PL3299607T3 - Sposób działania silnika z pilotującą komorą podrzędną w warunkach obciążenia częściowego - Google Patents
Sposób działania silnika z pilotującą komorą podrzędną w warunkach obciążenia częściowegoInfo
- Publication number
- PL3299607T3 PL3299607T3 PL17192456T PL17192456T PL3299607T3 PL 3299607 T3 PL3299607 T3 PL 3299607T3 PL 17192456 T PL17192456 T PL 17192456T PL 17192456 T PL17192456 T PL 17192456T PL 3299607 T3 PL3299607 T3 PL 3299607T3
- Authority
- PL
- Poland
- Prior art keywords
- engine
- operating
- load conditions
- partial load
- pilot subchamber
- Prior art date
Links
Classifications
-
- 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
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/10—Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder
- F02B19/1019—Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder with only one pre-combustion chamber
- F02B19/1023—Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder with only one pre-combustion chamber pre-combustion chamber and cylinder being fed with fuel-air mixture(s)
- F02B19/1071—Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder with only one pre-combustion chamber pre-combustion chamber and cylinder being fed with fuel-air mixture(s) pre-combustion chamber having only one orifice,(i.e. an orifice by means of which it communicates with the cylinder); the intake system comprising two distinct intake conduits
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/22—Rotary-piston machines or engines of internal-axis type with equidirectional movement of co-operating members at the points of engagement, or with one of the co-operating members being stationary, the inner member having more teeth or tooth- equivalents than the outer member
-
- 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
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/10—Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder
- F02B19/1004—Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder details of combustion chamber, e.g. mounting arrangements
- F02B19/1014—Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder details of combustion chamber, e.g. mounting arrangements design parameters, e.g. volume, torch passage cross sectional area, length, orientation, or the like
-
- 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
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/10—Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder
- F02B19/1019—Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder with only one pre-combustion chamber
- F02B19/108—Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder with only one pre-combustion chamber with fuel injection at least into pre-combustion chamber, i.e. injector mounted directly in 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
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/12—Engines characterised by precombustion chambers with positive ignition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
-
- 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
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B53/02—Methods of operating
-
- 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
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B53/10—Fuel supply; Introducing fuel to combustion space
-
- 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
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B53/12—Ignition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/04—Introducing corrections for particular operating conditions
- F02D41/045—Detection of accelerating or decelerating state
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/3094—Controlling fuel injection the fuel injection being effected by at least two different injectors, e.g. one in the intake manifold and one in the 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
- F02D41/30—Controlling fuel injection
- F02D41/38—Controlling fuel injection of the high pressure type
- F02D41/40—Controlling fuel injection of the high pressure type with means for controlling injection timing or duration
- F02D41/402—Multiple injections
- F02D41/403—Multiple injections with pilot injections
-
- 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
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B2053/005—Wankel engines
-
- 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
- F02B2275/32—Miller cycle
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US15/273,788 US10072559B2 (en) | 2016-09-23 | 2016-09-23 | Method of operating an engine having a pilot subchamber at partial load conditions |
EP17192456.6A EP3299607B1 (en) | 2016-09-23 | 2017-09-21 | Method of operating an engine having a pilot subchamber at partial load conditions |
Publications (1)
Publication Number | Publication Date |
---|---|
PL3299607T3 true PL3299607T3 (pl) | 2020-12-14 |
Family
ID=59982269
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL17192456T PL3299607T3 (pl) | 2016-09-23 | 2017-09-21 | Sposób działania silnika z pilotującą komorą podrzędną w warunkach obciążenia częściowego |
Country Status (6)
Country | Link |
---|---|
US (2) | US10072559B2 (pl) |
EP (1) | EP3299607B1 (pl) |
CA (1) | CA2978592A1 (pl) |
ES (1) | ES2797956T3 (pl) |
PL (1) | PL3299607T3 (pl) |
WO (1) | WO2018053622A1 (pl) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9038594B2 (en) | 2011-07-28 | 2015-05-26 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US9528434B1 (en) | 2011-07-28 | 2016-12-27 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US10557407B2 (en) | 2011-07-28 | 2020-02-11 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US10072559B2 (en) * | 2016-09-23 | 2018-09-11 | Pratt & Whitney Canada Corp. | Method of operating an engine having a pilot subchamber at partial load conditions |
US10711729B2 (en) * | 2017-07-19 | 2020-07-14 | Ford Global Technologies, Llc | Diesel engine dual fuel injection strategy |
US11408329B2 (en) * | 2019-12-19 | 2022-08-09 | Board Of Trustees Of Michigan State University | Engine turbulent jet ignition system |
EP4290061A1 (en) * | 2022-06-06 | 2023-12-13 | Volvo Construction Equipment AB | Fuel injection system and method |
Family Cites Families (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4060058A (en) | 1975-11-28 | 1977-11-29 | Ford Motor Company | Internal combustion engine control system |
US4259932A (en) * | 1976-05-26 | 1981-04-07 | Ford Motor Company | Internal combustion engine control system |
DE2841522A1 (de) | 1978-09-23 | 1980-04-03 | Porsche Ag | Gemischverdichtende fremdgezuendete viertakt-brennkraftmaschine mit ladungsschichtung |
US4239023A (en) * | 1978-12-07 | 1980-12-16 | Ford Motor Company | Fuel injection system for dual combustion chamber engine |
FR2460392A1 (fr) | 1979-06-29 | 1981-01-23 | Volzh Ob Proizv | Procede d'amenagement d'un moteur a combustion interne a plusieurs compartiments et pistons rotatifs et dispositif en comportant application |
US4594976A (en) | 1985-03-18 | 1986-06-17 | The Cessna Aircraft Company | Hybrid internal combustion reciprocating engine |
US4765293A (en) * | 1986-05-07 | 1988-08-23 | The Cessna Aircraft Company | Hybrid internal combustion reciprocating engine |
US4831993A (en) * | 1987-12-28 | 1989-05-23 | Erik Kelgard | Method of operating carburetted dual-fuel engines with diesel pilot oil injection |
JPH0237115A (ja) | 1988-07-25 | 1990-02-07 | Mazda Motor Corp | 燃料噴射式エンジン |
US5271357A (en) * | 1992-01-24 | 1993-12-21 | General Electric Company | Method of combustion for dual fuel engine |
DE19621297C1 (de) * | 1996-05-28 | 1997-12-04 | Man B & W Diesel Ag | Einrichtung zur Steuerung/Regelung der Zündöl-Einspritzung eines Gasmotors |
US6202601B1 (en) * | 2000-02-11 | 2001-03-20 | Westport Research Inc. | Method and apparatus for dual fuel injection into an internal combustion engine |
WO2004074655A1 (en) | 2003-02-24 | 2004-09-02 | Pratt & Whitney Canada Corp. | Low volumetric compression ratio integrated turbo-compound rotary engine |
DE102004006294B3 (de) * | 2004-02-09 | 2005-10-13 | Siemens Ag | Verfahren zur Gleichstellung der Einspritzmengenunterschiede zwischen den Zylindern einer Brennkraftmaschine |
US7243862B2 (en) * | 2004-04-07 | 2007-07-17 | Delphi Technologies, Inc. | Apparatus and method for mode-switching fuel injector nozzle |
DE102004023409B4 (de) * | 2004-05-12 | 2007-05-16 | Gottfried Schubert | Hochverdichtender Ottoverbrennungsmotor mit Drosselregelung, Fremdzündung und Kraftstoffdirekteinspritzung in eine Vorbrennkammer |
US7484405B2 (en) * | 2007-04-26 | 2009-02-03 | Gm Global Technology Operations, Inc. | System and method for engine sound calibration |
JP4315218B2 (ja) * | 2007-06-12 | 2009-08-19 | トヨタ自動車株式会社 | 燃料噴射制御装置 |
US7753036B2 (en) | 2007-07-02 | 2010-07-13 | United Technologies Corporation | Compound cycle rotary engine |
JP4404111B2 (ja) * | 2007-07-19 | 2010-01-27 | トヨタ自動車株式会社 | 内燃機関の燃料噴射制御装置 |
DE102008000552A1 (de) * | 2008-03-07 | 2009-09-10 | Robert Bosch Gmbh | Verfahren zum Betreiben eines selbstzündenden Verbrennungsmotors und entsprechende Steuervorrichtung |
US20120191325A1 (en) * | 2010-01-13 | 2012-07-26 | GM Global Technology Operations LLC | Injection fuel and load balancing control system |
JP5730679B2 (ja) | 2011-06-16 | 2015-06-10 | ヤンマー株式会社 | エンジン装置 |
US9038594B2 (en) | 2011-07-28 | 2015-05-26 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US10557407B2 (en) * | 2011-07-28 | 2020-02-11 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
CA2798599C (en) * | 2012-12-14 | 2013-11-12 | Westport Power Inc. | Skip-fire fuel injection system and method |
US9255543B2 (en) * | 2012-12-14 | 2016-02-09 | Hyundai Motor Company | Fuel injection amount compensating method |
US10280830B2 (en) | 2013-03-08 | 2019-05-07 | Pratt & Whitney Canada Corp. | System for pilot subchamber temperature control |
US9200563B2 (en) | 2013-03-12 | 2015-12-01 | Pratt & Whitney Canada Corp. | Internal combustion engine with common rail pilot and main injection |
KR20180017181A (ko) | 2015-06-17 | 2018-02-20 | 바르실라 핀랜드 오이 | 멀티-실린더 피스톤 엔진을 작동시키기 위한 방법 및 피스톤 엔진 |
US10041402B2 (en) * | 2016-05-12 | 2018-08-07 | Pratt & Whitney Canada Corp. | Internal combustion engine with split pilot injection |
US10072559B2 (en) * | 2016-09-23 | 2018-09-11 | Pratt & Whitney Canada Corp. | Method of operating an engine having a pilot subchamber at partial load conditions |
-
2016
- 2016-09-23 US US15/273,788 patent/US10072559B2/en active Active
-
2017
- 2017-09-06 CA CA2978592A patent/CA2978592A1/en active Pending
- 2017-09-07 WO PCT/CA2017/051049 patent/WO2018053622A1/en active Application Filing
- 2017-09-21 ES ES17192456T patent/ES2797956T3/es active Active
- 2017-09-21 PL PL17192456T patent/PL3299607T3/pl unknown
- 2017-09-21 EP EP17192456.6A patent/EP3299607B1/en active Active
-
2018
- 2018-08-10 US US16/100,611 patent/US10533486B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
WO2018053622A1 (en) | 2018-03-29 |
US20180347450A1 (en) | 2018-12-06 |
US20180087446A1 (en) | 2018-03-29 |
CA2978592A1 (en) | 2018-03-23 |
US10533486B2 (en) | 2020-01-14 |
EP3299607A1 (en) | 2018-03-28 |
EP3299607B1 (en) | 2020-04-15 |
ES2797956T3 (es) | 2020-12-04 |
US10072559B2 (en) | 2018-09-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
PL3299607T3 (pl) | Sposób działania silnika z pilotującą komorą podrzędną w warunkach obciążenia częściowego | |
PL3456939T3 (pl) | Sposób obsługi zespołu silnika | |
SG10201602096YA (en) | Core arrangement for turbine engine component | |
GB201407314D0 (en) | Control of a gas turbine engine | |
GB201502881D0 (en) | A method of controlling the stopping starting of an engine | |
GB201703067D0 (en) | Method for improving aircraft engine operating efficiency | |
GB2541435B (en) | A method of reducing NOx emissions from an engine | |
GB201512900D0 (en) | Gas turbine engine | |
PL3257753T3 (pl) | Przekładnia redukcyjna do silnika lotniczego | |
GB2544554B (en) | Gas turbine engine | |
GB201520623D0 (en) | Gas turbine engine | |
GB201502091D0 (en) | Method of controlling a cooling circuit of an internal combustion engine | |
GB201617374D0 (en) | Gas turbine engine | |
HK1252907A1 (zh) | 用於利用內燃機的運行實施的方法 | |
GB201601427D0 (en) | Setting control for gas turbine engine component(s) | |
GB2544553B (en) | Gas Turbine Engine | |
GB201514984D0 (en) | A method of operating an engine | |
GB201810685D0 (en) | Gas turbine engine | |
ZA201804249B (en) | A multi-fuel engine and method of controlling the same | |
SG10201603741QA (en) | Core assembly for gas turbine engine | |
GB201608234D0 (en) | Gas turbine engine | |
GB201512494D0 (en) | Gas turbine engine | |
GB2557271B (en) | A method of operating an engine assembly | |
GB201514401D0 (en) | A method of operating an internal combustion engine | |
GB201417211D0 (en) | A method of operating an internal combustion emgine |