EP1566539A1 - Brennstoffeinspritzdüse - Google Patents
Brennstoffeinspritzdüse Download PDFInfo
- Publication number
- EP1566539A1 EP1566539A1 EP05405036A EP05405036A EP1566539A1 EP 1566539 A1 EP1566539 A1 EP 1566539A1 EP 05405036 A EP05405036 A EP 05405036A EP 05405036 A EP05405036 A EP 05405036A EP 1566539 A1 EP1566539 A1 EP 1566539A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- nozzle
- longitudinal bore
- fuel
- valve seat
- head
- Prior art date
- Legal status (The legal status 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 status listed.)
- Granted
Links
Images
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
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/14—Arrangements of injectors with respect to engines; Mounting of injectors
-
- 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
-
- 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
Definitions
- the invention relates to a fuel injector for a Internal combustion engine, in particular a large diesel engine, according to the Generic term of the independent claim of the respective category.
- the nozzle head is a Verschleissteil that a high subject to thermal, mechanical and chemical stress collective.
- the mechanical loads are based, inter alia, on the high Injection pressure, which can be over a thousand bar.
- the thermal Burdens are caused by the high temperatures in the combustion chamber and the enormous temperature change between combustion temperature and Temperature causes the freshly supplied scavenging air while the chemical stress mainly in high temperature or Hot corrosion are justified.
- valve seat is usually slightly removed from the nozzle holes arranged so that an excessive admission with Heat of combustion is avoided.
- valve seat and nozzle holes brings the following problem with it.
- When stopping the fuel injection is Press the nozzle needle into the valve seat so that the fuel that flows downstream of the valve seat - between valve seat and nozzle holes - is no longer supplied with the feed pressure.
- This im Nozzle head remaining fuel can to some extent after Completion of injection through the nozzle holes badly atomized in the Combustor reach where it burns little or no. this leads to an additional pollution of the exhaust gas specifically smoke that means particles, and possibly deposits of unburned Fuel at all parts of the combustion chamber and the exhaust gas Components.
- a fuel injector for a Internal combustion engine in particular for a large diesel engine proposed, with a nozzle body and one with the nozzle body connected nozzle head, with one inside the nozzle body arranged nozzle needle whose end with a valve seat so cooperates, that the nozzle needle in an open position a passage releases the fuel at the valve seat and in a closed position the Closing passage, with a longitudinal bore extending from the valve seat extending the nozzle head, and having a flow diameter, and at least one nozzle hole, which from the longitudinal bore goes out and through which the fuel into a combustion chamber of Internal combustion engine can be introduced.
- the ratio of the length of the Longitudinal bore and the flow diameter of the longitudinal bore amounts at least 17, preferably at least 20 and more preferably more as 22.
- all the nozzle holes form together a total flow diameter for the fuel wherein the Flow diameter of the longitudinal bore at most 2 times, preferably at least 0.5 times and at most 1.5 times, of Total flow diameter of all nozzle holes amounts.
- the longitudinal bore in the region of the nozzle holes a Expand to.
- This local extension has two advantages. At given Number of nozzle holes can be the distance between each Junctions of the nozzle holes in the longitudinal bore chosen larger , whereby the mechanical pressure caused by the internal pressure Voltage peaks are reduced in the material of the nozzle head. moreover Local expansion facilitates the redirecting of the fuel flow the longitudinal hole in the nozzle holes, causing the hydraulic Friction losses are reduced when flowing into the nozzle holes.
- the extension may be asymmetrical with respect to Form longitudinal axis of the longitudinal bore. This is manufacturing technology easier to realize.
- the wall thickness of the nozzle head in the Area in which the nozzle holes are provided, made thinner be as in the area that has no nozzle holes. This has the Advantage that the nozzle holes will not be too long, causing too strong Bundling of the fuel jet is avoided.
- the advantageous asymmetry may also or additionally be generated thereby be that the longitudinal bore obliquely to the longitudinal axis of the nozzle head runs.
- each nozzle hole opens at an angle of more than 90 ° in the longitudinal bore, that is in the installed state run the Nozzle holes from the longitudinal bore obliquely downwards.
- the nozzle head is usually a wear part, such Embodiments of the fuel injector preferred in which the Nozzle head is detachably connected to the nozzle body.
- the fuel injection nozzle according to the invention is particularly suitable for Diesel engines, in particular for two-stroke large diesel engines.
- FIG. 1 shows in a longitudinal section for the understanding of the invention essential parts of an embodiment of an inventive Fuel injection nozzle, the entire with the reference numeral 1 provided is.
- the fuel injection nozzle 1 is shown in FIG. 1 installed in the cylinder head 10 of a two-stroke large diesel engine, For example, a marine engine, shown. In the assembled state protrudes the illustration according to the lower end of the fuel injector 1 in a Combustion chamber 20 of a cylinder of the diesel engine.
- the fuel injection nozzle 1 includes a nozzle body 2 and a Embodiment of a nozzle head 3, with the nozzle body. 2 connected is.
- the Connection by means of a holding sleeve 4, which at its lower end to Longitudinal axis A of the fuel injector 1 tapers.
- the longitudinal axis A is at the same time also the longitudinal axis A of the nozzle head 3.
- the retaining sleeve 4 is by means of a union nut 5 and an elastic element 45, for Example of a snap ring, attached to the nozzle body 2.
- the nozzle head 3 is supported in the tapered part of the retaining sleeve 4.
- the nozzle head 3 has a longitudinal bore 32 and in the region of his lower end at least one nozzle hole 31, typically z. For example, five Nozzle holes 31 extending from the longitudinal bore 32 and through which the fuel can escape into the combustion chamber 20.
- Fig. 2 shows a view of the lower part of the nozzle head 3, in which the Arrangement of the five nozzle holes 31 can be seen.
- the nozzle holes 31 extend from the longitudinal bore 32 downwardly inclined in the direction Combustion chamber 20, that is, each nozzle hole 31 opens at an angle ⁇ (Fig. 1) of more than 90 ° in the longitudinal bore 32 a.
- a pressure chamber 6 is provided, in which a feed line 12 opens for the fuel.
- the pressure chamber 6 is in Axial direction bounded by a valve seat 8.
- a nozzle needle 7 is arranged, which is substantially in Direction of the longitudinal axis A extends and with the valve seat. 8 interacts.
- the lower Tip of the nozzle needle 7 is pressed into the valve seat 8, so that the passage from the pressure chamber 6 in the downstream subsequent Longitudinal bore 32 is closed.
- the nozzle needle 7 is known per se Way spring loaded by means of a compression spring, not shown, and against biased the valve seat 8.
- the volume between the valve seat 8 and the nozzle holes 31 becomes commonly referred to as a blind hole.
- the longitudinal bore 32 is in the embodiment described here as configured in a substantially cylindrical bore, extending in the direction of Longitudinal axis A extends.
- the diameter D of the longitudinal bore 32 lays a flow diameter and thus a flow cross section, with what is available for the flow of the fuel Cross-sectional area in the longitudinal bore 32 is meant.
- the Longitudinal bore is not cylindrical but with changing Diameter, for example, conical, so is the flow cross-section or diameter of the longitudinal bore their minimum flow cross-section or diameter meant.
- the individual nozzle holes 31 are also in each case as a cylindrical bore designed. Their diameter b (Fig. 2) defines one each Flow cross section for the respective nozzle hole 31 fixed.
- the diameters b of the individual nozzle holes 31 can from nozzle hole to nozzle hole be different, or the diameter b may be for some or all Nozzle holes 31 be the same.
- the through the individual nozzle holes 31 each fixed flow cross-sections add up to a Total flow cross section of the nozzle holes. With the Total flow cross section of the nozzle holes 31 is thus the sum of Flow cross sections of all nozzle holes - here five - meant, so the entire flow cross-section, which is the fuel for the exit from the Longitudinal bore 32 in the combustion chamber 20 is available. The same applies to the total flow diameter of the nozzle holes 31
- the fuel injector 1 or the nozzle head 3 is so configured such that the ratio of the length L of the longitudinal bore 32 and the flow diameter of the longitudinal bore at least 17, preferably at least 20, and more preferably more than 22.
- the blind hole that is, the volume can be downstream of the valve seat 8 and upstream of the nozzle holes 31 in Compared to known designs by, for example, over 50% to reduce.
- This has the consequence that after completion of the injection process, when the nozzle needle 7 is again pressed sealingly into the valve seat 8, there is substantially less fuel downstream of the valve seat 8, because the blind hole is much smaller.
- the harmful emissions caused by fuel from the blind hole Termination of the injection process are caused in the combustion chamber and in the exhaust gas leading components are significantly reduced.
- the ratios given length L to flow diameter of Longitudinal bore 32 of at least 17, preferably at least 20 and more preferably more than 22 lead to a favorable reduction of Volume of the blind hole without the other hand, the hydrodynamic Properties significantly deteriorated or the pressure drop across the Nozzle head 3 becomes too big.
- the length L of the longitudinal bore for example, about 48.1 mm with a diameter of about 2.1 mm or about 70.7 mm with a diameter of about 2.9 mm.
- the nozzle head 3 is designed so that the Flow diameter of the longitudinal bore 32 at most twice the Total flow diameter of the nozzle holes 31 is.
- the Strömungs diemesserder Longitudinal bore 32 at least 0.5 times and at most 1.5 times of the total flow diameter of the nozzle holes 31 is.
- the fuel injector 1 operates as follows. Of the Fuel is introduced through the supply line 12 into the pressure chamber 6. To start the injection, for example via a valve Connection between a common rail pressure accumulator for the fuel and the pressure chamber 6 is opened or the fuel is from a Injection pump conveyed into the pressure chamber 6. There acts on the Fuel the nozzle needle 7 and do not lift it against the bias illustrated compression spring from the valve seat 8, so that the passage in the Nozzle head 3 is opened. The fuel flows through the longitudinal bore 32nd and is injected into the combustion chamber 20 through the nozzle holes 31.
- the pressure in the pressure chamber 6 by stopping the fuel extraction or by closing the connection with the Common rail accumulator reduces, so that the nozzle needle 7 through the Compressed spring is pressed back into the valve seat 8 and the passage for the Fuel closes. Due to the greatly reduced volume of the blind hole then passes clearly after closing the passage at the valve seat less fuel into the combustion chamber 20.
- the small diameter D of the Longitudinal bore 32 is realized, or the reduced blind hole volume is the Increases friction between the fuel and the wall of the bore. This is equivalent to a greater pressure drop or pressure loss, which is caused by the nozzle head 3.
- the friction caused by the Pressure drop in the inventive nozzle head 3 can well 50 - 100 bar be. In modern large diesel engines, which follow the common rail principle work and be completely electronically controlled, this one can friction-induced pressure drop can be easily compensated by the fuel pressure in the common rail pressure accumulator accordingly is increased. Thus, especially in the lower speed range ensures that for the actual injection of the fuel through the Nozzle holes 31 still sufficient pressure - for example, 500-700 bar - is present to a proper injection into the combustion chamber 20 to guarantee.
- the cross section of the nozzle holes 31 can be increased become. Furthermore, it is advantageous to the transition region between the Longitudinal bore 32 and the nozzle hole 31 each rounded off, whereby a stronger rounding allows easier inflow of the Fuel from the longitudinal bore 32 in the nozzle hole 31 and thus a Reduction of the flow resistance can be achieved.
- FIGS. 3 and 4 illustrated second embodiment of an inventive Nozzle head. Same or functionally equivalent parts are in the drawing figures each denoted by identical reference numerals.
- FIG. 3 shows a section through the second embodiment and FIG. 4 an enlarged view of the lower area of the nozzle head 3.
- FIG. 3 and FIG. 4 show the longitudinal bore 32 in this Embodiment in the region of the nozzle holes 31 an extension 321st on.
- five nozzle holes 31 provided analogous to the representation in FIG. 2.
- extension 321 can be the inflow of the fuel from the Longitudinal bore 32 facilitate the nozzle holes 31 and thus the Reduce drag because it's easier that Fuel flow from the larger cross section of the extension 321 to deflect out into the nozzle holes. Hydraulic friction at Inflow into the nozzle holes 31 is thus reduced.
- the extension also has an additional advantage.
- Given number of nozzle holes 31 of given diameter and given Rounding off at the junction may be the distance between the individual junctions of the nozzle holes 31 in the longitudinal bore 32nd be designed larger. This greater distance has the advantage of being of the Internal pressure caused mechanical stress peaks in the material of the Shrink nozzle head.
- extension 321 form asymmetrically with respect to the longitudinal axis of the longitudinal bore 32, as can be seen in particular in Fig. 4.
- the longitudinal axis of the Longitudinal bore 31 is identical in this embodiment with the Longitudinal axis A of the nozzle head 3 and the longitudinal axis of the Fuel injection nozzle 1.
- the longitudinal axis C of the extension 321 extends parallel but offset to the longitudinal axis A, so that the extension 321 asymmetrical or eccentric with respect to the longitudinal bore 32 is located.
- This measure has the advantage that by the comparatively small diameter D of the longitudinal bore 32 caused larger wall thickness of the nozzle head 3 through the extension 321 on the combustion chamber 20th facing side, ie where the nozzle holes 31 are provided, can be reduced.
- a large wall thickness can indeed under the aspect the mechanical resilience, but it also requires that the nozzle holes 31 each become longer.
- This can be disadvantageous affect, because too large a length of the nozzle holes to a strong Bundling of the fuel jet flowing through it can lead to what is can negatively affect the injection process. That can be explained by the Extension 321 avoid, because the wall thickness of the nozzle head 3 on the the combustion chamber 20 side facing smaller, and thus the Nozzle holes 31 become shorter.
- the asymmetrical design the extension 321 easier to manufacture.
- FIG. 5 A similar effect can be with the third shown in Fig. 5 Achieve embodiment of a nozzle head according to the invention.
- the longitudinal bore 32 extends obliquely to the Longitudinal axis A of the nozzle head.
- a ' designated longitudinal axis of the longitudinal bore 32 at one of zero different angles ⁇ to the longitudinal axis A of the nozzle head.
- the passage at the valve seat 8 in the open position of the Nozzle needle has an area that is at least as large as the Flow cross-section of the longitudinal bore 31. That is, in the open position the nozzle needle 7 is the flow cross-section between the nozzle needle and Valve seat 8 equal to or greater than the flow cross section of Longitudinal bore 32. Since the flow cross section of the longitudinal bore 32nd in turn larger than the total flow area of all nozzle holes 31, the flow cross-section takes downstream of the pressure chamber 6 in the Open position of the nozzle needle 7 no longer. This means one thing Reducing the flow rate of the fuel through a Enlargement of the flow cross-section would cause is excluded. This is advantageous in the fuel injector because Here a recovery of kinetic energy by extension of the Flow cross-section (diffuser effect) is inefficient.
- the production of the nozzle head for the inventive Fuel injector can with all known per se Machining methods take place.
- the production of the Longitudinal bore 32, the nozzle holes 31, the rounding and, where appropriate Extension 321 can be made by drilling and / or electrochemical Processing methods, eg. B. Elysieren done.
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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)
- Feeding And Controlling Fuel (AREA)
Abstract
Description
- Fig. 1:
- die wesentlichen Teile eines Ausführungsbeispiels einer erfindungsgemässen Brennstoffeinspritzdüse mit einem Ausführungsbeispiel eines erfindungsgemässen Düsenkopfs,
- Fig. 2:
- eine Ansicht auf den unteren Teil des Düsenkopfs,
- Fig. 3:
- den Düsenkopf eines zweiten Ausführungsbeispiels,
- "Fig. 4:
- eine grössere Darstellung des unteren Bereichs des Düsenkopfs aus Fig. 3, und
- Fig. 5:
- den Düsenkopf eines dritten Ausführungsbeispiels.
Claims (10)
- Brennstoffeinspritzdüse für eine Brennkraftmaschine, insbesondere für einen Grossdieselmotor mit einem Düsenkörper (2) und einem mit dem Düsenkörper (2) verbundenen Düsenkopf (3), mit einer im Innern des Düsenkörpers (2) angeordneten Düsennadel (7), deren Ende mit einem Ventilsitz (8) derart zusammenwirkt, dass die Düsennadel (7) in einer Offenstellung einen Durchlass für den Brennstoff am Ventilsitz (8) freigibt und in einer Schliessstellung den Durchlass verschliesst, mit einer Längsbohrung (32), die sich vom Ventilsitz (8) durch den Düsenkopf (3) erstreckt, und die einen Strömungsdurchmesser aufweist, sowie mit mindestens einem Düsenloch (31), welches von der Längsbohrung (32) ausgeht und durch welches der Brennstoff in einen Brennraum (20) der Brennkraftmaschine einbringbar ist, dadurch gekennzeichnet, dass das Verhältnis aus der Länge (L) der Längsbohrung (32) und dem Strömungsdurchmesser der Längsbohrung (32) mindestens 17, vorzugsweise mindestens 20 und besonders bevorzugt mehr als 22 beträgt.
- Brennstoffeinspritzdüse nach Anspruch 1, bei welcher alle Düsenlöcher (31) zusammen einen Gesamtströmungsdurchmesser für den Brennstoff bilden, wobei der Strömungsdurchmesser der Längsbohrung (32) höchstens das 2-fache, vorzugsweise mindestens das 0.5-fache und höchstens das 1.5-fache, des Gesamtströmungsdurchmessers aller Düsenlöcher (31) beträgt.
- Brennstoffeinspritzdüse nach Anspruch 1 oder 2, bei welchem die Längsbohrung (32) im Bereich der Düsenlöcher (31) eine Erweiterung (321) aufweist.
- Brennstoffeinspritzdüse nach Anspruch 3, bei welchem die Erweiterung (321) asymmetrisch bezüglich der Längsachse der Längsbohrung (32) ausgebildet ist.
- Brennstoffeinspritzdüse nach einem der Ansprüche 3 oder 4, bei welchem die Längsbohrung (32) schräg zur Längsachse (A) des Düsenkopfs (3) verläuft.
- Brennstoffeinspritzdüse nach einem der vorangehenden Ansprüche, bei welchem jedes Düsenloch (31) unter einem Winkel (α) von mehr als 90° in die Längsbohrung (32) einmündet.
- Brennstoffeinspritzdüse nach einem der vorangehenden Ansprüche, bei welchem der Übergangsbereich zwischen der Längsbohrung (32) und dem Düsenloch (31) jeweils abgerundet ausgestaltet ist.
- Brennstoffeinspritzdüse nach einem der vorangehenden Ansprüche, bei welchem der Durchlass am Ventilsitz (8) in der Offenstellung der Düsennadel (7) eine Fläche aufweist, die mindestens so gross ist wie der Strömungsquerschnitt der Längsbohrung (32).
- Brennstoffeinspritzdüse nach einem der vorangehenden Ansprüche bei welcher der Düsenkopf (3) abnehmbar mit dem Düsenkörper (2) verbunden ist.
- Dieselmotor, insbesondere Zweitakt-Grossdieselmotor, mit einer Brennstoffeinspritzdüse (1) gemäss einem der Ansprüche 1-9.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP05405036A EP1566539B1 (de) | 2004-02-23 | 2005-01-25 | Brennstoffeinspritzdüse |
| PL05405036T PL1566539T3 (pl) | 2004-02-23 | 2005-01-25 | Wtryskiwacz paliwa |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP04405099 | 2004-02-23 | ||
| EP04405099 | 2004-02-23 | ||
| EP05405036A EP1566539B1 (de) | 2004-02-23 | 2005-01-25 | Brennstoffeinspritzdüse |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1566539A1 true EP1566539A1 (de) | 2005-08-24 |
| EP1566539B1 EP1566539B1 (de) | 2009-01-14 |
Family
ID=34932043
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP05405036A Expired - Lifetime EP1566539B1 (de) | 2004-02-23 | 2005-01-25 | Brennstoffeinspritzdüse |
Country Status (8)
| Country | Link |
|---|---|
| EP (1) | EP1566539B1 (de) |
| JP (1) | JP2005240805A (de) |
| KR (1) | KR101264814B1 (de) |
| CN (1) | CN100564865C (de) |
| AT (1) | ATE421039T1 (de) |
| DE (1) | DE502005006448D1 (de) |
| DK (1) | DK1566539T3 (de) |
| PL (1) | PL1566539T3 (de) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2008005491A3 (en) * | 2006-07-06 | 2008-03-06 | Siemens Vdo Automotive Corp | Fuel injector having an internally mounted cross-flow nozzle for enhanced compressed natural gas jet spray |
| EP2031237A1 (de) * | 2007-08-31 | 2009-03-04 | Wärtsilä Schweiz AG | Einspritzdüse zum Einspritzen von Brennstoff |
| EP3267027A1 (de) * | 2016-07-07 | 2018-01-10 | Winterthur Gas & Diesel AG | Düsenkopf für eine brennstoffeinspritzdüse eines grossdieselmotors, sowie verfahren zum herstellen eines solchen |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101694199B (zh) * | 2009-08-20 | 2011-05-11 | 余姚市舒春机械有限公司 | 低速柴油机喷嘴 |
| DK181318B1 (en) * | 2022-02-18 | 2023-08-10 | Man Energy Solutions Filial Af Man Energy Solutions Se Tyskland | A fuel valve for a large turbocharged two-stroke uniflow crosshead internal combustion engine |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE482591C (de) * | 1927-04-30 | 1930-02-03 | Werke Kiel Akt Ges Deutsche | Brennstoffeinspritzventil fuer Brennkraftmaschinen |
| DE2948451A1 (de) * | 1979-12-01 | 1981-06-04 | Robert Bosch Gmbh, 7000 Stuttgart | Kraftstoffeinspritzduese fuer brennkraftmaschinen |
| DE3430772A1 (de) * | 1983-08-23 | 1985-03-14 | CKD Praha O.P., Prag/Praha | Einspritzduese fuer dieselmotoren |
| EP0446165A1 (de) * | 1990-03-06 | 1991-09-11 | Ail Corporation | Methode und Vorrichtung zum elektrochemischen Bearbeiten der Spritzöffnungen von Brennstoff-Einspritzdüsen |
| JPH10176631A (ja) * | 1996-12-18 | 1998-06-30 | Nippon Soken Inc | 燃料噴射弁 |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3234829A1 (de) * | 1982-09-21 | 1984-03-22 | Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5000 Köln | Einspritzvorrichtung fuer einen dieselmotor |
| JPH0639095Y2 (ja) * | 1988-03-09 | 1994-10-12 | 住友重機械工業株式会社 | ディーゼル機関用燃料噴射ノズル |
| JPH11117830A (ja) | 1997-10-20 | 1999-04-27 | Hitachi Ltd | インジェクタ |
| DE50309291D1 (de) * | 2002-04-11 | 2008-04-17 | Waertsilae Nsd Schweiz Ag | Düsenkopf für eine Brennstoffeinspritzdüse |
| KR101307563B1 (ko) | 2003-07-16 | 2013-09-12 | 베르트질레 슈바이츠 악티엔게젤샤프트 | 실린더부 내의 고압 피스톤용 피스톤 |
-
2005
- 2005-01-25 DK DK05405036T patent/DK1566539T3/da active
- 2005-01-25 PL PL05405036T patent/PL1566539T3/pl unknown
- 2005-01-25 AT AT05405036T patent/ATE421039T1/de not_active IP Right Cessation
- 2005-01-25 DE DE502005006448T patent/DE502005006448D1/de not_active Expired - Lifetime
- 2005-01-25 EP EP05405036A patent/EP1566539B1/de not_active Expired - Lifetime
- 2005-02-22 KR KR1020050014480A patent/KR101264814B1/ko not_active Expired - Fee Related
- 2005-02-22 JP JP2005044914A patent/JP2005240805A/ja active Pending
- 2005-02-23 CN CNB2005100519828A patent/CN100564865C/zh not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE482591C (de) * | 1927-04-30 | 1930-02-03 | Werke Kiel Akt Ges Deutsche | Brennstoffeinspritzventil fuer Brennkraftmaschinen |
| DE2948451A1 (de) * | 1979-12-01 | 1981-06-04 | Robert Bosch Gmbh, 7000 Stuttgart | Kraftstoffeinspritzduese fuer brennkraftmaschinen |
| DE3430772A1 (de) * | 1983-08-23 | 1985-03-14 | CKD Praha O.P., Prag/Praha | Einspritzduese fuer dieselmotoren |
| EP0446165A1 (de) * | 1990-03-06 | 1991-09-11 | Ail Corporation | Methode und Vorrichtung zum elektrochemischen Bearbeiten der Spritzöffnungen von Brennstoff-Einspritzdüsen |
| JPH10176631A (ja) * | 1996-12-18 | 1998-06-30 | Nippon Soken Inc | 燃料噴射弁 |
Non-Patent Citations (1)
| Title |
|---|
| PATENT ABSTRACTS OF JAPAN vol. 1998, no. 11 30 September 1998 (1998-09-30) * |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2008005491A3 (en) * | 2006-07-06 | 2008-03-06 | Siemens Vdo Automotive Corp | Fuel injector having an internally mounted cross-flow nozzle for enhanced compressed natural gas jet spray |
| EP2031237A1 (de) * | 2007-08-31 | 2009-03-04 | Wärtsilä Schweiz AG | Einspritzdüse zum Einspritzen von Brennstoff |
| EP3267027A1 (de) * | 2016-07-07 | 2018-01-10 | Winterthur Gas & Diesel AG | Düsenkopf für eine brennstoffeinspritzdüse eines grossdieselmotors, sowie verfahren zum herstellen eines solchen |
Also Published As
| Publication number | Publication date |
|---|---|
| ATE421039T1 (de) | 2009-01-15 |
| PL1566539T3 (pl) | 2009-05-29 |
| EP1566539B1 (de) | 2009-01-14 |
| DE502005006448D1 (de) | 2009-03-05 |
| DK1566539T3 (da) | 2009-04-14 |
| KR20060043061A (ko) | 2006-05-15 |
| JP2005240805A (ja) | 2005-09-08 |
| CN1661227A (zh) | 2005-08-31 |
| CN100564865C (zh) | 2009-12-02 |
| KR101264814B1 (ko) | 2013-05-15 |
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