WO2008071188A1 - A fuel injector for an internal combustion engine - Google Patents

A fuel injector for an internal combustion engine Download PDF

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Publication number
WO2008071188A1
WO2008071188A1 PCT/DK2006/050078 DK2006050078W WO2008071188A1 WO 2008071188 A1 WO2008071188 A1 WO 2008071188A1 DK 2006050078 W DK2006050078 W DK 2006050078W WO 2008071188 A1 WO2008071188 A1 WO 2008071188A1
Authority
WO
WIPO (PCT)
Prior art keywords
atomizer
cut
central bore
nozzle bores
fuel
Prior art date
Application number
PCT/DK2006/050078
Other languages
English (en)
French (fr)
Inventor
Johannes Flarup
Original Assignee
Man Diesel, Filial Af Man Diesel Se, Tyskland
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Man Diesel, Filial Af Man Diesel Se, Tyskland filed Critical Man Diesel, Filial Af Man Diesel Se, Tyskland
Priority to KR1020097012103A priority Critical patent/KR101043745B1/ko
Priority to JP2009540599A priority patent/JP5249943B2/ja
Priority to CN2006800566145A priority patent/CN101558231B/zh
Priority to PCT/DK2006/050078 priority patent/WO2008071188A1/en
Publication of WO2008071188A1 publication Critical patent/WO2008071188A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/042The valves being provided with fuel passages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M53/00Fuel-injection apparatus characterised by having heating, cooling or thermally-insulating means
    • F02M53/04Injectors with heating, cooling, or thermally-insulating means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1806Injection 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
    • F02M61/182Discharge orifices being situated in different transversal planes with respect to valve member direction of movement
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/06Fuel-injection apparatus having means for preventing coking, e.g. of fuel injector discharge orifices or valve needles

Definitions

  • the present invention relates to a fuel injector for an internal combustion engine, comprising at least a housing, a valve seat, a valve spindle, an atomizer, and a cut-off element; which atomizer has a central bore from which a plurality of nozzle bores extend through a side wall of the atomizer; which valve spindle has a valve element and is dis- placeable between a closed position, in which the valve element abuts the valve seat, and an open position, in which fuel is admitted past the valve seat and to the nozzle bores; which cut-off element is carried by a shaft on the valve spindle and comprises a first cylindrical section located in the central bore of the atomizer to close fuel access to inlet openings of a first group of nozzle bores, when the valve spindle is in the closed position.
  • JP3027191B2 corresponding to KR253673B describes a fuel injector for an internal combustion engine, comprising a displaceable valve spindle for opening and closing a flow passage to nozzle bores in a central bore of an atomizer.
  • the valve spindle has a foremost section with a cut-off element carried by a shaft and fitting in the central bore of the atomizer.
  • the cut-off element covers the inlet openings of the nozzle bore in the central bore.
  • the cut-off element exposes the inlet openings of the nozzle bores and fuel is supplied to the nozzle bores through one or more axial passages through the cut-off element.
  • WO 99/53196 corresponding to JP3308551B2 and CN1093226C describes a similar fuel injection device for internal combustion engines, especially two-stroke diesel engines, comprising an atomized protruding into an associated combustion chamber.
  • the conditions for fuel admission are approximately the same for all nozzle bores resulting in a stable jet.
  • Admission chambers depart from the central bore in the atomizer and are located at least at a part of the nozzle bores.
  • the diameter of the chambers is greater than the diameter of the nozzle bores.
  • the admission chambers are designed in such a way that at least similar length ratios exist for all nozzle bores in the row of nozzle bores.
  • the fuel is supplied to the nozzle bores via an internal flow passage in the cut-off element.
  • the fuel is consequently flowing inside the lower part of the shaft and forward through the cut-off element and out through the free end where the fuel cools the forward end of the central bore in the nozzle and thus cools the nozzle tip.
  • the fuel flows from the end of the central bore and towards the inlet openings to the nozzle bores.
  • the fuel injector according to the present invention is characterized in that, in the open position of the valve spindle, fuel is supplied to at least a second group of the nozzle bores through a passage between the circumference of the cut-off element and the central bore of the atomizer, and in that the cut-off element has a second cylindrical section for closing off inlet openings of the second group of nozzle bores from the fuel volume present in the central bore in between the second cylindrical section and the valve seat, when the valve spindle is in the closed position.
  • the flow of fuel through the internal flow passage in the cut-off element provides - as just mentioned in the above description - an important cooling effect to the nozzle tip.
  • the fuel flowing from the end of the central bore and towards the inlet openings to the nozzle bores has already been warmed by heat from the tip area at the point in time when the fuel is flowing out through the nozzle bores, and the cooling effect at the area of the nozzle bores is smaller because of this warming.
  • the cooling effect on the nozzle wall from the flow of fuel inside the cut-off element and in the shaft bore leading to the cut-off element is quite small.
  • the present invention provides an important cooling effect in the nozzle wall portion located on level with the cut-off element.
  • Dividing the fuel flow to the inlet openings into two different pathways results in a better cooling effect in the atomizer, also because fuel is flowing on a larger internal area of the atomizer than the atomizer bores.
  • the outside of the cut-off element is also cooled by the flow of fuel into the passage and this reduces the temperature level in the first cylindrical section.
  • the resulting lower temperatures on the inside of the central bore reduce the risk of carbon formation on the parts, and consequently also the risk of sticking of the cut-off element is reduced.
  • the increased cooling effect is obtained without sacrificing the advantages of the cut-off element in relation to avoiding fuel leaks through the nozzle bores when the fuel injector is closed, because the second cylindrical section prevent fuel from seeping into the nozzle bores when the fuel injector is closed.
  • nozzle bores in said first group have inlet openings arranged in a first row in the central bore of the atomizer; and the nozzle bores in said second group have inlet openings arranged in a second row in the central bore of the atomizer, which first and second rows are spaced apart in the axial direction of the atomizer.
  • the total number of nozzle bores arranged within a maximum angle of e.g. 120 degrees may be increased without compromising the strength of the side wall of the atomizer.
  • fuel in the open position of the valve spindle, fuel is supplied to the first row of the inlet openings of the nozzle bores through at least one internal passage of the cut-off element and to the second row of the inlet openings of the nozzle bores through an annular recess in the circumference of the cut-off element.
  • the recess in the cir- cumference is also separating the periphery of the cut-off element form the inside of the central bore when the fuel valve is in the closed position, and this separation in the closed position results in even less risk of carbon formation in the atomizer.
  • fuel in the open position of the valve spindle, fuel is supplied to the annular recess in the circumference of the cut-off element through a first section of the central bore of the atomizer having larger diameter than a second section of the central bore comprising both rows of the inlet openings of the nozzle bores.
  • the cooling effect may be further improved, because the larger diameter provides a larger internal area of the atomizer, and then the fuel flows across a larger surface area and provides a higher cooling effect. Consequently, the risk of carbon formation is further reduced.
  • the first cylindrical section and the second cylindrical section of the cut-off element have equal outer diameter, and the first and second cylindrical sections fit sealingly into the second section of the central bore.
  • the annular recess in the circumference of the cut-off element covers the first and second rows of the inlet openings of the nozzle bores.
  • the axial dimension of the annular recess may be long compared to the total axial dimension of the cut-off element, whereby a good cooling effect may be obtained by fuel flowing in the annular recess, thereby further reducing the risk of carbon formation.
  • an axial bore extends through the first and second sections of the cut-off element and opens out at a free end of the first section, and said bore communicates with the central bore of the atomizer through side openings in the shaft.
  • the first row of the inlet openings of the nozzle bores is located at a distance in the axial direction of the atomizer from a shoulder between the first and second sections of the central bore of the atomizer, said distance equalling the distance from the second cylindrical section of the cut-off element to the free end of the first cylindrical section of the cut-off element.
  • the nozzle bores are arranged in pairs of mutually parallel bores belonging to either row and having inlet openings at the same angular position of the central bore of the atomizer. This increases the strength of the nozzle for a given total number of nozzle bores.
  • the cut-off element in the open position of the valve spindle, seals against the central bore between the first and the second rows of the inlet openings of the nozzle bores.
  • the inlet openings of the nozzle bores in the first and the second row, respectively are arranged at the same axial position of the atomizer, and in that the nozzle bores of a row are directed in different angles in relation to the axial direction of the atom- izer.
  • Fig. 1 is a longitudinal sectional view of an embodiment of a fuel injector according to the present invention
  • Figs. 2 and 3 are enlarged views of the forward end of the fuel injector in closed position and in open position, respectively, Fig. 4 is an even more enlarged view of the forward end of an atomizer,
  • Figs. 5a-5e are sectional views along centre axes of pairs of nozzle bores
  • Fig. 5f is a cross-sectional view through the atomizer
  • Fig. 6 is an illustration of fuel injection into an engine cylinder provided with three fuel injectors.
  • Fig. 1 illustrates a fuel injector, generally designated 1, for injection of fuel, particularly heavy fuel oil.
  • the fuel injector has a housing 2 of elongate shape and provided with an upper flange 3 for mounting fuel injector 1 onto the cylinder of the internal combustion engine and a connection 4 for a fuel supply pipe, not shown, supplying pressurized fuel from e. g. a fuel pump or a high-pressure reservoir.
  • the engine is typically a two-stroke crosshead engine for ship propulsion or for stationary power production to a grid.
  • the engine can have a power per cylinder in the range from e.g. 150 kW to 7000 kW, and typically the individual cylinder is provided with several, such as two, three or four, fuel injectors.
  • An atomizer 5 projects through a forward end opening of the housing and extends into the combustion chamber of the engine cylinder, when fuel injector 1 is mounted on the engine.
  • Fuel delivered to the fuel injector can flow through a central bore 6 in connection 4 and a central channel 7 extending from bore 6 through a spring guide 8 and a circulation slider 9 to a pressure chamber 10 defined by circulation slider 9 and a guide 11 for the circulation slider.
  • circulation slider 9 When circulation slider 9 is in its forward position illustrated in Fig. 1, a forward end of circulation slider 9 closes a passage 12 leading to a channel 13 extending centrally through a pressure pipe 14, a pressure member 15 and an upper section 30 of a valve spindle generally designated 16.
  • central channel 13 communicates with a primary pressure chamber 18 through inclined channels 17.
  • the primary pressure chamber 18 is defined by upper section 30 of valve spindle 16, and a spindle guide 19 for upper section 30.
  • Valve spindle 16 has a valve element 20 with an annular valve seat area which abut a valve seat 21 when the valve spindle is in the closed position illustrated in Figs. 1 and 2. In this closed position there is no flow connection between primary pressure chamber 18 and a central bore 22 in the atomizer 5.
  • a compression spring 23 abuts a spring disc 24 and presses forwards in the closing direction on the upper section 30 of valve spindle 16 via a lower spring disc 25 so that valve element 20 is pressed sealingly against valve seat 21.
  • the upper bore 6 communicates with the cavity located around spring guide 8 through a transverse channel (not shown) in spring guide 8 so that preheated fuel can circulate in the upper part of the valve 1 in a well- known manner.
  • the fuel pressure in central channel 7 and the pressure chamber 10 rises, making the circulation slider 9 move upwards and cut off the transverse channel in spring guide 8.
  • the displacement of circulation slider 9 opens the passage 12, and the fuel pressure propagates through channel 13 and the inclined channels 17 to the primary pressure chamber 18.
  • valve spindle When the fuel pressure in primary pressure chamber 18 reaches the opening pressure of the fuel injector, determined by the pre- tensioning of spring 23, the valve spindle is displaced upwards and away from valve seat 21, and the fuel begins to flow past the valve seat 21 and down into the central bore 22 in atomizer 5.
  • FIG. 2 illustrates an embodiment where the tubular part of pressure member 15 extends into the upper section 30 to a position near inclined channels 17.
  • Valve spindle 16 continues on the forward side of valve element 20 in a shaft 26 extending into the central bore of the atomizer.
  • Shaft 26 is elongate and carries at the foremost end a cut-off element generally designated 27.
  • the cut-off element has a first cylindrical section 28 and a second cylindrical section 29, which cylindrical sections 28, 29 have a cylindrical outer surface fitting into the central bore of the atomizer in a fluid-sealing manner when the valve spindle is in the closed position.
  • a plurality of nozzle bores 31 is provided in the wall of the atomizer.
  • the nozzle bores are arranged with their inlet openings 32 in a first group and in a second group.
  • the inlet openings of the two groups can be arranged in an irregular pattern when viewed in the circumferential direction of the nozzle, or they can be arranged generally on a row or on several rows, or they can as illustrated on the drawings be arranged in a first row A and a second row B.
  • the first cylindrical section 28 When the valve spindle is in closed position the first cylindrical section 28 is positioned at the first row A of inlet openings 32 and extends into the end portion of the central bore 22 located between the first row A of inlet openings and the end bottom 33 of the central bore so that the first cylindrical section cuts off the flow connection between this end portion of the central bore and the first row A of inlet openings.
  • the valve spindle When the valve spindle is displaced away from the valve seat to the open position the first cylindrical section 28 is lifted free of the first row A of inlet openings, as illustrated in Figs. 3 and 4.
  • a second partial flow C of fuel continues to flow forward on the outside of shaft 26 into a passage 36 between the circumference of second cylindrical section 29 and the side wall of central bore 22.
  • the pas- sage extends forward past cylindrical section 29 and into the area in between the first cylindrical section 28 and the second cylindrical section 29.
  • a central flow passage 34 extends centrally through the cut-off element to side openings 35 in the shaft.
  • the central flow passage can be embodied as a single axial bore extending from the free end of the cut-off element to the side openings 35 in the shaft, or it can alternatively be embodied as several passages extending in the shaft from the free end of the cut-off element to side openings 35.
  • the central bore 22 of the atomizer has a first section 22' with a larger diameter than a second section 22" of the central bore.
  • the two rows A and B are both located in the second section 22" in the embodiments illustrated in Figs. 2 to 4.
  • the second section 22" has a diameter only slightly larger than the outer diameter of the first and second cylindrical sections 28, 29 so that the second section functions as a guide for the cut-off element and the first and second cylindrical sections 28, 29 fit into the second section 22" in a manner preventing fluid flow.
  • the cooling effect of the fluid flowing through recess 36 acts over the complete surface of the recess and not just in the angular sector where the nozzle bores are located.
  • the highest heat input to the atomizer is located in the area opposite the angular sector where the nozzle bores are located. And this heavily heat affected zone is not cooled at all from nozzle bores because no nozzle bores are located in the zone. This will be more clearly explained in the below description relating to Fig. 6.
  • the second cylindrical section 29 is displaced in direction towards the end bottom 33 of the central bore so that at least the forward portion of the second cylindrical section is located in the second section 22" and cuts off the flow connection between the first section 22' of the central bore 22 and the recess 36 with the second row B of inlet openings.
  • Figs. 2 and 3 the combustion chamber in the engine cylinder is denoted 37, and a combustion chamber wall surface 38 is illustrated in broken line.
  • the fuel injector housing 2 is located in a low temperature area cooled by the cylinder wall cooling, and the valve seat in side the housing is also located in this low temperature area.
  • the free end of the atomizer 5 extending beyond combustion chamber wall surface 38 into the combustion chamber is located in a highly heat affected area.
  • the nozzle bores 31 are oriented in different directions in order to produce the desired injection process. The different directions are relating to both the so-called horizontal direction, viz. an angular range of distributing fuel in the circumferential direction of the engine cylinder, and to the so-called vertical direction, viz. an angular range of distribut- ing the fuel in the height direction of the cylinder.
  • Fig. 5a to 5e illustrate an example of different vertical inclinations angles ⁇ of the nozzle bores.
  • the vertical inclinations angle ⁇ indicated is measured as the angle between the longitudinal axis of the nozzle bore and the horizontal direc- tion (perpendicular to the central axis of the cylindrical bore).
  • the vertical inclination angle can be different from one nozzle bore to another.
  • the nozzle bores indicated in Fig. 5a can have an angle ⁇ of 30°
  • the nozzle bores indicated in Fig. 5b can have an angle ⁇ of 20°
  • the nozzle bores indicated in Fig. 5c can have an angle ⁇ of 40°
  • the nozzle bores indicated in Fig. 5e can have an angle ⁇ of 30°.
  • the nozzle bores are arranged in pairs of mutually parallel bores belonging to either row. The consequence of this is that in each pair of nozzle bores located vertically above one another the nozzle bores are mutually parallel.
  • the nozzle bores are all located in an an- gular sector covering only a minor portion of the circumferential direction of the injector.
  • the reason for this is illustrated in Fig. 6 showing a cylinder viewed from the above.
  • the cylinder is provided with three fuel injectors 1 located close to the periphery of the engine cylinder.
  • the individual fuel injector only injects fuel in a sector directed to the next fuel injector.
  • the hot combustion zone from the combustion of fuel injected from the previous injector acts on the atomizer in the area located in direction of the previous injector.
  • the angular sector can be defined by the maximum horizontal angle ⁇ between the two nozzle bores extending in directions deviating the most from one another. This horizontal angle ⁇ is normally less than 120°, and preferably less than 100°.
  • the fuel injector need not be of a type having a compression spring 23.
  • the movements of the valve spindle between the open and the closed positions can be controlled hydraulically by the fuel pressure or by the use of control oil in a known manner. If the fuel is not heavy fuel oil the circulation slider 9 can be dispensed with.
  • the central bore of the atomizer can have a uniform inner diameter along its entire length, and the inlet openings 32 can be arranged in a non-row pattern, such as evenly distributed over a cylindrical area of the central bore, or distributed in V- shape or another convenient non-linear shape.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
PCT/DK2006/050078 2006-12-15 2006-12-15 A fuel injector for an internal combustion engine WO2008071188A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
KR1020097012103A KR101043745B1 (ko) 2006-12-15 2006-12-15 내연기관용 연료분사기
JP2009540599A JP5249943B2 (ja) 2006-12-15 2006-12-15 内燃機関のための燃料噴射器
CN2006800566145A CN101558231B (zh) 2006-12-15 2006-12-15 内燃机用的燃料喷射器
PCT/DK2006/050078 WO2008071188A1 (en) 2006-12-15 2006-12-15 A fuel injector for an internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/DK2006/050078 WO2008071188A1 (en) 2006-12-15 2006-12-15 A fuel injector for an internal combustion engine

Publications (1)

Publication Number Publication Date
WO2008071188A1 true WO2008071188A1 (en) 2008-06-19

Family

ID=38512503

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DK2006/050078 WO2008071188A1 (en) 2006-12-15 2006-12-15 A fuel injector for an internal combustion engine

Country Status (4)

Country Link
JP (1) JP5249943B2 (zh)
KR (1) KR101043745B1 (zh)
CN (1) CN101558231B (zh)
WO (1) WO2008071188A1 (zh)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101852157A (zh) * 2009-03-30 2010-10-06 瓦特西拉瑞士有限公司 用于内燃机的燃料喷射器
EP2543870A1 (en) * 2011-06-27 2013-01-09 MAN Diesel & Turbo, filal af MAN Diesel & Turbo SE, Tyskland A fuel valve for large turbocharged two stroke diesel engines
DE102013001098B3 (de) * 2013-01-23 2014-07-03 L'orange Gmbh Kraftstoffinjektor
EP2900947A4 (en) * 2012-09-25 2016-02-24 Hans Jensen Lubricators As INJECTION NOZZLE FOR INJECTING LUBRICATING OIL IN MOTOR CYLINDER AND USE THEREOF

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DK2386745T3 (da) * 2010-05-11 2013-03-04 Waertsilae Switzerland Ltd Brændstofindsprøjtningsindretning til motorer med indvendig forbrænding
DE102012208075A1 (de) * 2012-05-15 2013-11-21 Man Diesel & Turbo Se Injektor für eine Kraftstoffversorgungsanlage einer Brennkraftmaschine sowie Kraftstoffversorgungsanlage
JP5955258B2 (ja) 2013-03-29 2016-07-20 三菱重工業株式会社 燃料噴射装置及びディーゼル機関
KR101638815B1 (ko) * 2016-01-07 2016-07-25 한빛정공(주) 4 행정용 인젝션 밸브
CN106438148A (zh) * 2016-11-28 2017-02-22 哈尔滨工程大学 一种用于反作动式喷气阀的气体喷嘴
DE102018215891A1 (de) * 2018-09-19 2020-03-19 Robert Bosch Gmbh Vorrichtung zum Dosieren eines gasförmigen und eines flüssigen Kraftstoffs und ein Verfahren zum Betreiben dieser Vorrichtung

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GB610873A (en) * 1945-11-14 1948-10-21 Saurer Ag Adolph Improvements in and relating to injection nozzles for internal combustion engines
WO1993007386A1 (en) * 1991-10-04 1993-04-15 Man B&W Diesel A/S A fuel injector for internal combustion engines
WO1999053196A1 (de) * 1998-04-09 1999-10-21 Man B & W Diesel A/S Brennstoffeinspritzvorrichtung
EP1380750A1 (en) * 1999-06-25 2004-01-14 Delphi Technologies, Inc. Fuel injector
US6691935B1 (en) * 2000-02-07 2004-02-17 Robert Bosch Gmbh Injection nozzle

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JPH05321789A (ja) * 1992-05-15 1993-12-07 Kubota Corp ディーゼルエンジンの多孔ノズル形燃料噴射弁
JP2002357129A (ja) * 2001-05-30 2002-12-13 Toyota Motor Corp 内燃機関の燃料噴射装置

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB610873A (en) * 1945-11-14 1948-10-21 Saurer Ag Adolph Improvements in and relating to injection nozzles for internal combustion engines
WO1993007386A1 (en) * 1991-10-04 1993-04-15 Man B&W Diesel A/S A fuel injector for internal combustion engines
WO1999053196A1 (de) * 1998-04-09 1999-10-21 Man B & W Diesel A/S Brennstoffeinspritzvorrichtung
EP1380750A1 (en) * 1999-06-25 2004-01-14 Delphi Technologies, Inc. Fuel injector
US6691935B1 (en) * 2000-02-07 2004-02-17 Robert Bosch Gmbh Injection nozzle

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101852157A (zh) * 2009-03-30 2010-10-06 瓦特西拉瑞士有限公司 用于内燃机的燃料喷射器
KR20100109501A (ko) * 2009-03-30 2010-10-08 바르질라 스위츠랜드 리미티드 내연기관용 연료 주입기
KR101686671B1 (ko) * 2009-03-30 2016-12-14 바르질라 스위츠랜드 리미티드 내연기관용 연료 주입기
EP2543870A1 (en) * 2011-06-27 2013-01-09 MAN Diesel & Turbo, filal af MAN Diesel & Turbo SE, Tyskland A fuel valve for large turbocharged two stroke diesel engines
EP2900947A4 (en) * 2012-09-25 2016-02-24 Hans Jensen Lubricators As INJECTION NOZZLE FOR INJECTING LUBRICATING OIL IN MOTOR CYLINDER AND USE THEREOF
US9850868B2 (en) 2012-09-25 2017-12-26 Hans Jensen Lubricators A/S Injection nozzle for injecting lubricating oil in engine cylinders and use thereof
DE102013001098B3 (de) * 2013-01-23 2014-07-03 L'orange Gmbh Kraftstoffinjektor

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CN101558231B (zh) 2012-01-04
JP5249943B2 (ja) 2013-07-31
KR20090077858A (ko) 2009-07-15
CN101558231A (zh) 2009-10-14
KR101043745B1 (ko) 2011-06-22
JP2010512484A (ja) 2010-04-22

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