EP2884088B1 - Fuel injector - Google Patents

Fuel injector Download PDF

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Publication number
EP2884088B1
EP2884088B1 EP14189616.7A EP14189616A EP2884088B1 EP 2884088 B1 EP2884088 B1 EP 2884088B1 EP 14189616 A EP14189616 A EP 14189616A EP 2884088 B1 EP2884088 B1 EP 2884088B1
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EP
European Patent Office
Prior art keywords
nozzle needle
fuel injector
pressure
low
pressure chamber
Prior art date
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Active
Application number
EP14189616.7A
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German (de)
French (fr)
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EP2884088A1 (en
Inventor
Henning Kreschel
Sebastian Laechele
Holger Rapp
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
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Publication of EP2884088A1 publication Critical patent/EP2884088A1/en
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    • 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
    • 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
    • F02M61/12Other injectors with elongated valve bodies, i.e. of needle-valve type characterised by the provision of guiding or centring means for 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
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/70Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger
    • F02M2200/703Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger hydraulic
    • F02M2200/708Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger hydraulic with hydraulic chambers formed by a movable sleeve
    • 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
    • F02M2547/001Control chambers formed by movable sleeves
    • 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
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/0603Injectors peculiar thereto with means directly operating the valve needle using piezoelectric or magnetostrictive operating means

Definitions

  • the invention relates to a fuel injector for a fuel injection system, in particular a common rail injection system, having the features of the preamble of claim 1.
  • a fuel injector of the type mentioned above is an example of the published patent application DE 10 2008 040 680 A1 out.
  • the known fuel injector comprises for injecting fuel into a combustion chamber of an internal combustion engine an adjustable between an open position and a closed position, multi-part injection valve element, wherein a first part and a second part are coupled via a hydraulic coupler.
  • the hydraulic coupler is limited in the axial direction by a first guide for the first part and by a second guide for the second part.
  • the guides are acted upon radially from the outside by high pressure, while in the hydraulic coupler, a lower pressure is realized.
  • the radially outside applied higher pressure counteracts widening of the guides, so that the fuel injector can be operated comparatively low leakage.
  • the lower pressure in the hydraulic coupler also has the consequence that the parts of the injection valve element coupled thereto are permanently connected to each other during operation of the fuel injector and with considerable forces, so that from a functional point of view they can be regarded as one part. Further, it is proposed in this document that within the hydraulic coupler, a pressure stage is realized which causes a force acting in the closing direction of the injection valve element hydraulic force to accelerate the switching time of the injection valve element. In order to realize the pressure stage, the hydraulically coupled parts of the injection valve element have different diameters, the part lying closer to a nozzle hole arrangement having a smaller diameter than the part remote from the nozzle hole.
  • the fuel injector has a solenoid valve designed as a servo valve, which causes a pressure drop in a control chamber in the open position, which is limited in the axial direction of an end face of the injection valve element.
  • the pressure drop in the control chamber thus causes a relief of the injection valve element until it opens.
  • fuel injectors are for example off DE102008002415A known, which are connected directly via a magnetic or piezoelectric actuator.
  • the required opening force for opening the injection valve element or the nozzle needle must be taken into account when dimensioning the actuator.
  • the force applied by the actuator is transmitted via a switching chain on the end face of the nozzle needle.
  • the switching chain between the actuator and the nozzle needle may have a device for force and / or stroke ratio. Accordingly reduces or increases the required actuator force and increases or decreases in return the required Aktorhub.
  • the present invention seeks to provide a fuel injector for a fuel injection system, in particular a common rail injection system, which allows the use of comparatively small-volume actuators by reducing the required opening force.
  • a small-volume piezoelectric actuator should be possible, via which the fuel injector is directly switchable.
  • the proposed fuel injector comprises a nozzle body and an injector body, each enclosing a high-pressure chamber in which a single- or multi-part nozzle needle for releasing and closing at least one injection opening is received in a liftable manner.
  • the nozzle needle is guided by a low-pressure chamber which is sealed off via at least one guide gap between the nozzle needle and a body limiting the low-pressure space and / or a guide element supported thereon relative to the high-pressure chambers.
  • the nozzle needle has different sized guide diameter d o , d u .
  • the guide diameter d o which is farther away with respect to the injection opening, is smaller than the guide diameter d u , so that the nozzle needle is partially relieved of force in the opening direction.
  • the partial release of force of the nozzle needle causes a reduction in the required opening force, so that - with directly connected injectors - by a small-volume actuator, such as a piezoelectric actuator can be applied.
  • the partial force relief of the nozzle needle causes the switching times can be reduced because the required pressure drop in the control room can be realized faster.
  • the effect of the partial force relief of the nozzle needle can also be represented by the following formulas.
  • the body limiting the low-pressure chamber is a plate-shaped body component which is arranged between the nozzle body and the injector body and which is preferably braced axially with the nozzle body and the injector body via a nozzle retaining nut.
  • the body forms a fixed body component or housing part of the fuel injector.
  • the body limiting the low-pressure space has at least one flow channel for the hydraulic connection of the high pressure spaces formed in the nozzle body and in the injector body. The at least one flow channel ensures the supply of fuel to the at least one injection opening. It is thus part of the flow path of the fuel to be injected.
  • the body limiting the low-pressure space is received in a lift-movable manner in at least one of the high pressure spaces formed in the nozzle body and / or in the injector body.
  • the body limiting the low-pressure space does not necessarily have to be designed as a fixed body component or housing part.
  • the body can also be a coupler body of a hydraulic coupler, which preferably serves to reinforce the force of an actuator and forms a functional unit with it. This is particularly advantageous if the fuel injector is designed as a directly switchable injector.
  • the low-pressure space is connected via at least one connecting channel to a low-pressure region of the fuel injector.
  • the connecting channel is at least partially formed as a radially extending bore.
  • the radially extending Hole in the region of an outer peripheral surface of the low pressure space limiting body, which is preferably formed in this case as a plate-shaped body member, in the low pressure region.
  • the low-pressure region may comprise at least one axially extending connecting channel arranged radially outside with respect to the plate-shaped body component.
  • the low-pressure region is furthermore preferably connectable to a return line of the fuel injection system.
  • the pressure prevailing in the low-pressure chamber preferably corresponds to the return pressure of the fuel injection system.
  • the pressure prevailing in the low-pressure chamber can also be above the return pressure, so that a pressure is possible which lies between the return pressure and the high pressure of a high-pressure accumulator to which the fuel injector is preferably connected.
  • the intermediate pressure level in the low-pressure space can be generated in a manner known per se. For example, equal-pressure valves or pressure divider devices can be used.
  • the pressure in the low-pressure space is preferably at most 20 bar, preferably at most 10 bar, in order to achieve the desired effect of a partially force-loaded nozzle needle.
  • the nozzle needle is preferably in several parts, preferably in two parts, formed.
  • the multi-part design simplifies the realization of different sizes of guide diameter, since a diameter jump can be realized in each case in the region of the connection of two parts, which differ in terms of their diameter.
  • the nozzle needle comprises a first part and a second part having cooperating contact surfaces arranged in the low pressure space. The low pressure in the low pressure chamber and the high pressure applied externally cause a mechanical coupling of the two parts of the nozzle needle.
  • the first part and the second part of the nozzle needle have, in the region of their contact surfaces, a geometry forming a joint.
  • the joint in the contact area can compensate for any axial misalignment between the parts.
  • At least one guide of the nozzle needle is realized by a separate guide element, which is designed as a sleeve and is preferably supported by a biting edge on the body limiting the low-pressure space.
  • the trained as a sleeve separate guide element allows the compensation of any axial offset between the parts of the nozzle needle, since the sleeve relative to the body is radially displaceable.
  • the biting edge of the sleeve increases the sealing force in order to seal the low-pressure space with respect to one of the high-pressure chambers.
  • it is proposed that the sleeve is acted upon by the spring force of a spring in the direction of the body.
  • the sealing force is increased in the contact area of the sleeve with the body. Since the sleeve is surrounded on the outside by high pressure, the high pressure environment causes an additional hydraulic contact pressure. Further preferably, the lifting movement of the nozzle needle via an actuator is directly controlled.
  • the actuator may be, for example, a piezoelectric actuator or a magnetic actuator.
  • a directly controllable or switchable fuel injector has over an indirectly controllable or switchable fuel injector the advantage that no Abêtmenge accumulates, which must be returned and again promoted to high pressure. This can increase the efficiency of the system.
  • a hydraulic coupler is provided for the transmission of the force and / or the stroke of an actuator.
  • the hydraulic coupler has a coupler body with a hollow cylindrical projection for receiving an end portion of the nozzle needle and for forming a control chamber, wherein the control chamber is formed completely in the coupler body.
  • the hydraulic coupler has a coupler body on which a sealing sleeve for receiving an end portion of the nozzle needle and for forming a control chamber is supported.
  • a hollow cylindrical projection on the coupler body is thus unnecessary, which simplifies the production of the hydraulic coupler.
  • the sealing sleeve can also be displaced in the radial direction on Supported coupler body, so that it allows the compensation of any misalignment between the hydraulic coupler and the nozzle needle.
  • sealing sleeve Since the sealing sleeve is surrounded on all sides by high pressure, in the case of a short-term overpressure in the control chamber there is the risk that the sealing sleeve will detach from the coupler body and the control chamber will open. This can be counteracted by the fact that the one-piece solution described above (without separate sealing sleeve) or a sealing sleeve is selected, which has a radially inner biting edge, via which it is supported on the coupler body. In this way, acting on the sealing sleeve opening forces are avoided at a pressure in the control room.
  • the Indian FIG. 1 The nozzle body 1 and the injector body 2 are clamped together axially by means of a nozzle lock nut 26, wherein between the nozzle body 1 and the injector 2 in addition a plate-shaped body member as a Low-pressure chamber 7 limiting body 6 is inserted.
  • the low-pressure chamber 7 is connected via a connecting channel 13 designed as a radial bore to a low-pressure region 14, which is arranged radially outside with respect to the body 6.
  • an obliquely extending flow channel 15 is formed in the body 6, which connects the high-pressure chamber 3 of the nozzle body 1 with the high-pressure chamber 4 of the injector body 2.
  • the fuel injector further comprises a liftable nozzle needle 5 for releasing and closing at least one injection port (not shown).
  • the nozzle needle 5 extends from the high-pressure chamber 3 of the nozzle body 1 into the high-pressure chamber 4 of the injector body 2, being guided in the region of the low-pressure chamber 7 by the plate-shaped body component or body 6.
  • An upper end portion of the nozzle needle 5 is received in a sealing sleeve 23 which is supported on a coupler body 20 of a not shown hydraulic coupler 19 via a radially inner biting edge 24 and acted upon in the direction of the coupler body 20 by the spring force of a spring 17.
  • the coupler body 20, the sealing sleeve 23 and an end face 25 of the end portion of the nozzle needle 5 accommodated in the sealing sleeve 23 thus jointly delimit a control chamber 22 in which a control chamber pressure prevails which causes a pressure force acting on the nozzle needle 5 in the closing direction. If the nozzle needle 5 is raised to release the injection port, the pressure in the control chamber 22nd be lowered. This is done in the present case by actuation of an actuator (not shown), which may be formed for example as a piezoelectric actuator.
  • a reversal of the direction of movement and on the other an amplification of the actuator force or the Aktorhubes be effected via the switched between the piezoelectric actuator and the nozzle needle hydraulic coupler 19, so that the piezoelectric actuator for direct control of the lifting movement of the nozzle needle 5 can be used.
  • the nozzle needle 5 is partially relieved of force.
  • the partial release of force is caused by a diameter jump of the nozzle needle 5 in the region of the low-pressure space 7.
  • the diameter jump leads to the formation of a low pressure surrounded pressure stage 12, wherein the diameter d o of the nozzle needle 5 above the pressure stage 12 is smaller than the diameter d u below the pressure stage 12 is selected.
  • the diameters d o and d u together with the plate-shaped body component or the body 6 form guide gaps 8, 9, via which the low-pressure space 7 is sealed off from the high-pressure spaces 3, 4 by way of the gap seal.
  • the opening can be effected with a comparatively small actuator, in particular when the fuel injector is directly switchable via the actuator.
  • FIG. 2 is a modification of the fuel injector of FIG. 1 shown.
  • the guidance of the nozzle needle 5 is not effected via the plate-shaped body component or the body 6, but via sleeve-shaped guide elements 10, 11 supported thereon.
  • the support is in each case via a biting edge in order to optimize the sealing of the low-pressure chamber 7 with respect to the high-pressure chambers 3, 4.
  • the sleeve-shaped guide elements 10, 11 are acted upon in the direction of the body 6 in each case by the spring force of a spring 17, 18.
  • the sleeve-shaped guide element 10 is acted upon by the spring force of the spring 17, which at the same time holds the sealing sleeve 23 in contact with the coupler body 20.
  • the spring 17 is supported, on the one hand, on the sleeve-shaped guide element 10 and, on the other hand, on the sealing sleeve 23.
  • the sleeve-shaped guide member 11 is pressed by the spring force of the spring 18 to the body 6, which also serves as a closing spring and is supported on the nozzle needle 5.
  • the sleeve-shaped guide elements 10, 11 are radially displaceable relative to the presently formed as a plate-shaped body member body 6 and allow in this way the compensation of any Axis offset.
  • the guide gaps 8, 9 sealing the low-pressure space 7 are formed between the sleeve-shaped guide elements 10, 11 and the guide diameters d 0 , d u of the nozzle needle 5.
  • the low pressure chamber 7 is formed as a simple axial bore within the body 6, which is thus easy to manufacture.
  • FIG. 3 Another preferred embodiment is in FIG. 3 shown. This is different from the one of FIGS. 1 and 2 in that the nozzle needle 5 is designed in several parts, namely in two parts.
  • the two parts 5.1, 5.2 of the nozzle needle 5 each have a different diameter, wherein the diameter d o of the part 5.1 is smaller than the diameter d u of the part 5.2 is selected.
  • the parts 5.1, 5.2 form with the sleeve-shaped guide elements 10, 11 supported on the body 6 guiding gaps 8, 9, via which the low-pressure space 7 formed in the plate-shaped body component 6 is sealed against the high-pressure spaces 3, 4.
  • the contact area of the two parts 5. 1, 5.2 is located in the low-pressure chamber 7 and forms the pressure required to relieve the pressure of the nozzle needle 12 from.
  • a possible axial offset between the two parts 5.1, 5.2 can be effected by a radial displacement of the sleeve-shaped guide elements 10, 11 relative to the body 6.
  • FIG. 4 A modification of the embodiment of the FIG. 3 is in the FIG. 4 shown.
  • the two parts 5.1, 5.2 each have a geometry in the region of their contact surfaces, which cooperate forming a joint 16.
  • the contact surface of the part 5.1 is convex-shaped, while the contact surface of the part 5.2 has a concave-shaped depression, so that the contact region is reduced to a circular line.
  • the geometries also cause a self-centering of the two parts 5.1, 5.2 to each other.
  • FIG. 5 Another modification of the embodiment of the FIG. 3 is in the FIG. 5 shown.
  • FIGS. 6 to 9 Other modifications are in the FIGS. 6 to 9 shown. They are different from those of FIGS. 1 to 5 in particular, that the body 6 is not necessarily designed as a fixed plate-shaped body member which is axially braced between the nozzle body 1 and the injector body 2 by means of a nozzle lock nut 26. Accordingly, the body 6 may have any desired shape and / or be liftably received in the high-pressure space 3.
  • the nozzle needle 5 in one piece and - to form the pressure stage 12 - stepped formed.
  • the nozzle needle 5 has a guide diameter d u and above a guide diameter d o , where also d o ⁇ d u .
  • the guide diameter d u acts together with a sleeve-shaped guide element 11, which is supported on the body 6, forming a guide gap 9.
  • the guide gap 9 seals a trained in the body 6 low-pressure chamber 7, which is formed as an axial bore.
  • the axial bore is stepped, so that adjoining the low-pressure chamber 7 is a guide section which cooperates with the guide diameter d o of the nozzle needle 5 forming a guide gap 8.
  • the guide gap 8 seals the low-pressure chamber 7 against a further pressure chamber formed in the body 6, which may be designed as a control chamber 22 or as a coupler chamber of a hydraulic coupler.
  • the body 6 also serves as a coupler body 20 of the hydraulic coupler (see reference numerals in parentheses).
  • a coupler body 20 As a coupler body 20, the body 6 is received in a liftable manner in the high-pressure chamber 3.
  • the trained in the body 6 control chamber 22 and coupler space is bounded by an end face of the nozzle needle 5, so that prevails at the nozzle needle 5 of the prevailing in the control chamber 22 or coupler hydraulic pressure, via which the lifting movement of the nozzle needle 5 is preferably directly controlled.
  • the embodiment according to the FIG. 7 is different from that of FIG. 6 in that the nozzle needle 5 is formed in two parts and has a first part 5.1 with the guide diameter d o and a second part 5.2 with the guide diameter d u , again d o ⁇ d u . Since in the control chamber 22 or coupler space and in the high pressure chamber 3 prevail significantly higher pressures than in the low pressure chamber 7, the two parts 5.1, 5.2 of the nozzle needle 5 are pressed together with high forces and form a functional unit.
  • the advantage of this embodiment is in particular that the multi-part design of the nozzle needle 5 allows the compensation of an axial and / or angular offset.
  • the two parts 5.1, 5.2 the nozzle needle 5 are ground continuously when the guide diameter is equal to the outer diameter over the entire height of the part. While the first part 5.1 in this case has a convex end for abutment on and for mechanical coupling with the second part of the nozzle needle 5 5. 2, the second part 5. 2 ends in a flat end face. Other face geometries are also conceivable.
  • a modification of the embodiment of the FIG. 7 is in the FIG. 8 shown.
  • the first part 5.1 of the nozzle needle 5 is here performed stepped to make the first part 5.1 receiving bore in the body 6 as a simple axial bore.
  • FIG. 9 refer to. In contrast to the embodiment of FIG. 8 shows the FIG.
  • annular groove 27 connected to the flow channel 15 via a branch 15 'in the region of the guide of the first part 5.1 of the nozzle needle 5.
  • the guide gap 8 is connected in this way to the high-pressure chamber 3.
  • the annular groove 27 In the region of the annular groove 27 is located over the entire circumference of the first part 5.1 of the nozzle needle 5 high pressure. In this way, the annular groove 27 counteracts leakage from the control chamber 22 or coupler space in the direction of the low-pressure space 7.
  • Injektorlochepten that provide a constant coupler volume, for example in direct-switching injectors, causes a leakage from the coupler space in the low-pressure chamber, a permanent reduction of the coupler space pressure. This has the consequence that the injector behavior changes. This must be prevented.
  • the proposed high-pressure connection of the guide gap 8 represents a measure to effectively prevent leakage from the coupler space and thus a reduction of the coupler space pressure.
  • the in connection with the FIGS. 1 to 9 described features can each be used individually or in various combinations. In this way one obtains further modifications and / or alternative embodiments, all of which are part of the invention as defined in the appended claims.

Description

Die Erfindung betrifft einen Kraftstoffinjektor für ein Kraftstoffeinspritzsystem, insbesondere ein Common-Rail-Einspritzsystem, mit den Merkmalen des Oberbegriffs des Anspruchs 1.The invention relates to a fuel injector for a fuel injection system, in particular a common rail injection system, having the features of the preamble of claim 1.

Stand der TechnikState of the art

Ein Kraftstoffinjektor der vorstehend genannten Art geht beispielhaft aus der Offenlegungsschrift DE 10 2008 040 680 A1 hervor. Der bekannte Kraftstoffinjektor umfasst zum Einspritzen von Kraftstoff in einen Brennraum einer Brennkraftmaschine ein zwischen einer Öffnungsstellung und einer Schließstellung verstellbares, mehrteiliges Einspritzventilelement, wobei ein erstes Teil und ein zweites Teil über einen hydraulischen Koppler gekoppelt sind. Der hydraulische Koppler wird in axialer Richtung von einer ersten Führung für das erste Teil und von einer zweiten Führung für das zweite Teil begrenzt. Die Führungen sind radial außen von Hochdruck beaufschlagt, während im hydraulischen Koppler ein geringerer Druck realisiert ist. Der radial außen anliegende höhere Druck wirkt einem Aufweiten der Führungen entgegen, so dass der Kraftstoffinjektor vergleichsweise leckagearm betrieben werden kann. Der geringere Druck im hydraulischen Koppler hat ferner zur Folge, dass die hierüber gekoppelten Teile des Einspritzventilelements während des Betriebs des Kraftstoffinjektors permanent und mit erheblichen Kräften miteinander verbunden sind, so dass sie aus Funktionssicht als ein Teil betrachtet werden können. Ferner wird in dieser Druckschrift vorgeschlagen, dass innerhalb des hydraulischen Kopplers eine Druckstufe realisiert ist, die eine in Schließrichtung auf das Einspritzventilelement wirkende hydraulische Kraft zur Beschleunigung der Schaltzeit des Einspritzventilelements verursacht. Zur Realisierung der Druckstufe weisen die hydraulisch gekoppelten Teile des Einspritzventilelements unterschiedliche Durchmesser auf, wobei das näher an einer Düsenlochanordnung liegende Teil einen geringeren Durchmesser als das düsenlochferne Teil besitzt.A fuel injector of the type mentioned above is an example of the published patent application DE 10 2008 040 680 A1 out. The known fuel injector comprises for injecting fuel into a combustion chamber of an internal combustion engine an adjustable between an open position and a closed position, multi-part injection valve element, wherein a first part and a second part are coupled via a hydraulic coupler. The hydraulic coupler is limited in the axial direction by a first guide for the first part and by a second guide for the second part. The guides are acted upon radially from the outside by high pressure, while in the hydraulic coupler, a lower pressure is realized. The radially outside applied higher pressure counteracts widening of the guides, so that the fuel injector can be operated comparatively low leakage. The lower pressure in the hydraulic coupler also has the consequence that the parts of the injection valve element coupled thereto are permanently connected to each other during operation of the fuel injector and with considerable forces, so that from a functional point of view they can be regarded as one part. Further, it is proposed in this document that within the hydraulic coupler, a pressure stage is realized which causes a force acting in the closing direction of the injection valve element hydraulic force to accelerate the switching time of the injection valve element. In order to realize the pressure stage, the hydraulically coupled parts of the injection valve element have different diameters, the part lying closer to a nozzle hole arrangement having a smaller diameter than the part remote from the nozzle hole.

Der aus der DE 10 2008 040 680 A1 bekannte Kraftstoffinjektor wird indirekt geschaltet. Hierzu besitzt der Kraftstoffinjektor ein als Magnetventil ausgeführtes Servoventil, das in Offenstellung einen Druckabfall in einem Steuerraum bewirkt, der in axialer Richtung von einer Stirnfläche des Einspritzventilelements begrenzt wird. Der Druckabfall im Steuerraum bewirkt demnach eine Entlastung des Einspritzventilelements, bis dieses öffnet. Über die Abstimmung von Zu- und Ablaufdrosseln, die mit dem Steuerraum in Verbindung stehen, ist gewährleistet, dass der erforderliche Druckabfall zum Öffnen des Einspritzventilelements in einer definierten Zeitspanne nach dem Öffnen des Servoventils erreicht wird. Bei der Dimensionierung des Aktors zur Betätigung des Servoventils muss daher lediglich die zum Öffnen des Servoventils erforderliche Kraft berücksichtigt werden.The from the DE 10 2008 040 680 A1 known fuel injector is switched indirectly. For this purpose, the fuel injector has a solenoid valve designed as a servo valve, which causes a pressure drop in a control chamber in the open position, which is limited in the axial direction of an end face of the injection valve element. The pressure drop in the control chamber thus causes a relief of the injection valve element until it opens. By means of the coordination of inlet and outlet throttles, which are in communication with the control chamber, it is ensured that the required pressure drop for opening the injection valve element is achieved in a defined period of time after opening the servo valve. When sizing the actuator for actuating the servo valve, therefore, only the force required to open the servo valve must be taken into account.

Darüber hinaus sind Kraftstoffinjektoren beispielsweise aus DE102008002415A bekannt, die über einen Magnet- oder Piezoaktor direkt geschaltet werden. In diesem Fall muss bei der Dimensionierung des Aktors die erforderliche Öffnungskraft zum Öffnen des Einspritzventilelements bzw. der Düsennadel berücksichtigt werden. Die vom Aktor aufgebrachte Kraft wird über eine Schaltkette auf die Stirnfläche der Düsennadel übertragen. Um dabei eine Übersetzung der Aktorkraft und/oder des Aktorhubes zu bewirken, kann die Schaltkette zwischen dem Aktor und der Düsennadel eine Einrichtung zur Kraft- und/oder Hubübersetzung aufweisen. Entsprechend verringert oder erhöht sich die erforderliche Aktorkraft und erhöht oder verringert sich im Gegenzug der erforderliche Aktorhub.In addition, fuel injectors are for example off DE102008002415A known, which are connected directly via a magnetic or piezoelectric actuator. In this case, the required opening force for opening the injection valve element or the nozzle needle must be taken into account when dimensioning the actuator. The force applied by the actuator is transmitted via a switching chain on the end face of the nozzle needle. In order to effect a translation of the actuator force and / or the Aktorhubes, the switching chain between the actuator and the nozzle needle may have a device for force and / or stroke ratio. Accordingly reduces or increases the required actuator force and increases or decreases in return the required Aktorhub.

Ausgehend von dem vorstehend genannten Stand der Technik liegt der vorliegenden Erfindung die Aufgabe zugrunde, einen Kraftstoffinjektor für ein Kraftstoffeinspritzsystem, insbesondere ein Common-Rail-Einspritzsystem, anzugeben, der durch eine Reduzierung der erforderlichen Öffnungskraft den Einsatz vergleichsweise kleinvolumiger Aktoren erlaubt. Insbesondere soll der Einsatz eines kleinvolumigen Piezoaktors möglich sein, über den der Kraftstoffinjektor direkt schaltbar ist.Based on the above-mentioned prior art, the present invention seeks to provide a fuel injector for a fuel injection system, in particular a common rail injection system, which allows the use of comparatively small-volume actuators by reducing the required opening force. In particular, the use of a small-volume piezoelectric actuator should be possible, via which the fuel injector is directly switchable.

Die Aufgabe wird gelöst durch einen Kraftstoffinjektor mit den Merkmalen des Anspruchs 1. Vorteilhafte Weiterbildungen der Erfindung sind den Unteransprüchen zu entnehmen.The object is achieved by a fuel injector with the features of claim 1. Advantageous developments of the invention are described in the dependent claims.

Offenbarung der ErfindungDisclosure of the invention

Der vorgeschlagene Kraftstoffinjektor umfasst einen Düsenkörper und einen Injektorkörper, die jeweils einen Hochdruckraum umschließen, in denen eine ein- oder mehrteilige Düsennadel zum Freigeben und Verschließen wenigstens einer Einspritzöffnung hubbeweglich aufgenommen ist. Die Düsennadel ist dabei durch einen Niederdruckraum geführt, der über wenigstens einen Führungsspalt zwischen der Düsennadel und einem den Niederdruckraum begrenzenden Körper und/oder einem hieran abgestützten Führungselement gegenüber den Hochdruckräumen abgedichtet ist. Zur Ausbildung einer im Niederdruckraum angeordneten Druckstufe besitzt die Düsennadel unterschiedlich große Führungsdurchmesser do, du. Erfindungsgemäß ist vorgesehen, dass der in Bezug auf die Einspritzöffnung weiter entfernt liegende Führungsdurchmesser do kleiner als der Führungsdurchmesser du ist, so dass die Düsennadel in Öffnungsrichtung teilweise kraftentlastet ist. Die teilweise Kraftentlastung der Düsennadel bewirkt eine Reduzierung der erforderlichen Öffnungskraft, so dass diese - bei direkt geschalteten Injektoren - durch einen kleinvolumigen Aktor, beispielsweise einem Piezoaktor, aufgebracht werden kann. Bei indirekt geschalteten Injektoren bewirkt die teilweise Kraftentlastung der Düsennadel, dass die Schaltzeiten verringert werden können, da der erforderliche Druckabfall im Steuerraum schneller realisiert werden kann.The proposed fuel injector comprises a nozzle body and an injector body, each enclosing a high-pressure chamber in which a single- or multi-part nozzle needle for releasing and closing at least one injection opening is received in a liftable manner. The nozzle needle is guided by a low-pressure chamber which is sealed off via at least one guide gap between the nozzle needle and a body limiting the low-pressure space and / or a guide element supported thereon relative to the high-pressure chambers. To form a pressure chamber arranged in the low pressure chamber, the nozzle needle has different sized guide diameter d o , d u . According to the invention, it is provided that the guide diameter d o, which is farther away with respect to the injection opening, is smaller than the guide diameter d u , so that the nozzle needle is partially relieved of force in the opening direction. The partial release of force of the nozzle needle causes a reduction in the required opening force, so that - with directly connected injectors - by a small-volume actuator, such as a piezoelectric actuator can be applied. In indirectly connected injectors, the partial force relief of the nozzle needle causes the switching times can be reduced because the required pressure drop in the control room can be realized faster.

Die Wirkung der teilweisen Kraftentlastung der Düsennadel lässt sich auch anhand der nachfolgenden Formeln darstellen.The effect of the partial force relief of the nozzle needle can also be represented by the following formulas.

In Schließstellung der Düsennadel entspricht die erforderliche Öffnungskraft der hydraulischen Druckkraft Fsitz, welche die Düsennadel in ihren Sitz drückt. Für Fsitz gilt: F sitz = p π 4 d s 2 ,

Figure imgb0001
wobei p dem Hochdruck und ds dem Sitzdurchmesser eines Düsennadelsitzes entspricht. Die üblicherweise zusätzlich vorhandene Vorspannkraft einer in Schließrichtung wirkenden Feder ist dabei so gering, dass sie vernachlässigt werden kann.In the closed position of the nozzle needle corresponds to the required opening force of the hydraulic pressure force F seat , which presses the nozzle needle into its seat. For F seat : F Seat = p π 4 d s 2 .
Figure imgb0001
where p corresponds to the high pressure and d s corresponds to the seat diameter of a nozzle needle seat. The usually additionally existing biasing force of a spring acting in the closing direction is so small that it can be neglected.

Die Formel zeigt, dass der Sitzdurchmesser ds großen Einfluss auf Fsitz und damit auf die erforderliche Öffnungskraft besitzt. Durch die unterschiedlich großen Führungsdurchmesser der Düsennadel zur Realisierung einer Druckstufe kann die hydraulische Druckkraft Fsitz reduziert werden, denn es gilt nunmehr: F sitz = p π 4 d s 2 + d o 2 d u 2

Figure imgb0002
The formula shows that the seat diameter d s has a great influence on F seat and thus on the required opening force. Due to the different sized guide diameter of the nozzle needle for the realization of a pressure stage, the hydraulic pressure force F seat can be reduced because it now applies: F Seat = p π 4 d s 2 + d O 2 - d u 2
Figure imgb0002

Gemäß einer bevorzugten Ausführungsform der Erfindung ist der den Niederdruckraum begrenzende Körper ein zwischen dem Düsenkörper und dem Injektorkörper angeordnetes plattenförmiges Körperbauteil, das vorzugsweise über eine Düsenspannmutter mit dem Düsenkörper und dem Injektorkörper axial verspannt ist. In diesem Fall bildet der Körper ein feststehendes Körperbauteil bzw. Gehäuseteil des Kraftstoffinjektors aus. Alternativ oder ergänzend wird vorgeschlagen, dass vorzugsweise der den Niederdruckraum begrenzende Körper wenigstens einen Strömungskanal zur hydraulischen Verbindung der im Düsenkörper und im Injektorkörper ausgebildeten Hochdruckräume besitzt. Der wenigstens eine Strömungskanal stellt den Zulauf von Kraftstoff zu der wenigstens einen Einspritzöffnung sicher. Er ist somit Teil des Strömungspfads des einzuspritzenden Kraftstoffs.According to a preferred embodiment of the invention, the body limiting the low-pressure chamber is a plate-shaped body component which is arranged between the nozzle body and the injector body and which is preferably braced axially with the nozzle body and the injector body via a nozzle retaining nut. In this case, the body forms a fixed body component or housing part of the fuel injector. Alternatively or additionally, it is proposed that preferably the body limiting the low-pressure space has at least one flow channel for the hydraulic connection of the high pressure spaces formed in the nozzle body and in the injector body. The at least one flow channel ensures the supply of fuel to the at least one injection opening. It is thus part of the flow path of the fuel to be injected.

Gemäß einer alternativen bevorzugten Ausführungsform der Erfindung ist der den Niederdruckraum begrenzende Körper in wenigstens einem der im Düsenkörper und/oder im Injektorkörper ausgebildeten Hochdruckräume hubbeweglich aufgenommen. Der den Niederdruckraum begrenzende Körper muss demnach nicht zwingend als feststehendes Körperbauteil bzw. Gehäuseteil ausgebildet sein. Beispielsweise kann der Körper auch ein Kopplerkörper eines hydraulischen Kopplers sein, der vorzugsweise der Kraftverstärkung eines Aktors dient und mit diesem eine funktionale Einheit bildet. Dies ist insbesondere dann von Vorteil, wenn der Kraftstoffinjektor als direkt schaltbarer Injektor ausgebildet ist.According to an alternative preferred embodiment of the invention, the body limiting the low-pressure space is received in a lift-movable manner in at least one of the high pressure spaces formed in the nozzle body and / or in the injector body. Accordingly, the body limiting the low-pressure space does not necessarily have to be designed as a fixed body component or housing part. For example, the body can also be a coupler body of a hydraulic coupler, which preferably serves to reinforce the force of an actuator and forms a functional unit with it. This is particularly advantageous if the fuel injector is designed as a directly switchable injector.

Bevorzugt ist der Niederdruckraum über wenigstens einen Verbindungskanal an einen Niederdruckbereich des Kraftstoffinjektors angeschlossen. Dadurch ist sichergestellt, dass eine zusätzlich im Wege der Leckage in den Niederdruckraum gelangende Kraftstoffmenge nicht zu einer unerwünschten Druckerhöhung im Niederdruckraum führt. Vorzugsweise ist der Verbindungskanal zumindest abschnittsweise als radial verlaufende Bohrung ausgebildet. Weiterhin vorzugsweise mündet die radial verlaufende Bohrung im Bereich einer Außenumfangfläche des den Niederdruckraum begrenzenden Körpers, der in diesem Fall bevorzugt als plattenförmiges Körperbauteil ausgebildet ist, in den Niederdruckbereich. Der Niederdruckbereich kann hierzu wenigstens einen radial außen in Bezug auf das plattenförmige Körperbauteil angeordneten, axial verlaufenden Verbindungskanal umfassen. Der Niederdruckbereich ist weiterhin vorzugsweise an eine Rücklaufleitung des Kraftstoffeinspritzsystems anschließbar.Preferably, the low-pressure space is connected via at least one connecting channel to a low-pressure region of the fuel injector. This ensures that an additional amount of fuel entering the low-pressure space by means of the leakage does not lead to an undesired pressure increase in the low-pressure space. Preferably, the connecting channel is at least partially formed as a radially extending bore. Further preferably, the radially extending Hole in the region of an outer peripheral surface of the low pressure space limiting body, which is preferably formed in this case as a plate-shaped body member, in the low pressure region. For this purpose, the low-pressure region may comprise at least one axially extending connecting channel arranged radially outside with respect to the plate-shaped body component. The low-pressure region is furthermore preferably connectable to a return line of the fuel injection system.

Der im Niederdruckraum herrschende Druck entspricht vorzugsweise dem Rücklaufdruck des Kraftstoffeinspritzsystems. Darüber hinaus kann der im Niederdruckraumherrschende Druck aber auch über dem Rücklaufdruck liegen, so dass ein Druck möglich ist, der zwischen dem Rücklaufdruck und dem Hochdruck eines Hochdruckspeichers liegt, an den der Kraftstoffinjektor bevorzugt angeschlossen ist. Das Zwischendruckniveau im Niederdruckraum kann auf an sich bekannte Art erzeugt werden. Beispielsweise können Gleichdruckventile oder Druckteilereinrichtungen eingesetzt werden. Bevorzugt beträgt der Druck im Niederdruckraum jedoch maximal 20 bar, vorzugsweise maximal 10 bar, um den gewünschten Effekt einer teilweise kraftenlasteten Düsennadel zu erzielen.The pressure prevailing in the low-pressure chamber preferably corresponds to the return pressure of the fuel injection system. In addition, the pressure prevailing in the low-pressure chamber can also be above the return pressure, so that a pressure is possible which lies between the return pressure and the high pressure of a high-pressure accumulator to which the fuel injector is preferably connected. The intermediate pressure level in the low-pressure space can be generated in a manner known per se. For example, equal-pressure valves or pressure divider devices can be used. However, the pressure in the low-pressure space is preferably at most 20 bar, preferably at most 10 bar, in order to achieve the desired effect of a partially force-loaded nozzle needle.

Zur Ausbildung unterschiedlich großer Führungsdurchmesser ist die Düsennadel bevorzugt mehrteilig, vorzugsweise zweiteilig, ausgebildet. Die mehrteilige Ausbildung vereinfacht die Realisierung unterschiedlich großer Führungsdurchmesser, da ein Durchmessersprung jeweils im Bereich der Verbindung zweier Teile realisiert werden kann, die sich hinsichtlich ihres Durchmessers unterscheiden. Vorzugsweise umfasst die Düsenadel ein erstes Teil und ein zweites Teil, die zusammenwirkende Kontaktflächen besitzen, die im Niederdruckraum angeordnet sind. Der geringe Druck im Niederdruckraum und der außen anliegende hohe Druck bewirken eine mechanische Kopplung der beiden Teile der Düsennadel. Denn während das der Einspritzöffnung zugewandte zweite Teil stets von einer hydraulischen Öffnungskraft beaufschlagt ist, wird das erste Teil, das weiter entfernt von der Einspritzöffnung angeordnet ist, stets von einer hydraulischen Schließkraft beaufschlagt, so dass beide Teile axial gegeneinander gepresst werden und funktional eine Einheit bilden.To form different sizes of guide diameter, the nozzle needle is preferably in several parts, preferably in two parts, formed. The multi-part design simplifies the realization of different sizes of guide diameter, since a diameter jump can be realized in each case in the region of the connection of two parts, which differ in terms of their diameter. Preferably, the nozzle needle comprises a first part and a second part having cooperating contact surfaces arranged in the low pressure space. The low pressure in the low pressure chamber and the high pressure applied externally cause a mechanical coupling of the two parts of the nozzle needle. Because while the injection opening facing the second part is always acted upon by a hydraulic opening force, the first part, which is located further away from the injection opening, always acted upon by a hydraulic closing force, so that both parts are axially pressed against each other and form a functional unit ,

Als weiterbildende Maßnahme wird vorgeschlagen, dass das erste Teil und das zweite Teil der Düsennadel im Bereich ihrer Kontaktflächen eine ein Gelenk ausbildende Geometrie aufweisen. Durch das Gelenk im Kontaktbereich kann ein etwaiger Achsversatz zwischen den Teilen ausgeglichen werden. Zur Ausbildung eines Gelenks eignen sich insbesondere sphärisch geformte Kontaktflächen, wobei die eine Kontaktfläche konkav oder plan und die andere konvex geformt sein sollte.As a further development measure, it is proposed that the first part and the second part of the nozzle needle have, in the region of their contact surfaces, a geometry forming a joint. The joint in the contact area can compensate for any axial misalignment between the parts. To form a joint suitable in particular spherically shaped contact surfaces, wherein one contact surface should be concave or flat and the other convex.

Erfindungsgemäß ist wenigstens eine Führung der Düsennadel durch ein separates Führungselement realisiert wird, das als Hülse ausgebildet ist und vorzugsweise über eine Beißkante an dem den Niederdruckraum begrenzenden Körper abgestützt ist. Das als Hülse ausgebildete separate Führungselement ermöglicht den Ausgleich eines etwaigen Achsversatzes zwischen den Teilen der Düsennadel, da die Hülse gegenüber dem Körper radial verschiebbar ist. Die Beißkante der Hülse erhöht die Dichtkraft, um den Niederdruckraum gegenüber einem der Hochdruckräume abzudichten. Alternativ oder ergänzend wird vorgeschlagen, dass die Hülse von der Federkraft einer Feder in Richtung des Körpers beaufschlagt ist. Auch durch diese Maßnahme wird die Dichtkraft im Kontaktbereich der Hülse mit dem Körper erhöht. Da die Hülse außen von Hochdruck umgeben ist, wird durch die Hochdruckumgebung eine zusätzliche hydraulische Anpresskraft bewirkt. Weiterhin bevorzugt ist die Hubbewegung der Düsennadel über einen Aktor direkt steuerbar. Bei dem Aktor kann es sich beispielsweise um einen Piezoaktor oder einen Magnetaktor handeln. Ein direkt steuerbarer bzw. schaltbarer Kraftstoffinjektor besitzt gegenüber einem indirekt steuerbaren bzw. schaltbaren Kraftstoffinjektor den Vorteil, dass keine Absteuermenge anfällt, die rückgeführt und erneut auf Hochdruck gefördert werden muss. Dadurch kann der Wirkungsgrad des Systems erhöht werden. Alternativ oder ergänzend wird vorgeschlagen, dass ein hydraulischer Koppler zur Übersetzung der Kraft und/oder des Hubes eines Aktors vorgesehen ist.
Gemäß einer ersten bevorzugten Ausführungsform besitzt der hydraulische Koppler einen Kopplerkörper mit einem hohlzylinderförmigen Ansatz zur Aufnahme eines Endabschnitts der Düsennadel und zur Ausbildung eines Steuerraums, wobei der Steuerraum vollständig im Kopplerkörper ausgebildet ist.
Alternativ wird vorgeschlagen, dass der hydraulische Koppler einen Kopplerkörper besitzt, an dem eine Dichthülse zur Aufnahme eines Endabschnitts der Düsennadel und zur Ausbildung eines Steuerraums abgestützt ist. Ein hohlzylinderförmiger Ansatz am Kopplerkörper ist damit entbehrlich, was die Fertigung des hydraulischen Kopplers vereinfacht. Die Dichthülse kann zudem in radialer Richtung verschiebbar am Kopplerkörper abgestützt sein, so dass sie den Ausgleich eines etwaigen Achsversatzes zwischen dem hydraulischen Koppler und der Düsennadel ermöglicht.
Da die Dichthülse allseitig von Hochdruck umgeben ist, besteht bei einem kurzzeitigen Überdruck im Steuerraum die Gefahr, dass sich die Dichthülse vom Kopplerkörper löst und der Steuerraum öffnet. Dem kann dadurch entgegen gewirkt werden, dass die zuvor beschriebene einteilige Lösung (ohne separate Dichthülse) oder eine Dichthülse gewählt wird, die eine radial innen liegende Beißkante besitzt, über welche sie am Kopplerkörper abgestützt ist. Auf diese Weise werden auf die Dichthülse wirkende öffnende Kräfte bei einem Überdruck im Steuerraum vermieden.
According to the invention, at least one guide of the nozzle needle is realized by a separate guide element, which is designed as a sleeve and is preferably supported by a biting edge on the body limiting the low-pressure space. The trained as a sleeve separate guide element allows the compensation of any axial offset between the parts of the nozzle needle, since the sleeve relative to the body is radially displaceable. The biting edge of the sleeve increases the sealing force in order to seal the low-pressure space with respect to one of the high-pressure chambers. Alternatively or additionally, it is proposed that the sleeve is acted upon by the spring force of a spring in the direction of the body. Also by this measure, the sealing force is increased in the contact area of the sleeve with the body. Since the sleeve is surrounded on the outside by high pressure, the high pressure environment causes an additional hydraulic contact pressure. Further preferably, the lifting movement of the nozzle needle via an actuator is directly controlled. The actuator may be, for example, a piezoelectric actuator or a magnetic actuator. A directly controllable or switchable fuel injector has over an indirectly controllable or switchable fuel injector the advantage that no Absteuermenge accumulates, which must be returned and again promoted to high pressure. This can increase the efficiency of the system. Alternatively or additionally, it is proposed that a hydraulic coupler is provided for the transmission of the force and / or the stroke of an actuator.
According to a first preferred embodiment, the hydraulic coupler has a coupler body with a hollow cylindrical projection for receiving an end portion of the nozzle needle and for forming a control chamber, wherein the control chamber is formed completely in the coupler body.
Alternatively, it is proposed that the hydraulic coupler has a coupler body on which a sealing sleeve for receiving an end portion of the nozzle needle and for forming a control chamber is supported. A hollow cylindrical projection on the coupler body is thus unnecessary, which simplifies the production of the hydraulic coupler. The sealing sleeve can also be displaced in the radial direction on Supported coupler body, so that it allows the compensation of any misalignment between the hydraulic coupler and the nozzle needle.
Since the sealing sleeve is surrounded on all sides by high pressure, in the case of a short-term overpressure in the control chamber there is the risk that the sealing sleeve will detach from the coupler body and the control chamber will open. This can be counteracted by the fact that the one-piece solution described above (without separate sealing sleeve) or a sealing sleeve is selected, which has a radially inner biting edge, via which it is supported on the coupler body. In this way, acting on the sealing sleeve opening forces are avoided at a pressure in the control room.

Bevorzugte Ausführungsformen der Erfindung werden nachfolgend anhand der beigefügten Zeichnungen näher erläutert. Diese zeigen:

  • Figur 1 einen schematischen Längsschnitt durch einen Kraftstoffinjektor welcher nicht gemäß der Erfindung ausgeführt ist,
  • Figur 2 einen schematischen Längsschnitt durch einen Kraftstoffinjektor gemäß einer ersten bevorzugten Ausführungsform der Erfindung,
  • Figur 3 einen schematischen Längsschnitt durch einen Kraftstoffinjektor gemäß einer zweiten bevorzugten Ausführungsform der Erfindung,
  • Figur 4 einen schematischen Längsschnitt durch einen Kraftstoffinjektor gemäß einer dritten bevorzugten Ausführungsform der Erfindung,
  • Figur 5 einen schematischen Längsschnitt durch einen Kraftstoffinjektor gemäß einer vierten bevorzugten Ausführungsform der Erfindung,
  • Figur 6 einen schematischen Längsschnitt durch einen Kraftstoffinjektor gemäß einer fünften bevorzugten Ausführungsform der Erfindung,
  • Figur 7 einen schematischen Längsschnitt durch einen Kraftstoffinjektor gemäß einer sechsten bevorzugten Ausführungsform der Erfindung,
  • Figur 8 einen schematischen Längsschnitt durch einen Kraftstoffinjektor gemäß einer siebten bevorzugten Ausführungsform der Erfindung und
  • Figur 9 einen schematischen Längsschnitt durch einen Kraftstoffinjektor gemäß einer achten bevorzugten Ausführungsform der Erfindung, jeweils im Bereich eines von Niederdruck umgebenen Durchmessersprungs der Düsennadel.
Preferred embodiments of the invention are explained below with reference to the accompanying drawings. These show:
  • FIG. 1 a schematic longitudinal section through a fuel injector which is not executed according to the invention,
  • FIG. 2 a schematic longitudinal section through a fuel injector according to a first preferred embodiment of the invention,
  • FIG. 3 a schematic longitudinal section through a fuel injector according to a second preferred embodiment of the invention,
  • FIG. 4 a schematic longitudinal section through a fuel injector according to a third preferred embodiment of the invention,
  • FIG. 5 a schematic longitudinal section through a fuel injector according to a fourth preferred embodiment of the invention,
  • FIG. 6 a schematic longitudinal section through a fuel injector according to a fifth preferred embodiment of the invention,
  • FIG. 7 a schematic longitudinal section through a fuel injector according to a sixth preferred embodiment of the invention,
  • FIG. 8 a schematic longitudinal section through a fuel injector according to a seventh preferred embodiment of the invention and
  • FIG. 9 a schematic longitudinal section through a fuel injector according to an eighth preferred embodiment of the invention, in each case in the region of a diameter jump of the nozzle needle surrounded by low pressure.

Ausführliche Beschreibung der ZeichnungenDetailed description of the drawings

Der in der Figur 1 dargestellte Kraftstoffinjektor umfasst einen Düsenkörper 1 mit einem Hochdruckraum 3 und einen Injektorkörper 2 mit einem Hochdruckraum 4. Der Düsenkörper 1 und der Injektorkörper 2 sind mittels einer Düsenspannmutter 26 axial miteinander verspannt, wobei zwischen dem Düsenkörper 1 und dem Injektorkörper 2 zusätzlich ein plattenförmiges Körperbauteil als einen Niederdruckraum 7 begrenzender Körper 6 eingelegt ist. Der Niederdruckraum 7 ist über einen als Radialbohrung ausgeführten Verbindungskanal 13 mit einem Niederdruckbereich 14 verbunden, der radial außen in Bezug auf den Körper 6 angeordnet ist. Ferner ist im Körper 6 ein schräg verlaufender Strömungskanal 15 ausgebildet, welcher den Hochdruckraum 3 des Düsenkörpers 1 mit dem Hochdruckraum 4 des Injektorkörpers 2 verbindet.
Der in der Figur 1 dargestellte Kraftstoffinjektor umfasst darüber hinaus eine hubbewegliche Düsennadel 5 zum Freigeben und Verschließen wenigstens einer Einspritzöffnung (nicht dargestellt). Die Düsennadel 5 erstreckt sich vom Hochdruckraum 3 des Düsenkörpers 1 bis in den Hochdruckraum 4 des Injektorkörpers 2, wobei sie im Bereich des Niederdruckraums 7 durch das plattenförmige Körperbauteil bzw. den Körper 6 geführt ist. Ein oberer Endabschnitt der Düsennadel 5 ist in einer Dichthülse 23 aufgenommen, die an einem Kopplerkörper 20 eines nicht näher dargestellten hydraulischen Kopplers 19 über eine radial innen liegende Beißkante 24 abgestützt und in Richtung des Kopplerkörpers 20 von der Federkraft einer Feder 17 beaufschlagt ist. Der Kopplerkörper 20, die Dichthülse 23 und eine Stirnfläche 25 des in der Dichthülse 23 aufgenommenen Endabschnitts der Düsennadel 5 begrenzen somit gemeinsam einen Steuerraum 22, in dem ein Steuerraumdruck herrscht, der eine die Düsennadel 5 in Schließrichtung beaufschlagende Druckkraft bewirkt. Soll die Düsennadel 5 angehoben werden, um die Einspritzöffnung freizugeben, muss der Druck im Steuerraum 22 abgesenkt werden. Dies erfolgt vorliegend durch Betätigung eines Aktors (nicht dargestellt), der beispielsweise als Piezoaktor ausgebildet sein kann. Über den zwischen Piezoaktor und Düsennadel 5 geschalteten hydraulischen Koppler 19 kann zum Einen eine Umkehr der Bewegungsrichtung und zum Anderen eine Verstärkung der Aktorkraft bzw. des Aktorhubes bewirkt werden, so dass der Piezoaktor zur direkten Steuerung der Hubbewegung der Düsennadel 5 einsetzbar ist.
The Indian FIG. 1 The nozzle body 1 and the injector body 2 are clamped together axially by means of a nozzle lock nut 26, wherein between the nozzle body 1 and the injector 2 in addition a plate-shaped body member as a Low-pressure chamber 7 limiting body 6 is inserted. The low-pressure chamber 7 is connected via a connecting channel 13 designed as a radial bore to a low-pressure region 14, which is arranged radially outside with respect to the body 6. Further, an obliquely extending flow channel 15 is formed in the body 6, which connects the high-pressure chamber 3 of the nozzle body 1 with the high-pressure chamber 4 of the injector body 2.
The Indian FIG. 1 shown fuel injector further comprises a liftable nozzle needle 5 for releasing and closing at least one injection port (not shown). The nozzle needle 5 extends from the high-pressure chamber 3 of the nozzle body 1 into the high-pressure chamber 4 of the injector body 2, being guided in the region of the low-pressure chamber 7 by the plate-shaped body component or body 6. An upper end portion of the nozzle needle 5 is received in a sealing sleeve 23 which is supported on a coupler body 20 of a not shown hydraulic coupler 19 via a radially inner biting edge 24 and acted upon in the direction of the coupler body 20 by the spring force of a spring 17. The coupler body 20, the sealing sleeve 23 and an end face 25 of the end portion of the nozzle needle 5 accommodated in the sealing sleeve 23 thus jointly delimit a control chamber 22 in which a control chamber pressure prevails which causes a pressure force acting on the nozzle needle 5 in the closing direction. If the nozzle needle 5 is raised to release the injection port, the pressure in the control chamber 22nd be lowered. This is done in the present case by actuation of an actuator (not shown), which may be formed for example as a piezoelectric actuator. On the one hand, a reversal of the direction of movement and on the other an amplification of the actuator force or the Aktorhubes be effected via the switched between the piezoelectric actuator and the nozzle needle hydraulic coupler 19, so that the piezoelectric actuator for direct control of the lifting movement of the nozzle needle 5 can be used.

Bei einem erfindungsgemäßen Kraftstoffinjektor ist die Düsennadel 5 teilweise kraftentlastet. Die teilweise Kraftentlastung wird durch einen Durchmessersprung der Düsennadel 5 im Bereich des Niederdruckraums 7 bewirkt. Der Durchmessersprung führt zur Ausbildung einer von Niederdruck umgebenen Druckstufe 12, wobei der Durchmesser do der Düsennadel 5 oberhalb der Druckstufe 12 kleiner als der Durchmesser du unterhalb der Druckstufe 12 gewählt ist. Zugleich bilden die Durchmesser do und du gemeinsam mit dem plattenförmigen Körperbauteil bzw. dem Körper 6 Führungsspalte 8, 9 aus, über welche der Niederdruckraum 7 gegenüber den Hochdruckräumen 3, 4 im Wege der Spaltdichtung abgedichtet ist.In a fuel injector according to the invention, the nozzle needle 5 is partially relieved of force. The partial release of force is caused by a diameter jump of the nozzle needle 5 in the region of the low-pressure space 7. The diameter jump leads to the formation of a low pressure surrounded pressure stage 12, wherein the diameter d o of the nozzle needle 5 above the pressure stage 12 is smaller than the diameter d u below the pressure stage 12 is selected. At the same time, the diameters d o and d u together with the plate-shaped body component or the body 6 form guide gaps 8, 9, via which the low-pressure space 7 is sealed off from the high-pressure spaces 3, 4 by way of the gap seal.

Aufgrund der teilweisen Kraftentlastung der Düsennadel 5 kann das Öffnen mit einem vergleichsweise kleinen Aktor bewirkt werden, insbesondere wenn der Kraftstoffinjektor über den Aktor direkt schaltbar ist.Due to the partial power relief of the nozzle needle 5, the opening can be effected with a comparatively small actuator, in particular when the fuel injector is directly switchable via the actuator.

In der Figur 2 ist eine Abwandlung des Kraftstoffinjektors der Figur 1 dargestellt. Die Führung der Düsennadel 5 wird vorliegend nicht über das plattenförmige Körperbauteil bzw. den Körper 6, sondern über hieran abgestützte hülsenförmige Führungselemente 10, 11 bewirkt. Die Abstützung erfolgt jeweils über eine Beißkante, um die Abdichtung des Niederdruckraums 7 gegenüber den Hochdruckräumen 3, 4 zu optimieren. Zudem sind die hülsenförmigen Führungselemente 10, 11 in Richtung des Körpers 6 jeweils von der Federkraft einer Feder 17, 18 beaufschlagt. Vorliegend wird das hülsenförmige Führungselement 10 von der Federkraft der Feder 17 beaufschlagt, welche zugleich die Dichthülse 23 in Anlage mit dem Kopplerkörper 20 hält. Die Feder 17 ist hierzu einerseits an dem hülsenförmigen Führungselement 10 und andererseits an der Dichthülse 23 abgestützt. Das hülsenförmige Führungselement 11 wird über die Federkraft der Feder 18 an den Körper 6 gedrückt, welche zugleich als Schließfeder dient und an der Düsennadel 5 abgestützt ist. Die hülsenförmigen Führungselemente 10, 11 sind gegenüber dem vorliegend als plattenförmiges Körperbauteil ausgebildeten Körper 6 radial verschiebbar und ermöglichen auf diese Weise den Ausgleich eines etwaigen Achsversatzes. Die den Niederdruckraum 7 abdichtenden Führungsspalte 8, 9 werden zwischen den hülsenförmigen Führungselementen 10, 11 und den Führungsdurchmessern do, du der Düsennadel 5 ausgebildet. Der Niederdruckraum 7 ist als einfache Axialbohrung innerhalb des Körpers 6 ausgebildet, der somit einfach zu fertigen ist.In the FIG. 2 is a modification of the fuel injector of FIG. 1 shown. In the present case, the guidance of the nozzle needle 5 is not effected via the plate-shaped body component or the body 6, but via sleeve-shaped guide elements 10, 11 supported thereon. The support is in each case via a biting edge in order to optimize the sealing of the low-pressure chamber 7 with respect to the high-pressure chambers 3, 4. In addition, the sleeve-shaped guide elements 10, 11 are acted upon in the direction of the body 6 in each case by the spring force of a spring 17, 18. In the present case, the sleeve-shaped guide element 10 is acted upon by the spring force of the spring 17, which at the same time holds the sealing sleeve 23 in contact with the coupler body 20. For this purpose, the spring 17 is supported, on the one hand, on the sleeve-shaped guide element 10 and, on the other hand, on the sealing sleeve 23. The sleeve-shaped guide member 11 is pressed by the spring force of the spring 18 to the body 6, which also serves as a closing spring and is supported on the nozzle needle 5. The sleeve-shaped guide elements 10, 11 are radially displaceable relative to the presently formed as a plate-shaped body member body 6 and allow in this way the compensation of any Axis offset. The guide gaps 8, 9 sealing the low-pressure space 7 are formed between the sleeve-shaped guide elements 10, 11 and the guide diameters d 0 , d u of the nozzle needle 5. The low pressure chamber 7 is formed as a simple axial bore within the body 6, which is thus easy to manufacture.

Eine weitere bevorzugte Ausführungsform ist in der Figur 3 dargestellt. Diese unterscheidet sich von denen der Figuren 1 und 2 dadurch, dass die Düsennadel 5 mehrteilig, nämlich zweiteilig ausgebildet ist. Die beiden Teile 5.1, 5.2 der Düsennadel 5 weisen jeweils einen unterschiedlichen Durchmesser auf, wobei der Durchmesser do des Teils 5.1 kleiner als der Durchmesser du des Teils 5.2 gewählt ist. Die Teile 5.1, 5.2 bilden mit den am Körper 6 abgestützten hülsenförmigen Führungselementen 10, 11 Führungsspalte 8, 9 aus, über welche der im plattenförmigen Körperbauteil 6 ausgebildete Niederdruckraum 7 gegenüber den Hochdruckräumen 3, 4 abgedichtet ist. Der Kontaktbereich der beiden Teile 5. 1, 5.2 liegt im Niederdruckraum 7 und bildet die zur Kraftentlastung der Düsennadel erforderliche Druckstufe 12 aus. Ein etwaiger Achsversatz zwischen den beiden Teilen 5.1, 5.2 kann durch eine radiale Verschiebung der hülsenförmigen Führungselemente 10, 11 gegenüber dem Körper 6 bewirkt werden.Another preferred embodiment is in FIG. 3 shown. This is different from the one of FIGS. 1 and 2 in that the nozzle needle 5 is designed in several parts, namely in two parts. The two parts 5.1, 5.2 of the nozzle needle 5 each have a different diameter, wherein the diameter d o of the part 5.1 is smaller than the diameter d u of the part 5.2 is selected. The parts 5.1, 5.2 form with the sleeve-shaped guide elements 10, 11 supported on the body 6 guiding gaps 8, 9, via which the low-pressure space 7 formed in the plate-shaped body component 6 is sealed against the high-pressure spaces 3, 4. The contact area of the two parts 5. 1, 5.2 is located in the low-pressure chamber 7 and forms the pressure required to relieve the pressure of the nozzle needle 12 from. A possible axial offset between the two parts 5.1, 5.2 can be effected by a radial displacement of the sleeve-shaped guide elements 10, 11 relative to the body 6.

Eine Abwandlung der Ausführungsform der Figur 3 ist in der Figur 4 dargestellt. Um den Ausgleich eines etwaigen Achsversatzes zwischen den beiden Teilen 5.1, 5.2 zu ermöglichen, weisen diese im Bereich ihrer Kontaktflächen jeweils eine Geometrie auf, die ein Gelenk 16 ausbildend zusammenwirken. Vorliegend ist die Kontaktfläche des Teils 5.1 konvex geformt, während die Kontaktfläche des Teils 5.2 eine konkav geformte Vertiefung besitzt, so dass der Kontaktbereich auf eine Kreislinie reduziert wird. Die Geometrien bewirken zugleich eine Selbstzentrierung der beiden Teile 5.1, 5.2 zueinander.A modification of the embodiment of the FIG. 3 is in the FIG. 4 shown. In order to allow the compensation of any axial offset between the two parts 5.1, 5.2, they each have a geometry in the region of their contact surfaces, which cooperate forming a joint 16. In the present case, the contact surface of the part 5.1 is convex-shaped, while the contact surface of the part 5.2 has a concave-shaped depression, so that the contact region is reduced to a circular line. The geometries also cause a self-centering of the two parts 5.1, 5.2 to each other.

Eine weitere Abwandlung der Ausführungsform der Figur 3 ist in der Figur 5 dargestellt. Hier wurde auf die Anordnung einer Dichthülse 23 zur Ausbildung des Steuerraums 22 verzichtet. Stattdessen weist der Kopplerkörper 20 eines nicht näher dargestellten hydraulischen Kopplers 19 einen hohlzylinderförmigen Ansatz 21 zur Aufnahme des oberen Endabschnitts der Düsennadel 5 und zur Ausbildung des Steuerraums 22 auf. Da der Steuerraum 22 vollständig im Kopplerkörper 20 ausgebildet ist, besteht - im Unterschied zur Ausführungsform mit Dichthülse 23 - keine Gefahr, dass dieser öffnet.Another modification of the embodiment of the FIG. 3 is in the FIG. 5 shown. Here was dispensed with the arrangement of a sealing sleeve 23 for forming the control chamber 22. Instead, the coupler body 20 of a hydraulic coupler 19, not shown, a hollow cylindrical projection 21 for receiving the upper end portion of the nozzle needle 5 and the formation of the control chamber 22. Since the control chamber 22 is completely formed in the coupler body 20, there is no danger - in contrast to the embodiment with sealing sleeve 23 - that this opens.

Weitere Abwandlungen sind in den Figuren 6 bis 9 dargestellt. Sie unterscheiden sich von denen der Figuren 1 bis 5 insbesondere dadurch, dass der Körper 6 nicht zwingend als feststehendes plattenförmiges Körperbauteil ausgebildet ist, das zwischen dem Düsenkörper 1 und dem Injektorkörper 2 mittels einer Düsenspannmutter 26 axial verspannt ist. Der Körper 6 kann demnach eine beliebige Form besitzen und/oder im Hochdruckraum 3 hubbeweglich aufgenommen sein.Other modifications are in the FIGS. 6 to 9 shown. They are different from those of FIGS. 1 to 5 in particular, that the body 6 is not necessarily designed as a fixed plate-shaped body member which is axially braced between the nozzle body 1 and the injector body 2 by means of a nozzle lock nut 26. Accordingly, the body 6 may have any desired shape and / or be liftably received in the high-pressure space 3.

Bei der Ausführungsform der Figur 6 ist die Düsennadel 5 einteilig und - zur Ausbildung der Druckstufe 12 - gestuft ausgebildet. Unterhalb der Druckstufe 12 weist die Düsennadel 5 einen Führungsdurchmesser du und oberhalb einen Führungsdurchmesser do, wobei auch hier do < du ist. Der Führungsdurchmesser du wirkt mit einem hülsenförmigen Führungselement 11, das an dem Körper 6 abgestützt ist, einen Führungsspalt 9 bildend zusammen. Der Führungspalt 9 dichtet einen im Körper 6 ausgebildeten Niederdruckraum 7 ab, der als Axialbohrung ausgebildet ist. Die Axialbohrung ist gestuft ausgeführt, so dass sich an den Niederdruckraum 7 ein Führungsabschnitt anschließt, der mit dem Führungsdurchmesser do der Düsennadel 5 einen Führungspalt 8 bildend zusammenwirkt. Der Führungsspalt 8 dichtet den Niederdruckraum 7 gegenüber einem im Körper 6 ausgebildeten weiteren Druckraum ab, der als Steuerraum 22 oder als Kopplerraum eines hydraulischen Kopplers ausgelegt sein kann. Im letztgenannten Fall dient der Körper 6 zugleich als Kopplerkörper 20 des hydraulischen Kopplers (siehe Bezugszeichen in Klammern). Als Kopplerkörper 20 ist der Körper 6 hubbeweglich im Hochdruckraum 3 aufgenommen. Der im Körper 6 ausgebildete Steuerraum 22 bzw. Kopplerraum wird von einer Stirnfläche der Düsennadel 5 begrenzt, so dass an der Düsennadel 5 der im Steuerraum 22 oder Kopplerraum herrschende hydraulische Druck anliegt, über welche die Hubbewegung der Düsennadel 5 vorzugsweise direkt steuerbar ist.In the embodiment of the FIG. 6 is the nozzle needle 5 in one piece and - to form the pressure stage 12 - stepped formed. Below the pressure stage 12, the nozzle needle 5 has a guide diameter d u and above a guide diameter d o , where also d o <d u . The guide diameter d u acts together with a sleeve-shaped guide element 11, which is supported on the body 6, forming a guide gap 9. The guide gap 9 seals a trained in the body 6 low-pressure chamber 7, which is formed as an axial bore. The axial bore is stepped, so that adjoining the low-pressure chamber 7 is a guide section which cooperates with the guide diameter d o of the nozzle needle 5 forming a guide gap 8. The guide gap 8 seals the low-pressure chamber 7 against a further pressure chamber formed in the body 6, which may be designed as a control chamber 22 or as a coupler chamber of a hydraulic coupler. In the latter case, the body 6 also serves as a coupler body 20 of the hydraulic coupler (see reference numerals in parentheses). As a coupler body 20, the body 6 is received in a liftable manner in the high-pressure chamber 3. The trained in the body 6 control chamber 22 and coupler space is bounded by an end face of the nozzle needle 5, so that prevails at the nozzle needle 5 of the prevailing in the control chamber 22 or coupler hydraulic pressure, via which the lifting movement of the nozzle needle 5 is preferably directly controlled.

Die Ausführungsform gemäß der Figur 7 unterscheidet sich von der der Figur 6 dadurch, dass die Düsennadel 5 zweiteilig ausgebildet ist und ein erstes Teil 5.1 mit dem Führungsdurchmesser do und ein zweites Teil 5.2 mit dem Führungsdurchmesser du besitzt, wobei wiederum do < du ist. Da im Steuerraum 22 bzw. Kopplerraum und im Hochdruckraum 3 deutlich höhere Drücke als im Niederdruckraum 7 herrschen, werden die beiden Teile 5.1, 5.2 der Düsennadel 5 mit hohen Kräften aneinander gepresst und bilden funktional eine Einheit. Der Vorteil dieser Ausführungsform besteht insbesondere darin, dass die mehrteilige Ausführung der Düsennadel 5 den Ausgleich eines Achs- und/oder Winkelversatzes ermöglicht. Ferner können die beiden Teile 5.1, 5.2 der Düsennadel 5 durchgängig geschliffen werden, wenn der Führungsdurchmesser jeweils gleich dem Außendurchmesser über die gesamte Höhe des Teils ist. Während das erste Teil 5.1 vorliegend ein konvex geformtes Ende zur Anlage am und zur mechanischen Kopplung mit dem zweiten Teil 5. 2 der Düsennadel 5 besitzt, endet das zweite Teil 5. 2 in einer planebenen Stirnfläche. Andere Stirnflächengeometrien sind ebenfalls denkbar.
Eine Abwandlung der Ausführungsform der Figur 7 ist in der Figur 8 dargestellt. Das erste Teil 5.1 der Düsennadel 5 ist hier gestuft ausgeführt, um die das erste Teil 5.1 aufnehmende Bohrung im Körper 6 als einfache Axialbohrung gestalten zu können.
Eine Weiterbildung der Ausführungsform der Figur 8 ist der Figur 9 zu entnehmen. Im Unterschied zur Ausführungsform der Figur 8 weist die der Figur 9 eine mit dem Strömungskanal 15 über einen Abzweig 15' verbundene Ringnut 27 im Bereich der Führung des ersten Teils 5.1 der Düsennadel 5 auf. Der Führungsspalt 8 ist auf diese Weise an den Hochdruckraum 3 angeschlossen. Im Bereich der Ringnut 27 liegt über den gesamten Umfang des ersten Teils 5.1 der Düsennadel 5 Hochdruck an. Auf diese Weise wirkt die Ringnut 27 einer Leckage vom Steuerraum 22 bzw. Kopplerraum in Richtung des Niederdruckraums 7 entgegen. Bei Injektorkonzepten, die ein konstantes Kopplervolumen vorsehen, beispielsweise bei direkt schaltenden Injektoren, bewirkt eine Leckage vom Kopplerraum in den Niederdruckraum eine permanente Reduzierung des Kopplerraumdrucks. Dies hat zur Folge, dass sich das Injektorverhalten verändert. Dies gilt es zu verhindern. Die vorgeschlagene Hochdruckanbindung des Führungspalts 8 stellt eine Maßnahme dar, um eine Leckage aus dem Kopplerraum und damit eine Reduzierung des Kopplerraumdrucks wirksam zu verhindern.
Die in Zusammenhang mit den Figuren 1 bis 9 beschriebenen Merkmale können jeweils einzeln oder in verschiedenen Kombinationen zur Anwendung gelangen. Auf diese Weise gelangt man zu weiteren Abwandlungen und/oder alternativen Ausführungsformen, die allesamt Bestandteil der Erfindung sind, wie sie in den beigefügten Ansprüchen definiert ist.
The embodiment according to the FIG. 7 is different from that of FIG. 6 in that the nozzle needle 5 is formed in two parts and has a first part 5.1 with the guide diameter d o and a second part 5.2 with the guide diameter d u , again d o <d u . Since in the control chamber 22 or coupler space and in the high pressure chamber 3 prevail significantly higher pressures than in the low pressure chamber 7, the two parts 5.1, 5.2 of the nozzle needle 5 are pressed together with high forces and form a functional unit. The advantage of this embodiment is in particular that the multi-part design of the nozzle needle 5 allows the compensation of an axial and / or angular offset. Furthermore, the two parts 5.1, 5.2 the nozzle needle 5 are ground continuously when the guide diameter is equal to the outer diameter over the entire height of the part. While the first part 5.1 in this case has a convex end for abutment on and for mechanical coupling with the second part of the nozzle needle 5 5. 2, the second part 5. 2 ends in a flat end face. Other face geometries are also conceivable.
A modification of the embodiment of the FIG. 7 is in the FIG. 8 shown. The first part 5.1 of the nozzle needle 5 is here performed stepped to make the first part 5.1 receiving bore in the body 6 as a simple axial bore.
A development of the embodiment of FIG. 8 is the FIG. 9 refer to. In contrast to the embodiment of FIG. 8 shows the the FIG. 9 an annular groove 27 connected to the flow channel 15 via a branch 15 'in the region of the guide of the first part 5.1 of the nozzle needle 5. The guide gap 8 is connected in this way to the high-pressure chamber 3. In the region of the annular groove 27 is located over the entire circumference of the first part 5.1 of the nozzle needle 5 high pressure. In this way, the annular groove 27 counteracts leakage from the control chamber 22 or coupler space in the direction of the low-pressure space 7. In Injektorkonzepten that provide a constant coupler volume, for example in direct-switching injectors, causes a leakage from the coupler space in the low-pressure chamber, a permanent reduction of the coupler space pressure. This has the consequence that the injector behavior changes. This must be prevented. The proposed high-pressure connection of the guide gap 8 represents a measure to effectively prevent leakage from the coupler space and thus a reduction of the coupler space pressure.
The in connection with the FIGS. 1 to 9 described features can each be used individually or in various combinations. In this way one obtains further modifications and / or alternative embodiments, all of which are part of the invention as defined in the appended claims.

Claims (11)

  1. Fuel injector for a fuel injection system, in particular a common-rail injection system, comprising a nozzle body (1) and injector body (2) which in each case surround a high-pressure chamber (3, 4) in which a single-part or multi-part nozzle needle (5) for opening up and closing off at least one injection opening is received such that it can perform stroke movements, wherein the nozzle needle (5) is guided through a low-pressure chamber (7) which is sealed off with respect to the high-pressure chambers (3, 4) by way of at least one guide gap (8, 9) between the nozzle needle (5) and a guide element (10, 11), which guide element is in the form of a sleeve and is supported on a body (6) which delimits the low-pressure chamber (7), and wherein the nozzle needle (5), in order to form a pressure stage (12), arranged in the low-pressure chamber (7), has guide diameters (do, du) of different size, wherein that guide diameter (do) which is situated further remote from the injection opening is smaller than the guide diameter (du), such that the nozzle needle (5) is partially relieved of force in the opening direction.
  2. Fuel injector according to Claim 1,
    characterized in that the body (6) which delimits the low-pressure chamber (7) is a plate-shaped body component arranged between the nozzle body (1) and the injector body (2), which plate-shaped body component is preferably axially clamped to the nozzle body (1) and to the injector body (2) by way of a nozzle clamping nut (26) and/or has at least one flow duct (15) for the hydraulic connection of the high-pressure chambers (3, 4).
  3. Fuel injector according to Claim 1,
    characterized in that the body (6) which delimits the low-pressure chamber (7) is received, such that it can perform stroke movements, in the high-pressure chamber (3) and/or in the high-pressure chamber (4), wherein the body (6) is preferably a coupler body (20) of a hydraulic coupler (19).
  4. Fuel injector according to one of the preceding claims,
    characterized in that the low-pressure chamber (7) is connected via at least one connecting duct (13) to a low-pressure region (14) of the fuel injector, wherein the connecting duct (13) is preferably formed at least in sections as a radially running bore.
  5. Fuel injector according to one of the preceding claims,
    characterized in that the nozzle needle (5), in order to form the guide diameters (do, du) of different size, is of multi-part form, preferably of two-part form, wherein a first part (5.1) and a second part (5.2) preferably have interacting contact surfaces which are arranged in the low-pressure chamber (7).
  6. Fuel injector according to Claim 5,
    characterized in that the first part (5.1) and the second part (5.2) of the nozzle needle (5) have, in the region of their contact surfaces, a geometry which forms a joint (16).
  7. Fuel injector according to one of the preceding claims,
    characterized in that the guide element (10, 11) which is in the form of a sleeve is supported on the body (6) by way of a biting edge, and/or is forced in the direction of the body (6) by the spring force of a spring (17, 18).
  8. Fuel injector according to one of the preceding claims,
    characterized in that the stroke movement of the nozzle needle (5) is controllable directly by way of an actuator, and/or a hydraulic coupler (19) is provided for boosting the force and/or the stroke of an actuator.
  9. Fuel injector according to Claim 8,
    characterized in that the hydraulic coupler (19) has a coupler body (20) with a hollow cylindrical projection (21) for receiving an end section of the nozzle needle (5) and for forming a control chamber (22).
  10. Fuel injector according to Claim 8,
    characterized in that the hydraulic coupler (19) has a coupler body (20) on which there is supported a sealing sleeve (23) for receiving an end section of the nozzle needle (5) and for forming a control chamber (22).
  11. Fuel injector according to Claim 10,
    characterized in that the sealing sleeve (23) has a biting edge (24) situated radially at the inside, by way of which biting edge said sealing sleeve is supported on the coupler body (20).
EP14189616.7A 2013-12-10 2014-10-21 Fuel injector Active EP2884088B1 (en)

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