTN is on the piston 7 side. That is, by installing the fuel injection valve 5 so that the notch 32a of the injection port 32 faces the ignition plug 4, the reed fog 20L faces the spark plug 4 and the main spray 20M faces the piston 7. Is done.
- FIGS. 9 and 10 a cross-sectional view taken along the line AA in FIG. 9).
- the shape of the fuel spray injected from the injection port 32 of the fuel injection valve 5 is cut into the injection port. Since the notch 32a is provided, it is not symmetrical. Center line of fuel glow valve 5
- the mist angle ⁇ 1 of 20L is set to, for example, 30 °
- the mist angle ⁇ 2 of the main spray 20M is set to, for example, 20 °.
- the cross-sectional shape of the fuel spray is a shape having a gap 20A in a part of the spray due to the notch 32a provided in the injection port 32.
- the flow density of the lead spray 20L toward the ignition plug 4 is higher than the main spray 20M.
- the net ration (flying distance) L1 of the lead mist 20L is longer than the penetration L2 of the main mist 20M.
- the main spray 20M of the penetration L2 to the penetration L2 of 20L of the penetration L1 is j; dri: Ll ;; L2 i, here, 1.3 to 1.5.
- mist angle ⁇ 1 of the lead spray 20L and the mist angle ⁇ 2 of the main spray 20M can be variously changed depending on the shape of the notch 32a provided in the injection port 32.
- FIG. 11 is a side view of another example (5B) of the fuel injection valve 5, and FIG. 12 is a cross-sectional view of a main part thereof (a region X surrounded by a broken line in FIG. 11).
- the injection port 28 of the fuel injection valve 5B has a fuel injection port 32C that generates a lead spray 20L and a fuel injection port 32D that generates a main spray 20M. It has a structure.
- the fuel injection port 32C is formed at an angle of ⁇ 8 with respect to the central axis of the fuel injection valve 5B so that when the fuel injection valve is attached to the engine, the lead spray 20L force is directed to the spark plug electrode. Have been.
- the fuel injection port 32C has a larger diameter than the fuel injection port 32D.
- the fuel injection port 32D has a small diameter S, and a plurality of nozzles are provided to inject the amount of fuel required for operation, and the positions of the nozzles are dispersed so that the density of the main spray 20M is reduced. ing.
- FIG. 14 is a side view showing the shape of the fuel spray injected from the fuel injection valve 5B
- FIG. 15 is a sectional view taken along line AA of FIG.
- the shape of the main spray 20M emitted from the fuel injection port 32D of the fuel injection valve 5B is uniform in the circumferential direction.
- a high-pressure reed spray 20L is injected from the injection port 32C of the fuel injection valve 5B.
- the angle 0 10 between the main spray 20M and the lead spray 20L is, for example, 0 to 10 °.
- the solution LI is longer than the 20M main spray L2.
- the ratio L1ZL2 of the penetration L1 of 20L of the lead spray to the penetration L2 of the main spray 20M is, for example, 1.3 to 1.5.
- FIG. 17 Another example (5C) of the fuel injection valve 5 whose entirety is shown in FIG. 16 is shown in FIG. 17 in which a cross section of a main part (region X surrounded by a broken line in FIG. 16) is shown.
- the injection port 28 of the fuel injection valve 5C includes a conical valve 29, a plunger 30 connected to the conical valve 29, a spooler 31 for applying a turning force to the spray, an injection port 32, an axial groove 33, A radial groove 34 is provided.
- the axial direction of the injection port 32 provided at the tip of the injection port portion 28 is deflected by an angle of ⁇ 5 with respect to the center axis of the fuel injection valve 5C. The direction of deflection is determined so that when the fuel injection valve 5C is attached to the engine, the deflection is deflected toward the spark plug 4.
- the conical valve 29 When the conical valve 29 is opened, the fuel flows through the axial groove 33 and the radial groove 34, and the fuel to which the swirling force is applied is injected from the water outlet 32. Since the injection port 32 is deflected with respect to the center axis of the injection valve 5, the shape of the spray is asymmetric with respect to the center axis of the injection valve 5C.
- FIG. 18 shows the flow of fuel in the A-A section of the injection port 32 of the fuel injection valve 5C shown in FIG.
- the swirling force is given to the fuel by the swirler 31, the fuel swirls inside the injection port 32.
- the injection port 32 is deflected with respect to the center axis of the fuel injection valve 5, the center of rotation SC of the fuel in the injection port 32 is shifted from the center of the injection port 32 toward the PSTN.
- FIG. 19 shows the velocity distribution of the fuel in the swirling direction along the section AA in FIG. Since the swirl center SC of the fuel at the injection port is displaced from the central axis of the fuel injection valve 5, the rotational speed of the fuel on the IGN1P side is lower than the rotational speed of the fuel on the PSTN side.
- FIG. 20 is a side view showing the shape of the fuel spray injected from the fuel injection valve 5C
- FIG. 21 is a sectional view taken along line AA of FIG. Since the injection port 32 is deflected with respect to the central axis of the fuel injection valve 5, the fuel injection direction is curved in the deflection direction of the injection port 32.
- the penetration L1 on the deflection side (IGN-P side) is longer than the penetration L2 on the opposite side (PSTN side). This is for the following reason. As shown in Fig. 19, since the turning speed on the IGN-P side is lower than the turning speed on the PSTN side, the centrifugal force acting on the fuel in the injection port 32 is lower on the IGN-P side than on the PSTN side. weak.
- the liquid film thickness formed immediately below the injection port 32 becomes thicker on the IGN-P side and thinner on the PSTN side.
- the atomization force of the liquid film on the IGN-P side is worse than that on the PSTN side, and the particle size on the IGN-P side becomes larger than that on the PSTN side. Therefore, the fog injected from the fuel injector 5C is formed on the long lead fog 20L force SIGN-P side of the penetration and the short main fog 20M of the penetration is on the PSTN side. It is formed.
- a valve element for example, a conical valve
- the valve body opens for a predetermined time in accordance with an injection signal from the ECU, and fuel is injected.
- the valve body rebounds (punching), and excess fuel may be injected (secondary injection).
- the fuel injected by this secondary injection generally has a large particle size, has a strong penetration force, and is poorly vaporized, so it adheres to the crown surface of the piston, causing soot (smoke) and HC. .
- FIG. 22 shows a flowchart of combustion control in the spark ignition engine of this embodiment immediately after the start of the engine.
- the engine 1A is started by a starter (not shown)
- the temperature of the cooling water 2 of the engine is detected by the water temperature sensor 8 shown in FIG. 1, and a cooling water temperature signal 9 is input to the ECU 6 (301).
- the ECU 6 compares the temperature Tw of the engine cooling water 2 detected by the water temperature sensor 8 with a preset reference temperature Tc (302), and when the cooling water temperature Tw is lower than the reference temperature Tc, the engine 6 described later. No Perform machine operation control. If the cooling water temperature Tw is higher than the reference temperature Tc, non-warming operation control is performed (307).
- the non-warm-up operation control 307 refers to, for example, operation control in which the fuel injection timing, the ignition timing, and the opening of the tumble generating valve are set so that the fuel efficiency of the engine is maximized.
- the ECU 6 sends an opening signal to the throttle valve (not shown) from the ECU 6 and sets the throttle valve opening to the angle specified by the ECU. (303).
- the engine output required for the warm-up operation is set with the air-fuel ratio of the inside of the combustion chamber 25 set to 14 to 17 and the ignition timing set to 110 to 30 ° ATDC.
- the number of revolutions (the engine output is the indicated average effective pressure, 200 to 250 kPa in a row, the engine speed is 1000 to 2000 rpm in the case of! L). Set as degrees.
- the air volume at this time is, for example, about 50% in volumetric efficiency.
- the tumble generation valve opening signal 35 is sent from the ECU 6 to the tumble generation valve drive motor 21 to set the tumbler generation valve 12 to a predetermined opening (304).
- the angle of the tumble generating valve is determined in advance by a preliminary test or the like at a position where the rotation fluctuation of the engine during the warm-up operation becomes smaller than a predetermined rotation fluctuation.
- the opening of the tumble generating valve 12 is fully closed as shown in FIG. That is, the lower portion of the cross section of the intake passage 15 is completely closed by the tumble generation valve 12.
- a fuel injection signal 11 is sent from the ECU 6 to the fuel injection valve 5 so that the air-fuel ratio in the combustion chamber 25 becomes 14 to 17 in the latter half of the compression stroke. The fuel is sprayed toward (305).
- the timing of starting the fuel injection from the fuel injection valve 5 is, for example, 80 to 50 ° CA before the compression top dead center.
- the fuel injection period from the fuel injection valve 5 is, for example, 1.5 to 2.5 ms.
- the fuel pressure is, for example, 3 to: llMPa.
- an ignition signal 10 is sent from the ECU 6 to the spark plug 4, and the ignition signal is ignited by the spark plug 4 in the range of 10 to 30 ° ATDC (306).
- fuel injection start It should be noted that fuel injection start It is desirable that the time interval from ignition to ignition be 9 ms or more. Therefore, for example, when the engine speed is 1200 rpm and the fuel injection start timing is 70 ° CA before the compression top dead center, the ignition timing is desirably 15 ° ATDC or later.
- the intake valve 13 In the compression stroke following the intake stroke, the intake valve 13 is closed, and the piston 7 rises toward the top dead center. As the piston 7 rises, the volume inside the combustion chamber 25 decreases, and the shape of the combustion chamber 25 becomes flat.However, the concave groove 18 provided on the crown surface of the piston 7 causes the latter half of the compression stroke. In this case, the forward tumble flow 19 in the combustion chamber 25 is maintained without collapse.
- an injection signal 11 is sent from the ECU 6 to the fuel injection valve 5, and fuel is injected from the fuel injection valve 5 into the combustion chamber 25.
- the fuel pressure is adjusted during the injection period so that the average air-fuel ratio in the combustion chamber 25 is about 14 to 17.
- the fuel injection start timing is, for example, 80 to 50 ° CA before the compression top dead center, and the injection period is, for example, 1.5 to 2.5 ms.
- the fuel pressure is, for example, 3 to: L lMPa.
- the fuel spray injected from the fuel injection valve 5 is divided into a lead spray 20L toward the spark plug 4 side and a main spray toward the piston 7 side. It is composed of 20M.
- the lead mist 20L The net ration is longer than the 20M net mist.
- the speed of the reed fog 20L immediately after the injection is, for example, 60 to 80 mZs.
- the flow velocity of the forward tumble flow 19 in the same period is, for example, l O SOmZs when the engine speed is 1200 rpm. That is, the speed of the reed spray 20 L is much higher than the air flow speed of the forward tumble flow 19. For this reason, the air above the combustion chamber 25 is accelerated from the intake side to the exhaust side by the reed spray 20L.
- the air accelerated by the reed fog 20L becomes a rich mixture by vaporization of the reed fog 20L, passes through the upper part of the combustion chamber 25, and turns back on the exhaust side wall surface of the combustion chamber 25.
- An air-fuel mixture flow MF1 is formed along the surface of the piston 7 toward the center of the combustion chamber 25.
- the main spray 20M directed in the direction of the piston 7 has a traveling direction opposite to the direction of the forward tumble flow 19 flowing along the concave groove 18 in the crown surface of the piston 7.
- the penetration of 20M main spray is shorter than the penetration of 20L of lead fog, and the penetration force is weak.
- the main mist 20M collides with the forward tumble flow 19 flowing along the concave groove 18 in the crown face of the piston 7, and the momentum of each other is rapidly lost.
- the speed of the main spray 20M immediately after the shaking is 20 to 40 m / s, for example, which is higher than the air velocity of the forward tumbling flow 19 of 10 to 20 m / s. Therefore, as shown in FIG.
- the air on the surface of the piston 4 changes the flow direction due to the penetration force of the main spray 2QM, and forms a rich air-fuel mixture by the vaporization of the main spray 20M, and the combustion chamber from the intake side.
- the mixture flow MF2 is directed toward the center of 25.
- the main spray 20M is injected toward the crown surface of the piston 7, but since the main spray 20M is opposed to the direction of the tumble flow 19 in the combustion chamber 4, the speed of the main spray 20M is reduced. , Drops immediately after injection.
- the main spray 20M evaporates quickly, and a fuel liquid film is not easily generated on the crown surface of the piston 7.
- the mixed air flows MF 1 and MF 2 from opposite directions collide with each other, losing momentum, and the gas pressure in the combustion chamber 25 caused by the rise of the piston 7. Due to the rise, the movement of the mixture becomes slow, and the rich mixture M stays around the spark plug electrode 4E.
- the air-fuel mixture in the combustion chamber 25 is ignited by the ignition plug 4 based on the ignition signal from the ECU 6 near or after the top dead center.
- the mixture of HC, CO, H2, and O2 discharged into the exhaust passage 16 is promoted, and the oxidation reaction of HC proceeds rapidly.
- the exhaust gas temperature in the exhaust passage 16 increases, and the HC concentration decreases.
- the HC concentration at the time of warming up the engine can be reduced, and the temperature of the catalytic converter provided in the lower portion of the exhaust passage 16 can be quickly raised to a temperature at which the exhaust gas purification efficiency is high by the high-temperature exhaust gas.
- fuel is injected such that the air-fuel ratio becomes 14 to 17 in the latter half of the compression stroke.
- soot the amount of soot (smoke) increases.
- the piston A fuel liquid film (adhesion) is unlikely to be formed due to the collision of the main spray toward the piston crown surface.
- the lead spray is directed in the direction of the spark plug and adheres to the wall.
- the tamper generation valve 12 for generating a forward tumble flow in the combustion chamber 25 is set to a predetermined opening degree by the ECU 6.
- the opening of the tumble generating valve 12 is determined by preliminary tests or the like assuming that the rotation fluctuation and torque fluctuation of the engine during the warm-up operation become equal to or less than predetermined values. It is desirable to delay the ignition timing as much as possible in order to increase the exhaust gas temperature by increasing the HC combustion inside and suppress the generation of soot.
- the ignition timing is excessively retarded, the combustion deteriorates, and the rotation fluctuation and torque fluctuation of the engine increase. Therefore, in order to retard the ignition timing as much as possible, at the ignition timing, a mixture of a certain concentration is surely concentrated around the spark plug so that the ignition plug can reliably ignite even if the ignition is retarded. It is necessary.
- the opening degree 0 of the tumble generation valve 12 T is defined by the opening when the fully closed state of the tumble generation valve 12 as a reference (0 °).
- the engine speed variation rate ⁇ ⁇ is defined as a standard deviation with respect to the average engine speed e as shown in Expressions 1 and 2 below.
- N in Equations 1 and 2 is the number of sampling points of the engine speed.
- the engine speed Ne is determined by the rotation angle signal 38 from the rotation angle sensor 37 input to the ECU 6 and the reference position from the reference position sensor 40.
- the position signal 41 is detected by the ECU 6.
- the engine rotation fluctuation rate £ ⁇ ⁇ is calculated.
- the opening degree 0 T of tumble generating valve, the ⁇ rotational variation of the engine ⁇ is correlated, by optimally setting the opening degree 0 T of the tumble generation valve, the engine The rotation fluctuation rate can be minimized, and the ignition retard can be further increased.
- the injection direction of the reed mist and the direction of the forward tumble flow are equal, and the reed spray penetrates and flows from the exhaust side toward the center of the combustion chamber.
- the mixed air flow MF 1 becomes stronger.
- the main spray and the forward tumble flow are opposed to each other, and the mixture flow MF2 flowing from the intake side toward the center of the combustion chamber becomes weaker due to the penetration force of the main spray.
- the collision position between the mixed gas flow MF1 and the mixed gas flow MF2 is closer to the intake side than the position of the spark plug electrode 4 °.
- Fig. 33 and Fig. 34 show the behavior of the air-fuel mixture in the combustion chamber 25 when the forward tumble flow in the combustion chamber 25 where the opening 0 T of the tumble generation valve is too large during the warm-up operation is too weak. Show.
- the injection direction of the reed spray and the forward tumbling flow direction are equal, and the reed mist penetrates from the exhaust side toward the center of the combustion chamber.
- the flowing air mixture MF 1 becomes weaker.
- the raw spray and the forward tumble flow are opposed to each other, and the mixed airflow MF2 flowing from the intake side toward the center of the combustion chamber becomes stronger due to the penetration force of the main spray.
- the collision position between the mixed gas flow MF1 and the mixed gas flow MF2 is on the exhaust side from the position of the spark plug electrode 4 °.
- FIG. 33 shows that the collision position between the mixed gas flow MF1 and the mixed gas flow MF2 is on the exhaust side from the position of the spark plug electrode 4 °.
- the rich air-fuel mixture stagnates on the exhaust side of the spark plug electrode 4 ⁇ , the air-fuel mixture concentration at the spark plug electrode 4 ⁇ ⁇ becomes thin, and the ignition performance of the air-fuel mixture by the spark plug deteriorates.
- engine rotation fluctuations and torque fluctuations increase. That is, during warm-up operation, the opening ⁇ ⁇ of the tumble generating valve 12 needs to be set to the optimum opening in order to suppress the engine rotation fluctuation and torque fluctuation and further retard the ignition timing. is there.
- FIG. 35 is a flowchart showing the procedure of ignition timing optimal control during engine operation.
- ECU sets the ignition timing to 0 1GN Q (100).
- ⁇ ⁇ 0 ⁇ ° is the initial value of the ignition timing, and the ignition timing is set by preliminary tests and the like so that the engine rotation fluctuation and torque fluctuation are small and the combustion of the engine can be reliably maintained .
- 0 1G is, for example, 10 ° CA before the top dead center of the compression stroke.
- the calculated engine rotation fluctuation rate ⁇ ⁇ is set to a predetermined engine rotation fluctuation rate Is compared with the threshold a NC (103).
- Engine speed fluctuation threshold is set, for example, as an upper limit of the engine rotation fluctuation rate that can be allowed by the occupant of the vehicle during the warm-up operation.
- ⁇ 0 IGN is an ignition timing change angle that takes a positive value, for example, ⁇ CA. Then, the processing after 101 is repeated with the newly set ignition time 0 IGN Q.
- the combustion is unstable, and a new ignition timing is set to perform more stable combustion.
- the ignition timing is advanced from the current ignition timing 0 1GN D by ⁇ 0 IGN , and replaced with ⁇ 1GN 0 (104). And the newly set ignition timing GN . Repeat the steps from 101 onwards.
- FIG. 36 shows a flowchart of the optimization control of the tumble generating valve opening ⁇ ⁇ .
- the value of the counter ⁇ is initialized to 0 (201), Then, to set the opening degree of the tumble generation valve to an initial value 0 T D (2 02).
- the initial opening degree 0 ° of the tumble generating valve is set between the fully closed state and the fully opened state, and is, for example, 45 °.
- Kmax is the number of times that specifies how many times the tumble generation valve opening ⁇ is reset, and is, for example, a number of 100 or more.
- ⁇ e T is a preset change amount of the opening of the tumble generating valve, and is, for example, r.
- the opening of the tumble generating valve is set to 0 T (_), and the engine speed fluctuation rate ⁇ ⁇ (1) at that time is calculated using Equations 1 and 2 (206).
- Equation 4 (208).
- [d (j N / d 0 T] ( I) is, when the tumble generation valve closed only delta theta T, for the tumble control valve opening, the slope value of the engine rotational variation.
- [(1 and ( 10 1 (+) are the gradient values of the engine rotation fluctuation rate with respect to the tumble generation valve opening when the tumble generation valve is opened by e T.
- process 210 is performed.
- process 204 the value of the counter ⁇ is After exceed Kmax, exit the optimization control of the tumble control valve opening 0 T, proceeds to a process 102 in FIG. 35.
- the ignition timing is further delayed by optimally controlling the opening of the tumble generating valve so that the engine rotation fluctuation is minimized.
- the temperature of the exhaust gas rises, and the turbulence generator 50 ⁇ promotes the mixing of HC, 02, CO, and H2 in the exhaust passage 16, reduces HC due to HC combustion in the exhaust passage, and reduces the exhaust gas temperature.
- the effects of raising the temperature and activating the catalyst early can be further enhanced.
- the same effect as the optimal control of the tumble generating valve opening can be obtained by the optimal control of the fuel pressure.
- the ignition timing can be retarded even if the fuel fog penetration is adjusted by the fuel pressure.
- the ECU sets the ignition timing to e IGN Q in the flowchart shown in FIG. 37 for performing the optimal control of the ignition timing and the fuel pressure (600).
- e icN ° is an initial value of the ignition timing, and a preliminary test or the like sets an ignition timing at which engine rotation fluctuation and torque fluctuation are small and combustion of the engine can be reliably maintained .
- 0 IGN ° is, for example, 10 ° CA before compression top dead center.
- the optimization control of the later-described fuel pressure P f, the fuel pressure P f is the rotation fluctuation of the engine is set so that the torque fluctuation is minimized (601).
- Equation 1 it is the engine rotational variation sigma New force S calculated by Equation 2 (602).
- the calculated engine rotation fluctuation rate ⁇ ⁇ is compared with a preset threshold value NC of the engine rotation fluctuation rate (603).
- NC the engine rotation fluctuation rate
- the threshold ⁇ ⁇ ⁇ of the engine speed fluctuation rate Is set, for example, as the upper limit of the engine rotation fluctuation rate that can be tolerated by the occupant of the vehicle at the time of rotation.
- the new ignition timing should be changed to the current ignition timing ⁇ ⁇ (3 ⁇ °
- ⁇ 0 IGN is an ignition timing change angle that takes a positive value, for example, ⁇ CA.
- S IGN is the newly set ignition time
- the combustion is unstable, and a new ignition timing is set to perform more stable combustion.
- the ignition timing is advanced by 1e IGN from the current ignition timing e1GN °, and is replaced with ⁇ GN ° (604). Then, the process after 601 is repeated with the newly set ignition timing 0 IGN Q.
- the optimization control of the fuel pressure P f in FIG. 37 will be described with reference to FIG.
- the value of the counter K is initialized to 0 (701), and subsequently, the fuel pressure is set to the initial value P f ° (702).
- the initial value P f Q of the fuel pressure is set between the minimum fuel pressure and the maximum fuel pressure, and is, for example, 5 MPa.
- Kmax is the number of times to specify how many times the fuel pressure P f is reset, and is, for example, 100 or more.
- the engine rotation fluctuation rate ⁇ ⁇ ⁇ ⁇ ⁇ ⁇ at the current fuel pressure P f Q is calculated by the equations 1 and 2 (714).
- ⁇ ⁇ is a preset change amount of the fuel pressure, for example, 0.2 MPa.
- Equation 3 and 4 the gradient value of the engine rotation fluctuation rate with respect to the fuel pressure is obtained by using Equations 3 and 4 (708).
- [d CT N / dP f ] ( —) is a function of the fuel pressure when the fuel pressure is reduced by ⁇ ⁇ This is the gradient value of the rotation variation rate.
- [da N / dP f] (+) is, in the case of raising the fuel pressure only A Pf, for the fuel pressure, the slope value of the engine rotational variation.
- step 704 the value of the counter K is After exceed Kmax, exit the optimization control of the fuel pressure P f, moves to the process 602 of FIG. 37.
- the ignition timing can be further retarded by optimally controlling the fuel pressure so that the rotation fluctuation of the engine is minimized. it can.
- the temperature of the exhaust gas increases, and the turbulence generator 50A promotes the mixing of HC, 02, CO, and H2 in the exhaust passage 16, reduces HC by HC combustion in the exhaust passage, and raises the exhaust gas temperature. Temperature and the effect of early activation of the catalyst can be further enhanced.
- FIG. 39 shows a spark ignition engine 1B of the second embodiment.
- the spark ignition engine 1B of the second embodiment is an intake port injection type spark ignition engine, which is the most different from the first embodiment (in-cylinder injection type).
- FIG. 39 portions corresponding to the respective portions in FIG. 1 are denoted by the same reference numerals, and redundant description will be omitted. In the following, differences will be mainly described.
- the piston 7 is slidably fitted in the cylinder bore 60, and the combustion chamber 25 is formed above the piston 7.
- the intake passage 15 has a distal end (downstream end) branched in a bifurcated manner by a branch wall 61.
- This intake passage 15 with a bifurcated tip Intake ports 15a, 15b communicating with one side of the combustion chamber 25 and forming the distal end thereof are provided with intake valves 13a, 13b, respectively.
- the exhaust passage 16 also has a bifurcated branch at the tip (upstream end). The exhaust passage 16 communicates with the other side of the combustion chamber 60.
- Exhaust valves 14a and 14b are provided at exhaust ports 16a and 16b which form the distal end.
- a catalytic converter (not shown) is provided at the rear of the exhaust passage 16.
- the catalytic converter is, for example, a three-way catalytic converter, for example, a NOx adsorption catalytic converter, for example, an HC adsorption catalytic converter.
- these different types of catalytic converters may be used in combination.
- a single catalytic converter that combines the functions of these plural catalytic converters may be used.
- a throttle valve (not shown) is provided upstream of the intake passage 15, and the amount of air charged into the combustion chamber 25 is controlled by the opening of the throttle valve.
- the throttle valve is an electronically controlled throttle valve, and the opening of the throttle valve can be adjusted to an arbitrary opening by a throttle valve opening signal 36 from the ECU 6.
- a tumble generating valve 12 that opens and closes a lower half of the intake passage 15 is provided.
- the tumble generation valve 12 is rotated by a drive motor 21 directly connected to the valve shaft 22, and its opening is determined by a tumble generation valve opening signal 35 supplied from the ECU 6 to the drive motor 21.
- a fuel injection valve 5 for injecting fuel into the intake ports 15a and 15b is mounted above the tumble generating valve 12 in the intake passage 15, and an injection port 28 of the fuel injection valve 25 is provided inside the intake passage 15. It is provided to protrude.
- the front end of the spiral section 28, that is, the injection port 32 of the fuel injection valve 5 is located on the downstream side of the rotation shaft 22 of the tumble generating valve 12 and below it. Therefore, when the tumble generating valve 12 is closed, the fuel injection The valve outlet 32 of valve 5 is on the lower side.
- the fuel injection valve 5 is capable of injecting the fuel 20 in two directions, and the fuel injected from the fuel injection valve 5 is directed to the head of the intake valves 13a and 13b that open and close the intake boats 15a and 15b.
- the fuel injector 5 be capable of injecting fuel having a small particle diameter so that the fuel injected can be quickly vaporized in the combustion chamber 25, and the average particle diameter thereof is approximately 30 ⁇ or less. Is desirable.
- a method using assist air or a method using a porous nozzle can be considered.
- the injection amount and injection timing of the fuel injected from the fuel injection valve 5 are controlled by an injection signal 11 from the ECU 6.
- An ignition plug 4 is provided in the upper part of the combustion chamber 60, and the air-fuel mixture is ignited by the ignition plug 4.
- the ECU 6 outputs a pulse signal at every constant crank angle (for example, every 30 ° CA), a rotation angle signal 38 from the rotation angle sensor 37, and a pulse signal at every 720 ° CA.
- the reference position signal 41 is input.
- the ECU 6 detects the engine speed Ne and the reference crank position from the rotation angle signal 38 and the reference position signal 41.
- a turbulence generator 50 is provided in the exhaust passage 16 (exhaust manifold).
- the turbulence generator 50 is desirably mounted at a position where the temperature of exhaust gas discharged from the combustion chamber 25 is sufficiently high during a warm-up operation to be described later. It is generally within 500mm. Further, the exhaust temperature at the mounting position of the turbulence generator 50 during the warm-up operation described later is generally 600 ° C. or higher.
- a water temperature sensor 8 for detecting the temperature of the cooling water 2 is attached to the cylinder block 17, and a water temperature signal 9 is input to the ECU 6 from the water temperature sensor 8.
- FIG. 41 shows a flowchart of the combustion control executed by the ECU 6 immediately after the start of the engine 1B.
- the engine 1B is started by a starter (not shown)
- the temperature of the cooling water 2 is detected by the water temperature sensor 8, and a cooling water temperature signal 9 is input to the ECU 6 (401).
- the ECU 6 compares the coolant temperature Tw detected by the coolant temperature sensor 8 with a preset reference temperature Tc (402), and if the coolant temperature Tw is lower than the reference temperature Tc. In this case, warm-up operation control is performed. If the cooling water temperature Tw is higher than the reference temperature Tc, non-warm-up operation control is performed (407).
- non-warm-up operation control refers to, for example, operation control in which the fuel injection timing, the ignition timing, and the opening of the tumble generating valve are set so as to maximize the fuel efficiency of the engine.
- the ECU 6 sends an opening signal to the throttle valve to set the throttle valve opening to the angle specified by the ECU. (403).
- the engine output required for warm-up operation is set with the air-fuel ratio in the combustion chamber 25 set to 14 to 17 and the ignition timing set to 110 to 30 ° ATDC.
- the air volume at this time is, for example, about 50% in volumetric efficiency.
- the tumble generation valve opening signal 35 is sent from the ECU 6 to the tumble generation valve drive motor 21, and the tumble generation valve 12 is set to a predetermined opening (404).
- the angle of the tumble generating valve is determined in advance by a preliminary test or the like as an opening at which the rotation fluctuation of the engine during the warm-up operation becomes smaller than a predetermined value.
- the opening of the tumble generation valve 12 is fully closed as shown in FIG. That is, the lower half of the intake passage 15 is completely closed by the tumble generating valve 12.
- a fuel injection signal 11 is sent from the ECU 6 to the fuel injection valve 5 so that the air-fuel ratio in the combustion chamber 25 becomes 14 to 17 in the middle stage of the intake stroke. Then, fuel is injected (405).
- the timing of starting the fuel injection from the fuel injection valve 5 is, for example, 90 ° CA after the intake top dead center. Subsequent to the fuel injection, an ignition signal 10 is sent from the ECU 6 to the ignition plug 4 and is ignited by the ignition plug 4 in the range of 1-10 to 30 ° ATDC (406).
- FIGS. 42 to 45 show the process of forming the air-fuel mixture during the warm-up operation in the present embodiment.
- the tumble generation valve 12 closes and closes the lower section of the intake passage 15 so that the intake air is blocked.
- a high-speed air flow is generated in the upper half of the passage 15 and flows into the combustion chamber 25 from the upper portion (exhaust side) of the intake valve 13 to form a forward tumble flow 19 in the combustion chamber 25.
- the fuel spray 20 is injected during the intake stroke from the fuel injection valve 5 toward the umbrella intake side of the intake valve 13. At this time, the fuel spray 20 is closed by closing the tumble generation valve 12.
- the behavior of the fuel 20 is hardly affected by such high-speed airflow. Absent. In other words, the trajectory of the fuel system 20 collides with the intake side of the umbrella portion of the intake valve 13 without being bent by the high-speed airflow.
- the fuel 20 colliding with the umbrella intake side of the intake valve 13 is atomized there, enters the combustion chamber 25 while being vaporized from the periphery of the umbrella intake side of the intake valve 13, and forms an air-fuel mixture M.
- the air-fuel mixture M formed below the intake valve 13 is transported to the upper part of the combustion chamber by the forward tumble flow 19 generated in the combustion chamber 25, and the mixture shown in FIG.
- the air-fuel mixture M is stratified around the spark plug electrode 4E.
- an air-fuel mixture having excellent ignitability is formed around the spark plug electrode 4E, and the ignition is performed by the spark plug 4 immediately before or after the top dead center of the compression stroke, and the gas in the combustion chamber explodes. Swell.
- the adhesion of the fuel spray 20 to the intake passage wall surface can be reduced. HC emission can be reduced, and the mixture M can be reliably stratified around the ignition plug electrode 4E. Further, since the fuel injection timing is in the middle stage of the intake stroke as shown in FIG. 42, the air-fuel mixture M is concentrated only around the spark plug electrode 4E as shown in FIG. Therefore, even if the ignition timing is retarded to 110 to 30 ° ATDC, the mixture is reliably ignited and stable combustion is possible.
- the exhaust temperature is high due to the retarded ignition timing, and the mixture of HC, 02, CO, and H2 in the exhaust passage 16 is promoted by the turbulence generator 50 in the exhaust passage 16, so that the exhaust The oxidation reaction (combustion) of HC occurs rapidly in the passage 16. As a result, the exhaust gas temperature further increases, and the HC concentration decreases.
- the turbulence generator 50B shown in FIG. 46 is one in which constituent members (bar-shaped members) are arranged vertically or horizontally in a grid or mesh.
- the constituent members (bars) are arranged vertically and horizontally in a lattice or mesh shape. It gets narrower as it gets closer to the inner wall.
- the exhaust temperature near the inner wall surface of the exhaust passage 16 is lower than that at the center of the exhaust passage 16 due to heat radiation from the wall surface. Therefore, by increasing the density of the constituent members (rods) near the inner wall surface, the turbulence intensity near the wall surface increases, and the mixing of HC, 02, CO, and H2 near the wall surface is promoted. As a result, it is possible to prevent a decrease in the reaction rate of HC due to a decrease in the exhaust gas temperature near the wall surface.
- a turbulence generator 50D shown in FIG. 48 has a configuration in which annular members are concentrically arranged to form a web. In this arrangement, the density of the components near the wall can be changed more easily.
- the turbulence generator 50E shown in FIG. 49 is composed of a plurality of protrusions (rods) projecting inward from the inner wall surface of the exhaust passage 16.
- the protrusions are arranged radially at equal intervals.
- This turbulence generator 50E has a high effect of preventing a reduction in the speed of the HC oxidation reaction near the wall of the exhaust passage 16.
- due to its structure it is possible to form an object integrally with the exhaust passage 16, and there is an advantage that the manufacturing cost is reduced.
- the turbulence generator 50F shown in FIG. 50 is formed of an annular plate protruding inward from the inner wall surface of the exhaust passage 16 (see also FIG. 51 which is a cross section taken along line AA of FIG. 50). This also has a high effect of promoting the HC oxidation reaction near the wall surface of the exhaust passage 16. In addition, since it is constituted by an annular plate, its structural strength can be increased.
- the turbulence generator 50G shown in FIG. 52 and FIG. 53 is also formed of an annular body projecting inward from the inner wall surface of the exhaust passage 16, but has a triangular cross section. In this device, a turbulent flow ED is generated near the wall surface to promote the HC oxidation reaction near the wall surface, and HC, 02, etc.
- the turbulence generator 50H shown in FIG. 54 is composed of a step provided on the inner wall surface of the exhaust passage 16. In other words, the cross-sectional area of the exhaust passage 16 is widened in a step-like manner, and a separation flow is generated downstream of the step, thereby generating a turbulent flow ED. Further, the turbulence generator 501 shown in FIG. 55 has the cross-sectional area of the exhaust passage 16 narrowed in a step-like manner. In this case also, separation occurs in the wake of the step, and the turbulent flow ED can be generated. . Since the turbulence generators 50H and 501 shown in FIGS. 54 and 55 need only be changed in the thickness of the exhaust passage 16, the turbulence generator can be easily and inexpensively made.
- FIG. 56 shows an example in which the cross-sectional area of the portion of the exhaust passage 16 where the turbulence generator 50 is provided is made larger than the front and rear portions. In this example, it is possible to prevent an increase in exhaust resistance due to a decrease in the effective cross-sectional area of the exhaust passage 16 due to the provision of the turbulence generator 50 in the exhaust passage 16.
- FIG. 57 shows an example in which the exhaust passage 16 has a double pipe structure.
- FIGS. 58 and 59 show examples in which the turbulence generator 50 (50J) can be electrically heated.
- the exhaust passage 16 is made of a material having good electric conductivity
- the turbulence generator 50J is made of a material having a large electric resistance, such as nichrome or tungsten. 161 is an electrical insulating material.
- the switch S is turned on and the voltage is applied to the turbulence generator 50J from the battery EB, so that the turbulence generator 50J is heated by Joule heat. Thereby, the HC oxidation reaction in the exhaust passage 16 is further promoted.
- switch S turns OFF. As a result, wasteful power consumption is suppressed.
- FIG. 60 shows an example in which a gasket 55 inserted between the exhaust passage 16 (exhaust manifold) and the cylinder head 26 is provided integrally with the turbulence generator 50A.
- FIG. 63 shows a turbulent flow as shown in FIG. 62 between a pair of gaskets 55 inserted between the exhaust passage 16 (exhaust manifold) and the cylinder head 26 as shown in FIG.
- An example is shown in which a plate-like structure 56 provided with a tool 50A is fixed therebetween.
- the turbulence generator 50 can be easily provided in the exhaust passage 16 by sandwiching the plate-like structure 56 provided with the turbulence generator 50A between the two exhaust gaskets 55.
- the material of the gasket 55 and the material of the turbulence generator 50 can be made different from each other. There is an advantage.
- the size of the turbulence generator 50A be such that turbulence can be efficiently generated in the exhaust passage 16.
- the turbulence generation efficiency is calculated using the following equation 5 using the width W of the constituent members of the turbulence generator, the exhaust flow velocity u e in the exhaust passage 16, and the kinematic viscosity coefficient V of the exhaust gas. Is determined by the magnitude of the Reynolds number R e defined by When the Reynolds number defined by Equation 5 exceeds the critical Reynolds number Rec , Karman vortices are generated on the downstream side of the turbulence generator 50, and turbulence ED is promoted.
- the critical Reynolds number Rec is found to be about 100 by various experiments.
- the width W of the component of the turbulence generator 50 for generating the turbulence ED is determined by the following equation (6).
- u e is the average flow velocity of the exhaust gas in the exhaust passage, and is obtained by the following equation 7 in the case of a four-cycle engine.
- V T is the total emissions
- r s is the engine speed per second
- N e is engine revolutions per minute
- n c is the number of all the cylinders
- S Is the part where the turbulence generator 50 is attached This is a cross-sectional area of the exhaust passage 16. Note that in the case of a two-cycle engine, the exhaust flow velocity u e is twice the result of Equation 7.
- the simulation is the result of solving the conservative equations for the mass, momentum, and energy of the mixed gas, the mass conservation equation for the HC, the mass conservation equation for the combustion gas, and the equation of state for the mixed gas, and solving them using the finite volume method.
- the oxidation reaction of HC was modeled by a comprehensive reaction equation, and the oxidation reaction of HC was simulated.
- FIG. 65 is a computer simulation result showing exhaust gas velocity vectors when exhaust gas flows in from the left end and flows out from the right end.
- FIG. 66 is a computer simulation result showing contour lines of the relative concentration distribution of HC immediately before the oxidation reaction of HC starts.
- the relative concentration is represented by a mass concentration ratio when the concentration of HC flowing from the center of the left end is set to 1.
- FIG. 67 is a computer simulation result showing contour lines of the relative concentration distribution of HC after the start of the oxidation reaction of HC.
- the turbulence behind the turbulence generator 50 promotes the mixing of HC and air, and the HC concentration becomes uniform. From the HC concentration distribution after the HC oxidation reaction in Fig. 67, the HC oxidation reaction is promoted by mixing HC and air, and the HC concentration is rapidly reduced in the downstream part.
- Figure 68 shows the results of measurement of HC concentration in the exhaust passage by bench tests using actual engines.
- the engine used for the test was a 4-cylinder direct injection spark ignition engine with a total displacement of 1800 cm 3 .
- test conditions were: engine speed 1400r / min, indicated mean effective pressure 200kPa, air-fuel ratio 16, fuel injection timing 52 ° BTDC, ignition timing 8 ° BTDC, cooling water temperature 20 ° C.
- FIG. 60 A turbulence generator was provided on the gasket inserted between the cylinder head and the exhaust manifold (see Fig. 60). The HC concentration was measured at a position about 50 mm downstream of the exhaust manifold.
- Figure 69 is a longitudinal tomogram of the fuel fog used in the bench test of the direct injection spark ignition engine. The measurement was performed using a laser sheet light to visualize the central cross section of the fuel fog that was injected at a fuel pressure of 7 MPa and an injection pulse width of 1.3 msec in a static nitrogen atmosphere (temperature 20 ° C) pressurized to 0.5 MPa. It was taken with a high-speed camera. The observation period is 2.2 msec after the start of injection. From the results in Fig.
- the HC concentration when the turbulence generator is provided in the exhaust passage is reduced by about 40% compared to the case without the turbulence generator.
- FIG. 70 the correlation between the time interval from fuel injection to ignition and the HC concentration and the smoke concentration will be described with reference to FIGS. 70 and 71.
- FIG. 70 the correlation between the time interval from fuel injection to ignition and the HC concentration and the smoke concentration.
- Fig. 70 shows the correlation of the bench test results of HC concentration with respect to the time interval from the fuel injection start timing to the ignition timing.
- Fig. 71 shows the correlation of the results of the bench test of the smoke concentration with respect to the time interval from the fuel injection start timing to the ignition timing.
- the engine used for the HC concentration and smoke concentration tests shown in FIGS. 70 and 71 is a direct injection type spark ignition engine with a total displacement of 2000 cm 3 , DOHC, and four cylinders.
- the test conditions were an engine speed of 1200 rpm, an indicated mean effective pressure of 250 kPa, an engine cooling water temperature of 40 ° C, a fuel pressure of 9 MPa, and an air-fuel ratio of 15.
- the fuel injection timing is 80 ° BTDC 48 ° B TDC (start of injection) and the ignition timing is 0 ° ATDC-25 ° ATDC. From Figs. 70 and 71, there is a strong correlation between the time interval from the fuel injection start timing to the ignition timing and the HC concentration and smoke concentration, and the longer the time interval from the fuel injection start timing to the ignition timing becomes, the longer the time interval becomes. , HC concentration and smoke concentration tend to decrease.
- the ignition timing is retarded, so that the HC oxidation reaction in the exhaust passage proceeds, and the HC concentration decreases.
- the HC concentration can be reduced to the allowable upper limit or less.
- the smoke concentration can be made to be equal to or less than the allowable upper limit.
- both the HC concentration and the smoke concentration can be set to the allowable upper limit or less.
- the ignition timing is delayed from that in normal operation during warm-up operation when the temperature of the engine is low, etc.
- the turbulence in the exhaust stream containing a large amount of unburned HC, oxygen, and carbon monoxide discharged to the exhaust gas promotes the mixing of HC, oxygen, carbon monoxide, etc.
- the HC is burned in the furnace, and the exhaust gas temperature rises and the HC can be effectively reduced at the same time.
- the exhaust gas purifying catalytic converter can be quickly activated.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Health & Medical Sciences (AREA)
- Toxicology (AREA)
- Theoretical Computer Science (AREA)
- Signal Processing (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Electrical Control Of Ignition Timing (AREA)
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP03818113A EP1662134A1 (en) | 2003-08-15 | 2003-08-15 | Spark ignition engine and method of controlling combustion of the engine |
JP2005507758A JPWO2005017348A1 (ja) | 2003-08-15 | 2003-08-15 | 火花点火機関及びその燃焼制御方法 |
AU2003262235A AU2003262235A1 (en) | 2003-08-15 | 2003-08-15 | Spark ignition engine and method of controlling combustion of the engine |
CNA038268140A CN1802501A (zh) | 2003-08-15 | 2003-08-15 | 火花点火发动机及其燃烧控制方法 |
PCT/JP2003/010374 WO2005017348A1 (ja) | 2003-08-15 | 2003-08-15 | 火花点火機関及びその燃焼制御方法 |
US10/568,184 US7377261B2 (en) | 2003-08-15 | 2003-08-15 | Spark ignition engine and method of controlling combustion of the engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/JP2003/010374 WO2005017348A1 (ja) | 2003-08-15 | 2003-08-15 | 火花点火機関及びその燃焼制御方法 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2005017348A1 true WO2005017348A1 (ja) | 2005-02-24 |
Family
ID=34179390
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2003/010374 WO2005017348A1 (ja) | 2003-08-15 | 2003-08-15 | 火花点火機関及びその燃焼制御方法 |
Country Status (6)
Country | Link |
---|---|
US (1) | US7377261B2 (ja) |
EP (1) | EP1662134A1 (ja) |
JP (1) | JPWO2005017348A1 (ja) |
CN (1) | CN1802501A (ja) |
AU (1) | AU2003262235A1 (ja) |
WO (1) | WO2005017348A1 (ja) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101994628B (zh) * | 2009-08-11 | 2012-03-07 | 廊坊科森电器有限公司 | 汽油发动机点火自动控制方法及*** |
JP2015021390A (ja) * | 2013-07-16 | 2015-02-02 | 富士重工業株式会社 | インジェクタ |
CN113221473A (zh) * | 2020-10-12 | 2021-08-06 | 西北工业大学 | 发动机燃烧室内气体-液滴两相流动特性的数值模拟方法 |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2047079A1 (en) * | 2006-08-04 | 2009-04-15 | Toyota Jidosha Kabushiki Kaisha | Direct injection spark ignition internal combustion engine and fuel injection method for same |
US7658178B2 (en) * | 2007-06-07 | 2010-02-09 | Chrysler Group Llc | Engine event-based correction of engine speed fluctuations |
US9435308B2 (en) | 2011-07-11 | 2016-09-06 | Bosch Corporation | Fuel injection valve, internal combustion engine and fuel injection method |
KR101349522B1 (ko) * | 2012-06-20 | 2014-01-09 | 현대자동차주식회사 | 폐루프 제어 연료분사방법 |
US8935027B2 (en) * | 2012-08-06 | 2015-01-13 | GM Global Technology Operations LLC | Method and apparatus to effect catalyst light-off in a multi-mode powertrain system |
JP6056989B2 (ja) * | 2014-02-03 | 2017-01-11 | マツダ株式会社 | 直噴ガソリンエンジンの制御装置 |
US10570875B2 (en) * | 2016-09-29 | 2020-02-25 | Ford Global Technologies, Llc | Efficiency enhancement to a laser ignition system |
JP6555309B2 (ja) * | 2017-08-25 | 2019-08-07 | マツダ株式会社 | エンジンの燃料噴射装置 |
JP7189683B2 (ja) * | 2018-05-25 | 2022-12-14 | 株式会社Subaru | 内燃機関の吸気装置 |
US10947948B1 (en) | 2020-02-12 | 2021-03-16 | Ford Global Technologies, Llc | Systems and methods for ignition coil multiplexing in a pre-chamber system |
US11156198B1 (en) | 2020-07-02 | 2021-10-26 | Ford Global Technologies, Llc | Systems and methods for ignition coil multiplexing in a pre-chamber system |
US11319861B1 (en) | 2020-10-30 | 2022-05-03 | Ford Global Technologies, Llc | Exhaust conduit with a textured surface |
CN112412550A (zh) * | 2020-12-01 | 2021-02-26 | 沧州华润热电有限公司 | 一种汽轮机的暖机方法及暖机*** |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0783043A (ja) * | 1993-09-20 | 1995-03-28 | Nissan Motor Co Ltd | 排気管の構造 |
JPH07197808A (ja) * | 1993-12-29 | 1995-08-01 | Toyota Motor Corp | 排気ガス浄化用電気加熱式触媒装置 |
JPH081193U (ja) * | 1991-11-11 | 1996-07-30 | 新日本製鐵株式会社 | 排ガス浄化用メタル担体の構造 |
JPH08232645A (ja) * | 1994-12-28 | 1996-09-10 | Mazda Motor Corp | エンジンの排気ガス浄化装置及び排気ガス浄化方法 |
JPH09125944A (ja) * | 1995-11-08 | 1997-05-13 | Toyota Motor Corp | ディーゼル機関の排気浄化方法及び装置 |
JPH11166410A (ja) * | 1997-12-04 | 1999-06-22 | Hino Motors Ltd | 排ガス浄化装置 |
JP2003083128A (ja) * | 2001-09-12 | 2003-03-19 | Nissan Motor Co Ltd | 直噴式火花点火機関の制御装置 |
JP2003193841A (ja) * | 2001-12-25 | 2003-07-09 | Hitachi Ltd | 理論空燃比で成層燃焼するエンジン及び該エンジンの成層燃焼方法 |
JP2003214235A (ja) * | 2002-01-28 | 2003-07-30 | Mazda Motor Corp | 火花点火式直噴エンジンの制御装置 |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BR8706092A (pt) * | 1986-03-07 | 1988-01-19 | Bennett Automotive Technology | Sistema de ignicao a energia laser |
JP2509919B2 (ja) * | 1986-11-20 | 1996-06-26 | ヤマハ発動機株式会社 | 車両用エンジンの点火時期制御方法 |
JP3470392B2 (ja) | 1994-06-16 | 2003-11-25 | 新日本石油株式会社 | 有機性廃水の処理方法および処理装置 |
JP3348659B2 (ja) | 1998-02-13 | 2002-11-20 | 三菱自動車工業株式会社 | 筒内噴射型内燃機関 |
US7185631B2 (en) * | 2004-10-15 | 2007-03-06 | Nissan Motor Co., Ltd. | Combustion control system and method for direct-injection spark-ignition internal combustion engine |
-
2003
- 2003-08-15 EP EP03818113A patent/EP1662134A1/en not_active Withdrawn
- 2003-08-15 US US10/568,184 patent/US7377261B2/en not_active Expired - Fee Related
- 2003-08-15 JP JP2005507758A patent/JPWO2005017348A1/ja active Pending
- 2003-08-15 AU AU2003262235A patent/AU2003262235A1/en not_active Abandoned
- 2003-08-15 CN CNA038268140A patent/CN1802501A/zh active Pending
- 2003-08-15 WO PCT/JP2003/010374 patent/WO2005017348A1/ja active Application Filing
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH081193U (ja) * | 1991-11-11 | 1996-07-30 | 新日本製鐵株式会社 | 排ガス浄化用メタル担体の構造 |
JPH0783043A (ja) * | 1993-09-20 | 1995-03-28 | Nissan Motor Co Ltd | 排気管の構造 |
JPH07197808A (ja) * | 1993-12-29 | 1995-08-01 | Toyota Motor Corp | 排気ガス浄化用電気加熱式触媒装置 |
JPH08232645A (ja) * | 1994-12-28 | 1996-09-10 | Mazda Motor Corp | エンジンの排気ガス浄化装置及び排気ガス浄化方法 |
JPH09125944A (ja) * | 1995-11-08 | 1997-05-13 | Toyota Motor Corp | ディーゼル機関の排気浄化方法及び装置 |
JPH11166410A (ja) * | 1997-12-04 | 1999-06-22 | Hino Motors Ltd | 排ガス浄化装置 |
JP2003083128A (ja) * | 2001-09-12 | 2003-03-19 | Nissan Motor Co Ltd | 直噴式火花点火機関の制御装置 |
JP2003193841A (ja) * | 2001-12-25 | 2003-07-09 | Hitachi Ltd | 理論空燃比で成層燃焼するエンジン及び該エンジンの成層燃焼方法 |
JP2003214235A (ja) * | 2002-01-28 | 2003-07-30 | Mazda Motor Corp | 火花点火式直噴エンジンの制御装置 |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101994628B (zh) * | 2009-08-11 | 2012-03-07 | 廊坊科森电器有限公司 | 汽油发动机点火自动控制方法及*** |
JP2015021390A (ja) * | 2013-07-16 | 2015-02-02 | 富士重工業株式会社 | インジェクタ |
CN113221473A (zh) * | 2020-10-12 | 2021-08-06 | 西北工业大学 | 发动机燃烧室内气体-液滴两相流动特性的数值模拟方法 |
CN113221473B (zh) * | 2020-10-12 | 2022-06-07 | 西北工业大学 | 发动机燃烧室内气体-液滴两相流动特性的数值模拟方法 |
Also Published As
Publication number | Publication date |
---|---|
US20060219216A1 (en) | 2006-10-05 |
EP1662134A1 (en) | 2006-05-31 |
CN1802501A (zh) | 2006-07-12 |
US7377261B2 (en) | 2008-05-27 |
AU2003262235A1 (en) | 2005-03-07 |
JPWO2005017348A1 (ja) | 2006-10-12 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP6699050B2 (ja) | 予燃焼室および2つのスパークプラグを有するガソリン内燃エンジン | |
JP3073118B2 (ja) | 筒内噴射式内燃機関 | |
JP4032690B2 (ja) | 筒内噴射ガソリンエンジン | |
JP2001342836A (ja) | 火花点火式直噴エンジン | |
WO2005017348A1 (ja) | 火花点火機関及びその燃焼制御方法 | |
JP6323683B2 (ja) | エンジンの制御装置 | |
JP6784214B2 (ja) | 内燃機関の制御装置 | |
JP2002206446A (ja) | 内燃機関及び内燃機関の燃料噴射制御装置 | |
JP2001503832A (ja) | 燃料混合物を生成させる方法およびシリンダに対して開放されている予燃焼室内で燃料混合物に点火する方法 | |
JPH08284665A (ja) | エンジンの燃焼制御方法およびその装置 | |
CN107614856B (zh) | 内燃机控制装置以及内燃机控制方法 | |
JP2010150971A (ja) | 火花点火式直噴エンジン | |
CN107429625B (zh) | 直喷发动机的燃料喷射控制装置 | |
EP3770411A1 (en) | Fuel injection control device, and method of controlling injection of fuel | |
EP2522841B1 (en) | Fuel injection control device for internal-combustion engine | |
JP2000008913A (ja) | 火花点火機関の可変混合気濃度分布制御方法 | |
JP4161796B2 (ja) | 筒内噴射式火花点火機関の暖機制御方法 | |
JP2008157197A (ja) | 筒内噴射式火花点火内燃機関 | |
JP6943229B2 (ja) | 予混合圧縮着火式エンジン | |
JP2001271650A (ja) | 火花点火式直噴エンジン | |
JPWO2002020957A1 (ja) | 筒内噴射式火花点火機関 | |
JP3080079B2 (ja) | 筒内噴射式内燃機関の制御装置 | |
JP3269282B2 (ja) | 直噴型火花点火式内燃機関 | |
JP2007077996A (ja) | 内燃機関及び内燃機関の燃料噴射制御装置 | |
JP6965853B2 (ja) | 予混合圧縮着火式エンジン |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WWE | Wipo information: entry into national phase |
Ref document number: 03826814.0 Country of ref document: CN |
|
AK | Designated states |
Kind code of ref document: A1 Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NI NO NZ OM PG PH PL PT RO RU SC SD SE SG SK SL SY TJ TM TN TR TT TZ UA UG US UZ VC VN YU ZA ZM ZW |
|
AL | Designated countries for regional patents |
Kind code of ref document: A1 Designated state(s): GH GM KE LS MW MZ SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LU MC NL PT RO SE SI SK TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG |
|
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: 2005507758 Country of ref document: JP |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2006219216 Country of ref document: US Ref document number: 10568184 Country of ref document: US |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2003818113 Country of ref document: EP |
|
WWP | Wipo information: published in national office |
Ref document number: 2003818113 Country of ref document: EP |
|
WWP | Wipo information: published in national office |
Ref document number: 10568184 Country of ref document: US |