WO2007089203A1 - A two stroke combustion engine with liquid injection - Google Patents
A two stroke combustion engine with liquid injection Download PDFInfo
- Publication number
- WO2007089203A1 WO2007089203A1 PCT/SE2007/050049 SE2007050049W WO2007089203A1 WO 2007089203 A1 WO2007089203 A1 WO 2007089203A1 SE 2007050049 W SE2007050049 W SE 2007050049W WO 2007089203 A1 WO2007089203 A1 WO 2007089203A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- combustion chamber
- liquid
- introduction
- air
- injection
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 112
- 239000007788 liquid Substances 0.000 title claims abstract description 67
- 238000002347 injection Methods 0.000 title claims abstract description 42
- 239000007924 injection Substances 0.000 title claims abstract description 42
- 239000007789 gas Substances 0.000 claims abstract description 36
- 230000006835 compression Effects 0.000 claims abstract description 33
- 238000007906 compression Methods 0.000 claims abstract description 33
- 239000000446 fuel Substances 0.000 claims abstract description 24
- 238000000034 method Methods 0.000 claims description 29
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 8
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 claims description 6
- 239000007921 spray Substances 0.000 claims description 3
- 125000003158 alcohol group Chemical group 0.000 claims 1
- 239000012530 fluid Substances 0.000 description 7
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 6
- 239000000567 combustion gas Substances 0.000 description 5
- 238000001704 evaporation Methods 0.000 description 5
- 230000008020 evaporation Effects 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 238000004590 computer program Methods 0.000 description 2
- 230000001276 controlling effect Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000004913 activation Effects 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000002283 diesel fuel Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000004071 soot Substances 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D13/00—Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing
- F02D13/02—Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing during engine operation
- F02D13/0203—Variable control of intake and exhaust valves
- F02D13/0215—Variable control of intake and exhaust valves changing the valve timing only
-
- 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
- F02B47/00—Methods of operating engines involving adding non-fuel substances or anti-knock agents to combustion air, fuel, or fuel-air mixtures of engines
- F02B47/02—Methods of operating engines involving adding non-fuel substances or anti-knock agents to combustion air, fuel, or fuel-air mixtures of engines the substances being water or steam
-
- 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
- F02B47/00—Methods of operating engines involving adding non-fuel substances or anti-knock agents to combustion air, fuel, or fuel-air mixtures of engines
- F02B47/04—Methods of operating engines involving adding non-fuel substances or anti-knock agents to combustion air, fuel, or fuel-air mixtures of engines the substances being other than water or steam only
-
- 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
- F02M25/00—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
- F02M25/022—Adding fuel and water emulsion, water or steam
- F02M25/0227—Control aspects; Arrangement of sensors; Diagnostics; Actuators
-
- 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
- F02M25/00—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
- F02M25/022—Adding fuel and water emulsion, water or steam
- F02M25/025—Adding water
- F02M25/03—Adding water into the cylinder or the 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
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
-
- 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
Definitions
- the present invention relates to a method for the operation of a combustion engine that operates in accordance with the two stroke principle, comprising alternating power strokes and compression strokes, wherein the combustion engine comprises at least one cylinder and a piston that reciprocates in said cylinder, and a combustion chamber delimited by said cylinder and the piston, and at least one inlet for an introduction of combustion air into the combustion chamber, and at least one outlet for the discharge of exhaust gases from the combustion chamber.
- the invention also relates to a combustion engine that operates according to the two stroke principle, said principle comprising alternating power strokes and compression strokes, wherein the combustion engine comprises at least one cylinder and a piston that reciprocates in said cylinder, and a combustion chamber delimited by said cylinder and said piston, and at least one inlet for the introduction of combustion air into the combustion chamber, and at least one outlet for the discharge of exhaust gases from the combustion chamber.
- the inlet and/ or the outlet is, preferably, provided with a freely operable valve, but could, as an alternative, comprise a port which is opened and closed by the passing piston, said port being provided in the cylinder wall, preferably in the area of the lower dead centre of the piston.
- the freely operable valves are, preferably, controlled by a computer-based control system that, for example, may form part of an existing control system used for the control of the ignition and injection of fuel, water, water steam, etc. into the combustion chamber.
- the piston reciprocates between two end positions, an upper and a lower end position respectively.
- the motion of the piston from the upper end position to the lower end position is defined as a power stroke
- the motion of the piston from the lower end position to the upper end position is defined as a compression stroke.
- the discharge of exhaust gases is assumed to start and end simultaneously with the opening and the closure respectively of the corresponding valve or valves.
- the inlet of air is assumed to start and end simultaneously with the opening and clo- sure respectively of the corresponding valve or valves.
- the same assumption is made for the introduction of said liquid, which may be performed through a separate valve or a separate nozzle.
- HCCI Homogeneous Charge Compression Ignition
- the object of the present invention in connection with two stroke operation of the kind initially described, and in particular HCCI, is to provide a relative lowering of the temperature and the pressure in the combustion chamber in order to permit the introduction of a larger amount of oxidation fluid, for example air, into the combustion chamber and/ or in order to inhibit a too early ignition, and in order to enable a decrease in the amount of NOx of the exhaust gases after combustion.
- a larger amount of oxidation fluid for example air
- the object of the invention is achieved by means of the initially defined method, characterized in that, before or during one and the same compression stroke, a liquid other than fuel is injected into the combustion chamber in connection with the ending of a discharge of exhaust gases out of the combustion chamber and before the start of the introduction of air into the combustion chamber.
- the liquid is of such a kind that it will fully or partly evaporate under the pressure and at the temperature that exists in the combustion chamber during the injection moment.
- the amount of liquid, the temperature of the liquid or the composition thereof may be regulated.
- the liquid is to a major part comprised by- water.
- the invention defines a certain sequence by which at least the beginning of the discharge of exhaust gases precedes the beginning of the introduction of fresh air.
- a high pressure will exist in the combustion chamber when the piston reaches its lower dead centre, and at this stage exhaust gases will be able to leave through the outlet valve, which, preferably, is provided in the cylinder head.
- the liquid is injected.
- the temperature, and thereby the pressure, in the combustion chamber will decrease. Thanks to the lowering of the temperature, a larger amount of fresh air of a given pressure can be introduced during the subsequent step. Accordingly, a more efficient gas exchange is achieved.
- the liquid is assumed to be injected during the compression stroke but not during that part thereof during which the very compression takes place, which is exactly what prior art suggests. However, one of the dependent claims in the present invention specifies this possibility, however only as a supplement to this first injection.
- the heat in the remaining combustion gases will provide for a momentary evaporation of the liquid and a simultaneous cooling of the combustion gases, resulting in a lowering of the pressure.
- a larger mass of air can be introduced.
- the mean temperature of the gases in the combustion chamber can be controlled to a requested level.
- this is, in particular, an advantage during HCCI. If, for example, the liquid contains water, an evaporation of water is achieved.
- An advantage of such an evaporation and a subsequent cooling is the reduction of the formation of nitrogen oxides, NOx, during the combustion.
- the steam has the same effect as EGR, Exhaust Gas Recirculation, which is a common method of decreasing the generation of NOx.
- Preferred embodiments of the invention include the start of the injection of the liquid being begun within 20 crank angle degrees, preferably 10 crank angle degrees, and preferably 5 crank angle degrees from the moment when the discharge of exhaust gases out of the combustion chamber is ended.
- the injection of the liquid is initiated after, preferably immediately after, or even at the same moment as the discharge of ex- haust gases out of the combustion chamber is ended.
- the technical effect of the injection will thereby be the best.
- the injection of the liquid might begin during the time when there is still a discharge of exhaust gases. This may, in particular at high rotational speeds, be preferred in order to obtain a maximum technical effect.
- the time period between the closure of the outlet valve and the opening of the inlet valve will be shorter, and even negative, i.e. there will be an overlap between inlet and discharge, which might make it necessary to let the injection of the liquid overlap either the discharge of exhaust gases or the introduction of air or both. It might even be conceived to let the closure of the outlet valve occur after the closure of the inlet valve.
- the method is characterized in that the introduction of the air into the combustion chamber is initiated while the injection of the liquid is still going on. It is preferred that the injection of the liquid into the combustion chamber is ended before the introduction of air into the combustion chamber is ended. At the very latest, the injection of the liquid into the combustion chamber should be ended simultaneously with the ending of the introduction of the air into the combustion chamber.
- the introduction of a fuel to the combustion chamber may take place simultaneously with the injection of said liquid, and an introduction of a fuel to the combustion chamber may be done through the same valve as the one through which said liquid is injected.
- said liquid is injected together with an alcohol.
- the alcohol will thereby form at least a part of the fuel that is to be combusted during the power stroke that follows the compression stroke.
- a fuel is introduced into the combustion chamber simultaneously with the introduction of the air.
- this is the case during HCCI. It is also possible that the fuel be introduced separately at a later stage of the compression stroke.
- a second injection of a liquid other than fuel is performed during the compression stroke, when the introduction of the air to the combustion chamber has ended.
- This liquid may be of the same type or of another type than the previously injected liquid, and is likewise supposed to be evaporated and to lower the temperature and the pressure in the combustion chamber in order to reduce the remaining compression work, and thereby to improve the efficiency.
- the latter preferably comprises water.
- the liquid Before the liquid is introduced into the compression chamber it is pressurized and heated to such a degree that at least a part of the droplets of the spray will explode spontaneously upon entrance into the compression chamber.
- the object of the invention is also achieved with a combustion chamber as initially defined, characterized in that it comprises means to, before or during one and the same compression stroke, inject a liquid other than fuel into the combustion chamber, and a control unit with a software arranged so as to open the valve in order to, before or during one and the same compression stroke, inject said liquid in connection to the ending of a discharge of exhaust gases out of the combustion chamber and before the introduction of air into the combustion chamber is started.
- Said means may comprise a valve for the injection of said fuel, said valve then preferably being an operable valve, for example a pneumatically, hydraulically or electromagnetically operated valve.
- said means may comprise a control unit, with a software arranged so as to control the opening and closure of said valve in accordance with the suggested, inventive method.
- the inlet and outlet valves are so called operable valves, that is valves that are not mechanically connected to the crank shaft, but freely operable regardless of the crank shaft position.
- operable valves are referred to as valves to the combustion chamber of an engine cylinder, said valves being opened and closed through, for example, the action of a pressurized fluid, upon basis on signals from a computer-based, preferably electronic, control system.
- Fig. 1 is a schematic representation of a part of a combustion engine according to the invention
- Fig. 2 is a representation of a time schedule for the steps of an embodiment of the inventive method.
- Fig. 3 is a representation of a time schedule of the steps of a further embodiment of the inventive method.
- Fig. 1 schematically shows a part of a combustion engine according to the invention.
- the combustion engine is arranged to propel a vehicle, such as a car, a bus or a lorry. It comprises a cylinder 1 , a piston 2 provided to move reciprocatingly in the latter, a combustion chamber 3 delimited by the cylinder and the piston, an inlet valve 4, an outlet valve 5 and a valve or a nozzle 6 for the injection of a liquid other than fuel.
- the nozzle 6 may be used in order to, besides injecting said liquid, also inject at least a part of a fuel, such as an alcohol, such as ethanol.
- An exhaust gas system or the like may be connected to the outlet at which the outlet valve 5 is arranged.
- the piston 2 is under motion during a compression stroke in a two-stroke cycle, and air, possibly together with fuel, is flowing into the combustion chamber through the open inlet valve 3.
- the outlet valve 4 has just, when the piston 2 was in its lower dead centre position, opened, but is now closed.
- a circuit 7 is used for the operation of actuators to the valves 4 and 5 and the nozzle 6.
- a control unit 8 is operatively connected to the circuit 7 in order to provide for signal control of the circuit 7 and the valves 4 and 5 and the nozzle 6 connected to said circuit.
- the circuit 7 may comprise electric components and a pressure fluid circuit, preferably a pneumatic pressure fluid circuit.
- a pressure fluid circuit preferably a pneumatic pressure fluid circuit.
- it may comprise pilot valves, not shown, that are driven by electromagnets, for the purpose of controlling the flow of a pressure fluid, such as air, to actuator chambers, not shown, in order to operate actuator pistons arranged therein, by means of which the inlet valves 4 and the inlet valves 5 are driven.
- the control unit 8 decides when the operable valves 4 and 5 are to open or close and when the nozzle 6 is to open for the injection of said fluid.
- the evacuation of combustion gases a, the injection of a liquid other than fuel b and the introduction of air and fuel c may, according to the invention, take place in the following way:
- the outlet valve 5 is opened for the evacuation of combustion gases that, as a pulse, will flow out of the combustion chamber 3 as a result of the pressure there being substantially higher than in an exhaust gas system or an exhaust gas pipe connected to said outlet.
- the pressure in the combustion chamber 3 will be lower than in the air supply channel connected to the inlet.
- the pressure in the combustion chamber 3 is at its minimum, and, in a preferred embodiment, the outlet valve 5 should thereby be closed to stop the evacuation, and, shortly thereafter, the inlet valve 4 should be opened for the supply of air.
- a time period could, preferably, be permitted between the closure of the outlet valve 5 and the opening of the inlet valve 4, as shown in the embodiment of fig. 2.
- the nozzle 6 is activated for the injection of a liquid, preferably water, into the combustion chamber 3.
- a liquid preferably water
- the amount and composition, and temperature of the liquid should be adopted in order to let at least a major part of the liquid be evaporated immediately upon entrance into the combustion chamber 3, preferably during the above- mentioned time period between the closure of the outlet valve 5 and the opening of the inlet valve 4.
- a relative further lowering of the pressure will be achieved in the combustion chamber 3 in comparison to the case in which no liquid would have been injected.
- a precondition for the supply of a relatively larger amount of air of a given pressure has thereby been generated.
- the pressure reaches its maximum when the flow of air into the combustion chamber 3 automatically ends, and, in accordance with a preferred embodiment, the inlet valve 4 should be closed in as close connection with this moment as possible.
- the injection may continue also when the inlet valve 4 is kept open, and may even continue until the inlet valve 4 is closed.
- fig. 2 shows an embodiment in which the injection of the liquid is ended just before or simultaneously with the inlet valve being opened for the supply of air. It should be mentioned that, during increasing rotational speed, and for reasons discussed above, the previously mentioned time period may decrease and even cease and become substituted by an overlap of the discharge of the exhaust gases and the introduction of air, wherein the injection of said liquid may overlap said discharge as well as said introduction.
- the outlet valve 5 is opened at its earliest 90 crank angle degrees before the lower dead centre and closed at the latest 90 crank angle degrees after the lower dead centre.
- the inlet valve 4 should, under all circumstances, be opened after the opening of the outlet valve 5, but may be closed already before the closure of the outlet valve. There are 180 crank angle degrees between the lower dead centre and upper dead centre.
- Fig. 3 shows an alternative embodiment of the method according to invention, which is within the scope of the invention, such as described above.
- the outlet valve is opened at approximately -45 crank angle degrees, that is 45 degrees before the lower dead centre of the piston 2, and is closed approximately at 0 crank angle degrees.
- the inlet valve 4 is opened at -10 crank angle degrees and is closed at 35 crank angle degrees.
- the nozzle 6 is opened at -20 crank angle degrees, that is before the opening of the inlet valve 4, and is closed at 10 crank angle degrees, that is within the time period during which the inlet valve 4 is still open. Accordingly, fig. 3 shows one of many possible cases of overlapping of the method steps that are conceived according to the invention.
- Contemporary freely operable valve openers are electro-mechanically, hydraulically or pneumatically activated.
- Pneumatically activated valves may, for a given movable mass which is not larger than necessary for the relevant function, and with a lower consumption of energy, reach a certain lift height faster than the other methods of activation.
- the time passing between the opening of a valve, with said movable mass, to a certain lift height, and the closure thereof may, with pneumatically activated valves, be substantially shorter than the corresponding one for the other of said methods.
- the invention also relates to a computer program product stored on a readable computer program medium, for the implementation of the method according to the invention on a combustion engine according to the invention.
- the invention is not delimited to constant two-stroke operation but may comprise embodiments wherein two-stroke operation is alternated with four-stroke operation or in which strokes without any combustion take the place of the ordinary power strokes. Accordingly, the invention is assumed to be implemented during the part of the operation which comprises two-stroke operation, or at least during a part thereof.
- one and the same cylinder 2 may be provided with a plurality of inlet valves 4 and a plurality of outlet valves 5, as well as a plurality of nozzles 6 for the injection of liquid, wherein, preferably, the outlet valves and/ or the inlet valves are provided in the cylinder head.
- the valves advantageously, are operated by means of pressure fluid and freely operable, there is a possibility of individual control of the valves, and, for example, one of two outlet valves may open before and close before or after the other valve of said pair of valves. In such a case, the discharge of exhaust gases starts at the first moment at which any of the outlet valves is opened and it continuous to the last closure of any one of said outlet valves. This is also relevant for the inlet valves and for the injection nozzles if there is a plurality thereof.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2008553208A JP2009525431A (en) | 2006-01-31 | 2007-01-31 | Two-stroke combustion engine using liquid injection |
EP07709442A EP1984610A1 (en) | 2006-01-31 | 2007-01-31 | A two stroke combustion engine with liquid injection |
US12/162,005 US20090241895A1 (en) | 2006-01-31 | 2007-01-31 | Two stroke combustion engine with liquid injection |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0600198A SE529569C2 (en) | 2006-01-31 | 2006-01-31 | Two stroke internal combustion engine with liquid injection |
SE0600198-6 | 2006-01-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2007089203A1 true WO2007089203A1 (en) | 2007-08-09 |
Family
ID=38327686
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/SE2007/050049 WO2007089203A1 (en) | 2006-01-31 | 2007-01-31 | A two stroke combustion engine with liquid injection |
Country Status (8)
Country | Link |
---|---|
US (1) | US20090241895A1 (en) |
EP (1) | EP1984610A1 (en) |
JP (1) | JP2009525431A (en) |
KR (1) | KR20080092974A (en) |
CN (1) | CN101375038A (en) |
RU (1) | RU2008129123A (en) |
SE (1) | SE529569C2 (en) |
WO (1) | WO2007089203A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ITBO20090315A1 (en) * | 2009-05-15 | 2010-11-16 | Ponti Motors S R L | METHOD FOR THE SUPPLY OF A BURST ENGINE |
ITGE20100034A1 (en) * | 2010-04-13 | 2011-10-14 | Novatech Di Elisa Prandi | FULL RAIN: METHOD FOR THERMO-BARIC MOTOR CONTROL OF INTERNAL COMBUSTION OF THERMAL THINNER INJECTION. |
WO2016018184A1 (en) * | 2014-07-26 | 2016-02-04 | Ase Alternative Solar Energy Engine Ab | Method at a 2-stroke engine, and a 2-stroke engine operating according to said method |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103498720A (en) * | 2012-09-20 | 2014-01-08 | 摩尔动力(北京)技术股份有限公司 | Pressure range liquid cooled engine |
JP6011477B2 (en) * | 2013-06-28 | 2016-10-19 | 三菱自動車工業株式会社 | Engine control device |
CN103982331B (en) * | 2014-04-23 | 2016-06-08 | 镇江市博林光电科技有限公司 | Compression knock jet engine |
KR101893639B1 (en) | 2016-01-05 | 2018-10-04 | 신기식 | Loessal water including mineral elements |
SE541454C2 (en) * | 2017-10-16 | 2019-10-08 | Hedman Ericsson Patent Ab | Procedure for two-stroke engine, and two-stroke engine operating according to the procedure |
GB201717438D0 (en) * | 2017-10-24 | 2017-12-06 | Rolls Royce Plc | Apparatus amd methods for controlling reciprocating internal combustion engines |
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GB191011483A (en) * | 1909-05-15 | 1910-11-17 | Ernst Fredrik Nydahl | Improvements in Means for Admitting Water to the Combustion Chambers of Explosion Engines. |
EP0653558A1 (en) * | 1993-11-12 | 1995-05-17 | New Sulzer Diesel AG | Process and engine for reducing the nitrous oxide content of exhaust gas of a two stroke internal combustion Diesel engine |
EP0967371A1 (en) * | 1998-06-26 | 1999-12-29 | Wärtsilä NSD Schweiz AG | Two-stroke diesel engine |
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GB2082677B (en) * | 1980-08-27 | 1984-04-26 | Dal David John Van | Injection of fluid eg water into ic engines |
US4322950A (en) * | 1980-09-22 | 1982-04-06 | Jepsen Marshall P | Combined internal combustion and steam engine |
US5148776A (en) * | 1991-09-23 | 1992-09-22 | Connor Michael J | Coordinated water and fuel injection system |
US5875743A (en) * | 1997-07-28 | 1999-03-02 | Southwest Research Institute | Apparatus and method for reducing emissions in a dual combustion mode diesel engine |
US5832880A (en) * | 1997-07-28 | 1998-11-10 | Southwest Research Institute | Apparatus and method for controlling homogeneous charge compression ignition combustion in diesel engines |
JP3861479B2 (en) * | 1998-01-21 | 2006-12-20 | 三菱ふそうトラック・バス株式会社 | Water injection amount control device for fuel / water injection engines |
US6032617A (en) * | 1998-05-27 | 2000-03-07 | Caterpillar Inc. | Dual fuel engine which ignites a homogeneous mixture of gaseous fuel, air, and pilot fuel |
EP1099846B1 (en) * | 1999-11-10 | 2005-01-12 | Wärtsilä Schweiz AG | Method for operating a four stroke diesel engine |
US6443104B1 (en) * | 2000-12-15 | 2002-09-03 | Southwest Research Institute | Engine and method for controlling homogenous charge compression ignition combustion in a diesel engine |
US6505579B1 (en) * | 2001-09-25 | 2003-01-14 | Te-Fa Lee | System and process for water injection control of internal combustion engine |
SE524223C2 (en) * | 2001-10-04 | 2004-07-13 | Cargine Engineering Ab | Method for control of internal combustion engine with expansion rate and internal combustion engine |
JP4472932B2 (en) * | 2003-02-07 | 2010-06-02 | いすゞ自動車株式会社 | Engine combustion control device |
-
2006
- 2006-01-31 SE SE0600198A patent/SE529569C2/en not_active IP Right Cessation
-
2007
- 2007-01-31 US US12/162,005 patent/US20090241895A1/en not_active Abandoned
- 2007-01-31 KR KR1020087021103A patent/KR20080092974A/en not_active Application Discontinuation
- 2007-01-31 WO PCT/SE2007/050049 patent/WO2007089203A1/en active Application Filing
- 2007-01-31 JP JP2008553208A patent/JP2009525431A/en active Pending
- 2007-01-31 CN CNA2007800038971A patent/CN101375038A/en active Pending
- 2007-01-31 RU RU2008129123/06A patent/RU2008129123A/en unknown
- 2007-01-31 EP EP07709442A patent/EP1984610A1/en not_active Withdrawn
Patent Citations (3)
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GB191011483A (en) * | 1909-05-15 | 1910-11-17 | Ernst Fredrik Nydahl | Improvements in Means for Admitting Water to the Combustion Chambers of Explosion Engines. |
EP0653558A1 (en) * | 1993-11-12 | 1995-05-17 | New Sulzer Diesel AG | Process and engine for reducing the nitrous oxide content of exhaust gas of a two stroke internal combustion Diesel engine |
EP0967371A1 (en) * | 1998-06-26 | 1999-12-29 | Wärtsilä NSD Schweiz AG | Two-stroke diesel engine |
Cited By (4)
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ITBO20090315A1 (en) * | 2009-05-15 | 2010-11-16 | Ponti Motors S R L | METHOD FOR THE SUPPLY OF A BURST ENGINE |
WO2010131225A1 (en) * | 2009-05-15 | 2010-11-18 | Ponti Motors S.R.L. | A method for supplying an internal combustion engine |
ITGE20100034A1 (en) * | 2010-04-13 | 2011-10-14 | Novatech Di Elisa Prandi | FULL RAIN: METHOD FOR THERMO-BARIC MOTOR CONTROL OF INTERNAL COMBUSTION OF THERMAL THINNER INJECTION. |
WO2016018184A1 (en) * | 2014-07-26 | 2016-02-04 | Ase Alternative Solar Energy Engine Ab | Method at a 2-stroke engine, and a 2-stroke engine operating according to said method |
Also Published As
Publication number | Publication date |
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JP2009525431A (en) | 2009-07-09 |
SE0600198L (en) | 2007-08-01 |
US20090241895A1 (en) | 2009-10-01 |
SE529569C2 (en) | 2007-09-18 |
KR20080092974A (en) | 2008-10-16 |
CN101375038A (en) | 2009-02-25 |
EP1984610A1 (en) | 2008-10-29 |
RU2008129123A (en) | 2010-03-10 |
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