EP2499350B1 - Method of manufacturing a fuel injector - Google Patents

Method of manufacturing a fuel injector Download PDF

Info

Publication number
EP2499350B1
EP2499350B1 EP10762648.3A EP10762648A EP2499350B1 EP 2499350 B1 EP2499350 B1 EP 2499350B1 EP 10762648 A EP10762648 A EP 10762648A EP 2499350 B1 EP2499350 B1 EP 2499350B1
Authority
EP
European Patent Office
Prior art keywords
control chamber
valve needle
valve
volume
fuel
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.)
Not-in-force
Application number
EP10762648.3A
Other languages
German (de)
French (fr)
Other versions
EP2499350A1 (en
Inventor
Susanne Spindler
Stephan Amelang
Matthias Burger
Christian Faltin
Hans-Christoph Magel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
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 Robert Bosch GmbH filed Critical Robert Bosch GmbH
Publication of EP2499350A1 publication Critical patent/EP2499350A1/en
Application granted granted Critical
Publication of EP2499350B1 publication Critical patent/EP2499350B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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
    • F02M47/00Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure
    • F02M47/02Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure of accumulator-injector type, i.e. having fuel pressure of accumulator tending to open, and fuel pressure in other chamber tending to close, injection valves and having means for periodically releasing that closing pressure
    • F02M47/027Electrically actuated valves draining the chamber to release the closing pressure
    • 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
    • F02M61/168Assembling; Disassembling; Manufacturing; Adjusting
    • 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
    • F02M2200/80Fuel injection apparatus manufacture, repair or assembly
    • F02M2200/8084Fuel injection apparatus manufacture, repair or assembly involving welding or soldering
    • 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
    • F02M2200/80Fuel injection apparatus manufacture, repair or assembly
    • F02M2200/8092Fuel injection apparatus manufacture, repair or assembly adjusting or calibration
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49405Valve or choke making
    • Y10T29/49412Valve or choke making with assembly, disassembly or composite article making
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49405Valve or choke making
    • Y10T29/49412Valve or choke making with assembly, disassembly or composite article making
    • Y10T29/49425Valve or choke making with assembly, disassembly or composite article making including metallurgical bonding

Definitions

  • the invention relates to a method for producing a fuel injection valve according to the preamble of claim 1.
  • injector Such a method for producing a fuel injection valve (hereinafter also referred to in part as "injector”) is already well known and is used in particular in fuel injection valves in so-called common-rail injection systems. Hub-controlled common-rail injectors whose nozzle needle is servo-operated are known. Piezo and solenoid valves are used as pressure actuators, with which the servo circuit is controlled. For fast closing of the valve needle is often installed a permanent low-pressure stage, which exerts a permanent, closing force on the valve needle.
  • the disadvantage here is the relatively high leakage that occurs between the high and the low pressure side. Leakage inevitably results in a higher pumping capacity required in the common rail injection system and thus in system efficiency. This situation becomes problematic especially at higher pressures.
  • the latest injectors for highest injection pressures are designed low leakage, by dispensing with the low pressure stage. Due to the absence of the low-pressure stage, however, only low closing forces are available for the valve needle. As a result, the response time between the control of the valve needle and the start of injection relatively low. The response time is mainly dependent on the stiffness of the valve needle. Precisely because it is small in an injector without low-pressure stage, even a slight change in the needle stiffness leads to a large shift in the start of injection and the amount of fuel injected. The stiffness of the valve needle depends on the diameter and length of the valve needle.
  • the invention has the object, a method for producing a fuel injection valve according to the preamble of claim 1 such that the response time at fuel valves of different length or different length of their valve needles is at least substantially constant.
  • This object is achieved in a method for producing a fuel injection valve having the features of claim 1.
  • the invention is based on the idea to compensate for the different mechanical stiffness due to different lengths of the valve needles by a variation of the "hydraulic stiffness" of the valve connected to the valve needle in operative connection control space. This is based on the knowledge that the larger the volume is formed in the control chamber, the greater the delay or the response time until the injection openings are opened. In other words, this means that a relatively short and thus stiff valve needle is thereby compensated by being connected to a control chamber in operative connection, which has a relatively large storage volume of fuel and vice versa.
  • the valve needle consists of at least one arranged in the control chamber, standardized first portion which is connected on the side facing away from the control chamber with a second cylindrical portion and that the diameter of the second portion of the valve needle is varied, such that Shortening of the delay time increases the diameter of the valve needle and is reduced to an extension of the delay time of the diameter of the valve needle.
  • valve needles it is particularly advantageous to limit the number of possible different diameters of the valve needles if the diameter of the valve needle is varied in diameter steps and that fine adjustment of the delay time is achieved by adjusting the volume of the control chamber via a variation of the length of the second cylindrical section , It takes place hereby a combination of a valve needle with a certain diameter with a valve needle of a certain length, such that the in the control room protruding portion of the standardized first section forms a certain control volume.
  • connection between at least the second section of the valve needle and the standardized first section and optionally between the second section of the valve needle and the third section is preferably carried out by laser welding. As a result, high-strength compounds can be produced relatively economically.
  • Fuel valves produced in accordance with the inventive method can be produced particularly economically with respect to their overall length if the injector housing of the fuel injection valve has a standardized upper part with the closing element, an actuating mechanism for the closing element and optionally the valve piece and a standardized lower part with a nozzle body, and that between the Upper part and the lower part a total length of the injector housing defining central part is arranged.
  • a first fuel injection valve 10 is shown, as used in particular in so-called common-rail injection systems use.
  • the fuel injection valve 10 is connected via a supply line 1 with a fuel storage, a so-called rail 2, in connection.
  • the rail 2 is stored under high pressure, for example, a pressure of about 2000 bar, standing fuel.
  • the rail 2 is connected to a high-pressure fuel pump 3, which sucks and compresses fuel from a fuel reservoir, in particular a fuel tank 4.
  • Fuel not required by the fuel injection valve 10 is returned to the fuel tank 4 via a return line 5 under low pressure.
  • a fuel injection system 7 described so far has a separate fuel injection valve 10 for each cylinder of an internal combustion engine, all of which are connected to the rail 2.
  • the fuel injection valve 10 has a generally designated 11 injector housing.
  • the elongated injector housing 11 consists of three modules, a standardized upper part 12, a dependent on the length of the fuel injector 10, in particular annular, possibly formed with different diameters middle part 13 and a likewise standardized lower part 14.
  • a sealing ring 15 is inserted in a sealing groove, wherein the pressure-resistant connection between the central part 13 and the upper part 12, for example, by a circumferential laser welding or by a circumferential beading.
  • a screw connection 18 is formed in order to connect the middle part 13 to the lower part 14 in a pressure-resistant manner.
  • a pressure-balanced solenoid valve 20 is used or arranged, which has a magnetic core 21 and arranged in the magnetic core 21 magnetic coil 22.
  • the solenoid valve 20 also has a magnetic armature acting as a closing element 23, which is guided in an axially movable manner in a pin-shaped guide member 24.
  • the guide member 24 is disposed in a through hole 25 of the magnetic core 21 and has a step 26, between which and the facing side of the armature 23, a compression spring 28 is supported.
  • the compression spring 28 is in this case arranged in a spring chamber 29 which, like the region of the upper part 12 in which the magnetic core 21 is located, is connected at least indirectly to the return line 5 and thus to low pressure.
  • the armature 23 is pressed in the de-energized state of the solenoid 22 against a seat 30 of a valve member 32.
  • the valve member 32 is screwed into an upper portion of the central part 13 and in this case sits on a step 33 of the central part 13.
  • a through hole 34 is arranged with a flow restrictor 35.
  • the outflow throttle 35 is connected to a control chamber 37, which is formed as a blind hole 38 on the magnet armature 23 opposite side of the valve member 32.
  • In the blind hole 38 projects on the Abströmdrossel 35 opposite, open end, a first guide portion 39 of a valve needle 40 into it.
  • the substantially cylindrically shaped valve needle 40 has, at its end opposite the valve piece 32, a second guide section 41, to which a valve tip 42 adjoins.
  • a compression spring 43 which is supported between a collar 44 of the valve needle 40 and the facing end face of the valve member 32, the valve tip 42 is pressed against a seat 46 of a nozzle body 47.
  • the seat 46 defines a nozzle space 48, in FIG the at least one serving as a fuel outlet opening 49 through hole opens.
  • the nozzle body 47 is in this case inserted into the lower part 14 of the injector housing 11.
  • the outflow of the fuel from the control chamber 37 causes the valve needle 40 lifts from its seat 46, and fuel from the high pressure storage chamber 52 and the nozzle chamber 48 through the fuel outlet opening 49 flows out of the fuel injection valve 10 via the inlet line 1 and into the combustion chamber the internal combustion engine is discharged.
  • the valve needle 40 Due to its length L 1 and its material and thus its modulus of elasticity and its cross-sectional area A, the valve needle 40 has a certain rigidity. In the de-energized state of the solenoid valve 20, the valve needle 40 is pressed against the seat 46, wherein an elastic deformation of the valve needle 40 due to the material properties described above and the geometry of the valve needle 40 sets.
  • a fuel injection valve 10 a is shown, which differs from that in the Fig. 1 illustrated fuel injector 10 differs in that it has a total of a smaller overall length.
  • the smaller length is achieved by reducing or shortening the central part 13, while the lower part 14 and the upper part 12 are each formed as standardized components, which are present both in the fuel injection valve 10 and the fuel injection valve 10a in an identical manner.
  • the other, not directly with the central part 13 and the valve needle 40 operatively connected components in an identical manner are present.
  • the fuel injection valve 10a differs from the fuel injection valve 10 only in the length of the central part 13 and in the length of the valve needle 40a.
  • the fuel injection valve 10a with respect to the valve needle 40a has a lower response time, (provided that the valve needle 40 and the valve needle 40a from the same Material and have the same cross-sectional area A), the length L 2 of the valve needle 40a with respect to the length L 1 of the valve needle 40 is lower. This would thus also lead overall to a shortened drive time t of the fuel injection valve 10a.
  • the part of the activation time t which is influenced by the volume of the control chamber 37, is increased in the fuel injection valve 10a relative to the fuel injection valve 10. This is done by increasing the volume of the control chamber 37 such that the projecting into the control chamber 37 guide portion 39a of the valve needle 40a is reduced in its length. In other words, this means that the shortening of the drive time t due to the small length L 2 of the valve needle 40a is compensated by an extension of the proportion of the drive time t due to the increased volume of the control space 37.
  • a third fuel injection valve 60 and a fourth fuel injection valve 60a are shown.
  • the fuel injection valves 60, 60a differ from the fuel injection valves 10, 10a through the use of a differently constructed valve needle 62, 62a.
  • the valve needles 62 and 62a are each formed in three parts.
  • Each of the valve needles 62, 62a consists of a standardized, protruding into the control chamber 37 upper part 63 and a standardized lower part 64, which carries the second guide portion 41 and the valve tip 42.
  • the upper part 63 and the lower part 64 are interconnected by means of a cylindrically shaped middle part 65, 65a.
  • the laser welding is preferably used as connection technology between the middle part 65, 65a and the upper part 63 or between the middle part 65, 65a and the lower part 64.
  • the middle part 65 has a larger diameter D 1 , as the central part 65a with the diameter D 2nd
  • the central part 65 has a larger cross-sectional area A 1 than the central part 65 a with the cross-sectional area A 2 .
  • the driving time t in the fuel injection valves 60, 60a mainly by a variation of the diameter D or the cross-sectional area A of the central part 65, 65a influenced.
  • the different diameters D of the middle parts 65, 65a are present only in stages for reducing the variety of types, ie that only a limited number of diameters D is provided or are present in the production for mounting fuel injection valves 60, 60a ,
  • a coarse adjustment of the activation times t is effected via the variation or selection of the middle parts 65, 65a.
  • the smaller diameter D is always used. This has the consequence that (compared to the larger diameter D), the volume of the control chamber 37 is smaller, to compensate for the lower rigidity of the equipped with the relatively smaller diameter D middle part 65.
  • the fine tuning with respect to the actuation time t takes place at the selected diameter D now by a corresponding reduction or reduction of the length of the central part 65, 65 a in such a way that the region of the upper part 63, which is located in the valve piece 32, projects somewhat less into the control chamber 37.
  • the fuel injection valves 10, 10a and 60, 60a described so far can be modified or modified in a variety of ways.
  • the magnet assembly or the solenoid valve 20 may be constructed differently or replaced by a piezo.
  • the design of the fuel injection valves 10, 10a, 60, 60a can take place so that the solenoid valve 20 can already be closed again before the injection begins or the through-bore 34 is released. In this way, variations between successive injections and Jacobruckjankeiten can be reduced.

Description

Stand der TechnikState of the art

Die Erfindung betrifft ein Verfahren zum Herstellen eines Kraftstoffeinspritzventils nach dem Oberbegriff des Anspruchs 1.The invention relates to a method for producing a fuel injection valve according to the preamble of claim 1.

Ein derartiges Verfahren zum Herstellen eines Kraftstoffeinspritzventils (im Folgenden auch teilweise als "Injektor" bezeichnet) ist bereits allgemein bekannt und wird insbesondere bei Kraftstoffeinspritzventilen in so genannten Common-Rail-Einspritzsystemen angewandt. Bekannt sind dabei hubgesteuerte Common-Rail-Injektoren, deren Düsennadel servobetrieben ist. Als Drucksteller sind Piezo- und Magnetventile im Einsatz, mit denen der Servokreislauf gesteuert wird. Zum schnellen Schließen der Ventilnadel wird häufig eine dauerhafte Niederdruckstufe eingebaut, die eine permanente, schließende Kraft auf die Ventilnadel ausübt. Der Nachteil hierbei ist jedoch die relativ hohe Leckage, die sich zwischen der Hoch- und der Niederdruckseite einstellt. Eine Leckage führt unweigerlich zu einer höheren Pumpenleistung, die in dem Common-Rail-Einspritzsystem benötigt wird, und somit zu Einbußen in der Effizienz des Systems. Dieser Sachverhalt wird besonders bei höheren Drücken problematisch.Such a method for producing a fuel injection valve (hereinafter also referred to in part as "injector") is already well known and is used in particular in fuel injection valves in so-called common-rail injection systems. Hub-controlled common-rail injectors whose nozzle needle is servo-operated are known. Piezo and solenoid valves are used as pressure actuators, with which the servo circuit is controlled. For fast closing of the valve needle is often installed a permanent low-pressure stage, which exerts a permanent, closing force on the valve needle. The disadvantage here, however, is the relatively high leakage that occurs between the high and the low pressure side. Leakage inevitably results in a higher pumping capacity required in the common rail injection system and thus in system efficiency. This situation becomes problematic especially at higher pressures.

Aus diesem Grund werden neueste Injektoren für höchste Einspritzdrücke (gemeint sind hier Drücke im Bereich von etwa 2000bar) leckagearm ausgeführt, indem auf die Niederdruckstufe verzichtet wird. Durch das Fehlen der Niederdruckstufe stehen jedoch nur geringe Schließkräfte für die Ventilnadel zur Verfügung. Dadurch ist die Ansprechzeit zwischen der Ansteuerung der Ventilnadel und dem Einspritzbeginn relativ gering. Die Ansprechzeit ist vor allem von der Steifigkeit der Ventilnadel abhängig. Gerade weil sie bei einem Injektor ohne Niederdruckstufe gering ist, führt bereits eine kleinste Änderung der Nadelsteifigkeit zu einer großen Verschiebung des Spritzbeginns und der eingespritzten Kraftstoffmenge. Die Steifigkeit der Ventilnadel ist vom Durchmesser und der Länge der Ventilnadel abhängig. Will man Injektoren verschiedener Baulänge bezüglich ihrer Ansprechzeit gleich ausbilden, so muss für jedes Muster bzw, jede Länge des Injektors eine entsprechende Taillierung bzw. Durchmesservariation der Ventilnadel ausgeführt werden. Auf diese Art und Weise kann die Steifigkeit der Ventilnadeln für alle Injektoren angeglichen werden. Dies hat jedoch relativ hohe Rüstzeiten zur Folge. Ideal wäre eine reine Variation der Nadellänge, während der Nadeldurchmesser für alle Injektorbaulängen gleich ist. Dies ist jedoch aufgrund der daraus begründeten Unterschiede in der Steifigkeit der Ventilnadeln nicht möglich.For this reason, the latest injectors for highest injection pressures (meaning here pressures in the range of about 2000bar) are designed low leakage, by dispensing with the low pressure stage. Due to the absence of the low-pressure stage, however, only low closing forces are available for the valve needle. As a result, the response time between the control of the valve needle and the start of injection relatively low. The response time is mainly dependent on the stiffness of the valve needle. Precisely because it is small in an injector without low-pressure stage, even a slight change in the needle stiffness leads to a large shift in the start of injection and the amount of fuel injected. The stiffness of the valve needle depends on the diameter and length of the valve needle. If you want to form injectors of different lengths equal in terms of their response time, so must be performed for each pattern or each length of the injector a corresponding sidecut or diameter variation of the valve needle. In this way, the stiffness of the valve needles can be adjusted for all injectors. However, this results in relatively high set-up times. Ideal would be a pure variation of the needle length, while the needle diameter is the same for all injector lengths. However, this is not possible due to the resulting differences in the stiffness of the valve needles.

Aus der US 6 213 098 B1 ist bekannt, bei der Herstellung eines Kraftstoffeinspritzventils das Volumen des Steuerraums zur Erzeugung der gewünschten Dynamik anzupassen.From the US 6 213 098 B1 It is known to adjust the volume of the control chamber to produce the desired dynamics in the manufacture of a fuel injection valve.

Offenbarung der ErfindungDisclosure of the invention

Ausgehend von dem dargestellten Stand der Technik liegt der Erfindung die Aufgabe zugrunde, ein Verfahren zum Herstellen eines Kraftstoffeinspritzventils nach dem Oberbegriff des Anspruchs 1 derart weiterzubilden, dass die Ansprechzeit bei Kraftstoffirentilen unterschiedlicher Baulänge bzw. unterschiedlicher Länge ihrer Ventilnadeln zumindest weitgehend konstant ist. Diese Aufgabe wird bei einem Verfahren zum Herstellen eines Kraftstoffeinspritzventils mit den Merkmalen des Anspruchs 1 gelöst. Der Erfindung liegt dabei die Idee zugrunde, die unterschiedliche mechanische Steifigkeit aufgrund unterschiedlicher Längen der Ventilnadeln durch eine Variation der "hydraulischen Steifigkeit" des mit der Ventilnadel in Wirkverbindung geschalteten Steuerraums auszugleichen. Hierbei liegt die Erkenntnis zugrunde, dass je größer das Volumen im Steuerraum ausgebildet ist, desto größer ist die Verzögerung bzw, die Ansprechzeit bis zum Öffnen der Einspritzöffnungen. Mit anderen Worten gesagt bedeutet dies, dass eine relativ kurze und somit steife Ventilnadel dadurch ausgeglichen wird, indem diese mit einem Steuerraum in Wirkverbindung geschaltet wird, welcher ein relativ großes Speichervolumen an Kraftstoff aufweist und umgekehrt.Based on the illustrated prior art, the invention has the object, a method for producing a fuel injection valve according to the preamble of claim 1 such that the response time at fuel valves of different length or different length of their valve needles is at least substantially constant. This object is achieved in a method for producing a fuel injection valve having the features of claim 1. The invention is based on the idea to compensate for the different mechanical stiffness due to different lengths of the valve needles by a variation of the "hydraulic stiffness" of the valve connected to the valve needle in operative connection control space. This is based on the knowledge that the larger the volume is formed in the control chamber, the greater the delay or the response time until the injection openings are opened. In other words, this means that a relatively short and thus stiff valve needle is thereby compensated by being connected to a control chamber in operative connection, which has a relatively large storage volume of fuel and vice versa.

Vorteilhafte Weiterbildungen des erfindungsgemäßen Verfahrens zum Herstellen eines Kraftstoffeinspritzventils sind in den Unteransprüchen angegeben. In den Rahmen der Erfindung fallen sämtliche Kombinationen aus zumindest zwei von in der Beschreibung, den Ansprüchen und/oder den Figuren offenbarten Merkmalen.Advantageous developments of the method according to the invention for producing a fuel injection valve are specified in the subclaims. All combinations of at least two features disclosed in the description, the claims and / or the figures fall within the scope of the invention.

Erfindungsgemäß ist vorgesehen, dass die Ventilnadel aus zumindest einem im Steuerraum angeordneten, standardisierten ersten Abschnitt besteht, welcher auf der der Steuerkammer abgewandten Seite mit einem zweiten zylindrischen Abschnitt verbunden wird und, dass der Durchmesser des zweiten Abschnitts der Ventilnadel variiert wird, derart, dass zur Verkürzung der Verzugszeit der Durchmesser der Ventilnadel vergrößert und zu einer Verlängerung der Verzugszeit der Durchmesser der Ventilnadel verkleinert wird.According to the invention, it is provided that the valve needle consists of at least one arranged in the control chamber, standardized first portion which is connected on the side facing away from the control chamber with a second cylindrical portion and that the diameter of the second portion of the valve needle is varied, such that Shortening of the delay time increases the diameter of the valve needle and is reduced to an extension of the delay time of the diameter of the valve needle.

Hierbei ist es zu einer Begrenzung der Anzahl der möglichen unterschiedlichen Durchmesser der Ventilnadeln besonders vorteilhaft, wenn der Durchmesser der Ventilnadel in Durchmesserstufen variiert wird und, dass eine Feinabstimmung der Verzugszeit über eine Anpassung des Volumens des Steuerraums über eine Variation der Länge des zweiten zylindrischen Abschnitts erfolgt. Es findet hiermit eine Kombination einer Ventilnadel mit einem bestimmten Durchmesser mit einer Ventilnadel einer bestimmten Länge statt, derart, dass der in den Steuerraum hineinragende Abschnitt des standardisierten ersten Abschnitts ein bestimmtes Steuervolumen ausbildet.In this case, it is particularly advantageous to limit the number of possible different diameters of the valve needles if the diameter of the valve needle is varied in diameter steps and that fine adjustment of the delay time is achieved by adjusting the volume of the control chamber via a variation of the length of the second cylindrical section , It takes place hereby a combination of a valve needle with a certain diameter with a valve needle of a certain length, such that the in the control room protruding portion of the standardized first section forms a certain control volume.

Darüber hinaus ist es besonders vorteilhaft, wenn unter Berücksichtigung des minimal und maximal möglichen Volumens des Steuerraums und der zur Verfügung stehenden Durchmesserstufen der Ventilnadeln derjenige Durchmesser der Ventilnadel ausgewählt wird, welcher zu einem minimalen Volumen des Steuerraums führt. Dies bedeutet, dass stets die Ventilnadel ausgewählt wird, welche den geringsten Durchmesser aufweist. Die weitere Anpassung der Verzugszeit wird somit über eine Verlängerung bzw. Verkürzung der Ventilnadel ausgeführt.Moreover, it is particularly advantageous if, taking into account the minimum and maximum possible volume of the control chamber and the available diameter stages of the valve needles that diameter of the valve needle is selected, which leads to a minimum volume of the control chamber. This means that always the valve needle is selected, which has the smallest diameter. The further adaptation of the delay time is thus carried out via an extension or shortening of the valve needle.

Eine besonders wirtschaftliche Herstellbarkeit der Kraftstoffventile ergibt sich darüber hinaus, wenn der zweite Abschnitt der Ventilnadel auf der dem standardisierten ersten Abschnitt gegenüberliegenden Seite mit einem standardisierten dritten Abschnitt verbunden ist.In addition, a particularly economic manufacturability of the fuel valves results when the second section of the valve needle is connected to a standardized third section on the side opposite the standardized first section.

Die Verbindung zwischen zumindest dem zweiten Abschnitt der Ventilnadel und dem standardisierten ersten Abschnitt sowie ggf. zwischen dem zweiten Abschnitt der Ventilnadel und dem dritten Abschnitt erfolgt bevorzugt durch Laserschweißen. Dadurch lassen sich hochfeste Verbindungen relativ wirtschaftlich herstellen.The connection between at least the second section of the valve needle and the standardized first section and optionally between the second section of the valve needle and the third section is preferably carried out by laser welding. As a result, high-strength compounds can be produced relatively economically.

Besonders wirtschaftlich lassen sich nach dem erfindungsgemäßen Verfahren hergestellte Kraftstoffventile bezüglich ihrer Baulänge herstellen, wenn das Injektorgehäuse des Kraftstoffeinspritzventils ein standardisiertes Oberteil mit dem Schließelement, einem Betätigungsmechanismus für das Schließelement und ggf. dem Ventilstück und ein standardisiertes Unterteil mit einem Düsenkörper aufweist und, dass zwischen dem Oberteil und dem Unterteil ein die Gesamtbaulänge des Injektorgehäuses bestimmendes Mittelteil angeordnet ist.Fuel valves produced in accordance with the inventive method can be produced particularly economically with respect to their overall length if the injector housing of the fuel injection valve has a standardized upper part with the closing element, an actuating mechanism for the closing element and optionally the valve piece and a standardized lower part with a nozzle body, and that between the Upper part and the lower part a total length of the injector housing defining central part is arranged.

Weitere Vorteile des erfindungsgemäßen Verfahrens zum Herstellen eines Kraftstoffeinspritzventils sowie des Kraftstoffventils ergeben sich aus der nachfolgenden Beschreibung bevorzugter Ausführungsbeispiele sowie anhand der Zeichnungen.Further advantages of the method according to the invention for producing a fuel injection valve and the fuel valve will become apparent from the following description of preferred embodiments and from the drawings.

Diese zeigen in:

Fig. 1 und 2
erfindungsgemäße erste Kraftstoffeinspritzventile, bei denen deren Injektorgehäuse eine maximale bzw. eine minimale Baulänge aufweist, jeweils im Längsschnitt und
Fig. 3 und 4
zweite erfindungsgemäße Kraftstoffeinspritzventile, bei denen die Injektorgehäuse eine maximale bzw. eine minimale Gesamtlänge aufweisen, ebenfalls im Längsschnitt.
These show in:
Fig. 1 and 2
Inventive first fuel injectors, wherein the injector has a maximum or a minimum length, respectively in longitudinal section and
3 and 4
second fuel injection valves according to the invention, in which the injector have a maximum or a minimum overall length, also in longitudinal section.

Gleiche Bauteile bzw. Bauteile mit gleicher Funktion sind in den Figuren mit derselben Bezugsziffer versehen.Identical components or components with the same function are provided in the figures with the same reference numeral.

In der Fig. 1 ist ein erstes Kraftstoffeinspritzventil 10 dargestellt, wie es insbesondere in sogenannten Common-Rail-Einspritzsystemen Verwendung findet. Hierbei steht das Kraftstoffeinspritzventil 10 über eine Zulaufleitung 1 mit einem Kraftstoffspeicher, einem sogenannten Rail 2, in Verbindung. In dem Rail 2 ist unter hohem Druck, beispielsweise einem Druck von etwa 2000bar, stehender Kraftstoff gespeichert. Hierbei steht das Rail 2 mit einer Kraftstoffhochdruckpumpe 3 in Verbindung, welche aus einem Kraftstoffspeicher, insbesondere einem Kraftstofftank 4, Kraftstoff ansaugt und verdichtet. Von dem Kraftstoffeinspritzventil 10 nicht benötigter Kraftstoff wird über eine unter niedrigem Druck stehende Rücklaufleitung 5 wieder dem Kraftstofftank 4 rückgeführt.In the Fig. 1 a first fuel injection valve 10 is shown, as used in particular in so-called common-rail injection systems use. Here, the fuel injection valve 10 is connected via a supply line 1 with a fuel storage, a so-called rail 2, in connection. In the rail 2 is stored under high pressure, for example, a pressure of about 2000 bar, standing fuel. In this case, the rail 2 is connected to a high-pressure fuel pump 3, which sucks and compresses fuel from a fuel reservoir, in particular a fuel tank 4. Fuel not required by the fuel injection valve 10 is returned to the fuel tank 4 via a return line 5 under low pressure.

Ein soweit beschriebenes Kraftstoffeinspritzsystem 7 weist für jeden Zylinder einer Brennkraftmaschine ein eigenes Kraftstoffeinspritzventil 10 auf, die allesamt mit dem Rail 2 verbunden sind.A fuel injection system 7 described so far has a separate fuel injection valve 10 for each cylinder of an internal combustion engine, all of which are connected to the rail 2.

Das Kraftstoffeinspritzventil 10 weist ein insgesamt mit 11 bezeichnetes Injektorgehäuse auf. Hierbei besteht das längliche Injektorgehäuse 11 aus drei Baugruppen, einem standardisierten Oberteil 12, einem von der Baulänge des Kraftstoffeinspritzventils 10 abhängigen, insbesondere ringförmig, ggf. mit unterschiedlichen Durchmessern ausgebildeten Mittelteil 13 und einem ebenfalls standardisierten Unterteil 14. Zwischen dem Oberteil 12 und dem Mittelteil 13 ist in einer Dichtungsnut ein Dichtring 15 eingesetzt, wobei die druckfeste Verbindung zwischen dem Mittelteil 13 und dem Oberteil 12 beispielsweise durch eine umlaufende Laserverschweißung oder durch ein umlaufendes Bördeln erfolgt. Demgegenüber ist zwischen dem Mittelteil 13 und dem Unterteil 14 unter Zwischenlage eines Dichtrings 17 beispielhaft eine Schraubverbindung 18 ausgebildet, um das Mittelteil 13 mit dem Unterteil 14 druckfest zu verbinden.The fuel injection valve 10 has a generally designated 11 injector housing. Here, the elongated injector housing 11 consists of three modules, a standardized upper part 12, a dependent on the length of the fuel injector 10, in particular annular, possibly formed with different diameters middle part 13 and a likewise standardized lower part 14. Between the upper part 12 and the middle part thirteenth a sealing ring 15 is inserted in a sealing groove, wherein the pressure-resistant connection between the central part 13 and the upper part 12, for example, by a circumferential laser welding or by a circumferential beading. In contrast, between the middle part 13 and the lower part 14 with the interposition of a sealing ring 17 by way of example a screw connection 18 is formed in order to connect the middle part 13 to the lower part 14 in a pressure-resistant manner.

In dem Oberteil 12 ist ein druckausgeglichenes Magnetventil 20 eingesetzt bzw. angeordnet, welches einen Magnetkern 21 sowie eine in dem Magnetkern 21 angeordnete Magnetspule 22 aufweist. Das Magnetventil 20 weist weiterhin einen als Schließelement wirkenden Magnetanker 23 auf, der in einem stiftförmigen Führungsglied 24 axial beweglich geführt ist. Das Führungsglied 24 ist in einer Durchgangsbohrung 25 des Magnetkerns 21 angeordnet und weist eine Stufe 26 auf, zwischen der und der zugewandten Seite des Magnetankers 23 sich eine Druckfeder 28 abstützt. Die Druckfeder 28 ist hierbei in einem Federraum 29 angeordnet, welcher ebenso wie der Bereich des Oberteils 12, in dem sich der Magnetkern 21 befindet, zumindest mittelbar mit der Rücklaufleitung 5 und somit mit Niederdruck verbunden ist.In the upper part 12, a pressure-balanced solenoid valve 20 is used or arranged, which has a magnetic core 21 and arranged in the magnetic core 21 magnetic coil 22. The solenoid valve 20 also has a magnetic armature acting as a closing element 23, which is guided in an axially movable manner in a pin-shaped guide member 24. The guide member 24 is disposed in a through hole 25 of the magnetic core 21 and has a step 26, between which and the facing side of the armature 23, a compression spring 28 is supported. The compression spring 28 is in this case arranged in a spring chamber 29 which, like the region of the upper part 12 in which the magnetic core 21 is located, is connected at least indirectly to the return line 5 and thus to low pressure.

Der Magnetanker 23 wird in unbestromtem Zustand der Magnetspule 22 gegen einen Sitz 30 eines Ventilstücks 32 gedrückt. Hierbei ist das Ventilstück 32 in einen oberen Abschnitt des Mittelteils 13 eingeschraubt und sitzt hierbei an einer Stufe 33 des Mittelteils 13 auf. In der Längsachse des Ventilstücks 32 ist eine Durchgangsbohrung 34 mit einer Abströmdrossel 35 angeordnet. Die Abströmdrossel 35 ist mit einem Steuerraum 37 verbunden, welcher als Sacklochbohrung 38 auf der dem Magnetanker 23 gegenüberliegenden Seite des Ventilstücks 32 ausgebildet ist. In die Sacklochbohrung 38 ragt auf der der Abströmdrossel 35 gegenüberliegenden, offenen Stirnseite ein erster Führungsabschnitt 39 einer Ventilnadel 40 hinein.The armature 23 is pressed in the de-energized state of the solenoid 22 against a seat 30 of a valve member 32. Here, the valve member 32 is screwed into an upper portion of the central part 13 and in this case sits on a step 33 of the central part 13. In the longitudinal axis of the valve piece 32, a through hole 34 is arranged with a flow restrictor 35. The outflow throttle 35 is connected to a control chamber 37, which is formed as a blind hole 38 on the magnet armature 23 opposite side of the valve member 32. In the blind hole 38 projects on the Abströmdrossel 35 opposite, open end, a first guide portion 39 of a valve needle 40 into it.

Die im Wesentlichen zylindrisch ausgebildete Ventilnadel 40 weist an ihrem dem Ventilstück 32 gegenüberliegenden Ende einen zweiten Führungsabschnitt 41 auf, an den sich eine Ventilspitze 42 anschließt. Mittels einer Druckfeder 43, die sich zwischen einem Bund 44 der Ventilnadel 40 und der zugewandten Stirnfläche des Ventilstücks 32 abstützt, wird die Ventilspitze 42 gegen einen Sitz 46 eines Düsenkörpers 47 gedrückt. Der Sitz 46 begrenzt einen Düsenraum 48, in den wenigstens eine als Kraftstoffaustrittsöffnung 49 dienende Durchgangsbohrung mündet. Der Düsenkörper 47 ist hierbei in das Unterteil 14 des Injektorgehäuses 11 eingesetzt.The substantially cylindrically shaped valve needle 40 has, at its end opposite the valve piece 32, a second guide section 41, to which a valve tip 42 adjoins. By means of a compression spring 43, which is supported between a collar 44 of the valve needle 40 and the facing end face of the valve member 32, the valve tip 42 is pressed against a seat 46 of a nozzle body 47. The seat 46 defines a nozzle space 48, in FIG the at least one serving as a fuel outlet opening 49 through hole opens. The nozzle body 47 is in this case inserted into the lower part 14 of the injector housing 11.

Die Funktion eines soweit beschriebenen Kraftstoffeinspritzventils 10 ist bereits allgemein bekannt und wird daher wie folgt nur kurz erläutert: In unbestromtem Zustand des Magnetventils 20 wird der Magnetanker 23 durch die Kraft der Druckfeder 28 gegen den Sitz 30 gedrückt, sodass der Steuerraum 37 verschlossen ist. Weiterhin wird die Ventilnadel 40 mittels der Druckfeder 43 gegen den Sitz 46 gedrückt, sodass auch die Kraftstoffaustrittsöffnung 49 verschlossen ist. Bei einer Bestromung des Magnetventils 20 bzw. der Magnetspule 22 hebt der Magnetanker 23 von dem Sitz 30 ab, sodass ein Durchgang von dem unter hohem Kraftstoffdruck stehenden Steuerraum 37 in einen Ankerraum 51 geschaffen wird, der mit der Rücklaufleitung 5 in Verbindung steht. Das Abströmen des Kraftstoffes aus dem Steuerraum 37 bewirkt, dass die Ventilnadel 40 von ihrem Sitz 46 abhebt, und Kraftstoff aus dem über die Zulaufleitung 1 unter Hochdruck stehenden Hochdruckspeicherraum 52 und dem Düsenraum 48 durch die Kraftstoffaustrittsöffnung 49 aus dem Kraftstoffeinspritzventil 10 ausströmt und in den Brennraum der Brennkraftmaschine abgegeben wird.The function of a fuel injection valve 10 described so far is already well known and is therefore briefly explained as follows: In the de-energized state of the solenoid valve 20, the armature 23 is pressed by the force of the compression spring 28 against the seat 30, so that the control chamber 37 is closed. Furthermore, the valve needle 40 is pressed by means of the compression spring 43 against the seat 46, so that the fuel outlet opening 49 is closed. When the solenoid valve 20 or the solenoid 22 is energized, the magnet armature 23 lifts off from the seat 30, so that passage from the high-pressure fuel control chamber 37 into an armature space 51 is created, which communicates with the return line 5. The outflow of the fuel from the control chamber 37 causes the valve needle 40 lifts from its seat 46, and fuel from the high pressure storage chamber 52 and the nozzle chamber 48 through the fuel outlet opening 49 flows out of the fuel injection valve 10 via the inlet line 1 and into the combustion chamber the internal combustion engine is discharged.

Die Ventilnadel 40 weist aufgrund ihrer Länge L1 sowie ihres Materials und somit ihres Elastizitätsmoduls und ihrer Querschnittsfläche A eine bestimmte Steifigkeit auf. In unbestromtem Zustand des Magnetventils 20 wird die Ventilnadel 40 gegen den Sitz 46 gedrückt, wobei sich eine elastische Verformung der Ventilnadel 40 aufgrund der oben beschriebenen Materialeigenschaften sowie der Geometrie der Ventilnadel 40 einstellt. Beim Bestromen der Magnetspule 20 und des damit verbundenen Druckabbaus in dem Steuerraum 37 erfolgt das Abheben der Ventilnadel 40 von dem Sitz 46 erst, sobald der an der oberen Stirnfläche 53 der Ventilnadel 40 herrschende Druck bzw. die entsprechende Axialkraft soweit reduziert ist, bis die Ventilnadel 40 wieder ihre ursprüngliche Länge annimmt Gleichzeitig wird erwähnt, dass auch der Druckabbau im Steuerraum 37, d.h. der Zeitraum zwischen dem Abheben des Magnetankers 23 von dem Sitz 30 bis zur Reduktion derAxialkraft an der Stirnfläche 53, einen gewissen Zeitraum beansprucht, der von der Größe des Volumens des Steuerraums 37 abhängt. Die Summe der Verzögerungen, hervorgerufen zum einen durch den Druckabbau im Steuerraum 37 und zum anderen hinsichtlich der elastischen Verformung der Ventilnadel 40, wird als Verzugszeit oder Ansteuerzeit t bezeichnet.Due to its length L 1 and its material and thus its modulus of elasticity and its cross-sectional area A, the valve needle 40 has a certain rigidity. In the de-energized state of the solenoid valve 20, the valve needle 40 is pressed against the seat 46, wherein an elastic deformation of the valve needle 40 due to the material properties described above and the geometry of the valve needle 40 sets. When energizing the solenoid coil 20 and the associated pressure reduction in the control chamber 37, the lifting of the valve needle 40 from the seat 46 takes place only when the pressure prevailing on the upper end surface 53 of the valve needle 40 pressure or the corresponding axial force is reduced to the valve needle At the same time it is mentioned that also the pressure reduction in the control chamber 37, ie the period between the lifting of the armature 23 from the seat 30 to the reduction of the axial force on the end face 53, takes a certain period of time, which depends on the size of the Volume of the control room 37 depends. The sum of the delays caused by the pressure reduction in the first place Control chamber 37 and the other with respect to the elastic deformation of the valve needle 40, referred to as delay time or drive time t.

In der Fig. 2 ist ein Kraftstoffeinspritzventil 10a dargestellt, welches sich von dem in der Fig. 1 dargestellten Kraftstoffeinspritzventil 10 dadurch unterscheidet, dass es insgesamt eine kleinere Baulänge aufweist. Erfindungsgemäß ist vorgesehen, dass die kleinere Baulänge über eine Verkleinerung bzw. Verkürzung des Mittelteils 13 erfolgt, während das Unterteil 14 und das Oberteil 12 jeweils als standardisierte Bauteile ausgebildet sind, welche sowohl beim Kraftstoffeinspritzventil 10 als auch beim Kraftstoffeinspritzventil 10a in identischer Weise vorhanden sind. Gleichzeitig sind auch die übrigen, nicht direkt mit dem Mittelteil 13 und der Ventilnadel 40 in Wirkverbindung angeordneten Bauelemente in identischer Art und Weise vorhanden. Somit unterscheidet sich das Kraftstoffeinspritzventil 10a von dem Kraftstoffeinspritzventil 10 lediglich in der Länge des Mittelteils 13 sowie in der Länge der Ventilnadel 40a. Da die Länge L2 der Ventilnadel 40a, ebenso wie die Länge des Mittelteils 13 gegenüber dem Kraftstoffeinspritzventil 10 geringer ist, weist das Kraftstoffeinspritzventil 10a bezüglich der Ventilnadel 40a eine geringere Ansprechzeit auf, da (vorausgesetzt, dass die Ventilnadel 40 und die Ventilnadel 40a aus demselben Material bestehen und dieselbe Querschnittsfläche A aufweisen) die Länge L2 der Ventilnadel 40a gegenüber der Länge L1 der Ventilnadel 40 geringer ist. Dies würde somit insgesamt gesehen ebenfalls zu einer verkürzten Ansteuerzeit t des Kraftstoffeinspritzventils 10a führen. Um die Ansteuerzeiten t sowohl des Kraftstoffeinspritzventils 10 als auch des Einspritzventils 10a gleich groß auszubilden, ist es erfindungsgemäß vorgesehen, dass der Teil der Ansteuerzeit t, welcher durch das Volumen des Steuerraums 37 beeinflusst wird, bei dem Kraftstoffeinspritzventil 10a gegenüber dem Kraftstoffeinspritzventil 10 vergrößert ist. Dies erfolgt durch eine Vergrößerung des Volumens des Steuerraums 37 derart, dass der in den Steuerraum 37 hineinragende Führungsabschnitt 39a der Ventilnadel 40a in seiner Länge verringert ist. Mit anderen Worten gesagt bedeutet das, dass die Verkürzung der Ansteuerzeit t aufgrund der geringen Länge L2 der Ventilnadel 40a durch eine Verlängerung des Anteils der Ansteuerzeit t aufgrund des vergrößerten Volumens des Steuerraums 37 ausgeglichen wird.In the Fig. 2 a fuel injection valve 10 a is shown, which differs from that in the Fig. 1 illustrated fuel injector 10 differs in that it has a total of a smaller overall length. According to the invention, the smaller length is achieved by reducing or shortening the central part 13, while the lower part 14 and the upper part 12 are each formed as standardized components, which are present both in the fuel injection valve 10 and the fuel injection valve 10a in an identical manner. At the same time, the other, not directly with the central part 13 and the valve needle 40 operatively connected components in an identical manner are present. Thus, the fuel injection valve 10a differs from the fuel injection valve 10 only in the length of the central part 13 and in the length of the valve needle 40a. Since the length L 2 of the valve needle 40a, as well as the length of the central portion 13 with respect to the fuel injection valve 10 is lower, the fuel injection valve 10a with respect to the valve needle 40a has a lower response time, (provided that the valve needle 40 and the valve needle 40a from the same Material and have the same cross-sectional area A), the length L 2 of the valve needle 40a with respect to the length L 1 of the valve needle 40 is lower. This would thus also lead overall to a shortened drive time t of the fuel injection valve 10a. In order to make the actuation times t of both the fuel injection valve 10 and the injection valve 10a the same, it is provided according to the invention that the part of the activation time t, which is influenced by the volume of the control chamber 37, is increased in the fuel injection valve 10a relative to the fuel injection valve 10. This is done by increasing the volume of the control chamber 37 such that the projecting into the control chamber 37 guide portion 39a of the valve needle 40a is reduced in its length. In other words, this means that the shortening of the drive time t due to the small length L 2 of the valve needle 40a is compensated by an extension of the proportion of the drive time t due to the increased volume of the control space 37.

In den Fig. 3 und 4 ist ein drittes Kraftstoffeinspritzventil 60 und ein viertes Kraftstoffeinspritzventil 60a dargestellt. Die Kraftstoffeinspritzventile 60, 60a unter scheiden sich von den Kraftstoffeinspritzventilen 10, 10a durch die Verwendung einer anders aufgebauten Ventilnadel 62, 62a. Hierbei sind die Ventilnadeln 62 und 62a jeweils dreiteilig ausgebildet. Jede der Ventilnadeln 62, 62a besteht aus einem standardisierten, in den Steuerraum 37 hineinragenden Oberteil 63 sowie einem standardisierten Unterteil 64, welches den zweiten Führungsbereich 41 und die Ventilspitze 42 trägt. Das Oberteil 63 und das Unterteil 64 sind mittels eines zylindrisch ausgebildeten Mittelteils 65, 65a miteinander verbunden. Hierbei findet als Verbindungstechnik zwischen dem Mittelteil 65, 65a und dem Oberteil 63 bzw. zwischen dem Mittelteil 65, 65a und dem Unterteil 64 bevorzugt das Laserschweißen Verwendung.In the Fig. 3 and 4 For example, a third fuel injection valve 60 and a fourth fuel injection valve 60a are shown. The fuel injection valves 60, 60a differ from the fuel injection valves 10, 10a through the use of a differently constructed valve needle 62, 62a. Here, the valve needles 62 and 62a are each formed in three parts. Each of the valve needles 62, 62a consists of a standardized, protruding into the control chamber 37 upper part 63 and a standardized lower part 64, which carries the second guide portion 41 and the valve tip 42. The upper part 63 and the lower part 64 are interconnected by means of a cylindrically shaped middle part 65, 65a. In this case, the laser welding is preferably used as connection technology between the middle part 65, 65a and the upper part 63 or between the middle part 65, 65a and the lower part 64.

Wie man aus einer Zusammenschau der Fig. 3 und 4 erkennt, weist das Mittelteils 65 einen größeren Durchmesser D1 auf, als das Mittelteil 65a mit dem Durchmesser D2. Somit weist auch das Mittelteil 65 eine größere Querschnittsfläche A1 auf als das Mittelteil 65a mit der Querschnittsfläche A2. Während es bei den Kraftstoffeinspritzventilen 10 und 10a vorgesehen ist, die Ansteuerzeit t ausschließlich über eine Variation des Volumens des Steuerraums 37 zu beeinflussen, wird bei den Kraftstoffeinspritzventilen 60, 60a die Ansteuerzeit t hauptsächlich durch eine Variation des Durchmessers D bzw. der Querschnittsfläche A des Mittelteils 65, 65a beeinflusst. Hierbei ist es vorteilhafterweise vorgesehen, dass die unterschiedlichen Durchmesser D der Mittelteile 65, 65a zur Reduktion der Typenvielfalt lediglich in Stufen vorliegen, d.h., dass lediglich eine begrenzte Anzahl von Durchmessern D vorgesehen ist bzw. in der Fertigung zur Montage von Kraftstoffeinspritzventilen 60, 60a vorliegen. Ober die Variation bzw. Auswahl der Mittelteile 65, 65a wird dabei eine Grobanpassung der Ansteuerzeiten t bewirkt. Hierbei ist vorgesehen, dass, sollte sich eine bestimmte Ansteuerzeit t mittels zweier unterschiedlicher Durchmesser D verwirklichen lassen, stets der geringere Durchmesser D verwendet wird. Dies hat zur Folge, dass (im Vergleich zu dem größeren Durchmesser D) das Volumen des Steuerraums 37 kleiner ist, um die geringere Steifigkeit des mit dem relativ kleineren Durchmesser D ausgestatteten Mittelteils 65 auszugleichen. Die Feinabstimmung bezüglich der Ansteuerzeit t erfolgt bei dem gewählten Durchmesser D nunmehr durch eine entsprechende Verkürzung bzw. Reduzierung der Länge des Mittelteils 65, 65a derart, dass der Bereich des Oberteils 63, welcher sich in dem Ventilstück 32 befindet, etwas geringer in den Steuerraum 37 hineinragt.How to make a synopsis of the Fig. 3 and 4 detects, the middle part 65 has a larger diameter D 1 , as the central part 65a with the diameter D 2nd Thus, the central part 65 has a larger cross-sectional area A 1 than the central part 65 a with the cross-sectional area A 2 . While it is provided in the fuel injection valves 10 and 10a, to influence the driving time t exclusively by a variation of the volume of the control chamber 37, the driving time t in the fuel injection valves 60, 60a mainly by a variation of the diameter D or the cross-sectional area A of the central part 65, 65a influenced. In this case, it is advantageously provided that the different diameters D of the middle parts 65, 65a are present only in stages for reducing the variety of types, ie that only a limited number of diameters D is provided or are present in the production for mounting fuel injection valves 60, 60a , In this case, a coarse adjustment of the activation times t is effected via the variation or selection of the middle parts 65, 65a. In this case, it is provided that, should it be possible to realize a specific activation time t by means of two different diameters D, the smaller diameter D is always used. This has the consequence that (compared to the larger diameter D), the volume of the control chamber 37 is smaller, to compensate for the lower rigidity of the equipped with the relatively smaller diameter D middle part 65. The fine tuning with respect to the actuation time t takes place at the selected diameter D now by a corresponding reduction or reduction of the length of the central part 65, 65 a in such a way that the region of the upper part 63, which is located in the valve piece 32, projects somewhat less into the control chamber 37.

Hierbei lässt sich das Verhältnis aus der Vergrößerung des Ventilnadelhubs ΔH aufgrund der Vergrößerung des Volumens des Steuerraums 37 zur Verkürzung des Nadelhubs aufgrund der Verkürzung der Ventilnadel ΔL berechnen nach: ΔH / ΔL = E 37 x A 37 / ( E 65 ; 65 a x A 65 ; 65 a

Figure imgb0001

Wobei

  • E(37) der Elastizitätsmodul des Kraftstoffs im Bereich des Steuerraums 37,
  • A(37) die Querschnittsfläche A im Bereich des Steuerraums 37,
  • E(65; 65a) der Elastizitätsmodul des Abschnitts 65; 65a,
  • A(65; 65a) die Querschnittsfläche A im Bereich des Abschnitts 65; 65a bedeutet und wobei das Verhältnis ΔH / ΔL erfindungsgemäß zwischen 100 und 500 liegt.
Here, the ratio of the increase in the valve needle lift ΔH due to the increase in the volume of the control space 37 for shortening the needle stroke due to the shortening of the valve needle ΔL can be calculated by: AH / .DELTA.L = e 37 x A 37 / ( e 65 ; 65 a x A 65 ; 65 a
Figure imgb0001

In which
  • E (37) the modulus of elasticity of the fuel in the region of the control chamber 37,
  • A (37) the cross-sectional area A in the area of the control chamber 37,
  • E (65; 65a) is the modulus of elasticity of section 65; 65a,
  • A (65; 65a) the cross-sectional area A in the region of the section 65; 65a and wherein the ratio ΔH / ΔL according to the invention is between 100 and 500.

Die soweit beschriebenen Kraftstoffeinspritzventile 10, 10a und 60, 60a lassen sich in vielfältiger Art und Weise abwandeln bzw. modifizieren. Insbesondere kann auch die Magnetbaugruppe bzw. das Magnetventil 20 anders aufgebaut sein bzw. durch einen Piezo ersetzt werden. Auch wird ergänzend erwährt, dass die Auslegung der Kraftstoffeinspritzventile 10, 10a, 60, 60a so erfolgen kann, dass das Magnetventil 20 bereits wieder geschlossen sein kann, bevor die Einspritzung beginnt bzw. die Durchgangsbohrung 34 freigegeben wird. Auf diese Art und Weise lassen sich Streuungen zwischen hintereinander folgenden Einspritzungen sowie Gegendruckabhängigkeiten reduzieren.The fuel injection valves 10, 10a and 60, 60a described so far can be modified or modified in a variety of ways. In particular, the magnet assembly or the solenoid valve 20 may be constructed differently or replaced by a piezo. It is also shown in addition that the design of the fuel injection valves 10, 10a, 60, 60a can take place so that the solenoid valve 20 can already be closed again before the injection begins or the through-bore 34 is released. In this way, variations between successive injections and Gegenruckabhängigkeiten can be reduced.

Claims (6)

  1. Method for producing a fuel injection valve (10; 10a; 60; 60a), in which method a valve needle (40; 40a; 62; 62a) which closes off at least one fuel outlet orifice (49) is inserted into an injector housing (11), wherein the opposite end of the valve needle (40; 40a; 62; 62a) from the at least one fuel outlet orifice (49) is guided in a valve piece (32) which has a pressurized, fuel-filled control chamber (37), wherein the control chamber (37) can be closed off, on the side facing away from the valve needle (40; 40a; 62; 62a), by a closing element (23) which, when opened, forms a passage and which is connected at least indirectly to a fuel return line (5) at low pressure, wherein after the opening of the control chamber (37) by means of the closing element (23), fuel volume present in the control chamber (37) flows out through the passage, wherein the valve needle (40; 40a; 62; 62a) moves in the direction of the closing element (23), wherein the at least one fuel outlet orifice (49) is opened up, and wherein between the opening of the control chamber (37) and the opening of the at least one fuel outlet orifice (49) there is a delay time (t) owing to the size of the volume of the control chamber (37) and owing to the stiffness of the valve needle (40; 40a; 62; 62a) arising from the modulus of elasticity, the diameter (D) and the length (L) of the valve needle (40; 40a; 62; 62a),
    characterized
    in that the valve needle (62; 62a) is composed of at least a standardized first portion (63) arranged in the control chamber (37), which first portion is connected, on the side facing away from the control chamber (37), to a second cylindrical portion (65; 65a) of the valve needle (62; 62a), and in that the diameter (D) of the second cylindrical portion (65; 65a) is varied such that, to shorten the delay time (t), the diameter (D) of the second cylindrical portion (65; 65a) is increased and, to lengthen the delay time (t), the diameter (D) of the second cylindrical portion (65; 65a) is decreased, to attain equal delay times (t) in fuel injection valves (10; 10a; 60; 60a) with injector housings (11) of different length and with valve needles (40; 40a; 62; 62a) of different length, at least the volume of the control chamber (37) is adapted such that, to shorten the delay time (t), the volume of the control chamber (37) is decreased and, to lengthen the delay time (t), the volume of the control chamber (37) is increased, wherein the diameter (D) of the second cylindrical portion (65; 65a) is varied in diameter steps, and fine adjustment of the delay time (t) is carried out by means of an adaptation of the volume of the control chamber (37) by means of a variation of the length of the second cylindrical portion (65; 65a).
  2. Method according to Claim 1,
    characterized
    in that the geometry of the control chamber (37) in the region in which the valve needle (40; 40a; 62; 62a) is guided is in the form of a cylindrical bore (38) with always the same diameter and always the same depth, and in that the volume of the control chamber (37) is adapted by means of a shortening or lengthening of that portion (39; 39a) of the valve needle (40; 40a; 62; 62a) which is guided in the control chamber (37).
  3. Method according to Claim 1,
    characterized
    in that, taking into consideration the minimum and maximum possible volume of the control chamber (37) and the available diameter steps of the valve needle (62; 62a), that diameter (D) of the valve needles (62; 62a) is selected which leads to a minimum volume of the control chamber (37).
  4. Method according to Claim 3,
    characterized
    in that the ratio of the enlargement of the valve needle stroke ΔH owing to the enlargement of the volume of the control chamber (37) to the shortening of the needle stroke owing to the shortening of the valve needle ΔL is calculated as follows: ΔH / ΔL = E 37 x A 37 / ( E 65 ; 65 a x A 65 ; 65 a ,
    Figure imgb0003

    where
    E(37) is the modulus of elasticity of the fuel in the region of the control chamber (37),
    A (37) is the cross-sectional area (A) in the region of the control chamber (37),
    E(65; 65a) is the modulus of elasticity of the portion (65; 65a),
    A(65; 65a) is the cross-sectional area (A) in the region of the portion (65; 65a),
    and where
    the ratio ΔH / ΔL lies between 100 and 500.
  5. Method according to one of Claims 1, 3 and 4,
    characterized
    in that the second portion (65; 65a) of the valve needle (62; 62a) is connected, on the opposite side from the standardized first portion (63), to a standardized third portion (64).
  6. Method according to one of Claims 1, 3, 4 and 5,
    characterized
    in that the connection at least between the second portion (65; 65a) of the valve needle (62; 62a) and the standardized first portion (63) and if appropriate between the second portion (65; 65a) of the valve needle (62; 62a) and the third portion (64) is realized by laser welding.
EP10762648.3A 2009-11-10 2010-10-01 Method of manufacturing a fuel injector Not-in-force EP2499350B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102009046582A DE102009046582A1 (en) 2009-11-10 2009-11-10 Method for manufacturing a fuel injection valve and fuel injection valve
PCT/EP2010/064647 WO2011057863A1 (en) 2009-11-10 2010-10-01 Method for producing a fuel injection valve, and fuel injection valve

Publications (2)

Publication Number Publication Date
EP2499350A1 EP2499350A1 (en) 2012-09-19
EP2499350B1 true EP2499350B1 (en) 2014-08-20

Family

ID=43260297

Family Applications (1)

Application Number Title Priority Date Filing Date
EP10762648.3A Not-in-force EP2499350B1 (en) 2009-11-10 2010-10-01 Method of manufacturing a fuel injector

Country Status (6)

Country Link
US (1) US20120205470A1 (en)
EP (1) EP2499350B1 (en)
JP (1) JP2013510268A (en)
CN (1) CN102597485A (en)
DE (1) DE102009046582A1 (en)
WO (1) WO2011057863A1 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011077618A1 (en) * 2011-06-16 2012-12-20 Robert Bosch Gmbh Injector, in particular fuel injector for an internal combustion engine
DE102012220025A1 (en) * 2012-06-29 2014-01-02 Robert Bosch Gmbh Fuel injection valve for internal combustion engines
DE102014226407A1 (en) 2014-12-18 2016-06-23 Robert Bosch Gmbh Injector for fuels
EP3247895A1 (en) * 2015-01-23 2017-11-29 Sentec Ltd Solenoid-based fuel injector
JP6384366B2 (en) * 2015-03-09 2018-09-05 株式会社デンソー Fuel injection device
JP6708366B2 (en) * 2015-03-09 2020-06-10 株式会社デンソー Fuel injection device and method of manufacturing fuel injection device
JP6256440B2 (en) * 2015-06-26 2018-01-10 株式会社デンソー Injector
WO2016208130A1 (en) * 2015-06-26 2016-12-29 株式会社デンソー Injector
EP3153700A1 (en) * 2015-10-08 2017-04-12 Continental Automotive GmbH Valve assembly for an injection valve, injection valve and method for assembling an injection valve
CN106351775B (en) * 2016-11-24 2019-11-12 北油电控燃油喷射系统(天津)有限公司 A kind of control chamber middle high-pressure electric control fuel injector
US11174827B1 (en) 2020-09-18 2021-11-16 Caterpillar Inc. Fuel injector with internal radial seal with thin wall counterbore
US11248575B1 (en) 2020-09-18 2022-02-15 Caterpillar Inc. Fuel injector with internal leak passage to injector drain

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3941269B2 (en) * 1997-12-11 2007-07-04 株式会社デンソー Laser welding structure and method of metal member, and fuel injection valve
JPH11280606A (en) * 1998-03-31 1999-10-15 Denso Corp Fuel injection nozzle
EP1081372B1 (en) * 1999-08-31 2004-10-13 Denso Corporation Fuel injection device
JP3879909B2 (en) * 2001-03-29 2007-02-14 株式会社デンソー Fuel injection device
US7077381B2 (en) * 2001-07-31 2006-07-18 Caterpillar Inc. Desensitizing armature air gap to component distortion in a fuel injector
DE10145620B4 (en) * 2001-09-15 2006-03-02 Robert Bosch Gmbh Valve for controlling fluids
JP2003176763A (en) * 2001-12-11 2003-06-27 Denso Corp Fuel injection device
DE10247571A1 (en) * 2002-10-11 2004-04-22 Robert Bosch Gmbh Injector for the injection of fuel
DE102004017303A1 (en) * 2004-04-08 2005-10-27 Robert Bosch Gmbh injection
CN100593081C (en) * 2005-02-18 2010-03-03 罗伯特·博世有限公司 Injection nozzle
JP4325585B2 (en) * 2005-04-28 2009-09-02 株式会社デンソー Fuel injection valve and injection amount adjusting method thereof
DE102005059437A1 (en) * 2005-12-13 2007-06-14 Robert Bosch Gmbh fuel injector

Also Published As

Publication number Publication date
US20120205470A1 (en) 2012-08-16
JP2013510268A (en) 2013-03-21
DE102009046582A1 (en) 2011-05-12
WO2011057863A1 (en) 2011-05-19
CN102597485A (en) 2012-07-18
EP2499350A1 (en) 2012-09-19

Similar Documents

Publication Publication Date Title
EP2499350B1 (en) Method of manufacturing a fuel injector
EP1771650B1 (en) Fuel injector comprising a two-stage transmission element
EP1756415B1 (en) Fuel injector with variable actuator transmission
EP2386746B1 (en) Fuel injector
EP1705365B1 (en) Fuel injector with a direct control of the injection needle and a variable stroke amplifier
EP1759114A1 (en) Fuel injector with variable actuator transmission
EP1135602A1 (en) Valve for controlling a liquid
DE10221384A1 (en) Fuel injection device for an internal combustion engine
EP2310662B1 (en) Fuel injector
WO2004055357A1 (en) Bounce-free magnetic actuator for injection valves
DE102012220027A1 (en) Switching valve for common-rail fuel injector for injecting diesel into combustion chamber of internal combustion engine, has control space filled with fuel via hole, and closing element closing hole in position for pressure relief of space
EP2428672A2 (en) Fuel injector
WO2003054375A1 (en) Fuel injection device for an internal combustion engine
WO2017089011A1 (en) Fuel injector
DE102009027103A1 (en) Fuel injector for injecting fuel into high-pressure reservoir of internal combustion engine, has valve module housing resting on bearing surface of valve piece of injector, where stroke of actuator is set in direction by bearing surface
EP2185807B1 (en) Control valve for a fuel injector
EP2156044B1 (en) Injector having a pressure-compensated control valve
EP2126333B1 (en) Fuel injector comprising a coupler
DE102017219568A1 (en) Method for controlling a fuel injector
DE102011076956A1 (en) Fuel injector for internal combustion engine, has valve needle arranged in housing in longitudinally displaceable manner, where valve needle closes scum hole arranged in high-pressure space of housing
WO2010000528A1 (en) Solenoid valve for a fuel injector, and fuel injector
EP2204570B1 (en) Fuel injector
DE10059399B4 (en) Device for improving the injection sequence in fuel injection systems
DE102008041561A1 (en) Fuel injector, particularly common rail injector for injecting fuel into combustion chamber of internal combustion engine, comprises two injector valve element units that are coupled together over hydraulic coupler
DE102007001365A1 (en) Common rail injector, for injecting e.g. petrol, into combustion chamber of internal combustion engine, has switching chamber connected with low pressure area by connecting channel that is closed and opened by control valve

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20120611

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

DAX Request for extension of the european patent (deleted)
17Q First examination report despatched

Effective date: 20130404

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20140521

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 683619

Country of ref document: AT

Kind code of ref document: T

Effective date: 20140915

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502010007727

Country of ref document: DE

Effective date: 20141002

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20140820

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141120

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141222

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141121

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141120

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141220

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502010007727

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

Ref country code: LU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20141001

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20141031

26N No opposition filed

Effective date: 20150521

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20141120

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20141031

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20141031

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 6

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20141120

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20141001

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20101001

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 7

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 683619

Country of ref document: AT

Kind code of ref document: T

Effective date: 20151001

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20151001

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 8

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 9

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140820

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20181206

Year of fee payment: 9

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20191022

Year of fee payment: 10

Ref country code: IT

Payment date: 20191021

Year of fee payment: 10

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 502010007727

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200501

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201031

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201001