EP2462335B1 - Device for high-pressure fuel injection - Google Patents

Device for high-pressure fuel injection Download PDF

Info

Publication number
EP2462335B1
EP2462335B1 EP10728156A EP10728156A EP2462335B1 EP 2462335 B1 EP2462335 B1 EP 2462335B1 EP 10728156 A EP10728156 A EP 10728156A EP 10728156 A EP10728156 A EP 10728156A EP 2462335 B1 EP2462335 B1 EP 2462335B1
Authority
EP
European Patent Office
Prior art keywords
valve
pressure
valve needle
fuel injection
needle
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
EP10728156A
Other languages
German (de)
French (fr)
Other versions
EP2462335A1 (en
Inventor
Sebastian Jansen
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 EP2462335A1 publication Critical patent/EP2462335A1/en
Application granted granted Critical
Publication of EP2462335B1 publication Critical patent/EP2462335B1/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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/08Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series the valves opening in direction of fuel flow
    • 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
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/061Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/061Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
    • F02M51/0625Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures
    • F02M51/0635Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a plate-shaped or undulated armature not entering the winding
    • F02M51/0642Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a plate-shaped or undulated armature not entering the winding the armature having a valve attached thereto
    • F02M51/0653Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a plate-shaped or undulated armature not entering the winding the armature having a valve attached thereto the valve being an elongated body, e.g. a needle valve
    • 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
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/061Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
    • F02M51/0625Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures
    • F02M51/0635Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a plate-shaped or undulated armature not entering the winding
    • F02M51/066Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a plate-shaped or undulated armature not entering the winding the armature and the valve being allowed to move relatively to each other or not being attached to each other
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/10Other injectors with elongated valve bodies, i.e. of needle-valve type

Definitions

  • the present invention relates to a device for high-pressure fuel injection, which can be used in particular in internal combustion engines with direct injection in the stratified charge mode.
  • an injection valve with outwardly opening valve needle is disclosed, which is actuated by a solenoid actuator and having a guide element on the valve needle, which is guided in a valve housing, wherein the diameters of the guide element and a valve seat of the valve needle are selected so that the valve needle is essentially pressure balanced.
  • the high-pressure injection valves of the prior art are only insufficiently suitable to a simple and inexpensive to produce device for To provide high pressure injection for internal combustion engines with direct injection in stratified charge mode, which provides a high sealing force between the valve seat and valve needle in the closed state, and can be operated by a solenoid actuator with low actuation force or low power consumption and has a comparable switching dynamics as an injection valve with piezo actuator.
  • valve assembly according to the invention with the features of claim 1 has the advantage that it has a simple and thus more cost-effective design with a solenoid actuator that opens an outwardly opening valve needle due to effective on the valve needle pressure equalization with a significantly reduced operating force. Therefore, in the valve assembly according to the invention solenoid actuators with low power consumption, especially at injection pressures of 20 MPa or higher, can be used, which allow sufficient switching dynamics and reliable sealing of the valve needle valve seat of the valve in the closed state. This is inventively achieved in that when activating an electromagnetic actuator arranged between the high pressure region and low pressure region of the valve assembly control valve is opened in front of an outwardly opening valve needle.
  • a pressure equalization d. H. a pressure increase in the low pressure region, which causes a hydraulic force on an active surface of a valve element of the control valve in the opening direction of the valve needle and thereby significantly reduces an opening force of the electromagnetic actuator for the valve needle.
  • the control valve is opened by means of a freely movable magnet armature or a component connected to the magnet armature.
  • the device according to the invention for high-pressure fuel injection further comprises a driver attached to the valve needle with an armature contact region, wherein the driver is arranged in the starting position at a predetermined distance from the armature and the armature is movably disposed on the valve needle.
  • a closing spring for closing the valve needle also restores the armature. This ensures that upon activation of the electromagnetic actuator whose armature first moves from the starting position to the armature contact region of the driver and thereby opens the control valve for pressure equalization, without operating the valve needle. Only when the magnet armature is applied to the driver, the valve needle is actuated directly via the armature and opened.
  • a ring-cylindrical component is attached to the armature, wherein the valve seat of the control valve is arranged on a free end face of the annular-cylindrical component.
  • a gap seal is formed between the annular cylindrical component and the valve housing.
  • a diameter of the gap seal is formed larger than a diameter of the valve seat of the valve needle.
  • the distance from the starting position of the magnet armature to the driver attached to the valve needle is smaller than a total stroke of the magnet armature, ie, there is a residual stroke for opening the valve needle.
  • a first partial stroke the magnet armature from the starting position to the driver is a rapid opening of the control valve for pressure equalization and thus a rapid pressure equalization for the easier opening of the valve needle achieved, which is then opened with a second partial stroke.
  • a first partial stroke of the armature is first carried out by the driver to the closed position of the control valve and the control valve thus closed.
  • the valve element of the control valve acts as another actuated by the armature driver for the return of the valve needle.
  • the closing of the valve needle can be done faster by a hydraulic force in the closing direction of the valve needle supporting hydraulic force. This makes it possible to use magnetic actuators with low power consumption and to realize the switching dynamics required for gasoline injection during stratified operation of internal combustion engines.
  • the device for high-pressure fuel injection between the pressure chamber and the low-pressure region further comprises a throttle.
  • a leakage check valve can be inserted between the pressure chamber and the low-pressure region.
  • a leakage or return amount of fuel to a fuel return when opening the valve needle is significantly reduced.
  • the device according to the invention can be used very economically.
  • the leakage check valve has as closure member a collar-like extension formed on the valve needle and a seat which is formed on the valve housing.
  • FIGS. 1 to 6 a device 1 for high-pressure fuel injection according to a first preferred embodiment of the invention described in detail.
  • FIG. 1 shows a schematically simplified sectional view of the device according to the invention in the closed state.
  • the device 1 comprises a valve housing 2, an outwardly opening valve needle 3, which is arranged in the valve housing 2 in a pressure chamber 4 filled with fuel.
  • This pressure chamber 4 a fuel K is supplied via a fuel inlet 24 under pressure, wherein the valve needle 3 seals on a valve seat 16 on the valve housing 2.
  • the device 1 has a closing spring 5, which returns the valve needle 3 to a starting position, and an electromagnetic actuator 6 with a magnetic coil 63, an inner pole 62, a magnet housing 61 and a movably arranged magnet armature 7, the valve needle 3 via a thereto trained or attached driver 9 is actuated.
  • a control valve 8 having a valve element 10 and a valve seat 11 is arranged on an end region 29 of the valve needle 3 opposite the injection side.
  • the valve element 10 has a first active surface 13, which faces the pressure chamber 4, and a second active surface 14, which faces a pressure chamber 12, which communicates with a low-pressure region 19.
  • the valve element 10 of the control valve 8 is designed to release and close a connection between the pressure chamber 4 and the pressure chamber 12, the valve seat 11 of the control valve 8 being arranged on an end face of a ring-cylindrical component 17 fastened to the magnet armature 7. Between the outer circumference of the annular cylindrical member 17 and the valve housing 2, a gap seal 18 is formed with a small guide clearance.
  • FIG. 1 17 flow through openings 30, 31, for the supply of the fuel K are formed in the armature 7 and the annular cylindrical member. Accordingly, when the valve needle 3 is closed and the control valve 8 is closed, the high pressure of the fuel inlet 24 is present supplied fuel in all connected to the pressure chamber 4 interior spaces of the device. In the pressure chamber 12, there is low pressure, since it is connected via a throttle 21 to the fuel return 25 and the control valve 8 is closed.
  • a diameter ds of the valve seat 16 is selected to be smaller than a diameter d1 of the valve element 10, the valve needle 3 is additionally pressed, in addition to the force of the closing spring 5, into the valve seat 16 by a hydraulic force component resulting from this difference in diameter , As a result, a reliable sealing of the device 1 is ensured when the valve needle 3 is closed.
  • FIG. 2 shows an enlarged schematic sectional view showing a part of the device 1 of FIG. 1 illustrated in more detail.
  • a closed control valve 8 and inactivated electromagnetic actuator 6 whose armature 7 in its initial position.
  • the closing spring 5 acts on the armature 7 and is supported on the housing 2 from.
  • the axially freely movable armature 7 due to the spring force of the closing spring 5 a distance A to the driver 9 on the valve needle 3, and a distance H to the inner pole 62.
  • FIG. 3 shows a schematically simplified sectional view of the device 1 of FIG. 1 When opening the valve needle 3.
  • the magnetic coil 63 of the electromagnetic actuator 6 is energized (which is illustrated by a lightning-shaped symbol)
  • the armature 7 performs a first partial stroke in the direction of the inner pole 62, which corresponds to the degree of the distance A, until he the driver 9 touched.
  • the control valve 8 opens so that fuel K flows from the fuel inlet 24 into the pressure chamber 4 and via the flow opening 31 into the pressure chamber 12 (as indicated by an arrow B in FIG FIG. 3 is clarified).
  • the pressure in the pressure chamber 12 rises directly and causes a force on the valve needle 3, which results from the ratio of the hydraulically effective first and second active surfaces 13 and 14 on the valve element 10, which are each subjected to high pressure.
  • This resulting hydraulic force acts in the open control valve 8 in addition to Magnetic force of the armature 7 in the opening direction of the valve needle 3 and reduces the contact pressure of the valve needle 3 on the valve seat 16.
  • the valve needle 3 can now be taken or moved with little force from the armature 3 via the driver 9 in the opening direction, so that the valve needle 3 opens and the injection process can begin.
  • FIG. 4 shows a schematically simplified sectional view of the device of FIG. 1 with open valve needle. Due to the continued energization of the solenoid 63, the magnet armature 7 was pulled together with the valve needle 3 in the opening direction of the device 1 and has a second partial stroke to stop at the inner pole 62 executed, and thereby raised the valve needle 3 from the valve seat 16 to the outside and opened.
  • the second partial stroke for opening the valve needle 3 is here designed to be larger than the first partial stroke A for opening the control valve 8.
  • the effluent between the valve needle 3 and the valve housing 2 fuel spray is indicated by small arrows C in the FIG. 4 illustrated.
  • FIG. 5 shows an enlarged schematic sectional view showing a part of the device 1 of FIG. 4 illustrated in more detail.
  • open control valve 8 a portion of the fuel in the pressure chamber 12 via the throttle 21 (as illustrated by an arrow D) in the fuel return 25 as a leakage amount back.
  • This leakage amount through the throttle 21 is defined or limited to a predetermined value, so that the pressure drop in the pressure chamber 12 after switching off the electromagnetic actuator 6 (closing the valve needle 3) does not take too long and extends the dead times of the switching cycles and thus the switching dynamics deteriorated.
  • FIG. 6 is a schematically simplified sectional view of the device of FIG. 1 illustrated when closing the valve needle 3.
  • the state of the device 1 is shown, which adjusts after switching off the solenoid 63 of the electromagnetic actuator 6, wherein first the control valve 8 is closed. Thereafter, the pressure in the pressure chamber 12 drops due to the connection to the fuel return 25 via the throttle 21 again, so that the second effective surface 14 is acted upon only with the low pressure from the fuel return 25.
  • the first active surface 13 is still with the high pressure in the interior of the annular cylindrical member 17 acted upon.
  • a hydraulic closing force is generated which presses the valve needle 3 in addition to the spring force of the closing spring 5 in the valve seat 16 until the closed state of the valve needle 3 (see. FIG. 1 ) is restored and the injection process is completed.
  • the closing spring 5 acts on the magnet armature 7, the annular cylindrical component 17 and the valve element 10 on the valve needle 3.
  • FIGS. 7 to 10 a device 1 for high-pressure fuel injection according to a second preferred embodiment of the invention described in detail. Identical or functionally identical parts are denoted by the same reference numerals as in the first embodiment.
  • FIG. 7 shows a schematically simplified sectional view of a second embodiment of the inventive device 1 for high-pressure fuel injection with the valve needle closed 3.
  • the second embodiment of the device 1 according to the invention differs from the first embodiment described above in that in this case between the pressure chamber 12 and the low pressure region 19 of the fuel return 25, a leakage check valve 26 is arranged.
  • the leakage check valve 26 is a leakage amount to the fuel return 25, as occurs in the first embodiment in the throttle 21, drastically reduced.
  • the leakage check valve 26 has a collar-like extension 22 of the diameter at the end region 29 of the valve needle 3.
  • the leakage check valve 26 closes the pressure chamber 12 from the fuel return 25 in the closed state.
  • FIG. 7 shows how out, when the valve needle 3 is closed, the control valve 8 is closed and the leakage check valve 26 is opened so that a low pressure prevails in the pressure chamber 12.
  • FIG. 9 shows an enlarged schematic sectional view of a part of the device of FIG. 7 , which illustrates the pressure conditions when the valve needle 3 is closed. How out FIG. 9 can be seen, an annular groove 27 is formed in the valve housing 2 in a region between the annular cylindrical member 17 and the valve element 10 of the control valve 8 to an unimpeded fuel flow into the pressure chamber 12 with open control valve 8 (see FIG. 10 ).
  • the valve needle 3 is closed, the control valve 8 is closed and the leakage check valve 26 is opened.
  • FIG. 8 is a schematically simplified sectional view of the second embodiment of FIG. 7 when the valve needle 3 is open, in this state, the leakage check valve 26 is closed and the control valve 8 is opened.
  • high pressure prevails in the pressure chamber 12, so that the valve needle 3 can be opened with small forces. Since the leakage check valve 26 is closed, no amount of leakage into the fuel return 25 occurs.
  • the collar-like extension 22 of the leakage check valve 26 that adjoins the stop 23 at the same time defines a stroke stop of the opened valve needle 3.
  • FIG. 10 shows an enlarged schematic sectional view of a part of the device of FIG. 8 , which illustrates the pressure conditions when the valve needle 3 is open. How out FIG. 10 can be seen, in this case the control valve 8 is opened and the leakage check valve 26 is closed.
  • the high-pressure region 28 is in this case both in the control valve 8 and in the leakage check valve 26 formed while only in the fuel return 25 of the low pressure region 19 is formed.
  • the actuation of the valve needle 3 can be done directly by a low-cost electromagnetic actuator, even at high injection pressures of 20 MPa, with a sufficiently high switching dynamics , Because of the correspondingly low power requirement of the electromagnetic actuator, the control of the device 1 can therefore be compared with conventional, d. H. available power amplifiers for solenoid high-pressure injection valves. This contributes to a further cost reduction and thus to increased cost-effectiveness of the inventive device 1 for high-pressure fuel injection.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Fuel-Injection Apparatus (AREA)

Description

Stand der TechnikState of the art

Die vorliegende Erfindung betrifft eine Vorrichtung zur Kraftstoffhochdruckeinspritzung, die insbesondere bei Verbrennungsmotoren mit Direkteinspritzung im Schichtladebetrieb einsetzbar ist.The present invention relates to a device for high-pressure fuel injection, which can be used in particular in internal combustion engines with direct injection in the stratified charge mode.

Als Vorrichtungen zur Kraftstoffhochdruckeinspritzung bei Verbrennungsmotoren mit Direkteinspritzung werden Hochdruckeinspritzventile mit nach außen öffnender Ventilnadel verwendet, die wegen ihrer vorteilhaften Spraycharakteristik infolge des ringförmigen Spalts zwischen Ventilnadel und Ventilkörper besonders für Brennverfahren mit strahlgeführtem Schichtbetrieb geeignet sind. Jedoch ist bei Einspritzventilen mit nach außen öffnender Ventilnadel aufgrund des größeren Sitzdurchmessers der Ventilnadel die durch den Kraftstoffdruck erzeugte hydraulische Kraft deutlich höher als im Vergleich zu Einspritzventilen mit nach innen öffnender Nadel. Wegen der hohen Kräfte und kurzen Schaltzeiten werden daher üblicherweise Einspritzventile mit Piezoaktoren verwendet, die jedoch einen erhöhten Kostenaufwand verursachen.As devices for high-pressure fuel injection in internal combustion engines with direct injection high-pressure injection valves are used with outwardly opening valve needle, which are particularly suitable for combustion processes with beam-guided stratified operation due to their advantageous spray characteristics due to the annular gap between the valve needle and valve body. However, in injectors with outwardly opening valve needle, due to the larger seat diameter of the valve needle, the hydraulic force generated by the fuel pressure is significantly higher compared to injectors with inwardly opening needle. Because of the high forces and short switching times injectors are therefore usually used with piezo actuators, however, cause an increased cost.

Bei einem in EP 1783 358A1 beschriebenen Konzept ist ein Einspritzventil mit nach außen öffnender Ventilnadel offenbart, das durch einen Magnetaktuator betätigt wird und ein Führungselement an der Ventilnadel aufweist, das in einem Ventilgehäuse geführt ist, wobei die Durchmesser des Führungselements und eines Ventilsitzes der Ventilnadel so gewählt sind, dass die Ventilnadel im Wesentlichen druckausgeglichen ist.At an in EP 1783 358A1 described concept, an injection valve with outwardly opening valve needle is disclosed, which is actuated by a solenoid actuator and having a guide element on the valve needle, which is guided in a valve housing, wherein the diameters of the guide element and a valve seat of the valve needle are selected so that the valve needle is essentially pressure balanced.

Die Hochdruckeinspritzventile des Standes der Technik sind nur unzureichend geeignet, um eine einfache und kostengünstig herstellbare Vorrichtung zur Hochdruckeinspritzung für Verbrennungsmotoren mit Direkteinspritzung in Schichtladebetrieb bereitzustellen, die eine hohe Dichtkraft zwischen Ventilsitz und Ventilnadel im geschlossenen Zustand bereitstellt, sowie durch einen Magnetaktuator mit geringer Betätigungskraft bzw. geringem Leistungsbedarf betrieben werden kann und dabei eine vergleichbare Schaltdynamik wie ein Einspritzventil mit Piezoaktuator aufweist.The high-pressure injection valves of the prior art are only insufficiently suitable to a simple and inexpensive to produce device for To provide high pressure injection for internal combustion engines with direct injection in stratified charge mode, which provides a high sealing force between the valve seat and valve needle in the closed state, and can be operated by a solenoid actuator with low actuation force or low power consumption and has a comparable switching dynamics as an injection valve with piezo actuator.

Offenbarung der ErfindungDisclosure of the invention

Die erfindungsgemäße Ventilanordnung mit den Merkmalen des Patentanspruchs 1 weist demgegenüber den Vorteil auf, dass diese einen einfachen und damit kostengünstigeren Aufbau mit einem Magnetaktuator aufweist, der eine nach außen öffnende Ventilnadel aufgrund eines an der Ventilnadel wirksamen Druckausgleichs mit einer deutlich reduzierten Betätigungskraft öffnet. Daher können bei der erfindungsgemäßen Ventilanordnung Magnetaktuatoren mit niedrigem Leistungsbedarf, insbesondere auch bei Einspritzdrücken von 20 MPa oder höher, eingesetzt werden, die eine ausreichende Schaltdynamik sowie eine zuverlässige Abdichtung der Ventilnadel am Ventilsitz des Ventils in geschlossenem Zustand ermöglichen. Dies wird erfindungsgemäß dadurch erreicht, dass bei der Aktivierung eines elektromagnetischen Aktuators ein zwischen dem Hochdruckbereich und Niederdruckbereich der Ventilanordnung angeordnetes Steuerventil vor einer nach außen öffnenden Ventilnadel geöffnet wird. Durch die Freigabe einer Verbindung zwischen einem Druckraum im Hochdruckbereich und einer Druckkammer im Niederdruckbereich der Ventilanordnung erfolgt ein Druckausgleich, d. h. eine Druckerhöhung im Niederdruckbereich, der eine hydraulische Kraft auf eine Wirkfläche eines Ventilelements des Steuerventils in Öffnungsrichtung der Ventilnadel bewirkt und dadurch eine Öffnungskraft des elektromagnetischen Aktuators für die Ventilnadel deutlich reduziert. Hierdurch ist ein leichtes und schnelles Schalten möglich. Das Steuerventil wird dabei mittels eines frei beweglichen Magnetankers oder eines mit dem Magnetanker verbundenen Bauteils geöffnet.The valve assembly according to the invention with the features of claim 1 has the advantage that it has a simple and thus more cost-effective design with a solenoid actuator that opens an outwardly opening valve needle due to effective on the valve needle pressure equalization with a significantly reduced operating force. Therefore, in the valve assembly according to the invention solenoid actuators with low power consumption, especially at injection pressures of 20 MPa or higher, can be used, which allow sufficient switching dynamics and reliable sealing of the valve needle valve seat of the valve in the closed state. This is inventively achieved in that when activating an electromagnetic actuator arranged between the high pressure region and low pressure region of the valve assembly control valve is opened in front of an outwardly opening valve needle. By releasing a connection between a pressure chamber in the high pressure region and a pressure chamber in the low pressure region of the valve assembly, a pressure equalization, d. H. a pressure increase in the low pressure region, which causes a hydraulic force on an active surface of a valve element of the control valve in the opening direction of the valve needle and thereby significantly reduces an opening force of the electromagnetic actuator for the valve needle. As a result, an easy and fast switching is possible. The control valve is opened by means of a freely movable magnet armature or a component connected to the magnet armature.

Die Unteransprüche zeigen bevorzugte Weiterbildungen der Erfindung.The dependent claims show preferred developments of the invention.

Gemäß einer bevorzugten Ausgestaltung der Erfindung weist die erfindungsgemäße Vorrichtung zur Kraftstoffhochdruckeinspritzung ferner einen an der Ventilnadel befestigten Mitnehmer mit einem Ankerkontaktbereich auf, wobei der Mitnehmer in der Ausgangsposition in einem vorgegebenen Abstand vom Magnetanker angeordnet ist und der Magnetanker beweglich auf der Ventilnadel angeordnet ist. Eine Schließfeder zum Schließen der Ventilnadel stellt dabei auch den Magnetanker zurück. Dadurch wird gewährleistet, dass bei Aktivierung des elektromagnetischen Aktuators, dessen Magnetanker zuerst von der Ausgangsposition bis zum Ankerkontaktbereich des Mitnehmers bewegt und dadurch das Steuerventil zum Druckausgleich öffnet, ohne die Ventilnadel zu betätigen. Erst wenn der Magnetanker am Mitnehmer anliegt, wird die Ventilnadel direkt über den Magnetanker betätigt und geöffnet.According to a preferred embodiment of the invention, the device according to the invention for high-pressure fuel injection further comprises a driver attached to the valve needle with an armature contact region, wherein the driver is arranged in the starting position at a predetermined distance from the armature and the armature is movably disposed on the valve needle. A closing spring for closing the valve needle also restores the armature. This ensures that upon activation of the electromagnetic actuator whose armature first moves from the starting position to the armature contact region of the driver and thereby opens the control valve for pressure equalization, without operating the valve needle. Only when the magnet armature is applied to the driver, the valve needle is actuated directly via the armature and opened.

Vorzugsweise ist am Magnetanker ein ringzylindrisches Bauteil befestigt, wobei an einer freien Stirnseite des ringzylindrischen Bauteils der Ventilsitz des Steuerventils angeordnet ist. Dadurch wird ein einfacher Aufbau des Steuerventils mit einer minimalen Anzahl von Bauteilen erreicht.Preferably, a ring-cylindrical component is attached to the armature, wherein the valve seat of the control valve is arranged on a free end face of the annular-cylindrical component. As a result, a simple construction of the control valve is achieved with a minimum number of components.

Weiterhin bevorzugt ist zwischen dem ringzylindrischen Bauteil und dem Ventilgehäuse eine Spaltdichtung ausgebildet. Hierdurch wird eine einfache und kostengünstige Abdichtung zwischen den beiden Bauteilen mit einer geringen Leckagemenge realisiert.Further preferably, a gap seal is formed between the annular cylindrical component and the valve housing. As a result, a simple and cost-effective seal between the two components is realized with a small amount of leakage.

Besonders bevorzugt ist ein Durchmesser der Spaltdichtung größer als ein Durchmesser des Ventilsitzes der Ventilnadel ausgebildet. Auf diese Weise wird bei geöffnetem Steuerventil und erfolgtem Druckausgleich eine resultierende hydraulische Kraft in Öffnungsrichtung der Ventilnadel erzeugt und somit die vom Magnetanker zu überwindende Öffnungskraft der Ventilnadel reduziert. Bei geschlossenem Steuerventil resultiert durch den Niederdruck in der Druckkammer hingegen eine hydraulische Kraft in Schließrichtung der Ventilnadel, die eine zuverlässige Abdichtung des Ventils bewirkt.Particularly preferably, a diameter of the gap seal is formed larger than a diameter of the valve seat of the valve needle. In this way, a resulting hydraulic force is generated in the opening direction of the valve needle with open control valve and pressure equalization and thus reduces the force to be overcome by the armature opening force of the valve needle. When the control valve is closed by the low pressure in the pressure chamber, however, results in a hydraulic force in the closing direction of the valve needle, which causes a reliable seal of the valve.

Gemäß einer weiteren bevorzugten Ausgestaltung der Erfindung ist der Abstand von der Ausgangsposition des Magnetankers bis zum an der Ventilnadel befestigten Mitnehmer kleiner als ein Gesamthub des Magnetankers, d. h., es ergibt sich ein Resthub zum Öffnen der Ventilnadel. Durch einen ersten Teilhub des Magnetankers von der Ausgangsposition bis zum Mitnehmer wird ein schnelles Öffnen des Steuerventils für den Druckausgleich und somit ein rascher Druckausgleich für das erleichterte Öffnen der Ventilnadel erreicht, die danach mit einem zweiten Teilhub geöffnet wird. Beim Schließen der Ventilnadel wird zuerst ein erster Teilhub des Magnetankers vom Mitnehmer bis zur geschlossenen Stellung des Steuerventils ausgeführt und das Steuerventil somit geschlossen. Hierbei wirkt das Ventilelement des Steuerventils als ein weiterer vom Magnetanker betätigter Mitnehmer für die Rückstellung der Ventilnadel. Durch die am Steuerventil somit wieder auftretende Druckdifferenz zwischen dem Hochdruckbereich und dem Niederdruckbereich der Vorrichtung kann danach das Schließen der Ventilnadel durch eine in Schließrichtung der Ventilnadel unterstützend wirkende hydraulische Kraft schneller erfolgen. Dadurch kann die Verwendung von Magnetaktuatoren mit geringer Leistungsaufnahme ermöglicht und die für die Benzineinspritzung im Schichtbetrieb von Verbrennungsmotoren erforderliche Schaltdynamik realisiert werden.According to a further preferred embodiment of the invention, the distance from the starting position of the magnet armature to the driver attached to the valve needle is smaller than a total stroke of the magnet armature, ie, there is a residual stroke for opening the valve needle. Through a first partial stroke the magnet armature from the starting position to the driver is a rapid opening of the control valve for pressure equalization and thus a rapid pressure equalization for the easier opening of the valve needle achieved, which is then opened with a second partial stroke. When closing the valve needle, a first partial stroke of the armature is first carried out by the driver to the closed position of the control valve and the control valve thus closed. Here, the valve element of the control valve acts as another actuated by the armature driver for the return of the valve needle. By thus again occurring at the control valve pressure difference between the high pressure region and the low pressure region of the device, the closing of the valve needle can be done faster by a hydraulic force in the closing direction of the valve needle supporting hydraulic force. This makes it possible to use magnetic actuators with low power consumption and to realize the switching dynamics required for gasoline injection during stratified operation of internal combustion engines.

Gemäß einer weiteren bevorzugten Ausgestaltung der Erfindung weist die Vorrichtung zur Kraftstoffhochdruckeinspritzung zwischen der Druckkammer und dem Niederdruckbereich ferner eine Drossel auf. Dadurch wird auf einfache Weise ein rascher Druckabbau über einen Ringspalt zwischen der Ventilnadel und dem Ventilgehäuse in der Druckkammer bei geschlossenem Steuerventil und somit eine hohe Anpresskraft sowie eine gute Dichtwirkung zwischen der Ventilnadel und dem Ventilsitz erreicht.According to a further preferred embodiment of the invention, the device for high-pressure fuel injection between the pressure chamber and the low-pressure region further comprises a throttle. As a result, a quick pressure reduction over an annular gap between the valve needle and the valve housing in the pressure chamber with a closed control valve and thus a high contact pressure and a good sealing effect between the valve needle and the valve seat is achieved in a simple manner.

Alternativ zur Drossel kann zwischen der Druckkammer und dem Niederdruckbereich ein Leckagesperrventil eingesetzt werden. Hierdurch wird eine Leckage- bzw. Rücklaufmenge des Kraftstoffs zu einem Kraftstoffrücklauf beim Öffnen der Ventilnadel deutlich reduziert. Somit kann die erfindungsgemäße Vorrichtung sehr wirtschaftlich eingesetzt werden.As an alternative to the throttle, a leakage check valve can be inserted between the pressure chamber and the low-pressure region. As a result, a leakage or return amount of fuel to a fuel return when opening the valve needle is significantly reduced. Thus, the device according to the invention can be used very economically.

Vorzugsweise weist das Leckagesperrventil als Schließglied eine an der Ventilnadel gebildete kragenartige Erweiterung und einen Sitz auf, der am Ventilgehäuse gebildet ist. Hierdurch ist ein einfacher Aufbau des Leckagesperrventils mit einer minimalen Anzahl von Bauteilen realisierbar. Ferner kann dadurch eine sehr betriebssichere Vorrichtung bereitgestellt werden.Preferably, the leakage check valve has as closure member a collar-like extension formed on the valve needle and a seat which is formed on the valve housing. As a result, a simple construction of the leakage check valve with a minimum number of components can be realized. Furthermore, this can provide a very reliable device.

Kurze Beschreibung der ZeichnungShort description of the drawing

Nachfolgend werden Ausführungsbeispiele der Erfindung unter Bezugnahme auf die begleitende Zeichnung im Detail beschrieben. In der Zeichnung ist:

Figur 1
eine schematisch vereinfachte Schnittdarstellung der erfindungsgemäßen Vorrichtung bei geschlossener Ventilnadel
Figur 2
eine vergrößerte schematische Schnittdarstellung eines Teils der Vorrichtung von Figur 1,
Figur 3
eine schematisch vereinfachte Schnittdarstellung der Vorrichtung von Figur 1 beim Öffnen der Ventilnadel,
Figur 4
eine schematisch vereinfachte Schnittdarstellung der Vorrichtung von Figur 1 bei geöffneter Ventilnadel,
Figur 5
eine vergrößerte schematische Schnittdarstellung eines Teils der Vorrichtung von Figur 4,
Figur 6
eine schematisch vereinfachte Schnittdarstellung der Vorrichtung von Figur 1 beim Schließen der Ventilnadel,
Figur 7
eine schematisch vereinfachte Schnittdarstellung einer zweiten Ausführungsform der Vorrichtung bei geschlossener Ventilnadel,
Figur 8
eine schematisch vereinfachte Schnittdarstellung der Vorrichtung von Figur 7 bei geöffneter Ventilnadel,
Figur 9
eine vergrößerte schematische Schnittdarstellung eines Teils der Vorrichtung von Figur 7 bei geschlossener Ventilnadel, und
Figur 10
eine vergrößerte schematische Schnittdarstellung eines Teils der Vorrichtung von Figur 7 bei geöffneter Ventilnadel.
Hereinafter, embodiments of the invention will be described in detail with reference to the accompanying drawings. In the drawing is:
FIG. 1
a schematically simplified sectional view of the device according to the invention with a closed valve needle
FIG. 2
an enlarged schematic sectional view of a part of the device of FIG. 1 .
FIG. 3
a schematically simplified sectional view of the device of FIG. 1 when opening the valve needle,
FIG. 4
a schematically simplified sectional view of the device of FIG. 1 with open valve needle,
FIG. 5
an enlarged schematic sectional view of a part of the device of FIG. 4 .
FIG. 6
a schematically simplified sectional view of the device of FIG. 1 when closing the valve needle,
FIG. 7
a schematically simplified sectional view of a second embodiment of the device with the valve needle closed,
FIG. 8
a schematically simplified sectional view of the device of FIG. 7 with open valve needle,
FIG. 9
an enlarged schematic sectional view of a part of the device of FIG. 7 with closed valve needle, and
FIG. 10
an enlarged schematic sectional view of a part of the device of FIG. 7 with open valve needle.

Nachfolgend wird unter Bezugnahme auf die Figuren 1 bis 6 eine Vorrichtung 1 zur Kraftstoffhochdruckeinspritzung gemäß einem ersten bevorzugten Ausführungsbeispiel der Erfindung im Detail beschrieben.The following is with reference to the FIGS. 1 to 6 a device 1 for high-pressure fuel injection according to a first preferred embodiment of the invention described in detail.

Figur 1 zeigt eine schematisch vereinfachte Schnittdarstellung der erfindungsgemäßen Vorrichtung im geschlossenen Zustand. Wie aus der schematischen Schnittdarstellung von Figur 1 ersichtlich, umfasst die Vorrichtung 1 ein Ventilgehäuse 2, eine nach außen öffnende Ventilnadel 3, welche im Ventilgehäuse 2 in einem mit Kraftstoff gefüllten Druckraum 4 angeordnet ist. Diesem Druckraum 4 wird ein Kraftstoff K über einen Kraftstoffzulauf 24 unter Druck zugeführt, wobei die Ventilnadel 3 an einem Ventilsitz 16 am Ventilgehäuse 2 abdichtet. Ferner weist die Vorrichtung 1 eine Schließfeder 5, welche die Ventilnadel 3 in eine Ausgangsposition zurückführt, und einen elektromagnetischen Aktuator 6 mit einer Magnetspule 63, einem Innenpol 62, einem Magnetgehäuse 61 und einem beweglich angeordneten Magnetanker 7 auf, der die Ventilnadel 3 über einen daran ausgebildeten bzw. befestigten Mitnehmer 9 betätigt. Ein Steuerventil 8 mit einem Ventilelement 10 und einem Ventilsitz 11 ist an einem der Einspritzseite entgegengesetzten Endbereich 29 der Ventilnadel 3 angeordnet. FIG. 1 shows a schematically simplified sectional view of the device according to the invention in the closed state. As from the schematic sectional view of FIG. 1 As can be seen, the device 1 comprises a valve housing 2, an outwardly opening valve needle 3, which is arranged in the valve housing 2 in a pressure chamber 4 filled with fuel. This pressure chamber 4, a fuel K is supplied via a fuel inlet 24 under pressure, wherein the valve needle 3 seals on a valve seat 16 on the valve housing 2. Furthermore, the device 1 has a closing spring 5, which returns the valve needle 3 to a starting position, and an electromagnetic actuator 6 with a magnetic coil 63, an inner pole 62, a magnet housing 61 and a movably arranged magnet armature 7, the valve needle 3 via a thereto trained or attached driver 9 is actuated. A control valve 8 having a valve element 10 and a valve seat 11 is arranged on an end region 29 of the valve needle 3 opposite the injection side.

Das Ventilelement 10 weist eine erste Wirkfläche 13, die dem Druckraum 4 zugewandt ist, und eine zweite Wirkfläche 14 auf, die einer Druckkammer 12 zugewandt ist, die mit einem Niederdruckbereich 19 in Verbindung steht. Das Ventilelement 10 des Steuerventils 8 ist ausgelegt, um eine Verbindung zwischen dem Druckraum 4 und der Druckkammer 12 freizugeben und zu verschließen, wobei der Ventilsitz 11 des Steuerventils 8 an einer Stirnseite eines am Magnetanker 7 befestigten ringzylindrischen Bauteils 17 angeordnet ist. Zwischen dem Außenumfang des ringzylindrischen Bauteils 17 und dem Ventilgehäuse 2 ist eine Spaltdichtung 18 mit geringem Führungsspiel ausgebildet.The valve element 10 has a first active surface 13, which faces the pressure chamber 4, and a second active surface 14, which faces a pressure chamber 12, which communicates with a low-pressure region 19. The valve element 10 of the control valve 8 is designed to release and close a connection between the pressure chamber 4 and the pressure chamber 12, the valve seat 11 of the control valve 8 being arranged on an end face of a ring-cylindrical component 17 fastened to the magnet armature 7. Between the outer circumference of the annular cylindrical member 17 and the valve housing 2, a gap seal 18 is formed with a small guide clearance.

Wie aus Figur 1 ferner ersichtlich, sind im Magnetanker 7 und im ringzylindrischen Bauteil 17 Durchflussöffnungen 30, 31, für die Zuführung des Kraftstoffs K ausgebildet. Demzufolge liegt bei geschlossener Ventilnadel 3 und geschlossenem Steuerventil 8 der hohe Druck des über den Kraftstoffzulauf 24 zugeführten Kraftstoffs in allen mit der Druckkammer 4 verbundenen Innenräumen der Vorrichtung an. In der Druckkammer 12 herrscht Niederdruck, da diese über eine Drossel 21 mit dem Kraftstoffrücklauf 25 verbunden ist und das Steuerventil 8 geschlossen ist.How out FIG. 1 Furthermore, 17 flow through openings 30, 31, for the supply of the fuel K are formed in the armature 7 and the annular cylindrical member. Accordingly, when the valve needle 3 is closed and the control valve 8 is closed, the high pressure of the fuel inlet 24 is present supplied fuel in all connected to the pressure chamber 4 interior spaces of the device. In the pressure chamber 12, there is low pressure, since it is connected via a throttle 21 to the fuel return 25 and the control valve 8 is closed.

Da bei der erfindungsgemäßen Vorrichtung 1 ein Durchmesser ds des Ventilsitzes 16 kleiner gewählt ist als ein Durchmesser d1 des Ventilelements 10, wird die Ventilnadel 3 neben der Kraft der Schließfeder 5 zusätzlich auch durch eine hydraulische Kraftkomponente in den Ventilsitz 16 gedrückt, die aus dieser Durchmesserdifferenz resultiert. Dadurch ist eine zuverlässige Abdichtung der Vorrichtung 1 bei geschlossener Ventilnadel 3 gewährleistet.Since, in the device 1 according to the invention, a diameter ds of the valve seat 16 is selected to be smaller than a diameter d1 of the valve element 10, the valve needle 3 is additionally pressed, in addition to the force of the closing spring 5, into the valve seat 16 by a hydraulic force component resulting from this difference in diameter , As a result, a reliable sealing of the device 1 is ensured when the valve needle 3 is closed.

Figur 2 zeigt eine vergrößerte schematische Schnittdarstellung, die einen Teil der Vorrichtung 1 von Figur 1 detaillierter veranschaulicht. Wie aus der Abbildung von Figur 2 ersichtlich, befindet sich beim geschlossenen Zustand der Vorrichtung 1 mit geschlossenem Steuerventil 8 und inaktiviertem elektromagnetischen Aktuator 6 dessen Magnetanker 7 in seiner Ausgangsposition. Die Schließfeder 5 greift dabei am Magnetanker 7 an und stützt sich am Gehäuse 2 ab. In dieser Ausgangsposition weist der axial frei bewegliche Magnetanker 7 aufgrund der Federkraft der Schließfeder 5 einen Abstand A zum Mitnehmer 9 an der Ventilnadel 3, sowie einen Abstand H zum Innenpol 62 auf. FIG. 2 shows an enlarged schematic sectional view showing a part of the device 1 of FIG. 1 illustrated in more detail. As from the picture of FIG. 2 can be seen, located in the closed state of the device 1 with a closed control valve 8 and inactivated electromagnetic actuator 6 whose armature 7 in its initial position. The closing spring 5 acts on the armature 7 and is supported on the housing 2 from. In this initial position, the axially freely movable armature 7 due to the spring force of the closing spring 5 a distance A to the driver 9 on the valve needle 3, and a distance H to the inner pole 62.

Figur 3 zeigt eine schematisch vereinfachte Schnittdarstellung der Vorrichtung 1 von Figur 1 beim Öffnen der Ventilnadel 3. Hierbei wird die Magnetspule 63 des elektromagnetischen Aktuators 6 bestromt (was durch ein blitzförmiges Symbol verdeutlicht ist), wobei der Magnetanker 7 einen ersten Teilhub in Richtung zum Innenpol 62 ausführt, der dem Maß des Abstands A entspricht, bis er den Mitnehmer 9 berührt. Dadurch öffnet sich das Steuerventil 8, so dass Kraftstoff K vom Kraftstoffzulauf 24 in den Druckraum 4 und über die Durchflussöffnung 31 bis in die Druckkammer 12 strömt (wie dies durch einen Pfeil B in der Figur 3 verdeutlicht ist). Dadurch steigt der Druck in der Druckkammer 12 unmittelbar an und bewirkt eine Kraft auf die Ventilnadel 3, die aus dem Verhältnis der hydraulisch wirksamen ersten und zweiten Wirkflächen 13 und 14 am Ventilelement 10 resultiert, die jeweils mit hohem Druck beaufschlagt sind. Diese resultierende hydraulische Kraft wirkt bei geöffnetem Steuerventil 8 zusätzlich zur Magnetkraft des Magnetankers 7 in Öffnungsrichtung der Ventilnadel 3 und verringert die Anpresskraft der Ventilnadel 3 am Ventilsitz 16. Die Ventilnadel 3 kann nun mit geringer Kraft vom Magnetanker 3 über den Mitnehmer 9 in Öffnungsrichtung mitgenommen bzw. verschoben werden, so dass sich die Ventilnadel 3 öffnet und der Einspritzvorgang beginnen kann. FIG. 3 shows a schematically simplified sectional view of the device 1 of FIG. 1 When opening the valve needle 3. In this case, the magnetic coil 63 of the electromagnetic actuator 6 is energized (which is illustrated by a lightning-shaped symbol), the armature 7 performs a first partial stroke in the direction of the inner pole 62, which corresponds to the degree of the distance A, until he the driver 9 touched. As a result, the control valve 8 opens so that fuel K flows from the fuel inlet 24 into the pressure chamber 4 and via the flow opening 31 into the pressure chamber 12 (as indicated by an arrow B in FIG FIG. 3 is clarified). As a result, the pressure in the pressure chamber 12 rises directly and causes a force on the valve needle 3, which results from the ratio of the hydraulically effective first and second active surfaces 13 and 14 on the valve element 10, which are each subjected to high pressure. This resulting hydraulic force acts in the open control valve 8 in addition to Magnetic force of the armature 7 in the opening direction of the valve needle 3 and reduces the contact pressure of the valve needle 3 on the valve seat 16. The valve needle 3 can now be taken or moved with little force from the armature 3 via the driver 9 in the opening direction, so that the valve needle 3 opens and the injection process can begin.

Figur 4 zeigt eine schematisch vereinfachte Schnittdarstellung der Vorrichtung von Figur 1 bei geöffneter Ventilnadel. Durch die fortgesetzte Bestromung der Magnetspule 63 wurde der Magnetanker 7 zusammen mit der Ventilnadel 3 in Öffnungsrichtung der Vorrichtung 1 gezogen und hat einen zweiten Teilhub bis zum Anschlag am Innenpol 62 ausgeführt, und dadurch die Ventilnadel 3 vom Ventilsitz 16 nach außen angehoben und geöffnet. Der zweite Teilhub zum Öffnen der Ventilnadel 3 ist hierbei größer ausgelegt als der erste Teilhub A zum Öffnen des Steuerventils 8. Das zwischen der Ventilnadel 3 und dem Ventilgehäuse 2 ausströmende Kraftstoffspray ist durch kleine Pfeile C in der Figur 4 veranschaulicht. FIG. 4 shows a schematically simplified sectional view of the device of FIG. 1 with open valve needle. Due to the continued energization of the solenoid 63, the magnet armature 7 was pulled together with the valve needle 3 in the opening direction of the device 1 and has a second partial stroke to stop at the inner pole 62 executed, and thereby raised the valve needle 3 from the valve seat 16 to the outside and opened. The second partial stroke for opening the valve needle 3 is here designed to be larger than the first partial stroke A for opening the control valve 8. The effluent between the valve needle 3 and the valve housing 2 fuel spray is indicated by small arrows C in the FIG. 4 illustrated.

Figur 5 zeigt eine vergrößerte schematische Schnittdarstellung, die einen Teil der Vorrichtung 1 von Figur 4 detaillierter veranschaulicht. Wie aus der Abbildung von Figur 5 ersichtlich, strömt bei geöffnetem Steuerventil 8 ein Teil des Kraftstoffs in der Druckkammer 12 über die Drossel 21 (wie durch einen Pfeil D verdeutlicht) in den Kraftstoffrücklauf 25 als Leckagemenge zurück. Diese Leckagemenge durch die Drossel 21 ist definiert bzw. auf einen vorgegebenen Wert begrenzt, damit der Druckabfall in der Druckkammer 12 nach dem Abschalten des elektromagnetischen Aktuators 6 (Schließen der Ventilnadel 3) nicht zu lange dauert und die Pausenzeiten der Schaltzyklen verlängert und somit die Schaltdynamik verschlechtert. FIG. 5 shows an enlarged schematic sectional view showing a part of the device 1 of FIG. 4 illustrated in more detail. As from the picture of FIG. 5 can be seen with open control valve 8, a portion of the fuel in the pressure chamber 12 via the throttle 21 (as illustrated by an arrow D) in the fuel return 25 as a leakage amount back. This leakage amount through the throttle 21 is defined or limited to a predetermined value, so that the pressure drop in the pressure chamber 12 after switching off the electromagnetic actuator 6 (closing the valve needle 3) does not take too long and extends the dead times of the switching cycles and thus the switching dynamics deteriorated.

In Figur 6 ist eine schematisch vereinfachte Schnittdarstellung der Vorrichtung von Figur 1 beim Schließen der Ventilnadel 3 veranschaulicht. Hierbei ist der Zustand der Vorrichtung 1 gezeigt, der sich nach dem Abschalten der Magnetspule 63 des elektromagnetischen Aktuators 6 einstellt, wobei zuerst das Steuerventil 8 geschlossen wird. Danach sinkt der Druck in der Druckkammer 12 aufgrund der Verbindung zum Kraftstoffrücklauf 25 über die Drossel 21 wieder ab, so dass die zweite Wirkfläche 14 nur noch mit dem niedrigen Druck aus dem Kraftstoffrücklauf 25 beaufschlagt ist. Die erste Wirkfläche 13 ist noch mit dem hohen Druck im Inneren des ringzylindrischen Bauteils 17 beaufschlagt. Dadurch wird eine hydraulische Schließkraft erzeugt, die die Ventilnadel 3 zusätzlich zur Federkraft der Schließfeder 5 in den Ventilsitz 16 drückt, bis der geschlossene Zustand der Ventilnadel 3 (vgl. Figur 1) wieder hergestellt und der Einspritzvorgang beendet ist. Die Schließfeder 5 greift dabei über den Magnetanker 7, das ringzylindrische Bauteil 17 und das Ventilelement 10 an der Ventilnadel 3 an.In FIG. 6 is a schematically simplified sectional view of the device of FIG. 1 illustrated when closing the valve needle 3. Here, the state of the device 1 is shown, which adjusts after switching off the solenoid 63 of the electromagnetic actuator 6, wherein first the control valve 8 is closed. Thereafter, the pressure in the pressure chamber 12 drops due to the connection to the fuel return 25 via the throttle 21 again, so that the second effective surface 14 is acted upon only with the low pressure from the fuel return 25. The first active surface 13 is still with the high pressure in the interior of the annular cylindrical member 17 acted upon. As a result, a hydraulic closing force is generated which presses the valve needle 3 in addition to the spring force of the closing spring 5 in the valve seat 16 until the closed state of the valve needle 3 (see. FIG. 1 ) is restored and the injection process is completed. The closing spring 5 acts on the magnet armature 7, the annular cylindrical component 17 and the valve element 10 on the valve needle 3.

Dadurch, dass das Öffnen und Schließen der Ventilnadel 3 der erfindungsgemäßen Vorrichtung 1 zur Kraftstoffhochdruckeinspritzung hydraulisch unter Nutzung des im Inneren der Vorrichtung 1 herrschenden Hochdrucks in Verbindung mit den am Ventilelement 10 des Steuerventils 8 angeordneten ersten und zweiten Wirkflächen 13 und 14 unterstützt wird, kann die Vorrichtung 1 bereits mit verhältnismäßig geringen Magnetkräften eine hohe Schaltdynamik bei gleichzeitig hoher Dichtkraft bereitstellen.The fact that the opening and closing of the valve needle 3 of the device 1 according to the invention for high-pressure fuel injection is hydraulically assisted by using the prevailing inside the device 1 high pressure in conjunction with the arranged on the valve element 10 of the control valve 8 first and second active surfaces 13 and 14, the Device 1 already with relatively low magnetic forces provide a high switching dynamics at the same time high sealing force.

Nachfolgend wird unter Bezugnahme auf die Figuren 7 bis 10 eine Vorrichtung 1 zur Kraftstoffhochdruckeinspritzung gemäß einem zweiten bevorzugten Ausführungsbeispiel der Erfindung im Detail beschrieben. Gleiche bzw. funktional gleiche Teile sind mit den gleichen Bezugszeichen wie im ersten Ausführungsbeispiel bezeichnet.The following is with reference to the FIGS. 7 to 10 a device 1 for high-pressure fuel injection according to a second preferred embodiment of the invention described in detail. Identical or functionally identical parts are denoted by the same reference numerals as in the first embodiment.

Figur 7 zeigt eine schematisch vereinfachte Schnittdarstellung eines zweiten Ausführungsbeispiels der erfindungsgemäßen Vorrichtung 1 zur Kraftstoffhochdruckeinspritzung bei geschlossener Ventilnadel 3. Das zweite Ausführungsbeispiel der erfindungsgemäßen Vorrichtung 1 unterscheidet sich vom zuvor beschriebenen ersten Ausführungsbeispiel dadurch, dass hierbei zwischen der Druckkammer 12 und dem Niederdruckbereich 19 des Kraftstoffrücklaufs 25 ein Leckagesperrventil 26 angeordnet ist. Durch das Leckagesperrventil 26 wird eine Leckagemenge zum Kraftstoffrücklauf 25, wie sie beim ersten Ausführungsbeispiel in der Drossel 21 auftritt, drastisch reduziert. Das Leckagesperrventil 26 weist eine kragenartige Erweiterung 22 des Durchmessers am Endbereich 29 der Ventilnadel 3 auf. In Verbindung mit einem am Ausgang der Druckkammer 12 angeordneten Anschlag 23 am Ventilgehäuse 2 sperrt das Leckagesperrventil 26 im geschlossenem Zustand die Druckkammer 12 vom Kraftstoffrücklauf 25 ab. FIG. 7 shows a schematically simplified sectional view of a second embodiment of the inventive device 1 for high-pressure fuel injection with the valve needle closed 3. The second embodiment of the device 1 according to the invention differs from the first embodiment described above in that in this case between the pressure chamber 12 and the low pressure region 19 of the fuel return 25, a leakage check valve 26 is arranged. By the leakage check valve 26 is a leakage amount to the fuel return 25, as occurs in the first embodiment in the throttle 21, drastically reduced. The leakage check valve 26 has a collar-like extension 22 of the diameter at the end region 29 of the valve needle 3. In conjunction with a arranged at the output of the pressure chamber 12 stop 23 on the valve housing 2, the leakage check valve 26 closes the pressure chamber 12 from the fuel return 25 in the closed state.

Wie aus Figur 7 ferner ersichtlich, ist bei geschlossener Ventilnadel 3 das Steuerventil 8 geschlossen und das Leckagesperrventil 26 geöffnet, sodass in der Druckkammer 12 ein Niederdruck herrscht.How out FIG. 7 Furthermore, it can be seen, when the valve needle 3 is closed, the control valve 8 is closed and the leakage check valve 26 is opened so that a low pressure prevails in the pressure chamber 12.

Figur 9 zeigt eine vergrößerte schematische Schnittdarstellung eines Teils der Vorrichtung von Figur 7, die die Druckverhältnisse bei geschlossener Ventilnadel 3 veranschaulicht. Wie aus Figur 9 ersichtlich, ist eine Ringnut 27 im Ventilgehäuse 2 in einem Bereich zwischen dem ringzylindrischen Bauteil 17 und dem Ventilelement 10 des Steuerventils 8 ausgebildet, um einen ungehinderten Kraftstoffzufluss in die Druckkammer 12 bei geöffnetem Steuerventil 8 (vgl. hierzu Figur 10) zu ermöglichen. Bei geschlossener Ventilnadel 3 ist das Steuerventil 8 geschlossen und das Leckagesperrventil 26 geöffnet. Hierbei ist hinter dem geschlossenen Ventilelement 10 des Steuerventils 8, d. h. in der Ringnut 27, der Druckkammer 12 und im angrenzenden Kraftstoffrücklauf 25 Niederdruck vorhanden (gekennzeichnet mit dem Bezugszeichen 19), während in den übrigen Innenräumen der Vorrichtung 1 bis zum geschlossenen Ventilelement 10 Hochdruck anliegt (gekennzeichnet mit dem Bezugszeichen 28). FIG. 9 shows an enlarged schematic sectional view of a part of the device of FIG. 7 , which illustrates the pressure conditions when the valve needle 3 is closed. How out FIG. 9 can be seen, an annular groove 27 is formed in the valve housing 2 in a region between the annular cylindrical member 17 and the valve element 10 of the control valve 8 to an unimpeded fuel flow into the pressure chamber 12 with open control valve 8 (see FIG. 10 ). When the valve needle 3 is closed, the control valve 8 is closed and the leakage check valve 26 is opened. Here, behind the closed valve element 10 of the control valve 8, ie in the annular groove 27, the pressure chamber 12 and the adjacent fuel return 25 low pressure present (indicated by the reference numeral 19), while in the remaining interiors of the device 1 to the closed valve element 10 high pressure is applied (indicated by reference numeral 28).

Wie aus Figur 8 ersichtlich, die eine schematisch vereinfachte Schnittdarstellung der zweiten Ausführungsform von Figur 7 bei geöffneter Ventilnadel 3 zeigt, ist in diesem Zustand das Leckagesperrventil 26 geschlossen und das Steuerventil 8 geöffnet. Hierbei herrscht in der Druckkammer 12 Hochdruck, sodass die Ventilnadel 3 mit kleinen Kräften geöffnet werden kann. Da das Leckagesperrventil 26 geschlossen ist, tritt keine Leckagemenge in den Kraftstoffrücklauf 25 aus. Die am Anschlag 23 anliegende kragenartige Erweiterung 22 des Leckagesperrventils 26 definiert zugleich einen Hubanschlag der geöffneten Ventilnadel 3.How out FIG. 8 can be seen, which is a schematically simplified sectional view of the second embodiment of FIG. 7 when the valve needle 3 is open, in this state, the leakage check valve 26 is closed and the control valve 8 is opened. In this case, high pressure prevails in the pressure chamber 12, so that the valve needle 3 can be opened with small forces. Since the leakage check valve 26 is closed, no amount of leakage into the fuel return 25 occurs. The collar-like extension 22 of the leakage check valve 26 that adjoins the stop 23 at the same time defines a stroke stop of the opened valve needle 3.

Figur 10 zeigt eine vergrößerte schematische Schnittdarstellung eines Teils der Vorrichtung von Figur 8, die die Druckverhältnisse bei geöffneter Ventilnadel 3 veranschaulicht. Wie aus Figur 10 ersichtlich, ist hierbei das Steuerventil 8 geöffnet und das Leckagesperrventil 26 geschlossen. Der Hochdruckbereich 28 ist hierbei sowohl im Steuerventil 8 als auch im Leckagesperrventil 26 ausgebildet, während lediglich im Kraftstoffrücklauf 25 der Niederdruckbereich 19 ausgebildet ist. FIG. 10 shows an enlarged schematic sectional view of a part of the device of FIG. 8 , which illustrates the pressure conditions when the valve needle 3 is open. How out FIG. 10 can be seen, in this case the control valve 8 is opened and the leakage check valve 26 is closed. The high-pressure region 28 is in this case both in the control valve 8 and in the leakage check valve 26 formed while only in the fuel return 25 of the low pressure region 19 is formed.

Aufgrund der geringen Kräfte, die bei der erfindungsgemäßen Vorrichtung 1 zur Kraftstoffhochdruckeinspritzung zum Öffnen und Schließen der Ventilnadel 3 erforderlich sind, kann die Betätigung der Ventilnadel 3 direkt durch einen kostengünstigen elektromagnetischen Aktuator, auch bei hohen Einspritzdrücken von 20 MPa, mit einer ausreichend hohen Schaltdynamik erfolgen. Wegen des dementsprechend geringen Leistungsbedarfs des elektromagnetischen Aktuators kann die Ansteuerung der Vorrichtung 1 deshalb mit herkömmlichen, d. h. verfügbaren Endstufen für Magnet-Hochdruckeinspritzventile erfolgen. Dies trägt zu einer weiteren Kostenreduzierung und somit einer erhöhten Wirtschaftlichkeit der erfindungsgemäßen Vorrichtung 1 zur Kraftstoffhochdruckeinspritzung bei.Due to the low forces that are required in the inventive device 1 for high-pressure fuel injection for opening and closing the valve needle 3, the actuation of the valve needle 3 can be done directly by a low-cost electromagnetic actuator, even at high injection pressures of 20 MPa, with a sufficiently high switching dynamics , Because of the correspondingly low power requirement of the electromagnetic actuator, the control of the device 1 can therefore be compared with conventional, d. H. available power amplifiers for solenoid high-pressure injection valves. This contributes to a further cost reduction and thus to increased cost-effectiveness of the inventive device 1 for high-pressure fuel injection.

Claims (9)

  1. Device for high-pressure fuel injection, comprising
    - a valve housing (2),
    - an outwardly opening valve needle (3) which is arranged in the valve housing (2) in a fuel-filled pressure space (4) to which fuel (K) is supplied under pressure, wherein the valve needle (3) is sealed off at a valve seat (16),
    - a closing spring (5) which returns the valve needle (3) to a starting position,
    - an electromagnetic actuator (6) with a movably arranged magnet armature (7) for actuating the valve needle (3),
    characterized in that a control valve (8) with a valve element (10) and a valve seat (11) is provided, wherein the valve element (10) has a first active surface (13) and a second active surface (14), wherein the first active surface (13) faces the pressure space (4), the second active surface (14) faces a pressure chamber (12) which is connected to a low-pressure region (19), and the valve element (10) enables and closes a connection between the pressure space (4) and the pressure chamber (12), and the valve seat (11) is arranged on the magnet armature (7) or on a component connected to the magnet armature (7), wherein during an activation of the electromagnetic actuator (6) the control valve (8) opens ahead of the outwardly opening valve needle (3) in order to reduce an opening force for the valve needle (3) by enabling the connection between the pressure space (4) and the pressure chamber (12).
  2. Device for high-pressure fuel injection according to Claim 1, further comprising a driver (9) which is fastened to the valve needle (3) and has an armature contact region (20), wherein the driver (9) is arranged at a distance (A) from the magnet armature (7) in the starting position, and the magnet armature (7) is movably arranged on the valve needle (3).
  3. Device for high-pressure fuel injection according to Claim 1 or 2, characterized in that an annularly cylindrical component (17) is fastened to the magnet armature (7), wherein the valve seat (11) of the control valve (8) is arranged on a free end face of the annularly cylindrical component (17).
  4. Device for high-pressure fuel injection according to Claim 3, characterized in that a gap seal (18) is formed between the outer circumference of the annularly cylindrical component (17) and the valve housing (2).
  5. Device for high-pressure fuel injection according to Claim 4, characterized in that a diameter (d1) of the gap seal (18) is greater than a diameter (ds) of the valve seat (16).
  6. Device for high-pressure fuel injection according to Claims 2 to 5, characterized in that the distance (A) between driver (9) and magnet armature (7) in the starting position is smaller than a difference of a total travel (H) of the magnet armature (7) and the distance (A).
  7. Device for high-pressure fuel injection according to one of the preceding claims, characterized in that a throttle (21) is arranged between the pressure chamber (12) and the low-pressure region (19).
  8. Device for high-pressure fuel injection according to one of Claims 1 to 6, characterized in that a leakage shut-off valve (26) is arranged between the pressure chamber (12) and the low-pressure region (19).
  9. Device for high-pressure fuel injection according to Claim 8, characterized in that the leakage shut-off valve (26) comprises as closing member a collar-like extension (22) formed on the valve needle (3), and a seat (23) of the leakage shut-off valve (26) is formed on the valve housing (2).
EP10728156A 2009-08-05 2010-06-17 Device for high-pressure fuel injection Not-in-force EP2462335B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE200910028234 DE102009028234A1 (en) 2009-08-05 2009-08-05 Device for high-pressure fuel injection
PCT/EP2010/058580 WO2011015405A1 (en) 2009-08-05 2010-06-17 Device for high-pressure fuel injection

Publications (2)

Publication Number Publication Date
EP2462335A1 EP2462335A1 (en) 2012-06-13
EP2462335B1 true EP2462335B1 (en) 2013-03-06

Family

ID=42371483

Family Applications (1)

Application Number Title Priority Date Filing Date
EP10728156A Not-in-force EP2462335B1 (en) 2009-08-05 2010-06-17 Device for high-pressure fuel injection

Country Status (4)

Country Link
EP (1) EP2462335B1 (en)
KR (1) KR101762106B1 (en)
DE (1) DE102009028234A1 (en)
WO (1) WO2011015405A1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101776313B1 (en) 2011-06-30 2017-09-07 현대자동차주식회사 Low Pressure Injection Injector
KR101765938B1 (en) 2011-06-30 2017-08-07 현대자동차주식회사 Low Pressure Injection Injector
US8616474B2 (en) * 2011-09-09 2013-12-31 Continental Automotive Systems, Inc. High flow outward opening gaseous injector for automotive applications
DE102013206385A1 (en) 2013-04-11 2014-10-16 Robert Bosch Gmbh Valve for metering fluid
US9625264B1 (en) 2016-01-20 2017-04-18 Denso Corporation Systems and methods for displaying route information

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AUPN391295A0 (en) 1995-06-30 1995-07-27 Orbital Engine Company (Australia) Proprietary Limited Fuel injection apparatus
DE602005003964T2 (en) 2005-11-02 2008-05-08 Delphi Technologies, Inc., Troy Method for designing a fuel injection valve
DE102007038430A1 (en) 2007-08-14 2009-02-19 Robert Bosch Gmbh Fuel e.g. diesel fuel, injection valve mechanism for internal-combustion engine, has control valve provided with area whose pressure indirectly affects needle, where area is connected with pressure chamber, and closing body having stroke

Also Published As

Publication number Publication date
DE102009028234A1 (en) 2011-02-17
EP2462335A1 (en) 2012-06-13
KR20120040731A (en) 2012-04-27
KR101762106B1 (en) 2017-07-27
WO2011015405A1 (en) 2011-02-10

Similar Documents

Publication Publication Date Title
EP2183476B1 (en) Fuel injection valve with improved tightness on the sealing seat of a pressure-compensated control valve
DE102010028835A1 (en) fuel injector
EP3478957B1 (en) Valve for injecting gaseous fuel
EP2462335B1 (en) Device for high-pressure fuel injection
WO2007000371A1 (en) Injector with a pressure intensifier that can be switched on
DE102016220326A1 (en) Valve for metering a gaseous or liquid fuel
DE102012220860A1 (en) Fuel injector with magnetic actuator
DE102004015744A1 (en) Common rail injector
DE102014217441A1 (en) Electromagnetically actuated proportional valve
DE102005010453A1 (en) Fuel injection valve for internal combustion engines
DE102005015731A1 (en) Fuel injector with piezo actuator
EP2454467A1 (en) Valve arrangement
DE102012222127A1 (en) Fuel injector for injecting fuel into combustion chamber of internal combustion engine, has hydraulic coupler that is comprised of pair of coupler piston for separating two couplers
DE102015226070A1 (en) fuel injector
DE10224689A1 (en) Stroke-controlled valve as a fuel metering device of an injection system for internal combustion engines
DE102008042531A1 (en) Valve arrangement for fuel high pressure injection, comprises electromagnets, anchor, sliding sleeve and housing provided with spraying holes, where interior element divides interior space of housing
DE102011083260A1 (en) Fuel injection valve for internal combustion engines
EP1961953A1 (en) Multiway valve
EP3032090B1 (en) Switching or pressure control valve for a fuel injection system
DE102010044205A1 (en) fuel injector
WO2010108747A1 (en) Fuel injection device
DE102006036782B4 (en) injector
DE102015224421A1 (en) Electromagnetically actuated inlet valve and high-pressure pump with inlet valve
DE102007040248A1 (en) Control valve for a fuel injector
DE102014211469A1 (en) Nozzle assembly for a fuel injector and fuel injector

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: 20120305

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 SE SI SK SM TR

DAX Request for extension of the european patent (deleted)
GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

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 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

Ref country code: AT

Ref legal event code: REF

Ref document number: 599767

Country of ref document: AT

Kind code of ref document: T

Effective date: 20130315

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: 502010002475

Country of ref document: DE

Effective date: 20130502

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

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: 20130306

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: 20130606

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: 20130617

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: 20130606

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: 20130306

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20130306

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: 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: 20130607

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: 20130306

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: 20130306

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: 20130306

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

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: 20130306

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

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: 20130708

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: 20130306

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: 20130306

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: 20130306

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: 20130306

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: 20130706

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: 20130306

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

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: 20130306

BERE Be: lapsed

Owner name: ROBERT BOSCH G.M.B.H.

Effective date: 20130630

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: 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: 20130306

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: 20130306

26N No opposition filed

Effective date: 20131209

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502010002475

Country of ref document: DE

Effective date: 20131209

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: BE

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

Effective date: 20130630

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

Ref country code: IE

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

Effective date: 20130617

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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: 20130306

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: 20140630

Ref country code: CH

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

Effective date: 20140630

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: 20130306

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: 20130306

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: 20130306

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: 20130306

Ref country code: LU

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

Effective date: 20130617

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: 20100617

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 7

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

Ref country code: GB

Payment date: 20160628

Year of fee payment: 7

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 599767

Country of ref document: AT

Kind code of ref document: T

Effective date: 20150617

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

Ref country code: FR

Payment date: 20160621

Year of fee payment: 7

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

Ref country code: IT

Payment date: 20160621

Year of fee payment: 7

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: 20150617

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

Effective date: 20170617

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20180228

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: 20170617

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: 20170630

Ref country code: IT

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

Effective date: 20170617

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: 20130306

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

Ref country code: DE

Payment date: 20190822

Year of fee payment: 10

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 502010002475

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: 20210101