EP2204570B1 - Fuel injector - Google Patents

Fuel injector Download PDF

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Publication number
EP2204570B1
EP2204570B1 EP20090174566 EP09174566A EP2204570B1 EP 2204570 B1 EP2204570 B1 EP 2204570B1 EP 20090174566 EP20090174566 EP 20090174566 EP 09174566 A EP09174566 A EP 09174566A EP 2204570 B1 EP2204570 B1 EP 2204570B1
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EP
European Patent Office
Prior art keywords
nozzle needle
fuel injector
valve
pressure
fuel
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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
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EP20090174566
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German (de)
French (fr)
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EP2204570A1 (en
Inventor
Sebastian Jansen
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Robert Bosch GmbH
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Robert Bosch GmbH
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Publication of EP2204570A1 publication Critical patent/EP2204570A1/en
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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
    • F02M45/00Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship
    • F02M45/02Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts
    • F02M45/04Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts with a small initial part, e.g. initial part for partial load and initial and main part for full load
    • F02M45/08Injectors peculiar thereto
    • F02M45/086Having more than one injection-valve controlling discharge orifices
    • 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
    • F02M47/00Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure
    • F02M47/06Other fuel injectors peculiar thereto
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/042The valves being provided with fuel passages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1893Details of valve member ends not covered by groups F02M61/1866 - F02M61/188
    • 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
    • F02M2200/46Valves, e.g. injectors, with concentric valve bodies
    • 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
    • F02M2547/00Special features for fuel-injection valves actuated by fluid pressure
    • F02M2547/005Fuel injectors without fuel return, i.e. the pressure in the control chamber is released into the combustion chamber with fluid flow only in one direction

Definitions

  • the invention relates to a fuel injector for injecting fuel, in particular diesel or gasoline, into a combustion chamber of an internal combustion engine.
  • Common rail diesel injectors must open or close the flow cross section required for injection with high dynamics, so that fuel in the desired amount can flow into the combustion chamber. Due to the high fuel pressure (in future common-rail diesel systems up to 3000bar or more), the nozzle needle is pressed with great force into the nozzle needle seat. This hydraulic closing force must be overcome by the actuator of the nozzle needle when opening the fuel injector. Since the hydraulic closing force is so high in known Injektorannoen that direct actuation of the nozzle needle via an electromagnetic actuator is not possible, the nozzle needle is actuated hydraulically and / or via a piezoelectric actuator in today's fuel injectors via a servo circuit.
  • Servo driven fuel injectors include a control chamber, the pressure of which is lowered by opening a servo valve. This requires a fuel return line, since the amount of tax incurred with open servo valve at low pressure level must be returned to the fuel tank. In addition, in principle occur in some fuel injector concepts permanent leakage, which must also be returned. Both control amount and leakage lead to a significant undesirable power loss in the fuel injector, since the corresponding volume of fuel must be brought in addition to the actual injection quantity at rail pressure level. This power loss must be provided by the high-pressure pump and thus reduces the efficiency of the entire system. Furthermore, the return amount causes additional heating of the fuel injector and increases due to the required low pressure line system overhead.
  • a fuel injector which has two separate, successively openable fuel outlet regions.
  • the nozzle needle of the known fuel injector is switchable, at least at pressures beyond 1800bar, either only by means of a piezoelectric actuator and / or a possibly electromagnetically actuated servo circuit.
  • the invention has for its object to provide a fuel injector in which the applied by an actuator opening force for adjusting the nozzle needle is minimized.
  • the fuel injector should manage without a fuel return port. More preferably, the fuel injector should be actuated by means of an electromagnetic actuator.
  • the invention is based on the idea to associate the nozzle needle, preferably a nozzle needle tip, with a pressure equalization chamber delimited by the nozzle needle, whereby a hydraulic force acting in the opening direction on the nozzle needle is produced by establishing a hydraulic connection between the pressure equalization chamber and the pressure region the hydraulic closing force, at least partially, preferably completely, compensated, so that the opening force to be provided by the actuator for opening the nozzle needle, preferably to a minimum, is reduced.
  • the pressure region preferably adjoins the nozzle needle on a nozzle needle side remote from the pressure equalization chamber.
  • a pressure range of the fuel injector is understood to be the range in which injection pressure prevails at least approximately.
  • the valve for establishing the hydraulic connection between the pressure region and the pressure compensation chamber has a (substantially) smaller seat cross-section than the nozzle needle seat in order to ensure that the valve can be opened with a small actuator force.
  • the pressure region which can be hydraulically connected to the pressure equalization chamber via the valve is preferably a high pressure region of the fuel injector the preferred at least approximately rail pressure prevails.
  • injector can also be used for gasoline direct injection, wherein also in this case preferably at least approximately rail pressure prevails in the pressure range.
  • injector can also be used for gasoline direct injection, wherein also in this case preferably at least approximately rail pressure prevails in the pressure range.
  • rail pressure prevails in the pressure range.
  • the nozzle needle seat diameter can be increased, which causes a smaller internal throttling with open fuel injector, so that almost immediately before the at least one injection port rests the full rail pressure.
  • the comparatively expensive injectors with piezoelectric actuator costs can be saved.
  • the pressure compensation chamber is preferably separated hydraulically from an opening region of the at least one injection opening, preferably all of the injection openings, by means of an annular gap seal.
  • the fuel injector has only a single, in particular annular, discharge region, from which the at least one injection opening opens.
  • the injection opening is located in a region axially between a nozzle needle seat and the pressure compensation chamber.
  • the annular gap seal the hydraulic pressure equalization space of the Ausmündungs Scheme separates, radially between the nozzle needle and a nozzle body (housing part) is formed.
  • the annular gap seal is a guide gap between the nozzle needle and the nozzle body.
  • the pressure compensation chamber is arranged and dimensioned such that the hydraulic closing force acting on the nozzle needle is completely compensated, so that the actuator essentially only has to overcome frictional forces and closing spring forces for opening the nozzle needle.
  • the diameter of the annular gap seal ie preferably the diameter of the guide portion of the nozzle needle at least approximately, preferably corresponds exactly to the diameter of the nozzle needle seat.
  • valve for establishing a hydraulic connection between the pressure region and the pressure equalization chamber opens before opening the nozzle needle.
  • a hydraulic connection between the pressure region and the pressure equalization chamber is preferably produced before the start of the injection process, ie the hydraulic closing force is at least partially compensated in order then to be able to lift the nozzle needle from the nozzle needle seat with reduced actuator force.
  • the pressure build-up is preferably accelerated by the fact that the aforementioned, preferred annular gap seal separates the pressure equalization chamber from the outlet region of the at least one injection opening, so that a significant flow of fuel from the pressure compensation chamber into the combustion chamber is prevented by the injection opening.
  • the closing of the fuel injector is preferably carried out by first moving the nozzle needle back into its nozzle needle seat and then closing the valve so as to again hydraulically separate the pressure compensation chamber from the pressure region of the fuel injector.
  • a complete tightness of the fuel injector given.
  • the nozzle needle and the valve are assigned separate closing springs. By a suitable vote of the spring forces closing the nozzle needle can be ensured before the valve. Characterized in that the nozzle needle closes in front of the valve element of the valve, the displaced by the closing movement of the nozzle needle from the pressure compensation chamber fuel past the valve seat of the valve back into the pressure range.
  • the fuel injector has a single actuator. This is preferably used both for adjusting the nozzle needle between its open and closed position and for opening and closing the valve.
  • the actuator preferably acts both on a valve element of the valve and on the nozzle needle.
  • valve element in particular mechanically, is coupled to the nozzle needle, preferably in such a way that the valve opens at a time-shifted adjustment of the nozzle needle from its closed position.
  • valve element or a component permanently connected to the valve element is designed as a driver, which entrains the nozzle needle after lifting the valve element from its seat in the opening direction.
  • the closing movement of the driver preferably remains in contact with the nozzle needle until it rests on its nozzle needle seat. This can, as already indicated, by a corresponding vote of at least two closing springs (nozzle needle closing spring and valve closing spring) can be achieved.
  • valve closing spring is provided for closing the valve.
  • a nozzle needle closing spring is provided for closing the nozzle needle.
  • the spring forces of the valve closing spring and the nozzle needle closing spring are further preferably designed such that the nozzle needle reaches its closed position before the valve is closed and thus separates the pressure compensation chamber from the pressure region of the fuel injector.
  • a preferably concentric to the longitudinal central axis extending, connecting channel is provided, can flow through the fuel with the valve open from the pressure range in the pressure compensation chamber.
  • this protrudes Valve element of the valve in the axial direction into the nozzle needle in order to close the connecting channel, preferably after closing the fuel injector can.
  • the valve seat of the valve is for this purpose formed directly on the nozzle needle.
  • an embodiment of the fuel injector is particularly preferred, in which the fuel injector is return connection connection-free, that is, neither a control amount nor a leakage quantity is obtained, which must be transported back into the fuel tank.
  • the actuator for adjusting the nozzle needle and / or the valve is an electromagnetic actuator.
  • Fig. 1 is a designed as a common-rail injector fuel injector 1 for injecting fuel into a combustion chamber, not shown also one not shown internal combustion engine shown.
  • the fuel injector 1 is supplied, among other fuel injectors, not shown, via a supply line 2 with fuel under high pressure. In the case of forming the fuel injector as a diesel injector, this fuel pressure is preferably beyond 2000 bar.
  • a high-pressure pump 3 is provided, the fuel from a reservoir 4 (tank) in a high-pressure fuel storage 5 (Rail) conveys.
  • Fig. 1 results, the fuel injector 1 only an inlet port 6, but not a return port.
  • a nozzle needle 8 is guided axially adjustable.
  • the nozzle needle 8 protrudes into a pressure region 9 (here pressure chamber 10), which is designed for reasons of vibration reduction as a mini-rail.
  • the supply line 2 opens, so that at least approximately rail pressure prevails in the pressure region 9, which in turn corresponds approximately to the injection pressure.
  • Fig. 1 shows the fuel injector 1 in the closed state.
  • the nozzle needle 8 is located with a cone-shaped sealing surface 11 on a nozzle needle seat 12 formed by a peripheral shoulder of the nozzle body 7.
  • a hydraulic closing force On the nozzle needle 8 acts in the plane of the drawing down, ie in the closing direction, a hydraulic closing force, which is due to the pressurization befindlichem in the pressure region 9, under pressure fuel.
  • an actuator 14 designed as an electromagnetic actuator is provided, to which an anchor plate 15 is assigned.
  • the anchor plate 15 is also located in the pressure region 9 of the fuel injector. 1
  • FIG. 1 shows, located in the plane of the drawing directly axially below the nozzle needle seat 12, an annular Ausmündungs Scheme 16, from which a number of distributed over the circumference, introduced into the nozzle body 7 injection openings 17 open.
  • annular gap seal 19 (guide gap) is formed radially between the nozzle needle 8 and the nozzle body 7. Axial to the annular gap seal 19 is adjacent in the drawing level below a pressure compensation chamber 20 at. This is at least largely decoupled hydraulically via the annular gap seal 19 of the Ausmündungs Scheme 16.
  • the pressure compensation chamber 20 can be connected to the pressure region 9, which is arranged on the side remote from the pressure compensation chamber 20 nozzle needle side. Since the diameter of the nozzle body 7 in the guide section 18 corresponds to the diameter of the nozzle needle seat 12, the nozzle needle 8 is pressure-balanced in the axial direction at pressure-compensating space 20 connected to the pressure region 9.
  • the opening force of the (low-power) actuator 14 is sufficient to move the nozzle needle 8 from the illustrated closed position in an upward in the plane of the drawing open position, a hydraulic connection between the pressure region 9 and the pressure compensation chamber 20 must first be prepared. This is how it turns out Fig. 2 results, the actuator 14 energized. Due to the fixed connection between the armature plate 15 and the elongated valve member 21, the latter is moved in the drawing plane upwards, so that serving as a driver 24 circumferential collar 25 of the valve member 21 for axial abutment at a lower edge 26 of a through hole 27, the front side in the Nozzle needle 8 is introduced.
  • the passage opening 27 is penetrated in the axial direction by the valve element 21 - the driver 24 is thus trapped in an inner nozzle needle chamber 28.
  • Fig. 2 first opens the valve 13 so that fuel from the pressure range 9 can first flow through a radial bore 29 into the nozzle needle chamber 28 and from this through the central connecting channel 23 in the axial direction down into the pressure compensation chamber 20.
  • the connecting channel 23 is the only inlet and outlet opening of the pressure compensation chamber 20. From this open no injection openings.
  • the nozzle needle 8 is entrained in a further axial displacement movement of the valve element 21 in the plane of the drawing upwards (see. Fig. 3 ), whereby a hydraulic connection between the pressure region 9 and the Ausmündungs Scheme 16 is prepared so that fuel from the Ausmündungs Scheme 16 and from the pressure region 9 can flow directly through the injection openings 17 into the combustion chamber of the internal combustion engine.
  • the energization of the actuator 14 is interrupted.
  • valve element 21 is moved downwards in the plane of the drawing by means of a valve closing spring 32, which is supported at one end on a peripheral collar 33 of the valve element 21 and the other end, and the spring force of the valve closing spring 32 is less than the spring force of the nozzle needle spring 30. so that the downward movement of the valve element 21 and the nozzle needle 8 is initially coupled, before the nozzle needle 8 reaches its respective closed position in front of the valve element 21. Due to the closing movement of the nozzle needle, as in Fig. 4 indicated by arrows, fuel displaced from the pressure compensation chamber 20. This displaced fuel flows back through the connecting channel 23 and the radial bore 29 in the pressure region 9.
  • valve element 21 moves towards the valve seat 22 and closes the pressure compensation chamber 20 to prevent further leakage losses with the fuel injector closed from the pressure compensation chamber 20 via the annular gap seal 19 in the Ausmündungs Society 16 and from there via the injection openings 17 into the combustion chamber.
  • closing the valve 13 is again in Fig. 1 shown state reached.

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

Description

Stand der TechnikState of the art

Die Erfindung betrifft einen Kraftstoff-Injektor zum Einspritzen von Kraftstoff, insbesondere Diesel oder Benzin, in einen Brennraum einer Brennkraftmaschine.The invention relates to a fuel injector for injecting fuel, in particular diesel or gasoline, into a combustion chamber of an internal combustion engine.

Common-Rail-Diesel-Injektoren müssen den zur Einspritzung erforderlichen Strömungsquerschnitt mit hoher Dynamik öffnen bzw. schließen, so dass Kraftstoff in der gewünschten Menge in den Brennraum strömen kann. Aufgrund der hohen Kraftstoffdrücke (bei zukünftigen Common-Rail-Dieselsystemen bis zu 3000bar oder darüber) wird die Düsennadel mit großer Kraft in den Düsennadelsitz gedrückt. Diese hydraulische Schließkraft muss beim Öffnen des Kraftstoff-Injektors vom Aktuator der Düsennadel überwunden werden. Da die hydraulische Schließkraft bei bekannten Injektorkonzepten so hoch ist, dass eine direkte Betätigung der Düsennadel über einen elektromagnetischen Aktuator nicht möglich ist, wird die Düsennadel bei heutigen Kraftstoff-Injektoren über einen Servokreislauf hydraulisch und/oder über einen piezoelektrischen Aktuator betätigt. Kraftstoff-Injektoren mit Servokreislauf umfassen eine Steuerkammer, deren Druck durch Öffnen eines Servoventils abgesenkt wird. Dies erfordert eine Kraftstoffrückleitung, da die bei geöffnetem Servoventil anfallende Steuermenge auf niedrigem Druckniveau zurück in den Kraftstofftank geleitet werden muss. Darüber hinaus tritt prinzipbedingt bei einigen Kraftstoff-Injektorkonzepten eine permanente Leckage auf, die ebenfalls zurückgeführt werden muss. Sowohl Steuermenge als auch Leckage führen zu einer erheblichen unerwünschten Verlustleistung im Kraftstoff-Injektor, da das entsprechende Kraftstoffvolumen zusätzlich zur eigentlichen Einspritzmenge auf Raildruckniveau gebracht werden muss. Diese Verlustleistung muss von der Hochdruckpumpe bereitgestellt werden und reduziert somit den Wirkungsgrad des Gesamtsystems. Ferner bewirkt die Rücklaufmenge eine zusätzliche Erwärmung des Kraftstoff-Injektors und erhöht aufgrund der erforderlichen Niederdruckleitung den Systemaufwand.Common rail diesel injectors must open or close the flow cross section required for injection with high dynamics, so that fuel in the desired amount can flow into the combustion chamber. Due to the high fuel pressure (in future common-rail diesel systems up to 3000bar or more), the nozzle needle is pressed with great force into the nozzle needle seat. This hydraulic closing force must be overcome by the actuator of the nozzle needle when opening the fuel injector. Since the hydraulic closing force is so high in known Injektorkonzepten that direct actuation of the nozzle needle via an electromagnetic actuator is not possible, the nozzle needle is actuated hydraulically and / or via a piezoelectric actuator in today's fuel injectors via a servo circuit. Servo driven fuel injectors include a control chamber, the pressure of which is lowered by opening a servo valve. This requires a fuel return line, since the amount of tax incurred with open servo valve at low pressure level must be returned to the fuel tank. In addition, in principle occur in some fuel injector concepts permanent leakage, which must also be returned. Both control amount and leakage lead to a significant undesirable power loss in the fuel injector, since the corresponding volume of fuel must be brought in addition to the actual injection quantity at rail pressure level. This power loss must be provided by the high-pressure pump and thus reduces the efficiency of the entire system. Furthermore, the return amount causes additional heating of the fuel injector and increases due to the required low pressure line system overhead.

Aus der DE 27 102 16 A1 ist ein Kraftstoff-Injektor bekannt, der zwei voneinander getrennte, nacheinander öffenbare Kraftstoffaustrittsbereiche aufweist. Die Düsennadel des bekannten Kraftstoff-Injektors ist zumindest bei Drücken jenseits von 1800bar entweder nur mittels eines piezoelektrischen Aktuators und/oder eines, ggf. elektromagnetisch aktuierten Servokreislaufes schaltbar.From the DE 27 102 16 A1 a fuel injector is known, which has two separate, successively openable fuel outlet regions. The nozzle needle of the known fuel injector is switchable, at least at pressures beyond 1800bar, either only by means of a piezoelectric actuator and / or a possibly electromagnetically actuated servo circuit.

Offenbarung der ErfindungDisclosure of the invention

Der Erfindung liegt die Aufgabe zugrunde, einen Kraftstoff-Injektor vorzuschlagen, bei dem die von einem Aktuator aufzubringende Öffnungskraft zum Verstellen der Düsennadel minimiert ist. Bevorzugt soll der Kraftstoff-Injektor ohne einen Kraftstoff-Rücklaufanschluss auskommen. Weiter bevorzugt soll der Kraftstoff-Injektor mittels eines elektromagnetischen Aktuators betätigbar sein.The invention has for its object to provide a fuel injector in which the applied by an actuator opening force for adjusting the nozzle needle is minimized. Preferably, the fuel injector should manage without a fuel return port. More preferably, the fuel injector should be actuated by means of an electromagnetic actuator.

Diese Aufgabe wird mit einem Kraftstoff-Injektor mit den Merkmalen des Anspruchs 1 gelöst. Vorteilhafte Weiterbildungen der Erfindung 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.This object is achieved with a fuel injector having the features of claim 1. Advantageous developments of the invention 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.

Der Erfindung liegt der Gedanke zugrunde, der Düsennadel, vorzugsweise einer Düsennadelspitze, einen Druckausgleichsraum zuzuordnen, der von der Düsennadel begrenzt wird, wobei durch Herstellen einer hydraulischen Verbindung zwischen dem Druckausgleichsraum und dem Druckbereich eine in Öffnungsrichtung auf die Düsennadel wirkende hydraulische Kraft erzeugt wird, die die hydraulische Schließkraft, zumindest teilweise, vorzugsweise vollständig, kompensiert, so dass die von dem Aktuator bereitzustellende Öffnungskraft zum Öffnen der Düsennadel, vorzugsweise auf ein Minimum, reduziert wird. Bevorzugt grenzt der Druckbereich auf einer von dem Druckausgleichsraum abgewandten Düsennadelseite an die Düsennadel an. Unter einem Druckbereich des Kraftstoff-Injektors wird dabei der Bereich verstanden, indem zumindest näherungsweise Einspritzdruck herrscht. Aufgrund des Vorsehens des mittels eines Ventils mit dem Druckbereich des Kraftstoff-Injektors verbindbaren Druckausgleichsraums kann auf einen Niederdruckbereich und somit auf einen Kraftstoffrücklaufanschluss verzichtet werden, was sich positiv auf den Wirkungsgrad des Gesamtsystems auswirkt. Insbesondere können bei einem nach dem Konzept der Erfindung ausgebildeten Kraftstoff-Injektor sämtliche Anforderungen an die Dynamik und Sprayqualität erfüllt werden. Durch den Verzicht auf einen Kraftstoffrücklauf und den einfachen Aufbau des Kraftstoff-Injektors wird der Systemaufwand verringert, was zu einer Reduzierung der Kosten sowie einem geringeren Bauraumbedarf führt. Darüber hinaus wird, wie angedeutet, die hydraulische Verlustleistung des Kraftstoff-Injektors maßgeblich reduziert, da weder ein Leckagevolumenstrom noch ein Steuervolumenstrom anfallen. Hierdurch sinkt die von der Hochdruckpumpe zu fördernde Kraftstoffmenge, was eine geringere Pumpenleistung ermöglicht. Besonders bevorzugt weist das Ventil zum Herstellen der hydraulischen Verbindung zwischen dem Druckbereich und dem Druckausgleichsraum einen (wesentlich) geringeren Sitzquerschnitt auf als der Düsennadelsitz, um zu gewährleisten, dass das Ventil mit einer geringen Aktuatorkraft öffenbar ist. Im Fall der Ausbildung des Kraftstoff-Injektors als Diesel-Injektor, insbesondere als Common-Rail-Diesel-Injektor handelt es sich bei dem Druckbereich, der über das Ventil hydraulisch mit dem Druckausgleichsraum verbindbar ist, bevorzugt um einen Hochdruckbereich des Kraftstoff-Injektors, in dem bevorzugt zumindest näherungsweise Raildruck herrscht.The invention is based on the idea to associate the nozzle needle, preferably a nozzle needle tip, with a pressure equalization chamber delimited by the nozzle needle, whereby a hydraulic force acting in the opening direction on the nozzle needle is produced by establishing a hydraulic connection between the pressure equalization chamber and the pressure region the hydraulic closing force, at least partially, preferably completely, compensated, so that the opening force to be provided by the actuator for opening the nozzle needle, preferably to a minimum, is reduced. The pressure region preferably adjoins the nozzle needle on a nozzle needle side remote from the pressure equalization chamber. A pressure range of the fuel injector is understood to be the range in which injection pressure prevails at least approximately. Due to the provision of connectable by means of a valve with the pressure range of the fuel injector pressure compensation chamber can be dispensed with a low pressure region and thus to a fuel return port, which has a positive effect on the efficiency of the overall system. In particular, in a fuel injector designed according to the concept of the invention, all requirements for dynamics and spray quality can be met. By dispensing with a fuel return and the simple structure of the fuel injector, the system cost is reduced, resulting in a reduction in costs and a smaller space requirement. In addition, as indicated, the hydraulic power loss of the fuel injector significantly reduced because neither a leakage volume flow nor a control volume flow incurred. This reduces the amount of fuel to be delivered by the high-pressure pump, which enables a lower pump capacity. Particularly preferably, the valve for establishing the hydraulic connection between the pressure region and the pressure compensation chamber has a (substantially) smaller seat cross-section than the nozzle needle seat in order to ensure that the valve can be opened with a small actuator force. In the case of the embodiment of the fuel injector as a diesel injector, in particular as a common rail diesel injector, the pressure region which can be hydraulically connected to the pressure equalization chamber via the valve is preferably a high pressure region of the fuel injector the preferred at least approximately rail pressure prevails.

Neben einer Ausbildung des Kraftstoff-Injektors als Diesel-Injektor ist ein nach dem Konzept der Erfindung ausgebildeter Injektor auch zur Benzin-Direkteinspritzung einsetzbar, wobei auch in diesem Fall im Druckbereich bevorzugt zumindest näherungsweise Raildruck herrscht. Gegenüber bekannten magnetisch betriebenen Benzin-Injektoren lassen sich durch die verringerte Betätigungskraft erhebliche Dynamikvorteile (kürzere Schaltzeiten) erzielen. Zudem kann der Düsennadelsitzdurchmesser vergrößert werden, was bei geöffnetem Kraftstoff-Injektor eine geringere interne Drosselung bewirkt, so dass unmittelbar vor der mindestens einen Einspritzöffnung nahezu der volle Raildruck anliegt. Im Vergleich zu den vergleichsweise teueren Injektoren mit Piezoaktor können zudem Kosten eingespart werden.In addition to a design of the fuel injector as a diesel injector trained according to the concept of the invention injector can also be used for gasoline direct injection, wherein also in this case preferably at least approximately rail pressure prevails in the pressure range. Compared to known magnetically operated gasoline injectors can be achieved by the reduced actuation force significant dynamics advantages (shorter switching times). In addition, the nozzle needle seat diameter can be increased, which causes a smaller internal throttling with open fuel injector, so that almost immediately before the at least one injection port rests the full rail pressure. In addition to the comparatively expensive injectors with piezoelectric actuator costs can be saved.

In Weiterbildung der Erfindung ist mit Vorteil vorgesehen, dass unmittelbar aus dem Druckausgleichsraum keine Einspritzöffnung ausmündet. Der Druckausgleichsraum ist bevorzugt mittels einer Ringspaltdichtung hydraulisch von einem Ausmündungsbereich der mindestens einen Einspritzöffnung, vorzugsweise sämtlicher Einspritzöffnungen, getrennt. Besonders bevorzugt weist der Kraftstoff-Injektor dabei nur einen einzigen, insbesondere ringförmigen Ausmündungsbereich auf, aus dem die mindestens eine Einspritzöffnung ausmündet. Bevorzugt befindet sich die Einspritzöffnung in einem Bereich axial zwischen einem Düsennadelsitz und dem Druckausgleichsraum. Besonders bevorzugt ist es, wenn die Ringspaltdichtung, die den Druckausgleichsraum hydraulisch von dem Ausmündungsbereich trennt, radial zwischen der Düsennadel und einem Düsenkörper (Gehäuseteil) gebildet ist. Ganz besonders bevorzugt handelt es sich bei der Ringspaltdichtung um einen Führungsspalt zwischen Düsennadel und Düsenkörper.In a further development of the invention is advantageously provided that no injection opening directly from the pressure equalization chamber. The pressure compensation chamber is preferably separated hydraulically from an opening region of the at least one injection opening, preferably all of the injection openings, by means of an annular gap seal. Particularly preferably, the fuel injector has only a single, in particular annular, discharge region, from which the at least one injection opening opens. Preferably, the injection opening is located in a region axially between a nozzle needle seat and the pressure compensation chamber. It is particularly preferred if the annular gap seal, the hydraulic pressure equalization space of the Ausmündungsbereich separates, radially between the nozzle needle and a nozzle body (housing part) is formed. Most preferably, the annular gap seal is a guide gap between the nozzle needle and the nozzle body.

Wie eingangs angedeutet, ist eine Ausführungsform besonders bevorzugt, bei der der Druckausgleichsraum derart angeordnet und dimensioniert ist, dass die auf die Düsennadel wirkende hydraulische Schließkraft vollständig kompensiert wird, so dass der Aktuator im Wesentlichen nur Reibungskräfte und Schließfederkräfte zum Öffnen der Düsennadel überwinden muss. Zur Realisierung einer vollkommenen Druckausgeglichenheit der Düsennadel in axialer Richtung ist es bevorzugt, wenn der Durchmesser der Ringspaltdichtung, also bevorzugt der Durchmesser des Führungsabschnitts der Düsennadel zumindest näherungsweise, vorzugsweise exakt dem Durchmesser des Düsennadelsitzes entspricht.As indicated above, an embodiment is particularly preferred in which the pressure compensation chamber is arranged and dimensioned such that the hydraulic closing force acting on the nozzle needle is completely compensated, so that the actuator essentially only has to overcome frictional forces and closing spring forces for opening the nozzle needle. To realize a perfect pressure balance of the nozzle needle in the axial direction, it is preferred if the diameter of the annular gap seal, ie preferably the diameter of the guide portion of the nozzle needle at least approximately, preferably corresponds exactly to the diameter of the nozzle needle seat.

Besonders bevorzugt ist eine Ausführungsform des Kraftstoff-Injektors, bei der das Ventil zum Herstellen einer hydraulischen Verbindung zwischen Druckbereich und Druckausgleichsraum vor dem Öffnen der Düsennadel öffnet. Anders ausgedrückt wird bevorzugt vor dem Beginn des Einspritzvorgangs eine hydraulische Verbindung zwischen dem Druckbereich und dem Druckausgleichsraum hergestellt, also die hydraulische Schließkraft zumindest teilweise kompensiert, um dann die Düsennadel mit reduzierter Aktuatorkraft vom Düsennadelsitz abheben zu können. Bei geöffnetem Ventil strömt, im Fall der Ausbildung des Kraftstoff-Injektors als Diesel-Injektor, unter hohem Druck stehender Kraftstoff in den, insbesondere unterhalb der Düsennadel angeordneten Druckausgleichsraum, so dass sich in diesem unmittelbar zumindest näherungsweise Raildruck aufbaut was dann den erwünschten Druckausgleich der Düsennadel bewirkt. Der Druckaufbau wird dabei bevorzugt dadurch beschleunigt, dass die vorerwähnte, bevorzugte Ringspaltdichtung den Druckausgleichsraum vom Ausmündungsbereich der mindestens einen Einspritzöffnung trennt, so dass ein nennenswerter Kraftstoffstrom aus dem Druckausgleichsraum in den Brennraum durch die Einspritzöffnung verhindert wird.Particularly preferred is an embodiment of the fuel injector, wherein the valve for establishing a hydraulic connection between the pressure region and the pressure equalization chamber opens before opening the nozzle needle. In other words, a hydraulic connection between the pressure region and the pressure equalization chamber is preferably produced before the start of the injection process, ie the hydraulic closing force is at least partially compensated in order then to be able to lift the nozzle needle from the nozzle needle seat with reduced actuator force. When the valve is open, in the case of the formation of the fuel injector as a diesel injector, fuel under high pressure flows into the pressure equalization chamber, especially below the nozzle needle, so that at least approximately rail pressure builds up in it, which then results in the desired pressure compensation of the nozzle needle causes. The pressure build-up is preferably accelerated by the fact that the aforementioned, preferred annular gap seal separates the pressure equalization chamber from the outlet region of the at least one injection opening, so that a significant flow of fuel from the pressure compensation chamber into the combustion chamber is prevented by the injection opening.

Das Schließen des Kraftstoffinjektors erfolgt bevorzugt indem zunächst die Düsennadel zurück in ihren Düsennadelsitz bewegt und anschließend das Ventil geschlossen wird, um somit den Druckausgleichsraum wieder hydraulisch von dem Druckbereich des Kraftstoff-Injektors zu trennen. Somit ist im geschlossenen Zustand des Kraftstoff-Injektors eine vollständige Dichtheit des Kraftstoff-Injektors gegeben. Wie später noch erläutert werden wird, ist es besonders bevorzugt, wenn der Düsennadel und dem Ventil separate Schließfedern zugeordnet sind. Durch eine geeignete Abstimmung der Federkräfte kann ein Schließen der Düsennadel vor dem Ventil sichergestellt werden. Dadurch, dass die Düsennadel vor dem Ventilelement des Ventils schließt, kann der durch die Schließbewegung der Düsennadel aus dem Druckausgleichsraum verdrängte Kraftstoff am Ventilsitz des Ventils vorbei zurück in den Druckbereich strömen.The closing of the fuel injector is preferably carried out by first moving the nozzle needle back into its nozzle needle seat and then closing the valve so as to again hydraulically separate the pressure compensation chamber from the pressure region of the fuel injector. Thus, in the closed state of the fuel injector, a complete tightness of the fuel injector given. As will be explained later, it is particularly preferred if the nozzle needle and the valve are assigned separate closing springs. By a suitable vote of the spring forces closing the nozzle needle can be ensured before the valve. Characterized in that the nozzle needle closes in front of the valve element of the valve, the displaced by the closing movement of the nozzle needle from the pressure compensation chamber fuel past the valve seat of the valve back into the pressure range.

Der Erfindung ist mit Vorteil vorgesehen, dass der Kraftstoff-Injektor einen einzigen Aktuator aufweist. Dieser dient bevorzugt sowohl zum Verstellen der Düsennadel zwischen ihrer Öffnungs- und ihrer Schließstellung als auch zum Öffnen und Schließen des Ventils. Hierzu wirkt der Aktuator bevorzugt sowohl auf ein Ventilelement des Ventils als auch auf die Düsennadel.The invention is advantageously provided that the fuel injector has a single actuator. This is preferably used both for adjusting the nozzle needle between its open and closed position and for opening and closing the valve. For this purpose, the actuator preferably acts both on a valve element of the valve and on the nozzle needle.

Ganz besonders bevorzugt ist es dabei, wenn das Ventilelement, insbesondere mechanisch, mit der Düsennadel gekoppelt ist, vorzugsweise derart, das ein Öffnen des Ventils zu einem zeitversetzten Verstellen der Düsennadel aus ihrer Schließstellung heraus führt. Dabei ist bevorzugt das Ventilelement oder ein fest mit dem Ventilelement verbundenes Bauteil als Mitnehmer ausgebildet, der die Düsennadel nach dem Abheben des Ventilelementes von seinem Sitz in Öffnungsrichtung mitnimmt. Bei der Schließbewegung bleibt der Mitnehmer bevorzugt solange in Kontakt mit der Düsennadel, bis diese auf ihrem Düsennadelsitz anliegt. Dies kann, wie bereits angedeutet, durch eine entsprechende Abstimmung von mindestens zwei Schließfedern (Düsennadelschließfeder und Ventilschließfeder) erreicht werden.It is very particularly preferred in this case if the valve element, in particular mechanically, is coupled to the nozzle needle, preferably in such a way that the valve opens at a time-shifted adjustment of the nozzle needle from its closed position. In this case, preferably, the valve element or a component permanently connected to the valve element is designed as a driver, which entrains the nozzle needle after lifting the valve element from its seat in the opening direction. During the closing movement of the driver preferably remains in contact with the nozzle needle until it rests on its nozzle needle seat. This can, as already indicated, by a corresponding vote of at least two closing springs (nozzle needle closing spring and valve closing spring) can be achieved.

Wie bereits angedeutet, ist es besonders bevorzugt, wenn zum Schließen des Ventils eine Ventilschließfeder vorgesehen ist. Bevorzugt ist zusätzlich zur Ventilschließfeder eine Düsennadelschließfeder zum Schließen der Düsennadel vorgesehen. Die Federkräfte der Ventilschließfeder und der Düsennadelschließfeder sind weiter bevorzugt derart ausgebildet, dass die Düsennadel ihre Schließposition erreicht, bevor das Ventil geschlossen wird und somit den Druckausgleichsraum vom Druckbereich des Kraftstoff-Injektors trennt.As already indicated, it is particularly preferred if a valve closing spring is provided for closing the valve. Preferably, in addition to the valve closing spring, a nozzle needle closing spring is provided for closing the nozzle needle. The spring forces of the valve closing spring and the nozzle needle closing spring are further preferably designed such that the nozzle needle reaches its closed position before the valve is closed and thus separates the pressure compensation chamber from the pressure region of the fuel injector.

Konstruktiv vorteilhaft ist eine Ausführungsform, bei der in der Düsennadel ein, vorzugsweise konzentrisch zu deren Längsmittelachse verlaufender, Verbindungskanal vorgesehen ist, durch den Kraftstoff bei geöffnetem Ventil aus dem Druckbereich in den Druckausgleichsraum strömen kann. Bevorzugt ragt das Ventilelement des Ventils in axialer Richtung in die Düsennadel hinein, um den Verbindungskanal, vorzugsweise nach dem Schließen des Kraftstoff-Injektors schließen zu können. Besonders bevorzugt ist der Ventilsitz des Ventils hierzu unmittelbar an der Düsennadel ausgebildet.Constructively advantageous is an embodiment in which in the nozzle needle a, preferably concentric to the longitudinal central axis extending, connecting channel is provided, can flow through the fuel with the valve open from the pressure range in the pressure compensation chamber. Preferably, this protrudes Valve element of the valve in the axial direction into the nozzle needle in order to close the connecting channel, preferably after closing the fuel injector can. Particularly preferably, the valve seat of the valve is for this purpose formed directly on the nozzle needle.

Wie eingangs angedeutet, ist eine Ausführungsform des Kraftstoff-Injektors besonders bevorzugt, bei der der Kraftstoff-Injektor rücklaufanschlussfrei ist, also weder eine Steuermenge noch eine Leckagemenge anfällt, die in den Kraftstofftank zurücktransportiert werden müssen.As indicated at the outset, an embodiment of the fuel injector is particularly preferred, in which the fuel injector is return connection connection-free, that is, neither a control amount nor a leakage quantity is obtained, which must be transported back into the fuel tank.

Zwar ist auch eine Ausführungsform des Kraftstoff-Injektors mit Piezoaktuator möglich. Aus Kostengründen ist jedoch eine Ausführungsform bevorzugt, bei der der Aktuator zum Verstellen der Düsennadel und/oder des Ventils ein elektromagnetischer Aktuator ist.Although an embodiment of the fuel injector with piezo actuator is possible. For cost reasons, however, an embodiment is preferred in which the actuator for adjusting the nozzle needle and / or the valve is an electromagnetic actuator.

Weitere Vorteile, Merkmale und Einzelheiten der Erfindung ergeben sich aus der nachfolgenden Beschreibung bevorzugter Ausführungsbeispiele sowie anhand der Zeichnungen.Further advantages, features and details of the invention will become apparent from the following description of preferred embodiments and from the drawings.

Diese zeigen in:

Fig. 1:
einen Kraftstoff-Injektor mit Druckausgleichsraum und einem diesen zugeordneten Ventil in einem geschlossen Zustand,
Fig. 2:
den Kraftstoff-Injektor gemäß Fig. 1 mit geöffnetem Ventil vor Beginn des Einspritzvorgangs,
Fig. 3:
den Kraftstoff-Injektor gemäß den Fig. 1 und 2 während des Einspritzvorgangs und
Fig. 4:
den Kraftstoff-Injektor gemäß den Fig. 1 bis 3 bei beendetem Einspritzvorgang jedoch bei noch geöffnetem Ventil.
These show in:
Fig. 1:
a fuel injector with pressure compensation chamber and a valve associated therewith in a closed state,
Fig. 2:
according to the fuel injector Fig. 1 with the valve open before starting the injection process,
3:
the fuel injector according to the Fig. 1 and 2 during the injection process and
4:
the fuel injector according to the Fig. 1 to 3 when the injection process is completed, however, with the valve still open.

In den Figuren sind gleiche Elemente und Elemente mit der gleichen Funktion mit den gleichen Bezugszeichen gekennzeichnet.In the figures, like elements and elements having the same function are denoted by the same reference numerals.

In Fig. 1 ist ein als Common-Rail-Injektor ausgebildeter Kraftstoff-Injektor 1 zum Einspritzen von Kraftstoff in einen nicht gezeigten Brennraum einer ebenfalls nicht gezeigten Brennkraftmaschine gezeigt. Der Kraftstoff-Injektor 1 wird neben anderen, nicht gezeigten Kraftstoff-Injektoren über eine Versorgungsleitung 2 mit unter hohem Druck stehendem Kraftstoff versorgt. Im Falle der Ausbildung des Kraftstoff-Injektors als Diesel-Injektor liegt dieser Kraftstoffdruck bevorzugt jenseits von 2000bar. Zur Erzeugung des Kraftstoffdrucks ist eine Hochdruckpumpe 3 vorgesehen, die Kraftstoff aus einem Vorratsbehälter 4 (Tank) in einen Kraftstoff-Hochdruckspeicher 5 (Rail) befördert.In Fig. 1 is a designed as a common-rail injector fuel injector 1 for injecting fuel into a combustion chamber, not shown also one not shown internal combustion engine shown. The fuel injector 1 is supplied, among other fuel injectors, not shown, via a supply line 2 with fuel under high pressure. In the case of forming the fuel injector as a diesel injector, this fuel pressure is preferably beyond 2000 bar. To generate the fuel pressure, a high-pressure pump 3 is provided, the fuel from a reservoir 4 (tank) in a high-pressure fuel storage 5 (Rail) conveys.

Wie sich aus Fig. 1 ergibt, weist der Kraftstoff-Injektor 1 lediglich einen Zulaufanschluss 6, nicht jedoch einen Rücklaufanschluss auf.As it turned out Fig. 1 results, the fuel injector 1 only an inlet port 6, but not a return port.

Innerhalb eines Düsenkörpers 7 ist eine Düsennadel 8 axial verstellbar geführt. Die Düsennadel 8 ragt in einen Druckbereich 9 (hier Druckraum 10), der aus Gründen der Schwingungsreduzierung als Mini-Rail ausgebildet ist. In den Druckbereich 9 mündet die Versorgungsleitung 2, so dass im Druckbereich 9 zumindest näherungsweise Raildruck herrscht, der wiederum näherungsweise dem Einspritzdruck entspricht.Within a nozzle body 7, a nozzle needle 8 is guided axially adjustable. The nozzle needle 8 protrudes into a pressure region 9 (here pressure chamber 10), which is designed for reasons of vibration reduction as a mini-rail. In the pressure region 9, the supply line 2 opens, so that at least approximately rail pressure prevails in the pressure region 9, which in turn corresponds approximately to the injection pressure.

Fig. 1 zeigt den Kraftstoff-Injektor 1 im geschlossen Zustand. In diesem liegt die Düsennadel 8 mit einer konusförmigen Dichtfläche 11 auf einem von einer Umfangsschulter des Düsenkörpers 7 gebildeten Düsennadelsitz 12 auf. Auf die Düsennadel 8 wirkt in der Zeichnungsebene nach unten, d.h. in Schließrichtung eine hydraulische Schließkraft, die auf die Druckbeaufschlagung mit im Druckbereich 9 befindlichem, unter Druck stehendem Kraftstoff zurückzuführen ist. Fig. 1 shows the fuel injector 1 in the closed state. In this, the nozzle needle 8 is located with a cone-shaped sealing surface 11 on a nozzle needle seat 12 formed by a peripheral shoulder of the nozzle body 7. On the nozzle needle 8 acts in the plane of the drawing down, ie in the closing direction, a hydraulic closing force, which is due to the pressurization befindlichem in the pressure region 9, under pressure fuel.

Zum Öffnen der Düsennadel 8 sowie zum Öffnen eines später noch zu erläuternden Ventils 13 ist ein als elektromagnetischer Aktuator ausgebildeter Aktuator 14 vorgesehen, dem eine Ankerplatte 15 zugeordnet ist. Die Ankerplatte 15 befindet sich ebenfalls im Druckbereich 9 des Kraftstoff-Injektors 1.To open the nozzle needle 8 and to open a valve 13 to be explained later, an actuator 14 designed as an electromagnetic actuator is provided, to which an anchor plate 15 is assigned. The anchor plate 15 is also located in the pressure region 9 of the fuel injector. 1

Wie sich weiter aus Fig. 1 ergibt, befindet sich in der Zeichnungsebene unmittelbar axial unterhalb des Düsennadelsitzes 12 ein ringförmiger Ausmündungsbereich 16, aus dem eine Anzahl von über den Umfang verteilten, in den Düsenkörper 7 eingebrachten Einspritzöffnungen 17 ausmünden.How to get out Fig. 1 shows, located in the plane of the drawing directly axially below the nozzle needle seat 12, an annular Ausmündungsbereich 16, from which a number of distributed over the circumference, introduced into the nozzle body 7 injection openings 17 open.

Axial in der Zeichnungsebene unten grenzt an den ringförmigen Ausmündungsbereich 16, der im geschlossenen Zustand des Kraftstoff-Injektors 1 hydraulisch von dem Druckbereich 9 getrennt ist, ein Führungsabschnitt 18 an, in dem die Düsennadel 8 am Innenumfang einer Sacklochbohrung im Düsenkörper 7 geführt ist. Im Führungsabschnitt 18 ist radial zwischen der Düsennadel 8 und dem Düsenkörper 7 eine Ringspaltdichtung 19 (Führungsspalt) ausgebildet. Axial an die Ringspaltdichtung 19 grenzt in der Zeichnungsebene unten ein Druckausgleichsraum 20 an. Dieser ist zumindest weitgehend hydraulisch über die Ringspaltdichtung 19 von dem Ausmündungsbereich 16 entkoppelt. Über das Ventil 13 ist der Druckausgleichsraum 20 mit dem Druckbereich 9 verbindbar, der auf der von dem Druckausgleichsraum 20 abgewandten Düsennadelseite angeordnet ist. Da der Durchmesser des Düsenkörpers 7 im Führungsabschnitt 18 dem Durchmesser des Düsennadelsitzes 12 entspricht, ist die Düsennadel 8 bei mit dem Druckbereich 9 verbundenem Druckausgleichsraum 20 in axialer Richtung druckausgeglichen.Axially in the plane of the drawing below, adjacent to the annular discharge area 16, which is hydraulically separated from the pressure area 9 in the closed state of the fuel injector 1, adjoins a guide section 18, in which the Nozzle needle 8 is guided on the inner circumference of a blind hole in the nozzle body 7. In the guide section 18, an annular gap seal 19 (guide gap) is formed radially between the nozzle needle 8 and the nozzle body 7. Axial to the annular gap seal 19 is adjacent in the drawing level below a pressure compensation chamber 20 at. This is at least largely decoupled hydraulically via the annular gap seal 19 of the Ausmündungsbereich 16. Via the valve 13, the pressure compensation chamber 20 can be connected to the pressure region 9, which is arranged on the side remote from the pressure compensation chamber 20 nozzle needle side. Since the diameter of the nozzle body 7 in the guide section 18 corresponds to the diameter of the nozzle needle seat 12, the nozzle needle 8 is pressure-balanced in the axial direction at pressure-compensating space 20 connected to the pressure region 9.

Durch eine, vorzugsweise nur geringfügige, Variation der Durchmesser des Düsennadelsitzes 12 und des Führungsabschnittes 18 bzw. der Ringspaltdichtung 19 kann bei Bedarf eine, vorzugsweise kleine, schließende oder öffnende Druckstufe realisiert werden.By a, preferably only slight, variation of the diameter of the nozzle needle seat 12 and the guide portion 18 and the annular gap seal 19, if necessary, a, preferably small, closing or opening pressure stage can be realized.

In dem in Fig. 1 gezeigten, vollständig geschlossenen Zustand des Kraftstoff-Injektors 1 liegt sowohl die Düsennadel 8 an ihrem Düsennadelsitz 12 als auch ein axial verstellbares Ventilelement 21 des Ventils 13 an seinem Ventilsitz 22 an. Der Ventilsitz 22 ist an die Düsennadel 8 angeformt. Solange das Ventilelement 21 mit seiner Stirnseite am Ventilsitz 22 anliegt, kann kein Kraftstoff aus dem Druckbereich 9 durch einen zentrisch in der Düsennadel 8 angeordneten Verbindungskanal 23 in den Druckausgleichsraum 20 strömen, so dass im Druckausgleichsraum 20 zumindest näherungsweise Brennraumdruck vorherrscht, also ein (wesentlich) geringerer Druck als im Druckraum 9.In the in Fig. 1 shown, fully closed state of the fuel injector 1 is both the nozzle needle 8 at its nozzle needle seat 12 and an axially adjustable valve element 21 of the valve 13 at its valve seat 22 at. The valve seat 22 is integrally formed on the nozzle needle 8. As long as the valve element 21 rests with its end face on the valve seat 22, no fuel from the pressure region 9 can flow through a centrally arranged in the nozzle needle 8 connecting channel 23 into the pressure compensation chamber 20, so that at least approximately combustion chamber pressure prevails in the pressure compensation chamber 20, so a (essential) lower pressure than in the pressure chamber 9.

Damit die Öffnungskraft des (leistungsschwachen) Aktuators 14 ausreicht, die Düsennadel 8 aus der dargestellten Schließstellung in eine in der Zeichnungsebene nach oben verstellte Öffnungsstellung zu bewegen, muss zunächst eine hydraulische Verbindung zwischen dem Druckbereich 9 und dem Druckausgleichsraum 20 hergestellt werden. Hierzu wird, wie sich aus Fig. 2 ergibt, der Aktuator 14 bestromt. Aufgrund der festen Verbindung zwischen Ankerplatte 15 und dem langgestreckten Ventilelement 21 wird letzteres in der Zeichnungsebene nach oben bewegt, so dass ein als Mitnehmer 24 dienender Umfangsbund 25 des Ventilelementes 21 zur axialen Anlage an einem unteren Rand 26 einer Durchgangsöffnung 27 kommt, die stirnseitig in die Düsennadel 8 eingebracht ist.Thus, the opening force of the (low-power) actuator 14 is sufficient to move the nozzle needle 8 from the illustrated closed position in an upward in the plane of the drawing open position, a hydraulic connection between the pressure region 9 and the pressure compensation chamber 20 must first be prepared. This is how it turns out Fig. 2 results, the actuator 14 energized. Due to the fixed connection between the armature plate 15 and the elongated valve member 21, the latter is moved in the drawing plane upwards, so that serving as a driver 24 circumferential collar 25 of the valve member 21 for axial abutment at a lower edge 26 of a through hole 27, the front side in the Nozzle needle 8 is introduced.

Die Durchgangsöffnung 27 wird in axialer Richtung von dem Ventilelement 21 durchsetzt - der Mitnehmer 24 ist somit in einer inneren Düsennadelkammer 28 gefangen.The passage opening 27 is penetrated in the axial direction by the valve element 21 - the driver 24 is thus trapped in an inner nozzle needle chamber 28.

Wie sich aus Fig. 2 ergibt, öffnet zunächst das Ventil 13, so dass Kraftstoff aus dem Druckbereich 9 zunächst über eine Radialbohrung 29 in die Düsennadelkammer 28 und von dieser durch den zentrischen Verbindungskanal 23 in axialer Richtung nach unten in den Druckausgleichsraum 20 strömen kann. Der Verbindungskanal 23 ist die einzige Ein- und Auslauföffnung des Druckausgleichsraums 20. Aus diesem münden keine Einspritzöffnungen aus. Aufgrund des Kraftstoffstroms aus dem Druckbereich 9 in den Druckausgleichsraum 20 entsteht eine in Öffnungsrichtung wirkende hydraulische Kraft, die bei dem gezeigten Ausführungsbeispiel die in Schließrichtung wirkende hydraulische Kraft vollständig kompensiert, so dass auf die Düsennadel 8 in axialer Richtung nach unten lediglich noch die Federkraft einer Düsennadelschließfeder 30 wirkt, die sich stirnseitig an der Düsennadel 8 sowie auf der gegenüberliegenden Seite an einer Scheibe 31 abstützt, welche wiederum mit dem Düsenkörper 7 verschraubt ist.As it turned out Fig. 2 results, first opens the valve 13 so that fuel from the pressure range 9 can first flow through a radial bore 29 into the nozzle needle chamber 28 and from this through the central connecting channel 23 in the axial direction down into the pressure compensation chamber 20. The connecting channel 23 is the only inlet and outlet opening of the pressure compensation chamber 20. From this open no injection openings. Due to the fuel flow from the pressure region 9 in the pressure compensation chamber 20 creates an acting in the opening direction hydraulic force completely compensated in the embodiment shown, the force acting in the closing direction hydraulic force, so that the nozzle needle 8 in the axial direction down only the spring force of a nozzle needle closing spring 30 acts, which is supported on the front side of the nozzle needle 8 and on the opposite side of a disc 31, which in turn is bolted to the nozzle body 7.

Durch die zuvor beschriebene mechanische Kopplung zwischen dem Ventilelement 21 und der Düsennadel 8 über den Mitnehmer 24 wird bei einer weiteren axialen Verstellbewegung des Ventilelementes 21 in der Zeichnungsebene nach oben die Düsennadel 8 mitgenommen (vgl. Fig. 3), wodurch eine hydraulische Verbindung zwischen dem Druckbereich 9 und dem Ausmündungsbereich 16 hergestellt wird, so dass Kraftstoff aus dem Ausmündungsbereich 16 bzw. aus dem Druckbereich 9 unmittelbar durch die Einspritzöffnungen 17 in den Brennraum der Brennkraftmaschine ausströmen kann. Zum Beenden des Einspritzvorgangs wird die Bestromung des Aktuators 14 unterbrochen. Hierdurch wird das Ventilelement 21 mittels einer Ventilschließfeder 32, die sich einenends an einem Umfangsbund 33 des Ventilelementes 21 und anderenends an einer Scheibe 34 abstützt, in der Zeichnungsebene nach unten bewegt, wobei die Federkraft der Ventilschließfeder 32 geringer ist als die Federkraft der Düsennadelfeder 30, so dass die Abwärtsbewegung des Ventilelementes 21 und der Düsennadel 8 zunächst gekoppelt verläuft, bevor die Düsennadel 8 vor dem Ventilelement 21 ihre jeweilige Schließstellung erreicht. Durch die Schließbewegung der Düsennadel wird, wie in Fig. 4 durch Pfeile angedeutet, Kraftstoff aus dem Druckausgleichsraum 20 verdrängt. Dieser verdrängte Kraftstoff strömt durch den Verbindungskanal 23 und die Radialbohrung 29 zurück in den Druckbereich 9. Unterstützt durch die Federkraft der Ventilschließfeder 32 bewegt sich das Ventilelement 21 weiter in Richtung Ventilsitz 22 und verschließt den Druckausgleichsraum 20, um weitere Leckageverluste bei geschlossenem Kraftstoff-Injektor aus dem Druckausgleichsraum 20 über die Ringspaltdichtung 19 in den Ausmündungsbereich 16 und von dort aus über die Einspritzöffnungen 17 in den Brennraum zu vermeiden. Nach Schließen des Ventils 13 wird wieder der in Fig. 1 gezeigte Zustand erreicht.By the above-described mechanical coupling between the valve element 21 and the nozzle needle 8 via the driver 24, the nozzle needle 8 is entrained in a further axial displacement movement of the valve element 21 in the plane of the drawing upwards (see. Fig. 3 ), whereby a hydraulic connection between the pressure region 9 and the Ausmündungsbereich 16 is prepared so that fuel from the Ausmündungsbereich 16 and from the pressure region 9 can flow directly through the injection openings 17 into the combustion chamber of the internal combustion engine. To end the injection process, the energization of the actuator 14 is interrupted. As a result, the valve element 21 is moved downwards in the plane of the drawing by means of a valve closing spring 32, which is supported at one end on a peripheral collar 33 of the valve element 21 and the other end, and the spring force of the valve closing spring 32 is less than the spring force of the nozzle needle spring 30. so that the downward movement of the valve element 21 and the nozzle needle 8 is initially coupled, before the nozzle needle 8 reaches its respective closed position in front of the valve element 21. Due to the closing movement of the nozzle needle, as in Fig. 4 indicated by arrows, fuel displaced from the pressure compensation chamber 20. This displaced fuel flows back through the connecting channel 23 and the radial bore 29 in the pressure region 9. Supported by the spring force of the valve closing spring 32, the valve element 21 moves towards the valve seat 22 and closes the pressure compensation chamber 20 to prevent further leakage losses with the fuel injector closed from the pressure compensation chamber 20 via the annular gap seal 19 in the Ausmündungsbereich 16 and from there via the injection openings 17 into the combustion chamber. After closing the valve 13 is again in Fig. 1 shown state reached.

Claims (11)

  1. Fuel injector for injecting fuel into a combustion chamber of an internal combustion engine, having a nozzle needle (8) which can be adjusted by means of an actuator (14) between a closed position and an open position which permits the flow of fuel from a pressure region (9) through at least one injection opening (17), characterized
    in that the pressure region (9) can be connected by means of a valve (13) to a pressure equalization chamber (20) which is delimited by the nozzle needle (8), wherein the pressure equalization chamber (20) and the pressure chamber (9) are arranged on mutually opposite sides of the nozzle needle (8), wherein the actuator (14) for adjusting the nozzle needle (8) serves simultaneously for adjusting a valve element (21) of the valve (13), and wherein the valve element (21) opens the connection between the pressure equalization chamber (20) and the pressure region (9) when in an open position and blocks said connection when in a closed position, a hydraulic closing force acting on the nozzle needle (8) in the closing direction being able to be at least partially compensated owing to the hydraulic connection.
  2. Fuel injector according to Claim 1,
    characterized
    in that the pressure equalization chamber (20) is hydraulically separated from a mouth region (16) of the at least one injection opening (17), preferably from the entire injection opening (17), by means of an annular gap seal (19).
  3. Fuel injector according to one of Claims 1 and 2, characterized
    in that the diameter of the annular gap seal (19) at least approximately corresponds to the diameter of a nozzle needle seat (12).
  4. Fuel injector according to one of the preceding claims,
    characterized
    in that the valve (13) can be opened before the nozzle needle (8) is lifted out of its closed position.
  5. Fuel injector according to one of the preceding claims,
    characterized
    in that the valve (13) can be closed after the nozzle needle (8) reaches the closed position.
  6. Fuel injector according to Claim 1,
    characterized
    in that the valve element (21) is coupled in particular mechanically to the nozzle needle (8), preferably in such a way that an opening of the valve (13) leads to a time-offset adjustment of the nozzle needle (8) out of its closed position.
  7. Fuel injector according to one of Claims 1 and 6, characterized
    in that a valve closing spring (32) is provided for closing the valve (13).
  8. Fuel injector according to one of the preceding claims,
    characterized
    in that a nozzle needle closing spring (30) is provided for closing the nozzle needle (8).
  9. Fuel injector according to one of the preceding claims,
    characterized
    in that, in the nozzle needle (8), there is provided a connecting duct (23) which runs preferably concentrically with respect to the longitudinal central axis of said nozzle needle and through which, when the valve (13) is open, fuel can flow from the pressure region (9) into the pressure equalization chamber (20).
  10. Fuel injector according to one of the preceding claims,
    characterized
    in that the fuel injector (1) has no return connection.
  11. Fuel injector according to one of the preceding claims,
    characterized
    in that the actuator (14) is an electromagnetic actuator (14).
EP20090174566 2008-12-30 2009-10-30 Fuel injector Not-in-force EP2204570B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE200810055177 DE102008055177A1 (en) 2008-12-30 2008-12-30 Fuel injector

Publications (2)

Publication Number Publication Date
EP2204570A1 EP2204570A1 (en) 2010-07-07
EP2204570B1 true EP2204570B1 (en) 2013-03-13

Family

ID=41668289

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20090174566 Not-in-force EP2204570B1 (en) 2008-12-30 2009-10-30 Fuel injector

Country Status (2)

Country Link
EP (1) EP2204570B1 (en)
DE (1) DE102008055177A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014206210A1 (en) * 2014-04-01 2015-10-01 Robert Bosch Gmbh fuel injector

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2710216A1 (en) 1977-03-09 1978-09-14 Bosch Gmbh Robert FUEL INJECTOR
ATE53436T1 (en) * 1986-04-15 1990-06-15 Voest Alpine Automotive INJECTION NOZZLE FOR COMBUSTION ENGINES.
DE102005005713A1 (en) * 2005-02-08 2006-08-10 Siemens Ag Jet construction group with injection valve for internal combustion engine has two recesses in jet needle

Also Published As

Publication number Publication date
DE102008055177A1 (en) 2010-07-01
EP2204570A1 (en) 2010-07-07

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