DK171975B1 - Fuel injector for a large two-stroke internal combustion engine - Google Patents
Fuel injector for a large two-stroke internal combustion engine Download PDFInfo
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- DK171975B1 DK171975B1 DK015694A DK15694A DK171975B1 DK 171975 B1 DK171975 B1 DK 171975B1 DK 015694 A DK015694 A DK 015694A DK 15694 A DK15694 A DK 15694A DK 171975 B1 DK171975 B1 DK 171975B1
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- nebulizer
- section
- bore
- valve
- slider
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/188—Spherical or partly spherical shaped valve member ends
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- 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
- F02M47/00—Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure
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- 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
- F02M53/00—Fuel-injection apparatus characterised by having heating, cooling or thermally-insulating means
- F02M53/04—Injectors with heating, cooling, or thermally-insulating means
- F02M53/043—Injectors with heating, cooling, or thermally-insulating means with cooling means other than air cooling
-
- 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
- F02M61/04—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
-
- 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
- F02M61/04—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
- F02M61/042—The valves being provided with fuel passages
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- 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
- F02M61/04—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
- F02M61/10—Other injectors with elongated valve bodies, i.e. of needle-valve type
- F02M61/12—Other injectors with elongated valve bodies, i.e. of needle-valve type characterised by the provision of guiding or centring means for valve bodies
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- 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
- F02M61/166—Selection of particular materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/20—Closing valves mechanically, e.g. arrangements of springs or weights or permanent magnets; Damping of valve lift
-
- 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
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Fuel-Injection Apparatus (AREA)
- Nozzles (AREA)
Description
DK 171975 B1DK 171975 B1
Opfindelsen angår en brændselsinjektor til en stor totakts forbrændingsmotor, såsom en dieselmotor til skibsfremdrivning, med et langstrakt ydre hus til montering i et vandkølet cylinderdæksel på en sådan 5 måde, at ventilen har et øvre kølet ventilafsnit og et nedre i det væsentlige ukølet ventilafsnit, der omfatter i det mindste forstøverens nedre del med tværgående forstøverhuller, som udgår fra en central langsgående forstøverboring, og hvor en ventilglider har et øvre 10 afsnit, der bærer en bevægelig ventildel for et i det kølede ventilafsnit beliggende primært ventilsæde til åbning og lukning af brændselsinjektoren, og et tyndt nedre afsnit, der strækker sig ned i forstøverboringen og bærer et i det nedre ventilafsnit beliggende sekun-15 dært lukkeorgan for brændselsstrømningen til forstøverhullerne.The invention relates to a fuel injector for a large two-stroke internal combustion engine, such as a ship propulsion diesel engine, with an elongated outer housing for mounting in a water-cooled cylinder cover in such a way that the valve has an upper cooled valve section and a lower substantially non-cooled valve section which at least comprises the lower portion of the nebulizer with transverse nebulizer holes starting from a central longitudinal nebulizer bore and wherein a valve slider has an upper 10 section carrying a movable valve member for a primary valve seat located in the refrigerated valve section for opening and closing the fuel injector; and a thin lower section extending into the nebulizer bore and carrying a secondary valve member located in the lower valve section for the fuel flow to the nebulizer holes.
Til firtaktsmotorer kendes brændselsinjektorer, hvor det primære ventilsæde ligger umiddelbart over forstøverhullerne, se fx EP-A-0 451 408. Den forreste 20 del af injektoren med ventilsædet er her kølet af kølevandet i cylinderdækslet, idet dette har så lille tykkelse, og injektorhuset er så kort, at afkølingen virker helt ned til spidsen af injektoren. Som følge af kølingen kan forstøveren og ventilsædet være af hærdet 25 stål.For four stroke engines, fuel injectors are known, where the primary valve seat is immediately above the nebulizer holes, see for example EP-A-0 451 408. Here, the front part 20 of the injector with the valve seat is cooled by the cooling water in the cylinder cover, since it is so small in thickness and the injector housing is so short that the cooling works all the way down to the tip of the injector. As a result of the cooling, the nebulizer and valve seat may be of hardened 25 steel.
Ved store totaktsmotorer er cylinderdækslet så tykt, at injektorens nedre ventilafsnit strækker sig et så langt stykke fra injektorens anlægsflade mod det kølende dæksel nedefter til forstøverboringerne, at det 30 nedre afsnit i det væsentlige er ukølet og bliver opvarmet til høj temperatur af motorens forbrændingsgasser. Da de høje temperaturer kan føre til svigtende funktion af det primære ventilsæde, fx på grund af tilkoksning eller materialenedbrydning, er det primære 35 ventilsæde i disse injektorer beliggende oppe i det DK 171975 B1 2 øvre, kølede ventilafsnit. Dette medfører, at strømningspassagen mellem det primære ventilsæde og forstøverhullerne bliver lang og får stort volumen, der typisk andrager fra 2-3 % af det brændselsvolumen, som 5 indsprøjtes i løbet af en motorcyklus.In large two stroke engines, the cylinder cover is so thick that the lower valve section of the injector extends so far from the injector's abutment surface to the cooling cover down to the nebulizer bores that the lower portion is substantially uncooled and heated to high temperature by the engine's combustion gases. Since the high temperatures can lead to failure of the primary valve seat, for example due to coking or material degradation, the primary valve seat in these injectors is located in the upper, cooled valve section. This means that the flow passage between the primary valve seat and the nebulizer holes becomes long and receives a large volume, typically amounting to 2-3% of the fuel volume injected during a motor cycle.
Når det primære ventilsæde lukkes ved afslutningen af brændselsindsprøjtningen, bliver brændselsmængden i passagen mellem ventilsædet og forstøverhullerne afskåret fra brændslets leveringstryk. Denne brændsels-10 mængde kan sive eller dryppe ud gennem forstøverboringerne i den periode, hvor injektoren i og for sig er lukket. Da denne restmængde af brændsel ikke forstøves ind i forbrændingskammeret, opnås ingen eller kun meget ringe forbrænding af brændslet. Det uforbrændte brændsel 15 fører til tilkoksning af forbrændingskammeret og af de strømningsmæssigt efterfølgende motorkomponenter samt til en i miljømæssig henseende uheldig udledning af brændsel med udstødsgassen og naturligvis også til forøget brændselsforbrug.When the primary valve seat is closed at the end of the fuel injection, the amount of fuel in the passage between the valve seat and the nebulizer holes is cut off from the fuel delivery pressure. This amount of fuel can seep or drip through the atomizer bores during the period when the injector is closed by itself. Since this residual amount of fuel is not atomized into the combustion chamber, no or very little combustion of the fuel is obtained. The unburned fuel 15 leads to the boiling of the combustion chamber and of the flow components which follow, as well as to an environmentally unfavorable discharge of fuel with the exhaust gas and of course also to increased fuel consumption.
20 Størstedelen af disse ulemper er afhjulpet med brændselsinjektoren, beskrevet i WO 93/07386, der er af den indledningsvis nævnte type. Ventilglideren bærer her et sekundært lukkeorgan i form af en ring, som i injektorens lukkede stilling strækker sig ned forbi 25 forstøverhullerne og afspærrer disse, så oliemængden i passagen under det primære ventilsæde er hindret i udstrømning gennem forstøverhullerne, når injektoren er lukket. Ved injektorens åbnebevægelse glider ringen opad i forstøverboringen, så forstøverhullerne blotlægges.The majority of these disadvantages are remedied with the fuel injector described in WO 93/07386 which is of the type mentioned initially. Here, the valve slider carries a secondary closure member in the form of a ring which extends downwardly past the atomizer holes in the closed position of the injector so that the amount of oil in the passage below the primary valve seat is prevented from flowing through the atomizer holes when the injector is closed. At the injector open movement, the ring slides upwards into the nebulizer bore to expose the nebulizer holes.
30 Den centrale forstøverboring har konstant diameter for at tillade indsætning og forskydning af den glidende ring i boringen.The central nebulizer bore has a constant diameter to allow insertion and displacement of the sliding ring in the bore.
I praksis har injektoren med sekundært lukkeorgan vist sig at medføre større forbrug af brændsel især ved 35 høje motorbelastninger. Dette skyldes antagelig ændrede 3 DK 171975 B1 indsprøjtningsforhold, når injektoren står åben, og olien forstøves ind i forbrændingskammeret.In practice, the secondary closure injector has been found to lead to greater fuel consumption especially at 35 high engine loads. This is probably due to changed injection conditions when the injector is open and the oil is atomized into the combustion chamber.
Opfindelsen har til formål at anvise en brændselsinjektor, som på trods af et forholdsvist højt tempera-5 turniveau i området omkring forstøverhullerne både er i stand til at begrænse udledningen af brændsel, når injektoren er lukket, og at give en fordelagtig god indsprøjtning og fordeling af brændslet, når injektoren er åben.The invention has for its object to provide a fuel injector which, despite a relatively high temperature level in the area around the atomizer holes, is both capable of limiting the discharge of fuel when the injector is closed, and to provide an advantageous good injection and distribution of fuel when the injector is open.
10 Med henblik herpå er brændselsinjektoren ifølge opfindelsen ejendommelig ved, at forstøverboringen har et i det nedre ventilafsnit beliggende område med mindskende diameter i nedadgående retning, at forstøverhullerne udgår fra boringsafsnittet med mindre diameter, 15 og at ventilgliderens nedre afsnit ender i nivaeu over det øverste forstøverhul, og det sekundære lukkeorgan er beliggende ved området for boringens diameterformindskelse, når glideren står i sin lukkestilling.To this end, the fuel injector according to the invention is characterized in that the nebulizer bore has a downwardly decreasing diameter downstream section, that the nebulizer holes extend from the smaller diameter bore section, and that the lower section of the valve slide ends in level above the upper nebulizer hole. and the secondary closure member is located at the region of the diameter reduction of the bore when the slider is in its closing position.
Det har overraskende vist sig, at brændselsin-20 jektoren ifølge opfindelsen opfylder ovennævnte formål.Surprisingly, it has been found that the fuel injector according to the invention fulfills the above purpose.
Det sekundære lukkeorgan hindrer den oveniiggende brændselsmængde i at trænge ned til forstøverhullerne, når injektoren er lukket. En forklaring af det mindskede brændselsforbrug, når injektoren står åben, kan an-25 tagelig findes i det forhold, at boringsafsnittet førende til forstøverhullerne har en fordelagtig lille diameter, hvilket giver ensartede strømningsforhold til forstøverhullerne. Da ventilglideren i enhver stilling er afsluttet i niveau oven over forstøverhullerne, er 30 brændselsstrømningen til disse huller antagelig kun i ringe grad påvirket af tilstedeværelsen af et sekundært lukkeorgan.The secondary closure means prevents the excess amount of fuel from penetrating to the nebulizer holes when the injector is closed. An explanation of the reduced fuel consumption when the injector is open can be reasonably found in the fact that the bore section leading to the nebulizer holes has an advantageously small diameter, which gives uniform flow conditions to the nebulizer holes. Since the valve slider is completed in any position above the atomizer holes, the fuel flow to these holes is probably only slightly affected by the presence of a secondary closure.
I ventilens lukkede stilling hindrer det primære ventilsæde brændselstrykket på pumpesiden i at påvirke 35 området omkring det sekundære lukkeorgan. Der er således DK 171975 B1 4 ikke noget nævneværdigt trykfald over lukkeorganet, hvilket giver frihed til at udforme dette på en måde, så lukkeorganet i sin lukkede stilling kun påvirker forstøverens materiale med særdeles små kræfter.In the closed position of the valve, the primary valve seat prevents the fuel pressure on the pump side from affecting the area around the secondary closing means. Thus, there is no appreciable pressure drop across the closure means, which gives freedom to design this in a way that the closure means in its closed position only affects the material of the atomizer with very small forces.
5 Ventilgiiderens afslutning i afstand fra det øverste forstøverhul giver også den fordel, at gliderspidsen ikke påvirkes af de erosionskræfter, som fremkommer omkring forstøverhullerne, når ventilen åbner.The end of the valve guide at a distance from the upper nebulizer hole also gives the advantage that the slider tip is not affected by the erosion forces that appear around the nebulizer holes when the valve opens.
10 I en foretrukken udførelsesform har det sekundære lukkeorgan et cylindrisk parti, der kan glide tætnende ind i forstøverboringens afsnit med mindre diameter. Når glideren bevæges nedefter hen mod lukkestillingen, forskydes det cylindriske parti ned i forstøverboringens 15 smallere nedre afsnit, så strømningsforbindelsen mellem forstøverhullerne og det overliggende bredere afsnit af forstøverboringen bliver afbrudt. Det cylindriske parti påvirker kun selve forstøveren med den lille friktionskraft, som fremkommer, når overfladerne glider forbi 20 hinanden. I injektorens lukkede stilling ligger det cylindriske parti optaget inden i forstøverboringens nedre afsnit uden at forstøveren påvirkes af.egentlige lukkekræfter.In a preferred embodiment, the secondary closure member has a cylindrical portion which can slide sealingly into the smaller diameter section of the nebulizer bore. As the slider is moved downward toward the closing position, the cylindrical portion is displaced into the narrower lower portion of the nebulizer bore 15 so that the flow connection between the nebulizer holes and the overlying wider portion of the nebulizer bore is interrupted. The cylindrical portion only affects the nebulizer itself with the small frictional force that results when the surfaces slip past one another. In the closed position of the injector, the cylindrical portion is accommodated within the lower portion of the nebulizer bore without the nebulizer being affected by actual closing forces.
I en fremstillingsmæssig særlig enkel udførelses-25 form er ventilgliderens tynde nedre afsnit med det sekundære lukkeorgan en stiv forlængelse af gliderens øvre afsnit. Det tynde afsnits stivhed bevirker, at gliderspidsen holdes koaksial med gliderens øvre afsnit og dermed også koaksial med forstøverboringen.In a particularly simple embodiment, the thin lower section of the valve slide with the secondary closure means is a rigid extension of the upper section of the slide. The stiffness of the thin section causes the slider tip to be held coaxial with the upper section of the slider and thus also coaxial with the nebulizer bore.
30 I en alternativ udførelsesform er ventilgliderens tynde nedre afsnit en tværfleksibel forlængelse af dens øvre afsnit, og det nedre afsnit har i niveau over det sekundære lukkeorgan et styr, der centrerer lukkeorganet i forstøverboringen gennem anlæg mod væggen af boringens 35 afsnit med større diameter. Det separate styr til 5 DK 171975 B1 centrering af gliderspidsen er ganske vist vanskeligere at fremstille end et cylindrisk, glat nedre afsnit, men til gengæld er der ikke behov for, at gliderens nedre afsnit er oprettet i forhold til det øvre afsnit, idet 5 spidsen af glideren er selvcentrerende i forstøverboringen. Dette letter i væsentlig grad monteringen af glideren i injektoren og sikrer god centrering af gliderspidsen selv efter lang tids drift. Den selvoprettende gliderspids er særlig fordelagtig i de til-10 fælde, hvor gliderens nedre afsnit er en separat, udskiftelig enhed.In an alternative embodiment, the thin lower portion of the valve slider is a transverse extension of its upper portion, and the lower portion has a level above the secondary closure means centering the closure member of the nebulizer bore through abutment against the wall of the larger diameter bore 35. The separate guide for centering the slider tip is more difficult to manufacture than a cylindrical, smooth lower section, but on the other hand there is no need for the lower section of the slider to be created relative to the upper section, with the 5 tip of the slider is self-centering in the nebulizer bore. This significantly facilitates mounting of the slider in the injector and ensures good centering of the slider even after long periods of operation. The self-erecting slider tip is particularly advantageous in cases where the lower section of the slider is a separate, replaceable unit.
Det foretrækkes, at styret er udformet som flere radialt udstående, langsgående flige på gliderens nedre afsnit, og at fligenes øvre og nedre ender fortrinsvis 15 er tilspidsede. De langsgående flige forstyrrer kun i ringe grad den nedovergående strømning af brændsel, når injektoren står åben. Strømningsforstyrrelserne kan yderligere mindskes ved at fligenes ender er tilspidsede, så strømningen får glat afløb fra fligene. Af hensyn 20 til bedst mulige strømningsforhold i forstøverens nederste afsnit, kan gliderens nedre frie ende hensigtsmæssigt være konisk, så der ikke opsættes for mange hvirvler i brændslet, når det ved passage af det sekundære lukkeorgan skifter fra at strømme uden om 25 glideren til selv at udfylde hele boringens tværsnit.It is preferred that the guide is configured as a plurality of radially extending longitudinal tabs on the lower portion of the slider and that the upper and lower ends of the tabs are preferably tapered. The longitudinal tabs only slightly interfere with the downward flow of fuel when the injector is open. The flow disturbances can be further mitigated by the ends of the tabs being tapered so that the flow gets smooth drainage from the tabs. For best flow conditions in the lower section of the nebulizer, the lower free end of the slider may conveniently be tapered so that not too many swirls are set up in the fuel as it passes through the secondary closing means from flowing out of the slider to even fill the entire cross-section of the bore.
Navnlig hvis brændslet er gasformigt kan det være hensigtsmæssigt at udforme injektoren, så det sekundære lukkeorgan i sin lukkede stilling ligger an mod en skråflade i boringens område med mindskende diameter, 30 og at lukkeorganet er forskydeligt i gliderens længderetning og fjederbelastet til bevægelse bort fra gliderens øvre afsnit. Skråfladen virker som ventilsæde, men som følge af det sekundære lukkeorgans forskydelighed i forhold til gliderens øvre afsnit, kan lukkeorga-35 net højest presses an mod sædet med kraften frembragt 6 DK 171975 B1 af den tilhørende fjeder. Fjederkraften kan afpasses efter styrken af materialet i forstøveren, dvs. fjederkraften kan eksempelvis vælges så lille, at sædematerialet stort set ikke belastes af lukkeorganet.In particular, if the fuel is gaseous, it may be convenient to design the injector so that the secondary closure member in its closed position abuts a bevel surface in the bore of decreasing diameter, and that the closure member is slidable in the longitudinal direction of the slider and spring-loaded for movement away from the top of the slider. section. The inclined surface acts as a valve seat, but due to the secondary closure member's displacement relative to the upper section of the slider, the closure member can be pressed against the seat at the maximum with the force produced by the associated spring. The spring force can be adjusted to the strength of the material in the nebulizer, ie. for example, the spring force can be selected so small that the seat material is largely unloaded by the closing means.
5 Det foretrækkes, at ventilgliderens nedre tynde afsnit med det sekundære lukkeorgan er en separat enhed, som er aftageligt fastgjort til det øvre afsnit. Dette gør det muligt at udskifte det sekundære lukkeorgan uafhængigt af gliderens øvre afsnit, og endvidere opnås 10 den fremstillingsmæssige fordel, at de to afsnit kan fremstilles hver for sig, dvs. også i hvert sit materiale, hvis det ønskes at lukkeorganet er af et mere temperaturbestandigt materiale end gliderens øvre afsnit.It is preferred that the lower thin section of the valve slide with the secondary closure means be a separate unit which is removably attached to the upper section. This makes it possible to replace the secondary closure member independently of the upper section of the slider, and furthermore, the manufacturing advantage is obtained that the two sections can be manufactured separately, ie. also in its own material, if it is desired that the closing means be of a more temperature resistant material than the upper section of the slider.
15 For at opnå størst mulig begrænsning i olietabet i perioder, hvor injektoren er lukket, foretrækkes det, at forstøverboringernes område med mindskende diameter ligger væsentligt tættere på forstøverhullerne end på det primære ventilsæde. Dermed begrænses forstøverborin-20 gens volumen under det sekundære lukkeorgan.In order to achieve the greatest possible reduction in the oil loss during periods when the injector is closed, it is preferred that the area of the nebulizer bores with diminishing diameter is substantially closer to the nebulizer holes than to the primary valve seat. Thus, the volume of nebulizer drilling is limited below the secondary closure means.
For at opnå god start på forstøvningen af brændslet ved åbning af injektoren, kan denne hensigtsmæssigt være udformet, så det sekundære lukkeorgan først åbner for forstøverboringens afsnit med mindre diameter, når 25 gliderens bevægelige ventildel er bevæget et forudbestemt stykke bort fra det primære ventilsæde. Dermed kan brændslets tryk i forstøverboringens afsnit med større diameter opbygges til passende højt tryk, inden lukkeorganet åbner for brændslets adgang til boringen førende 30 til forstøverhullerne. Når brændslet begynder at sprøjte ud gennem forstøverhullerne sker dette derfor ved højere tryk, hvilket fremmer forstøvningen. Forsinkelsen af lukkeorganets åbning kan i en udførelsesform afpasses ved hjælp af længden af det cylindriske parti, der kan 35 glide tætnende ind i forstøverboringen, og i en anden 7 DK 171975 B1 udførelsesform afpasses forsinkelsen ved hjælp af beliggenheden af et stop, som trækker et forskydeligt lukkeorgan med sig i gliderens bevægelse.To obtain a good start on the fuel atomization by opening the injector, it may conveniently be designed so that the secondary closure means only opens to the smaller diameter section of the nebulizer bore when the slider movable valve portion is moved a predetermined distance away from the primary valve seat. Thus, the pressure of the fuel in the larger diameter section of the nebulizer bore can be built up to suitably high pressure before the closing means opens for the fuel's access to the bore leading to the nebulizer holes. Therefore, when the fuel starts to spray out through the nebulizer holes, this occurs at higher pressure, which promotes the nebulization. In one embodiment, the delay of the closing member can be adjusted by the length of the cylindrical portion which can slide sealingly into the nebulizer bore, and in another embodiment, the delay is adjusted by the location of a stop pulling a slidable closure member with it in the slider movement.
Eksempler på udførelsesformer for opfindelsen 5 beskrives herefter nærmere med henvisning til den skematiske tegning, hvor fig. 1 viser et længdesnit gennem en første udførelsesform for en brændselsinjektor, fig. 2 og 3 i større skala det nederste afsnit af 10 en anden udførelsesform for injektor henholdsvis i åben og lukket stilling, fig. 4 og 5 tilsvarende billeder af en tredje udførelsesform monteret i et cylinderdæksel, og fig. 6 og 7 tilsvarende billeder af en fjerde 15 udførelsesform.Examples of embodiments of the invention 5 will now be described in more detail with reference to the schematic drawing, in which 1 is a longitudinal section through a first embodiment of a fuel injector; FIG. 2 and 3, on a larger scale, the lower section of 10 shows another embodiment of the injector in the open and closed positions, respectively; 4 and 5 show similar views of a third embodiment mounted in a cylinder cover; and FIGS. 6 and 7 show similar images of a fourth embodiment.
I fig. 1 ses en generelt med 1 betegnet brændselsinjektor eller brændselsventil med en øvre flange 2 til fastspænding af injektoren i motoren. Flangen har en opadvendende studs 3, hvortil kan fastspændes et ikke 20 vist trykrør, der tilfører brændsel under tryk fra en passende kilde, såsom en brændselspumpe eller et højtryksreservoir .In FIG. 1, there is generally shown a fuel injector or fuel valve 1 with an upper flange 2 for clamping the injector in the engine. The flange has an upwardly extending studs 3 to which a pressure tube (not shown) can be clamped which supplies fuel under pressure from a suitable source, such as a fuel pump or a high pressure reservoir.
Injektoren har i sin nedre ende en forstøver 4. Brændslet kan føres fra tilslutningen ved studsen 3 ned 25 mod forstøveren 4 gennem en øvre strømningspassage 5, der fra en central boring 6 i studsen går gennem et fjederstyr 7 og en cirkulationsglider 8 ned til et trykkammer 9 afgrænset af glideren 8 og et styr 10 for denne. På undersiden af et sæde 11 kan brændslet strømme 30 videre ned mod forstøveren gennem en midterste strømningspassage 12 i form af en central boring i et trykrør 13, et trykstykke 14 og en ventilglider 15, hvori den centrale boring er forbundet med et primært trykkammer 16 gennem flere skråboringer 17. Den midterste strøm-35 ningspassage er nedadtil afsluttet ved et primært 8 DK 171975 B1 ventilsæde 18. Under dette ventilsæde kan brændslet i injektorens åbne stilling strømme videre gennem en nedre str.ømningspassage 19 i form af en central boring 20 ( se fig. 2) ved bunden af et gliderstyr 21 for ventilgli-5 deren 15 og en dermed koaksial forstøverboring.The injector has at its lower end a nebulizer 4. The fuel can be fed from the connection at the bore 3 down 25 to the nebulizer 4 through an upper flow passage 5 passing from a central bore 6 in the bore through a spring guide 7 and a circulation slide 8 down to a pressure chamber. 9 defined by the slider 8 and a guide 10 therefor. On the underside of a seat 11, fuel flow 30 may further descend toward the nebulizer through a central flow passage 12 in the form of a central bore in a pressure tube 13, a pressure member 14 and a valve slider 15, wherein the central bore is connected to a primary pressure chamber 16 through several diaphragm bores 17. The middle flow passage downwards is completed by a primary valve seat 18. Under this valve seat, the fuel in the open position of the injector can flow further through a lower flow passage 19 in the form of a central bore 20 (see Fig. 2) at the bottom of a slide guide 21 for the valve slide 15 and a coaxial nebulizer bore thereof.
Den centrale langsgående forstøverboring omfatter et øvre boringsafsnit 22 med større diameter, som gennem et område 23 med mindskende diameter går over i et nedre boringsafsnit med mindre diameter, hvorfra udgår 10 forstøverhuller 24 som vist i de efterfølgende figurer.The central longitudinal nebulizer bore comprises a larger diameter upper bore portion 22 which, through a diminishing diameter region 23, passes into a lower diameter lower bore portion from which 10 nebulizer holes 24 emerge as shown in the following figures.
Når injektoren står i sin lukkede stilling vist i fig. 1 er den øvre strømningspassage 5 gennem en ikke vist tværkanal i fjederstyret 7 forbundet med det omkring fjederstyret beliggende hulrum, så der i 15 injektorens øverste del på velkendt vis kan cirkulere forvarmet brændsel. Det kan her bemærkes, at injektoren i fig. 1 er bestemt til indsprøjtning af olie, navnlig heavy fuel oil. Når brændselsindsprøjtningen skal initieres, stiger olietrykket i den øvre strømnings-20 passage 5 og i trykkammeret 9, så cirkulationsglideren 8 bevæges opad og afspærrer den tværgående cirkulationspassage. Samtidig åbnes strømningspassagen forbi sædet 11 og trykket forplanter sig ned gennem den midterste strømningspassage 12 og skråboringerne 17 til det 25 primære trykkammer 18. En trykfjeder 25 ligger an mod en øvre fjedertallerken 26 og presser gennem en nedre fjedertallerken 27 nedad på ventilglideren 15, så en i forhold til det primære ventilsæde 18 bevægelige ventildel 28 i form af en ringformet konisk flade på 30 ventilglideren presses tætnende an mod ventilsædet 18.When the injector is in its closed position shown in FIG. 1, the upper flow passage 5 is connected through a spring channel 7 not shown in the spring guide 7 to the cavity located around the spring guide, so that in the upper part of the injector well-known fuel can circulate in a well known manner. It may be noted here that the injector of FIG. 1 is intended for injection of oil, in particular heavy fuel oil. When the fuel injection is to be initiated, the oil pressure rises in the upper flow passage 5 and in the pressure chamber 9, so that the circulation slide 8 moves upwards and blocks the transverse circulation passage. At the same time, the flow passage past the seat 11 is opened and the pressure propagates down through the middle flow passage 12 and the inclined bores 17 to the primary pressure chamber 18. A pressure spring 25 abuts an upper spring plate 26 and presses through a lower spring plate 27 downwards on the valve slide 15, relative to the primary valve seat 18, movable valve member 28 in the form of an annular tapered surface of the valve slider is pressed tightly against the valve seat 18.
Når olietrykket i det primære trykkammer 16 når op på ventilens åbningstryk, der er bestemt af forspændin-geri af trykfjederen 25, bevæges ventilglideren 15 opefter samtidig med, at olien begynder at strømme forbi 35 det primære ventilsæde 18.As the oil pressure in the primary pressure chamber 16 reaches the opening pressure of the valve, which is determined by biasing of the compression spring 25, the valve slider 15 is moved upward as the oil begins to flow past the primary valve seat 18.
9 DK 171975 B19 DK 171975 B1
Den bevægelige ventildel 28 afgrænser det øvre afsnit af ventilglideren 15 fra et tyndt nedre afsnit 30 af glideren. I udførelsesformen vist i fig. 1 er det nedre afsnit 30 cylindrisk og har en diameter, der er 5 en anelse mindre end diameteren af forstøverboringens afsnit 29 med mindre diameter, så gliderens nedre afsnit 30 kan glide tætnende ind i det nedre boringsafsnit 29.The movable valve member 28 defines the upper portion of the valve slide 15 from a thin lower portion 30 of the slide. In the embodiment shown in FIG. 1, the lower section 30 is cylindrical and has a diameter 5 slightly smaller than the diameter of the smaller diameter 29 section of the nebulizer bore, so that the lower section 30 of the slider can slide sealingly into the lower bore section 29.
Da det nedre afsnit 30 rager et stykke ned i boringsafsnittet 29, når injektoren er lukket, opbygges trykket 10 ved åbning af ventilen i det øvre boringsafsnit 22, inden gliderens nedre afsnit 30 løftes op af boringsafsnittet 29, hvorved der åbnes for oliestrømningen til forstøverhullerne. Trykopbygningen i olien inden den endelige tilledning til forstøverhullerne fremmer 15 finforstøvningen af olien ved initieringen af forstøvningen.As the lower section 30 projects a bit down into the bore section 29 when the injector is closed, the pressure 10 is built up by opening the valve in the upper bore section 22, before the lower section 30 of the slider is lifted up by the bore section 29, thereby opening up the oil flow to the nebulizer holes. The pressure buildup in the oil prior to final feeding to the nebulizer holes promotes fine atomization of the oil upon initiation of the nebulization.
De i fig. 1 ikke viste forstøverhuller ligger nede ved afslutningen af boringsafsnittet 29, dvs. flere boringsdiametre i afstand fra ventilglideren 15's nedre 20 koniske spids, når glideren står i sin viste lukkestil-lirig. Ventilgliderens nedre afsnit 30 har i det væsentlige konstant diameter, men behøver kun præcis bearbejdning på det som lukkeorgan 32 virkende nederste stykke, der glider ind i forstøverboringens nedre afsnit 25 29.The 1, nebulizer holes not shown at the end of bore section 29, i.e. several bore diameters spaced from the lower 20 tapered tip of the valve slide 15 as the slide is in its shown closure state. The lower section 30 of the valve slider is substantially constant in diameter, but only needs precise machining on the lower portion acting as a closing member 32 which slides into the lower section 25 29 of the nebulizer bore.
Ventilglideren 15's nedre afsnit 30 er i den første udførelsesform vist i fig. 1 udført ud i ét stykke med ventilgliderens øvre afsnit og som en stiv forlængelse heraf, hvorved det nedre afsnit 30 uden yderligere 30 styring end det øvre gliderafsnits lejring i glidestyret 21 ligger centreret i forhold til forstøverboringen.The lower portion 30 of the valve slide 15 is shown in the first embodiment in FIG. 1, integral with the upper section of the valve slider and as a rigid extension thereof, whereby the lower section 30 without further control than the bearing of the upper slide section in the slide guide 21 is centered relative to the nebulizer bore.
En anlægsflade 31 ved forenden af injektorhuset 2a ligger i injektorens monterede stilling spændt ned mod en opadvendende konisk flade på motorens cylinderdæksel.A abutment surface 31 at the front end of the injector housing 2a lies in the injector's mounted position clamped down against an upwardly tapered surface of the cylinder cover of the engine.
35 Denne anlægsflade er det nederste sted, hvor injektoren 10 DK 171975 B1 udsættes for en væsentlig kølevirkning, der fremkommer fordi dækslet er kølet af et i motoren cirkulerende kølemiddel, der ved anlægsfladen 31 holder dækseltemperaturen på eksempelvis 80°C. Ovenover den koniske 5 anlægsflade 31 svarer injektorens temperatur stort set til temperaturen af den i injektoren cirkulerende olie, der kan være forvarmet til eksempelvis 120°C. Forstøverafsnittet beliggende under den skrå anlægsflade 31 er i det mindste i sin nederste del i kontakt med de 10 høje temperaturer i cylinderens forbrændingskammer. Den nederste del af forstøveren er derfor i praksis ukølet.This abutment surface is the lower place where the injector 10 DK 171975 B1 is subjected to a significant cooling effect which results from the cover being cooled by a refrigerant circulating in the motor which at the abutment surface 31 maintains the cover temperature of, for example, 80 ° C. Above the tapered contact surface 31, the injector temperature corresponds substantially to the temperature of the oil circulating in the injector, which may be preheated to, for example, 120 ° C. The nebulizer section located beneath the inclined abutment surface 31 is at least in its lower part in contact with the 10 high temperatures in the combustion chamber of the cylinder. The lower part of the nebulizer is therefore in practice uncooled.
Som helhed kan ventilen 1 således siges at være opdelt i et øvre kølet ventilafsnit la beliggende ovenover anlægsfladen 31 og et nedre i det væsentlige ukølet 15 ventilafsnit lb, der strækker sig fra den nedre ende af forstøveren 4 og op i nærheden af anlægsfladen 31.As a whole, the valve 1 can thus be said to be divided into an upper cooled valve section 1a located above the abutment surface 31 and a lower substantially uncooled valve section 1b extending from the lower end of the nebulizer 4 and up to the abutment surface 31.
Forstøveren 4 er af et højtemperaturbestandigt materiale, som også kan modstå brændslets erosionspåvirkninger i området omkring forstøverhullerne. Da 20 hærdet stål ikke er i stand til at modstå det høje temperaturniveau i det ukølede ventilafsnit lb, er forstøveren fremstillet af eksempelvis Stellite 6 eller en anden højtemperaturbestandig legering, såsom INCONEL ALLOY ma758 som beskrevet i EP-A-0 569 655.The atomizer 4 is of a high temperature resistant material that can also withstand the erosion effects of the fuel in the area around the atomizer holes. Since 20 hardened steels are not able to withstand the high temperature level in the uncooled valve section 1b, the nebulizer is made of, for example, Stellite 6 or another high temperature resistant alloy such as INCONEL ALLOY ma758 as described in EP-A-0 569 655.
25 Det ses, at det primære ventilsæde er beliggende i det kølede ventilafsnit, mens både lukkeorganet 32 og det øverste stykke af boringens afsnit 29 er beliggende i det ukølede ventilafsnit lb. Da lukkeorganet 32 stort set ikke belaster forstøverens materiale med kræfter 30 virkende i længderetningen har både lukkeorgan og forstøver lang levetid på trods af det høje temperaturniveau .It will be seen that the primary valve seat is located in the cooled valve section, while both the closing member 32 and the upper portion of the bore section 29 are located in the uncooled valve section 1b. Since the closure member 32 does not substantially burden the nebulizer material with longitudinal forces 30, both the closure member and nebulizer have a long service life despite the high temperature level.
I den efterfølgende beskrivelse af andre udførelsesformer anvendes samme henvisningstal som ovenfor for 35 elementer med samme funktion.In the following description of other embodiments, the same reference numerals as above are used for 35 elements having the same function.
11 DK 171975 B111 DK 171975 B1
Den i fig. 2 og 3 viste anden udførelsesform for brændselsinjektoren er også til en motor, der anvender olie som brændsel. Ventilgliderens tynde nedre afsnit 30 er her en separat udskiftelig enhed, der ved sin øvre 5 ende har udvendigt gevind, der er skruet op i et indvendigt gevind i en central boring 40 ved den nedre ende af ventilgliderens øvre afsnit, indtil en krave 41 på det nedre afsnit 30 ligger an mod det øvre afsnits endeflade. En sikringsstift 45 indsat i flugtende 10 boringer i gliderens øvre og nedre afsnit drejnings-fikserer det nedre afsnit 30 til gliderens øvre afsnit.The FIG. 2 and 3, the second embodiment of the fuel injector is also for an engine that uses oil as fuel. The thin lower section 30 of the valve slide is here a separate interchangeable unit having at its upper end an external thread screwed up into an inner thread in a central bore 40 at the lower end of the upper section of the valve slide until a collar 41 on it the lower section 30 abuts the end surface of the upper section. A locking pin 45 inserted into flushing 10 bores in the upper and lower sections of the slider rotates the lower section 30 to the upper section of the slider.
Hvis det nedre gliderafsnit 30 bliver slidt eller beskadiget, kan sikringsstiften 45 udtages, og det nedre afsnit 30 kan udskiftes med et nyt. Derved undgås 15 udskiftning af hele glideren.If the lower slide section 30 becomes worn or damaged, the lock pin 45 can be removed and the lower section 30 can be replaced with a new one. This avoids 15 replacement of the entire slide.
Det nedre afsnit 30 er langstrakt, tyndt og fleksibelt i tværretningen bedømt i forhold til ventilgliderens øvre afsnit. Når glideren står i lukkestillingen vist i fig. 3 rager lukkeorganet 32, dannet af 20 det forreste cylindriske stykke af afsnittet 30, ned i boringsafsnittet 29 og hindrer olien i det øvre boringsafsnit 22 i at trænge ned til forstøverhullerne 24. Oliemængden i boringsafsnittet 29 under spidsen af ventilglideren udgør omkring 10% af den totale oliemæng-25 de, der befinder sig under det primære ventilsæde 18.The lower section 30 is elongated, thin and flexible in the transverse direction judged in relation to the upper section of the valve slider. When the slider is in the closing position shown in FIG. 3, the closure member 32 formed by the front cylindrical portion of section 30 projects into the bore section 29 and prevents the oil in the upper bore section 22 from penetrating to the atomizer holes 24. The amount of oil in the bore section 29 below the tip of the valve slider constitutes about 10% of that. total oil volumes under the primary valve seat 18.
Lukkeorganet 32 er centreret i forstøverboringen ved hjælp af et styr 42, der glider langs en styreflade 43 i forstøverboringen. Styret 42 består af flere, eksempelvis fire radialt udstående, langsgående flige, 30 hvis øvre og nedre ender er tilspidsede. Olien kan strømme forbi styret 42 gennem de langsgående mellemrum mellem fligene.The closure means 32 is centered in the nebulizer bore by means of a guide 42 sliding along a guide surface 43 in the nebulizer bore. The guide 42 consists of several, for example, four radially extending longitudinal tabs 30, the upper and lower ends of which are pointed. The oil can flow past guide 42 through the longitudinal spaces between the tabs.
I fig. 2 ses ventilglideren 15 i sin fuldt åbne stilling, hvor olien strømmer forbi det primære ventil-35 sæde 18 og ned i forstøverboringen, hvor olien i området 12 DK 171975 B1 23 med mindskende diameter passerer forbi ventilgliderens koniske frie ende 44 og strømmer videre ned til forstøverhullerne 24 som en samlet strømning, der dækker hele forstøverboringens tværsnit. Afstanden mellem 5 gliderens frie ende 44 og forstøverhullerne er antagelig tilstrækkelig stor til, at oliestrømningen ind i forstøverhullerne i det væsentlige er upåvirket af, at gliderens nedre afsnit 30 strækker sig langt ned i fortøverboringen.In FIG. 2, the valve slide 15 is seen in its fully open position where the oil flows past the primary valve seat 18 and down into the nebulizer bore, where the oil in the area of decreasing diameter passes past the tapered free end 44 of the valve slide and flows further down to the nebulizer holes 24 as a total flow covering the entire cross-section of the nebulizer bore. The distance between the free end 44 of the slider and the nebulizer holes is probably large enough that the oil flow into the nebulizer holes is substantially unaffected by the lower portion 30 of the slider extending far down into the nebulizer bore.
10 Antallet af forstøverhuller 24 i spidsen af forstøveren afhænger af den effekt, som motorens arbejdscylinder skal yde og af antallet af injektorer pr. cylinder. Der kan eksempelvis være 4 eller 5 forstøverhuller, som alle udmunder på samme side af 15 forstøveren, så længdeakserne for de to yderste forstøverhuller indbyrdes højst danner en vinkel på 100° og ofte på kun 80° eller mindre. Olien forstøves således ud i en vifteformet byge af finfordelte oliepartikler.The number of nebulizer holes 24 at the tip of the nebulizer depends on the power that the working cylinder of the engine is to produce and the number of injectors per unit. cylinder. For example, there may be 4 or 5 nebulizer holes, all of which open on the same side of the nebulizer, so that the longitudinal axes of the two outer nebulizer holes form at most an angle of 100 ° and often of only 80 ° or less. Thus, the oil is atomized into a fan-shaped burst of finely divided oil particles.
Herefter beskrives injektorer til indsprøjtning af 20 gasformigt brændsel. Injektorerne er i princippet opbygget på samme måde som ovenfor beskrevet bortset fra, at ventilglideren løftes ved hjælp af styreolie, som påvirker et dertil indrettet stempelareal på glideren, og at gassen tilledes sideværts ind i den 25 nedre del af ventilhuset gennem en tilgangskanal 50 i dækslet antydet ved 51 og en skråkanal 52 i ventilhuset 33.Next, injectors for injecting 20 gaseous fuel are described. The injectors are in principle constructed in the same manner as described above except that the valve slide is lifted by means of control oil which affects a piston area thereon and the gas is fed laterally into the lower part of the valve housing through an inlet channel 50 in the cover. indicated at 51 and an inclined channel 52 in the valve body 33.
Skråkanalen 52 udmunder i et trykkammer 53, der ligger umiddelbart over det primære ventilsæde 18.The oblique duct 52 opens into a pressure chamber 53 located immediately above the primary valve seat 18.
30 Opbygningen og virkemåden af en sådan gasinjektor er iøvrigt velkendt i teknikken. Injektoren skal indsprøjte et forholdsvis stort gasvolumen i løbet af en motorcyklus. Strømningspassagerne i injektoren må derfor have passende stort tværsnitsareal, hvilket betyder at 35 forstøverboringen og dermed også selve forstøveren får 13 DK 171975 B1 stor diameter. Injektorens anlægsflade 31', der presses an .mod en kølende konisk flade på dækslet 51 er derfor udformet på selve forstøveren 4, så injektorhusets yderdiameter kan holdes passende lille. Det fremgår 5 iøvrigt af fig. 4, at dækslet nær fladen 54 har kølekanaler 55. Den under anlægsfladen 31’ beliggende del af forstøveren påvirkes af det meget høje temperaturniveau i forbrændingskammeret 56 og er i praksis ukølet.The construction and operation of such a gas injector is otherwise well known in the art. The injector must inject a relatively large volume of gas during a motor cycle. The flow passages in the injector must therefore have a suitably large cross-sectional area, which means that the nebulizer bore and thus also the nebulizer itself has a large diameter. The injector abutment surface 31 ', which is pressed against a cooling conical surface on the cover 51, is therefore formed on the nebulizer 4 itself, so that the outer diameter of the injector housing can be kept suitably small. It can be seen otherwise in FIG. 4, that the cover near the surface 54 has cooling ducts 55. The part of the nebulizer located below the abutment surface 31 'is affected by the very high temperature level in the combustion chamber 56 and is in practice uncooled.
Da gassen er væsentlig mere letstrømmende end olie, 10 og forstøverboringerne har væsentlig større diameter end i de ovennævnte udførelsesformer, er det mest hensigtsmæssigt, at lukkeorganet på ventilgliderens nedre afsnit 30 ligger an mod en konisk skråflade 57 i boringens område med nedefter mindskende diameter. Lukkeorganet 15 kan være en ventilnål 58, som vist i fig. 4 og 5, eller en kugleformet ventildel 59, som vist i fig. 6 og 7.Since the gas is substantially more flowable than oil, 10 and the nebulizer bores are substantially larger in diameter than in the above embodiments, it is most convenient that the closure member of the lower section 30 of the valve slider abuts against a tapered bevel surface 57 in the downwardly decreasing diameter bore. The closure member 15 may be a valve needle 58, as shown in FIG. 4 and 5, or a spherical valve member 59, as shown in FIG. 6 and 7.
Lukkeorganet trykkes ikke mod skråfladen 57 med en ventillukkekraft af samme størrelsesorden som lukkekraften virkende på det primære ventilsæde 18, men er kun 20 påvirket mod lukket stilling af en svag trykfjeder. Der kan eksempelvis være tale om en trykfjeder 61, som ligger optaget i et hulrum i ventilgliderens øvre afsnit og trykker på hele det nedre gliderafsnit 30, der er forskydeligt lejret i en central boring i det øvre 25 afsnit, eller der kan være tale om en trykfjeder 60 (se fig. 6 og 7), der ligger omkring det nedre gliderafsnit 30 og påvirker ventildelen 59, der er længdeforskydeligt lejret på det nedre afsnit 30.The closing means is not pressed against the inclined surface 57 with a valve closing force of the same magnitude as the closing force acting on the primary valve seat 18, but is only 20 actuated against the closed position by a weak compression spring. For example, it may be a compression spring 61 which is accommodated in a cavity in the upper section of the valve slide and presses the entire lower slide section 30 slidably mounted in a central bore in the upper 25 section, or it may be a compression spring 60 (see Figs. 6 and 7) located around the lower slider section 30 and actuates the valve member 59 longitudinally slidably mounted on the lower section 30.
Det i fig. 4 og 5 viste forskydeligt lejrede 30 gliderafsnit 30 bærer den ene part af en bajonetkobling, fx flere udragende flige ved sin øvre ende. Disse flige kan føres op gennem modsvarende noter i enden af ventilgliderens øvre afsnit. Når fligene er ført op i hulrummet, kan det nedre afsnit drejes til sin monterede 35 stilling, hvor fligenes underside ved anlæg mod bunden 14 DK 171975 B1 af hulrummet virker som stop for den nedovergående forskydning af afsnittet 30 i forhold til ventilgliderens øvre afsnit.The FIG. 4 and 5, slidably 30 sliding sections 30 shown carry one portion of a bayonet coupling, e.g., several projecting tabs at its upper end. These tabs can be brought up through corresponding notes at the end of the upper section of the valve slide. When the tabs are raised into the cavity, the lower section can be rotated to its mounted position, where the underside of the tabs upon abutment to the bottom 14 acts as a stop for the downward displacement of the section 30 relative to the upper section of the valve slide.
Ventildelen 59 vist i fig. 6 og 7 er begrænset i 5 sin forskydning bort fra ventilgliderens øvre afsnit af et stop i form af en krave 62, der griber ind over et fortykket nederste parti af gliderafsnittet 30.The valve member 59 shown in FIG. 6 and 7 are restricted in their displacement away from the upper portion of the valve slide by a stop in the form of a collar 62 which engages over a thickened lower portion of the slide section 30.
Det er klart, at elementer fra de forskellige beskrevne udførelsesformer kan kombineres på forskellig 10 vis til nye udførelsesformer.It is to be understood that elements of the various embodiments described can be combined in various ways for new embodiments.
Claims (10)
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DK015694A DK171975B1 (en) | 1994-02-07 | 1994-02-07 | Fuel injector for a large two-stroke internal combustion engine |
EP95909652A EP0744007B1 (en) | 1994-02-07 | 1995-02-06 | A fuel injector for a large two-stroke internal combustion engine |
JP07520326A JP3081646B2 (en) | 1994-02-07 | 1995-02-06 | Fuel injection system for large two-stroke internal combustion engine |
HR0156/94A HRP950053B1 (en) | 1994-02-07 | 1995-02-06 | Fuel injector for a large two stroke internal combustion engine |
ES95909652T ES2109094T3 (en) | 1994-02-07 | 1995-02-06 | FUEL INJECTOR FOR AN INTERNAL COMBUSTION ENGINE OF TWO TIMES OF LARGE DIMENSIONS. |
KR1019960703079A KR100335666B1 (en) | 1994-02-07 | 1995-02-06 | A fuel injector for a large two - stroke internal combustion engine |
CN95191514A CN1057366C (en) | 1994-02-07 | 1995-02-06 | Fuel injector for large two-stroke IC engine |
PCT/DK1995/000053 WO1995021324A1 (en) | 1994-02-07 | 1995-02-06 | A fuel injector for a large two-stroke internal combustion engine |
DE69500921T DE69500921T2 (en) | 1994-02-07 | 1995-02-06 | FUEL INJECTION VALVE FOR A LARGE TWO-STROKE COMBUSTION ENGINE |
PL95315808A PL175740B1 (en) | 1994-02-07 | 1995-02-06 | Fuel injector for a large two-stroke internal combustion engine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DK15694 | 1994-02-07 | ||
DK015694A DK171975B1 (en) | 1994-02-07 | 1994-02-07 | Fuel injector for a large two-stroke internal combustion engine |
Publications (2)
Publication Number | Publication Date |
---|---|
DK15694A DK15694A (en) | 1995-08-08 |
DK171975B1 true DK171975B1 (en) | 1997-09-01 |
Family
ID=8090392
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DK015694A DK171975B1 (en) | 1994-02-07 | 1994-02-07 | Fuel injector for a large two-stroke internal combustion engine |
Country Status (10)
Country | Link |
---|---|
EP (1) | EP0744007B1 (en) |
JP (1) | JP3081646B2 (en) |
KR (1) | KR100335666B1 (en) |
CN (1) | CN1057366C (en) |
DE (1) | DE69500921T2 (en) |
DK (1) | DK171975B1 (en) |
ES (1) | ES2109094T3 (en) |
HR (1) | HRP950053B1 (en) |
PL (1) | PL175740B1 (en) |
WO (1) | WO1995021324A1 (en) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DK174075B1 (en) * | 1996-06-20 | 2002-05-21 | Man B & W Diesel As | Fuel injector for an internal combustion engine |
EP0961024B1 (en) * | 1998-05-29 | 2010-01-13 | Wärtsilä Schweiz AG | Fuel injection nozzle |
WO2000006891A1 (en) * | 1998-07-24 | 2000-02-10 | Man B & W Diesel A/S | A fuel valve for an internal combustion engine |
DE10019153A1 (en) * | 2000-04-18 | 2001-10-25 | Bosch Gmbh Robert | Fuel injection valve for IC engines has valve bore with valve member and valve piston loaded by hydraulic closing force to engage on valve member |
DE10129308C1 (en) * | 2001-06-18 | 2002-11-28 | Man B & W Diesel As Kopenhagen | Fuel feed device for 2-stroke diesel engine used for e.g., for a ships drive, has at least one valve closure of fuel injection valves for each engine cylinder de-activated at partial load by associated control piston |
DE502004009930D1 (en) * | 2003-07-17 | 2009-10-01 | Ganser Hydromag | FUEL INJECTION VALVE FOR INTERNAL COMBUSTION ENGINES |
JP2005315101A (en) * | 2004-04-27 | 2005-11-10 | Isuzu Motors Ltd | Gas fuel injection valve |
CN100351512C (en) * | 2004-07-15 | 2007-11-28 | 于魁江 | Electric control oil atomizer |
JP4161974B2 (en) * | 2005-03-28 | 2008-10-08 | トヨタ自動車株式会社 | Control device for diesel internal combustion engine |
JP5312148B2 (en) * | 2009-03-30 | 2013-10-09 | 株式会社ケーヒン | Fuel injection valve |
CN104093968B (en) * | 2012-02-07 | 2016-10-12 | 甘瑟-许德罗玛格股份公司 | Fuelinjection nozzle and for spraying the device of fuel |
DE102012208087B4 (en) * | 2012-05-15 | 2024-03-14 | Man Energy Solutions Se | Fuel injector |
DK178692B1 (en) * | 2015-04-22 | 2016-11-21 | Man Diesel & Turbo Filial Af Man Diesel & Turbo Se Tyskland | A fuel valve for a large two-stroke self-igniting internal combustion engine |
CN106321315A (en) * | 2016-11-24 | 2017-01-11 | 余姚市舒春机械有限公司 | Marine high-power diesel engine injection device |
DK179146B1 (en) * | 2016-12-13 | 2017-12-04 | Man Diesel & Turbo Filial Af Man Diesel & Turbo Se Tyskland | Nozzle for fuel valve for injecting fuel into the cylinders of a large turbocharged two-stroke compression-ignited internal combustion engineand and an engine therefore |
DK179281B1 (en) * | 2016-12-13 | 2018-04-03 | Man Diesel & Turbo Filial Af Man Diesel & Turbo Se Tyskland | Nozzle for fuel valve for injecting fuel into the cylinders of a large turbocharged two-stroke compression-ignited internal combustion engine |
SE540338C2 (en) * | 2016-12-22 | 2018-07-10 | Scania Cv Ab | Fuel injector |
DK180809B1 (en) * | 2020-12-09 | 2022-04-07 | Man Energy Solutions Filial Af Man Energy Solutions Se Tyskland | Internal combustion engine |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2837606A1 (en) * | 1978-08-29 | 1980-03-06 | Daimler Benz Ag | Multi-jet fuel injector for Diesel IC engine - has pre-injection chamber with member controlling nozzle ducts on spring-loaded piston inside injector needle |
JPS58113575A (en) * | 1981-12-28 | 1983-07-06 | Komatsu Ltd | Fuel injector in engine |
IT1240173B (en) * | 1990-04-06 | 1993-11-27 | Weber Srl | ELECTROMAGNETICALLY OPERATED FUEL INJECTION DEVICE FOR AN INTERNAL COMBUSTION ENGINE |
DE4025945C2 (en) * | 1990-08-16 | 1998-10-08 | Bosch Gmbh Robert | Method of adjusting a fuel injector and fuel injector |
DK167502B1 (en) * | 1991-10-04 | 1993-11-08 | Man B & W Diesel Gmbh | FUEL ENGINE FOR COMBUSTION ENGINES |
-
1994
- 1994-02-07 DK DK015694A patent/DK171975B1/en not_active IP Right Cessation
-
1995
- 1995-02-06 EP EP95909652A patent/EP0744007B1/en not_active Expired - Lifetime
- 1995-02-06 JP JP07520326A patent/JP3081646B2/en not_active Expired - Fee Related
- 1995-02-06 ES ES95909652T patent/ES2109094T3/en not_active Expired - Lifetime
- 1995-02-06 HR HR0156/94A patent/HRP950053B1/en not_active IP Right Cessation
- 1995-02-06 KR KR1019960703079A patent/KR100335666B1/en not_active IP Right Cessation
- 1995-02-06 CN CN95191514A patent/CN1057366C/en not_active Expired - Fee Related
- 1995-02-06 DE DE69500921T patent/DE69500921T2/en not_active Expired - Fee Related
- 1995-02-06 WO PCT/DK1995/000053 patent/WO1995021324A1/en active IP Right Grant
- 1995-02-06 PL PL95315808A patent/PL175740B1/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
CN1057366C (en) | 2000-10-11 |
WO1995021324A1 (en) | 1995-08-10 |
PL315808A1 (en) | 1996-12-09 |
DK15694A (en) | 1995-08-08 |
DE69500921T2 (en) | 1998-03-12 |
ES2109094T3 (en) | 1998-01-01 |
HRP950053A2 (en) | 1997-02-28 |
PL175740B1 (en) | 1999-02-26 |
DE69500921D1 (en) | 1997-11-27 |
KR960706605A (en) | 1996-12-09 |
EP0744007B1 (en) | 1997-10-22 |
EP0744007A1 (en) | 1996-11-27 |
JP3081646B2 (en) | 2000-08-28 |
JPH09508456A (en) | 1997-08-26 |
CN1140483A (en) | 1997-01-15 |
HRP950053B1 (en) | 1998-12-31 |
KR100335666B1 (en) | 2002-11-23 |
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