EP0683862B1 - Electromagnetic valve - Google Patents

Electromagnetic valve Download PDF

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Publication number
EP0683862B1
EP0683862B1 EP95900661A EP95900661A EP0683862B1 EP 0683862 B1 EP0683862 B1 EP 0683862B1 EP 95900661 A EP95900661 A EP 95900661A EP 95900661 A EP95900661 A EP 95900661A EP 0683862 B1 EP0683862 B1 EP 0683862B1
Authority
EP
European Patent Office
Prior art keywords
valve
core
armature
longitudinal axis
wedge
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP95900661A
Other languages
German (de)
French (fr)
Other versions
EP0683862A1 (en
Inventor
Ferdinand Reiter
Martin Maier
Jörg HEYSE
Norbert Keim
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from DE4421935A external-priority patent/DE4421935A1/en
Application filed by Robert Bosch GmbH filed Critical Robert Bosch GmbH
Publication of EP0683862A1 publication Critical patent/EP0683862A1/en
Application granted granted Critical
Publication of EP0683862B1 publication Critical patent/EP0683862B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/061Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
    • F02M51/0625Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures
    • F02M51/0664Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/061Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
    • F02M51/0614Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of electromagnets or fixed armature
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/061Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
    • F02M51/0625Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/061Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
    • F02M51/0625Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures
    • F02M51/0664Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding
    • F02M51/0671Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding the armature having an elongated valve body attached thereto
    • F02M51/0682Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding the armature having an elongated valve body attached thereto the body being hollow and its interior communicating with the fuel flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • 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
    • F02M61/166Selection of particular materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/168Assembling; Disassembling; Manufacturing; Adjusting
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/02Fuel-injection apparatus having means for reducing wear
    • 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
    • F02M2200/50Arrangements of springs for valves used in fuel injectors or fuel injection pumps
    • F02M2200/505Adjusting spring tension by sliding spring seats
    • 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
    • F02M2200/90Selection of particular materials
    • F02M2200/9038Coatings
    • 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
    • F02M2200/90Selection of particular materials
    • F02M2200/9053Metals
    • F02M2200/9061Special treatments for modifying the properties of metals used for fuel injection apparatus, e.g. modifying mechanical or electromagnetic properties

Definitions

  • the invention is based on an electromagnetically actuated Valve according to the genus of the main claim. It are already different electromagnetically operated Valves, in particular fuel injection valves, where wear-resistant components with wear-resistant Layers are provided.
  • DE-OS 32 30 844 is also known anchor and Stop surface of a fuel injector with wear-resistant Surfaces. These surfaces can be nickel-plated, for example, with an additional one Be provided layer, or nitrided, that is Storage of nitrogen must be hardened.
  • DE-OS 38 10 826 is a fuel injector described, in which at least one stop surface is designed to be extremely spherical to achieve an exact air gap, centered on the stop surface a round body insert made of non-magnetic, high-strength material is formed.
  • a fuel injector is also from EP-OS 0 536 773 known, at the anchor on its cylindrical Circumferential surface and an annular stop surface Hard metal layer is applied by electroplating.
  • This layer of chrome or nickel has, for example a thickness of 15 to 25 ⁇ m.
  • the galvanic Coating results in a slightly wedge-shaped layer thickness distribution, being minimal on the outer edges thicker layer is reached.
  • the layer thickness distribution is physical predefined and can hardly be influenced. After a certain Operating time widens the stop surface due to wear and tear in an undesirable manner, causing Changes in anchor pull-in and drop-out times result.
  • the electromagnetically actuated valve according to the invention with the characterizing features of the main claim has the advantage that at least one of the abutting components is designed in such a way that, after a wear-resistant surface has been produced, it is ensured that the stop surface is not undesirably worn even after a long period of operation is increased so that the pulling and falling times of the movable component remain almost constant.
  • This is achieved in that at least one of the abutting components has a wedge-shaped surface before the wear resistance is generated.
  • This wedge-shaped surface can be precisely adapted to different circumstances in order to achieve a magnetic and hydraulic optimum.
  • the wedge-shaped surface shape of the at least one component e.g. B. the anchor, it also allows that also non-galvanic and magnetic wear-resistant layers can be applied without the need for in a very small impact area remains unfulfilled.
  • a particular advantage is that the surface in its highest, closest to the opposite component Area of at least one of the abutting ones Components are made wear-resistant in that using a method known per se, e.g. one Nitriding processes such as plasma nitriding or gas nitriding or similar is hardened.
  • Embodiments of the invention are in the drawing shown in simplified form and in the description below explained in more detail.
  • 1 shows a fuel injector
  • Figure 2 shows an enlarged stop of the Injector in the area of the core and armature
  • Figure 3 a first embodiment of an inventive wedge-shaped anchor
  • Figure 4 shows a second embodiment a wedge anchor
  • Figure 5 a third Embodiment of a wedge anchor.
  • the electromagnetic shown in Figure 1 for example actuatable valve in the form of an injection valve for fuel injection systems of mixture compression, spark-ignited internal combustion engines has one of a magnetic coil 1 surrounding, as a fuel inlet connector serving core 2, which for example is tubular here and is constant over its entire length Has outer diameter.
  • a fuel inlet connector serving core 2 which for example is tubular here and is constant over its entire length Has outer diameter.
  • stepped bobbin 3 takes a winding of Magnet coil 1 and in connection with the a core 2 having a constant outer diameter a particularly compact design of the injection valve in the Magnetic coil area 1.
  • a tubular metal Intermediate part 12 connected for example by welding and partially surrounds the core end 9 axially.
  • the stepped bobbin 3 partially overlaps the core 2 and with a step 15 of larger diameter the intermediate part 12 at least partially axially.
  • a tubular valve seat support 16 Downstream of the Coil body 3 and the intermediate part 12 extends a tubular valve seat support 16, for example is firmly connected to the intermediate part 12.
  • a longitudinal bore 17 In the valve seat carrier 16 runs a longitudinal bore 17 which is concentric to the valve longitudinal axis 10 is formed.
  • a tubular valve needle for example 19 arranged at its downstream End 20 with a spherical valve closing body 21 the extent of which, for example, five flattenings 22 Flowing past the fuel are provided, for example is connected by welding.
  • the injection valve is actuated in a known manner Way electromagnetic.
  • a return spring 25 or closing the injection valve serves the electromagnetic circuit with the magnetic coil 1, the core 2 and an anchor 27.
  • the anchor 27 is with the end of the valve needle facing away from the valve closing body 21 19 connected by a first weld 28 and aligned to core 2.
  • the end of the valve seat carrier 16 facing away from the core 2 is shown in FIG the longitudinal bore 17 is a cylindrical valve seat body 29, which has a fixed valve seat, by welding tightly assembled.
  • valve closing body 21 For guiding the valve closing body 21 during the axial movement the valve needle 19 with the armature 27 along the Longitudinal valve axis 10 serves a guide opening 32 of the valve seat body 29.
  • the spherical valve closing body 21 acts with the shape of a truncated cone in the direction of flow tapered valve seat of the valve seat body 29 together.
  • the valve seat body 29 On its end facing away from the valve closing body 21 is the valve seat body 29 with, for example Pot-shaped spray plate 34 concentrically and firm, connected.
  • the spray plate 34 runs at least one, for example run four formed by eroding or stamping Spray openings 39.
  • the insertion depth of the valve seat body 29 with the pot-shaped spray disk 34 determines the default setting of the stroke of the valve needle 19.
  • Flow bore 46 of the core 2 inserted adjusting sleeve 48 is used to adjust the Spring preload of the adjoining the adjusting sleeve 48 Return spring 25, which in turn is with its opposite Supported on the valve needle 19.
  • the injection valve is largely with a plastic coating 50 enclosed, starting from the core 2 in axial direction via the solenoid coil 1 to the valve seat support 16 extends.
  • This plastic encapsulation 50 belongs, for example, to a co-molded electric Connector 52.
  • a fuel filter 61 projects into the flow bore 46 of the Core 2 at its inlet end 55 and provides for filtering out such fuel components, which due to their size in the injector blockages or cause damage.
  • the one marked with a circle in FIG. 1 is shown Range of one end position of the valve needle 19, in which the armature 27 at the core end 9 of the core 2 strikes, shown on a different scale.
  • metallic layers 65 on the core end 9 of the core 2 and on the anchor 27, for example of chrome or nickel layers, by means of electroplating.
  • the layers 65 are both on a End face perpendicular to the longitudinal axis 10 of the valve 67 and at least partially on a peripheral surface 66 the anchor 27 applied.
  • These layers are 65 particularly wear-resistant and reduce with their small size Surface a hydraulic gluing of the striking surfaces, but without being able to prevent it safely.
  • the Layer thickness of these layers 65 is generally between 10 and 25 ⁇ m.
  • Anchor 27 in the area of its upper end face 67 shown that before coating or generating the wear resistance of the surface a wedge section 73 with an inclined, oblique course opposite the valve longitudinal axis 10, so that the armature 27 there has a wedge shape.
  • the inclination of the wedge section 73 of the End face 67 of armature 27 extends in the exemplary embodiment in Figure 3 inside, including a wedge section 73 of the end face 67 is inclined to the outside can be ( Figure 4).
  • the wedge shape of the anchor 27 in The area of the end face 67 is already in the mechanical Editing, for example by a corresponding ground countersinking tool.
  • the end face 67 at least in the area at its highest point, by treating the surface made wear-resistant by means of a hardening process will.
  • a hardening process e.g. the well-known Nitriding processes such as plasma nitriding or gas nitriding suitable.
  • a stop section 68 of the end face 67 is provided, which over a width a radially inwards perpendicular to the longitudinal axis of the valve 10 extends and serves as a stop surface.
  • This Stop section 68 represents the entire operating time an almost completely constant in width a Annular surface.
  • the abutment surface wear at Continuous operation is precisely defined.
  • the stop surface width is that of the width a of the stop section 68 corresponds, constant even with wear remains, is a constant contact width during the Striking core 2 and anchor 27 over the entire Lifespan available, which also affects the hydraulic conditions in the gap between the core 2 and the armature 27 remain constant, which is a particular advantage.
  • at least the surface of the stop section 68 also wear-resistant thanks to a hardening process be made so that no additional Layer 65 must be applied to the end face 67.
  • Anchors 27 are shown in FIGS. 4 and 5.
  • An anchor 27 is shown in which the wedge section 73 the end face 67 is inclined to the outside.
  • FIG. 5 An embodiment of the armature 27 according to the invention, in which the end face 67 only through the wedge section 73 is shown, Figure 5. This is completely on the one with at least a small radial extension Stop section 68 omitted; rather there is one Wedge on the entire face 67 before, there is So no longitudinal axis 10 perpendicular to the valve Area of the end face 67. Especially for very small ones Angles of the wedge section 73 are then more stable Stop before, so that even in continuous operation a defined The stop surface remains.
  • the slope of the wedge portion 73 in Direction to the valve longitudinal axis 10 is also an embodiment analogous to that shown in FIG. 4 Embodiment conceivable in which the wedge section 73 extends in the direction away from the valve longitudinal axis 10, is designed inclined outwards.

Description

Stand der TechnikState of the art

Die Erfindung geht aus von einem elektromagnetisch betätigbaren Ventil nach der Gattung des Hauptanspruchs. Es sind bereits verschiedene elektromagnetisch betätigbare Ventile, insbesondere Brennstoffeinspritzventile bekannt, bei denen verschleißbeanspruchte Bauteile mit verschleißfesten Schichten versehen sind.The invention is based on an electromagnetically actuated Valve according to the genus of the main claim. It are already different electromagnetically operated Valves, in particular fuel injection valves, where wear-resistant components with wear-resistant Layers are provided.

Aus der DE-OS 29 42 928 ist bereits bekannt, verschleißfeste diamagnetische Materialschichten an verschleißbeanspruchten Teilen, wie Anker und Düsenkörper, aufzutragen. Diese aufgebrachten Schichten dienen der Begrenzung des Hubes der Ventilnadel, wodurch die Auswirkungen des Restmagnetismus auf die bewegten Teile des Brennstoffeinspritzventils minimiert werden.From DE-OS 29 42 928 it is already known to be wear-resistant diamagnetic material layers on wear-stressed Parts such as anchors and nozzle body. These applied layers serve to limit the Stroke of the valve needle, reducing the effects of residual magnetism on the moving parts of the fuel injector be minimized.

Aus der DE-OS 32 30 844 ist ebenfalls bekannt, Anker und Anschlagfläche eines Brennstoffeinspritzventils mit verschleißfesten Oberflächen zu versehen. Diese Oberflächen können beispielsweise vernickelt, also mit einer zusätzlichen Schicht versehen sein, oder nitriert, also durch Einlagerung von Stickstoff gehärtet sein. From DE-OS 32 30 844 is also known anchor and Stop surface of a fuel injector with wear-resistant Surfaces. These surfaces can be nickel-plated, for example, with an additional one Be provided layer, or nitrided, that is Storage of nitrogen must be hardened.

Außerdem ist bereits aus der DE-OS 37 16 072 bekannt, für durch Verschleiß und Korrosion besonders beanspruchte Teile eines Einspritzventils Molybdänhartschichten zu verwenden, die dünn ausgebildet sind und nachträglich mit Diamanten bearbeitet werden können.It is also known from DE-OS 37 16 072 for particularly stressed by wear and corrosion Parts of an injector to use hard molybdenum layers who are thin and subsequently with Diamonds can be edited.

In der DE-OS 38 10 826 ist ein Brennstoffeinspritzventil beschrieben, bei dem wenigstens eine Anschlagfläche kugelkalottenförmig ausgeführt ist, um einen äußerst exakten Luftspalt zu erreichen, wobei mittig an der Anschlagfläche ein Rundkörpereinsatz aus nichtmagnetischem, hochfestem Werkstoff ausgebildet ist.In DE-OS 38 10 826 is a fuel injector described, in which at least one stop surface is designed to be extremely spherical to achieve an exact air gap, centered on the stop surface a round body insert made of non-magnetic, high-strength material is formed.

Aus der EP-OS 0 536 773 ist ebenfalls ein Brennstoffeinspritzventil bekannt, bei dem am Anker an dessen zylindrischer Umfangsfläche und ringförmiger Anschlagfläche eine Hartmetallschicht durch Galvanisieren aufgetragen ist. Diese Schicht aus Chrom oder Nickel besitzt beispielsweise eine Dicke von 15 bis 25 µm. Infolge der galvanischen Beschichtung entsteht eine gering keilige Schichtdickenverteilung, wobei an den äußeren Kanten eine minimal dickere Schicht erreicht wird. Durch die galvanisch abgeschiedenen Schichten ist die Schichtdickenverteilung physikalisch vorgegeben und kaum beeinflußbar. Nach einer gewissen Betriebszeit verbreitert sich die Anschlagfläche durch Verschleiß in unerwünschter Weise, wodurch sich Änderungen bei der Anzugs- und Abfallzeit des Ankers ergeben.A fuel injector is also from EP-OS 0 536 773 known, at the anchor on its cylindrical Circumferential surface and an annular stop surface Hard metal layer is applied by electroplating. This layer of chrome or nickel has, for example a thickness of 15 to 25 µm. As a result of the galvanic Coating results in a slightly wedge-shaped layer thickness distribution, being minimal on the outer edges thicker layer is reached. By the galvanically separated Layers the layer thickness distribution is physical predefined and can hardly be influenced. After a certain Operating time widens the stop surface due to wear and tear in an undesirable manner, causing Changes in anchor pull-in and drop-out times result.

Vorteile der ErfindungAdvantages of the invention

Das erfindungsgemäße elektromagnetisch betätigbare Ventil mit den kennzeichnenden Merkmalen des Hauptanspruchs hat demgegenüber den Vorteil, daß wenigstens eines der aneinander anschlagenden Bauteile so gestaltet ist, daß nach dem Erzeugen einer verschleißfesten Oberfläche gewährleistet ist, daß die Anschlagfläche auch nach längerer Betriebszeit nicht durch Verschleiß in unerwünschter Weise vergrößert wird, so daß die Anzugs- und Abfallzeiten des beweglichen Bauteils nahezu konstant bleiben. Das wird dadurch erreicht, daß wenigstens eines der aneinander anschlagenden Bauteile bereits vor dem Erzeugen der Verschleißfestigkeit eine keilige Oberfläche besitzt. Diese keilige Oberfläche läßt sich zur Erzielung eines magnetischen und hydraulischen Optimums jeweils an verschiedene Gegebenheiten genau anpassen.
Durch die in den Unteransprüchen aufgeführten Maßnahmen sind vorteilhafte Weiterbildungen und Verbesserungen des im Hauptanspruch angegebenen elektromagnetisch betätigbaren Ventils, insbesondere Brennstoffeinspritzventils möglich.
The electromagnetically actuated valve according to the invention with the characterizing features of the main claim has the advantage that at least one of the abutting components is designed in such a way that, after a wear-resistant surface has been produced, it is ensured that the stop surface is not undesirably worn even after a long period of operation is increased so that the pulling and falling times of the movable component remain almost constant. This is achieved in that at least one of the abutting components has a wedge-shaped surface before the wear resistance is generated. This wedge-shaped surface can be precisely adapted to different circumstances in order to achieve a magnetic and hydraulic optimum.
The measures listed in the subclaims permit advantageous developments and improvements of the electromagnetically actuated valve specified in the main claim, in particular fuel injection valve.

Besonders vorteilhaft ist es, die äußerst genaue Oberflächengestalt wenigstens eines der anschlagenden Bauteile mechanisch mit einem geschliffenen Senkwerkzeug herzustellen. So sind sehr präzise Abmessungen erreichbar. Mit Hilfe der sehr genau geschliffenen Werkzeuge können engere Fertigungstoleranzen als bisher eingehalten werden, so daß es beim Betrieb des Einspritzventils zu einer sehr geringen Streuung der Anzugs- und insbesondere Abfallzeit des Ankers kommt.It is particularly advantageous to have the extremely precise surface shape at least one of the striking components mechanically using a ground countersink tool. In this way, very precise dimensions can be achieved. With Using the very precisely ground tools can be tighter Manufacturing tolerances are adhered to so far, so that it to a very low level when operating the injector Scatter the suit and especially fall time of the Anchor is coming.

Vorteilhaft ist zudem, daß durch einen keiligen Anker und/oder Kern ein hydraulisches Kleben vollständig ausgeschlossen ist, da auch bei weitgehend eben abgeschiedenen Schichten die Keiligkeit auf jeden Fall vorhanden bleibt. Die Schichten an wenigstens einem der anschlagenden Bauteile besitzen nämlich nur einen Bruchteil der Keiligkeit der Bauteile selbst. It is also advantageous that a wedge anchor and / or core hydraulic adhesion completely excluded is there, even with largely flat ones Layers the wedge is definitely present. The layers on at least one of the striking components have only a fraction of the wedge of the components themselves.

Die keilige Oberflächengestalt des mindestens einen Bauteils, z. B. des Ankers, erlaubt es zudem, daß auch nichtgalvanische und magnetische verschleißfeste Schichten aufgebracht werden können, ohne daß die Forderung nach einem sehr kleinen Anschlagbereich unerfüllt bleibt.The wedge-shaped surface shape of the at least one component, e.g. B. the anchor, it also allows that also non-galvanic and magnetic wear-resistant layers can be applied without the need for in a very small impact area remains unfulfilled.

Ein besonderer Vorteil besteht darin, daß die Oberfläche in ihrem höchsten, dem gegenüberliegenden Bauteil nächstliegenden Bereich wenigstens eines der aneinanderanschlagenden Bauteile dadurch verschleißfest gemacht wird, daß sie mittels eines an sich bekannten Verfahrens, z.B. einem Nitrierverfahren wie Plasmanitrieren oder Gasnitrieren o.ä. gehärtet wird.A particular advantage is that the surface in its highest, closest to the opposite component Area of at least one of the abutting ones Components are made wear-resistant in that using a method known per se, e.g. one Nitriding processes such as plasma nitriding or gas nitriding or similar is hardened.

Zeichnungdrawing

Ausführungsbeispiele der Erfindung sind in der Zeichnung vereinfacht dargestellt und in der nachfolgenden Beschreibung näher erläutert. Es zeigen Figur 1 ein Brennstoffeinspritzventil, Figur 2 einen vergrößerten Anschlag des Einspritzventils im Bereich von Kern und Anker, Figur 3 ein erstes Ausführungsbeispiel eines erfindungsgemäß ausgebildeten keiligen Ankers, Figur 4 ein zweites Ausführungsbeispiel eines keiligen Ankers und Figur 5 ein drittes Ausführungsbeispiel eines keiligen Ankers.Embodiments of the invention are in the drawing shown in simplified form and in the description below explained in more detail. 1 shows a fuel injector, Figure 2 shows an enlarged stop of the Injector in the area of the core and armature, Figure 3 a first embodiment of an inventive wedge-shaped anchor, Figure 4 shows a second embodiment a wedge anchor and Figure 5 a third Embodiment of a wedge anchor.

Beschreibung der AusführungsbeispieleDescription of the embodiments

Das in der Figur 1 beispielsweise dargestellte elektromagnetisch betätigbare Ventil in der Form eines Einspritzventils für Brennstoffeinspritzanlagen von gemischverdichtenden, fremdgezündeten Brennkraftmaschinen hat einen von einer Magnetspule 1 umgebenen, als Brennstoffeinlaßstutzen dienenden Kern 2, der beispielsweise hier rohrförmig ausgebildet ist und über seine gesamte Länge einen konstanten Außendurchmesser aufweist. Ein in radialer Richtung gestufter Spulenkörper 3 nimmt eine Bewicklung der Magnetspule 1 auf und ermöglicht in Verbindung mit dem einen konstanten Außendurchmesser aufweisenden Kern 2 einen besonders kompakten Aufbau des Einspritzventils im Bereich der Magnetspule 1.The electromagnetic shown in Figure 1, for example actuatable valve in the form of an injection valve for fuel injection systems of mixture compression, spark-ignited internal combustion engines has one of a magnetic coil 1 surrounding, as a fuel inlet connector serving core 2, which for example is tubular here and is constant over its entire length Has outer diameter. One in the radial direction stepped bobbin 3 takes a winding of Magnet coil 1 and in connection with the a core 2 having a constant outer diameter a particularly compact design of the injection valve in the Magnetic coil area 1.

Mit einem unteren Kernende 9 des Kerns 2 ist konzentrisch zu einer Ventillängsachse 10 dicht ein rohrförmiges metallenes Zwischenteil 12 beispielsweise durch Schweißen verbunden und umgibt dabei das Kernende 9 teilweise axial. Der gestufte Spulenkörper 3 übergreift teilweise den Kern 2 und mit einer Stufe 15 größeren Durchmessers das Zwischenteil 12 zumindest teilweise axial. Stromabwärts des Spulenkörpers 3 und des Zwischenteils 12 erstreckt sich ein rohrförmiger Ventilsitzträger 16, der beispielsweise fest mit dem Zwischenteil 12 verbunden ist. In dem Ventilsitzträger 16 verläuft eine Längsbohrung 17, die konzentrisch zu der Ventillängsachse 10 ausgebildet ist. In der Längsbohrung 17 ist eine zum Beispiel rohrförmige Ventilnadel 19 angeordnet, die an ihrem stromabwärtigen Ende 20 mit einem kugelförmigen Ventilschließkörper 21, an dessen Umfang beispielsweise fünf Abflachungen 22 zum Vorbeiströmen des Brennstoffs vorgesehen sind, beispielsweise durch Schweißen verbunden ist.With a lower core end 9 of the core 2 is concentric to a valve longitudinal axis 10 tightly a tubular metal Intermediate part 12 connected for example by welding and partially surrounds the core end 9 axially. The stepped bobbin 3 partially overlaps the core 2 and with a step 15 of larger diameter the intermediate part 12 at least partially axially. Downstream of the Coil body 3 and the intermediate part 12 extends a tubular valve seat support 16, for example is firmly connected to the intermediate part 12. In the valve seat carrier 16 runs a longitudinal bore 17 which is concentric to the valve longitudinal axis 10 is formed. In the longitudinal bore 17 is a tubular valve needle, for example 19 arranged at its downstream End 20 with a spherical valve closing body 21 the extent of which, for example, five flattenings 22 Flowing past the fuel are provided, for example is connected by welding.

Die Betätigung des Einspritzventils erfolgt in bekannter Weise elektromagnetisch. Zur axialen Bewegung der Ventilnadel 19 und damit zum Öffnen entgegen der Federkraft einer Rückstellfeder 25 bzw. Schließen des Einspritzventils dient der elektromagnetische Kreis mit der Magnetspule 1, dem Kern 2 und einem Anker 27. Der Anker 27 ist mit dem dem Ventilschließkörper 21 abgewandten Ende der Ventilnadel 19 durch eine erste Schweißnaht 28 verbunden und auf den Kern 2 ausgerichtet. In das stromabwärts liegende, dem Kern 2 abgewandte Ende des Ventilsitzträgers 16 ist in der Längsbohrung 17 ein zylinderförmiger Ventilsitzkörper 29, der einen festen Ventilsitz aufweist, durch Schweißen dicht montiert.The injection valve is actuated in a known manner Way electromagnetic. For axial movement of the valve needle 19 and thus to open against the spring force a return spring 25 or closing the injection valve serves the electromagnetic circuit with the magnetic coil 1, the core 2 and an anchor 27. The anchor 27 is with the end of the valve needle facing away from the valve closing body 21 19 connected by a first weld 28 and aligned to core 2. In the downstream The end of the valve seat carrier 16 facing away from the core 2 is shown in FIG the longitudinal bore 17 is a cylindrical valve seat body 29, which has a fixed valve seat, by welding tightly assembled.

Zur Führung des Ventilschließkörpers 21 während der Axialbewegung der Ventilnadel 19 mit dem Anker 27 entlang der Ventillängsachse 10 dient eine Führungsöffnung 32 des Ventilsitzkörpers 29. Der kugelförmige Ventilschließkörper 21 wirkt mit dem sich in Strömungsrichtung kegelstumpfförmig verjüngenden Ventilsitz des Ventilsitzkörpers 29 zusammen. An seiner dem Ventilschließkörper 21 abgewandten Stirnseite ist der Ventilsitzkörper 29 mit einer beispielsweise topfförmig ausgebildeten Spritzlochscheibe 34 konzentrisch und fest, verbunden. Im Bodenteil der Spritzlochscheibe 34 verläuft wenigstens eine, beispielsweise verlaufen vier durch Erodieren oder Stanzen ausgeformte Abspritzöffnungen 39.For guiding the valve closing body 21 during the axial movement the valve needle 19 with the armature 27 along the Longitudinal valve axis 10 serves a guide opening 32 of the valve seat body 29. The spherical valve closing body 21 acts with the shape of a truncated cone in the direction of flow tapered valve seat of the valve seat body 29 together. On its end facing away from the valve closing body 21 is the valve seat body 29 with, for example Pot-shaped spray plate 34 concentrically and firm, connected. In the bottom part of the spray plate 34 runs at least one, for example run four formed by eroding or stamping Spray openings 39.

Die Einschubtiefe des Ventilsitzkörpers 29 mit der topfförmigen Spritzlochscheibe 34 bestimmt die Voreinstellung des Hubs der Ventilnadel 19. Dabei ist die eine Endstellung der Ventilnadel 19 bei nicht erregter Magnetspule 1 durch die Anlage des Ventilschließkörpers 21 am Ventilsitz des Ventilsitzkörpers 29 festgelegt, während sich die andere Endstellung der Ventilnadel 19 bei erregter Magnetspule 1 durch die Anlage des Ankers 27 am Kernende 9 ergibt, also genau in dem Bereich, der erfindungsgemäß ausgebildet und durch einen Kreis näher gekennzeichnet ist.The insertion depth of the valve seat body 29 with the pot-shaped spray disk 34 determines the default setting of the stroke of the valve needle 19. Here is the one end position the valve needle 19 when the solenoid is not energized 1 by the installation of the valve closing body 21 on the valve seat of the valve seat body 29 set while the other end position of the valve needle 19 when the solenoid coil is energized 1 results from the installation of the armature 27 at the core end 9, So exactly in the area that is designed according to the invention and is identified by a circle.

Eine in eine konzentrisch zur Ventillängsachse 10 verlaufende Strömungsbohrung 46 des Kerns 2 eingeschobene Einstellhülse 48, die beispielsweise aus gerolltem Federstahlblech ausgeformt ist, dient zur Einstellung der Federvorspannung der an der Einstellhülse 48 anliegenden Rückstellfeder 25, die sich wiederum mit ihrer gegenüberliegenden Seite an der Ventilnadel 19 abstützt. Das Einspritzventil ist weitgehend mit einer Kunststoffumspritzung 50 umschlossen, die sich vom Kern 2 ausgehend in axialer Richtung über die Magnetspule 1 bis zum Ventilsitzträger 16 erstreckt. Zu dieser Kunststoffumspritzung 50 gehört beispielsweise ein mitangespritzter elektrischer Anschlußstecker 52.One in a concentric to the longitudinal axis 10 of the valve Flow bore 46 of the core 2 inserted adjusting sleeve 48, for example made of rolled spring steel sheet is shaped, is used to adjust the Spring preload of the adjoining the adjusting sleeve 48 Return spring 25, which in turn is with its opposite Supported on the valve needle 19. The injection valve is largely with a plastic coating 50 enclosed, starting from the core 2 in axial direction via the solenoid coil 1 to the valve seat support 16 extends. About this plastic encapsulation 50 belongs, for example, to a co-molded electric Connector 52.

Ein Brennstoffilter 61 ragt in die Strömungsbohrung 46 des Kerns 2 an dessen zulaufseitigem Ende 55 hinein und sorgt für die Herausfiltrierung solcher Brennstoffbestandteile, die aufgrund ihrer Größe im Einspritzventil Verstopfungen oder Beschädigungen verursachen könnten.A fuel filter 61 projects into the flow bore 46 of the Core 2 at its inlet end 55 and provides for filtering out such fuel components, which due to their size in the injector blockages or cause damage.

In der Figur 2 ist der in Figur 1 mit einem Kreis gekennzeichnete Bereich der einen Endstellung der Ventilnadel 19, in dem der Anker 27 an dem Kernende 9 des Kerns 2 anschlägt, in einem anderen Maßstab dargestellt. Bereits bekannt ist das Aufbringen von metallischen Schichten 65 auf dem Kernende 9 des Kerns 2 und auf dem Anker 27, beispielsweise von Chrom- oder Nickelschichten, mittels Galvanisierens. Dabei werden die Schichten 65 sowohl auf eine senkrecht zur Ventillängsachse 10 verlaufende Stirnfläche 67 als auch zumindest teilweise auf eine Umfangsfläche 66 des Ankers 27 aufgebracht. Diese Schichten 65 sind besonders verschleißfest und reduzieren mit ihrer kleinen Oberfläche ein hydraulisches Kleben der anschlagenden Flächen, ohne es jedoch sicher verhindern zu können. Die Schichtdicke dieser Schichten 65 beträgt im allgemeinen zwischen 10 und 25 µm.In FIG. 2, the one marked with a circle in FIG. 1 is shown Range of one end position of the valve needle 19, in which the armature 27 at the core end 9 of the core 2 strikes, shown on a different scale. Already it is known to apply metallic layers 65 on the core end 9 of the core 2 and on the anchor 27, for example of chrome or nickel layers, by means of electroplating. The layers 65 are both on a End face perpendicular to the longitudinal axis 10 of the valve 67 and at least partially on a peripheral surface 66 the anchor 27 applied. These layers are 65 particularly wear-resistant and reduce with their small size Surface a hydraulic gluing of the striking surfaces, but without being able to prevent it safely. The Layer thickness of these layers 65 is generally between 10 and 25 µm.

Für die Funktion des Einspritzventils ist es notwendig, daß Kern 2 und Anker 27 nur in einem relativ kleinen Bereich, beispielsweise nur im äußeren, von der Ventillängsachse 10 abgewandten Bereich der oberen Stirnfläche des Ankers 27 anschlagen. Diese Forderung wird gerade durch die galvanische Beschichtung erreicht. Bei der galvanischen Beschichtung tritt an den Kanten der zu beschichtenden Teile, hier Kern 2 und Anker 27, eine Feldlinienkonzentration auf, die dazu führt, daß eine keilige Schichtdickenverteilung, wie sie in Figur 2 angedeutet ist, auftritt. Die aufgebrachte keilige Schicht 65 wird also beim Betrieb des Einspritzventils nur in einem kleinen Bereich beansprucht. Beim Dauerbetrieb liegt allerdings nicht mehr eine definierte Anschlagfläche vor, da durch mehrere Millionen Anschläge Teile der Schicht 65 abgetragen werden, so daß sich die Anschlagfläche immer weiter vergrößert und somit die Keiligkeit ständig weiter reduziert wird.For the function of the injection valve it is necessary that core 2 and anchor 27 only in a relatively small Area, for example only in the outer, from the valve longitudinal axis 10 area of the upper end face facing away anchor 27. This demand is just now achieved by the galvanic coating. With the galvanic Coating occurs at the edges of the coating parts, here core 2 and anchor 27, a field line concentration on, which leads to a wedge Layer thickness distribution, as indicated in Figure 2 is occurs. The wedge-shaped layer 65 applied So when operating the injector only in a small one Area occupied. However, in continuous operation no longer a defined stop surface because parts of layer 65 removed by several million attacks be so that the stop surface always further increases and thus the wedge is constantly increasing is reduced.

Demgegenüber ist in der Figur 3 ein Teil des erfindungsgemäßen Ankers 27 im Bereich seiner oberen Stirnfläche 67 gezeigt, die bereits vor der Beschichtung oder dem Erzeugen der Verschleißfestigkeit der Oberfläche einen Keilabschnitt 73 mit einem geneigten, schrägen Verlauf gegenüber der Ventillängsachse 10 aufweist, so daß der Anker 27 dort eine Keilform hat. Die Neigung des Keilabschnitts 73 der Stirnfläche 67 des Ankers 27 verläuft bei dem Ausführungsbeispiel in Figur 3 nach innen, wobei auch ein Keilabschnitt 73 der Stirnfläche 67 geneigt nach außen ausgebildet sein kann (Figur 4). Die Keilform des Ankers 27 im Bereich der Stirnfläche 67 wird bereits bei der mechanischen Bearbeitung, beispielsweise durch ein entsprechend geschliffenes Senkwerkzeug, hergestellt.In contrast, part of the invention is shown in Figure 3 Anchor 27 in the area of its upper end face 67 shown that before coating or generating the wear resistance of the surface a wedge section 73 with an inclined, oblique course opposite the valve longitudinal axis 10, so that the armature 27 there has a wedge shape. The inclination of the wedge section 73 of the End face 67 of armature 27 extends in the exemplary embodiment in Figure 3 inside, including a wedge section 73 of the end face 67 is inclined to the outside can be (Figure 4). The wedge shape of the anchor 27 in The area of the end face 67 is already in the mechanical Editing, for example by a corresponding ground countersinking tool.

Während die bei galvanisch abgeschiedenen Schichten 65 entstehende Schichtdickenverteilung physikalisch vorgegeben und kaum beeinflußbar ist, kann die Keiligkeit des Ankers 27 vor der Beschichtung bzw. dem Erzeugen der Verschleißfestigkeit entsprechend geforderter Werte so vorbestimmt und gefertigt werden, daß bei der Benutzung jeweils ein magnetisches und hydraulisches Optimum erreicht wird. Ein hydraulisches Kleben des Ankers 27 am Kern 2 ist durch den keiligen Anker nun vollständig ausgeschlossen, da auch bei weitgehend eben abgeschiedenen (auch magnetischen) Schichten 65 die Keiligkeit auf jeden Fall vorhanden ist. Mit Hilfe sehr genau geschliffener Senkwerkzeuge können engere Fertigungstoleranzen für die Keiligkeit als bisher eingehalten werden, so daß es beim Betrieb des Einspritzventils zu einer noch geringeren Streuung der Anzugs- und Abfallzeit des Ankers 27 kommt. Der geneigte Keilabschnitt 73 der Stirnfläche 67 erlaubt es zudem, daß auch nichtgalvanische, verschleißfeste Schichten, die auch magnetisch sein dürfen, aufgebracht werden können, ohne daß die Forderung nach einem sehr kleinen Anschlagbereich unerfüllt bleibt.While the layers 65 resulting layer thickness distribution is physically predetermined and can hardly be influenced, the wedge of the Anchor 27 before coating or generating wear resistance predetermined in accordance with the required values and be made that when used each achieved a magnetic and hydraulic optimum becomes. Hydraulic bonding of the armature 27 to the core 2 is now completely excluded by the wedge anchor, because even with largely flat (also magnetic) Layers 65 definitely have the wedge is. With the help of very precisely ground countersinking tools can have tighter manufacturing tolerances for the wedge than have been observed so far, so that it is in operation of the injection valve to an even smaller spread of suit and fall time of the anchor 27 comes. The inclined one Wedge section 73 of the end face 67 also allows that also non-galvanic, wear-resistant layers that too may be magnetic, can be applied without that the requirement for a very small stop area remains unfulfilled.

Außerdem kann die Stirnfläche 67, zumindest im Bereich ihres höchsten Punktes, durch eine Behandlung der Oberfläche mittels eines Härteverfahrens verschleißfest gemacht werden. Als Härteverfahren sind hierzu z.B. die bekannten Nitrierverfahren wie Plasmanitrieren oder Gasnitrieren geeignet.In addition, the end face 67, at least in the area at its highest point, by treating the surface made wear-resistant by means of a hardening process will. As a hardening process, e.g. the well-known Nitriding processes such as plasma nitriding or gas nitriding suitable.

Bei dem Ausführungsbeispiel nach Figur 3 ist ausgehend von der Umfangsfläche 66 des Ankers 27 zunächst ein Anschlagabschnitt 68 der Stirnfläche 67 vorgesehen, der sich über eine Breite a radial nach innen senkrecht zur Ventillängsachse 10 erstreckt und als Anschlagfläche dient. Dieser Anschlagabschnitt 68 stellt über die gesamte Betriebsdauer eine fast vollständig konstant in ihrer Breite a bleibende Ringfläche dar. Der Anschlagflächenverschleiß bei Dauerbetrieb ist damit genau definiert. Um ein hydraulisches und magnetisches Optimum zu erreichen, ist der Keilabschnitt 73 idealerweise um einen Winkel zwischen >0° und <=1° gegenüber dem Anschlagabschnitt 68 geneigt. Die minimal keilige, z. B. aus Chrom gebildete Schicht 65, die auf der Stirnfläche 67 abgeschieden wird, besitzt nur einen Bruchteil der Neigung des sich an den Anschlagabschnitt 68 nach innen anschließenden, geneigten Keilabschnitts 73 des Ankers 27. Folglich bleibt die vor dem Beschichten am Anker 27 vorgesehene Neigung des Keilabschnittes 73 vollständig erhalten bzw. wird minimal verstärkt.In the embodiment of Figure 3 is based on the peripheral surface 66 of the armature 27 is initially a stop section 68 of the end face 67 is provided, which over a width a radially inwards perpendicular to the longitudinal axis of the valve 10 extends and serves as a stop surface. This Stop section 68 represents the entire operating time an almost completely constant in width a Annular surface. The abutment surface wear at Continuous operation is precisely defined. To be a hydraulic and to achieve the magnetic optimum is Wedge section 73 ideally by an angle between> 0 ° and <= 1 ° inclined with respect to the stop section 68. The minimally wedge-shaped, e.g. B. made of chrome layer 65, the is deposited on the end face 67, only has a fraction of the slope of the abutting portion 68 inclined wedge section adjoining the inside 73 of anchor 27. Consequently, that remains before Coating provided on the armature 27 inclination of the wedge section 73 completely preserved or minimally reinforced.

Da die Anschlagflächenbreite, die der Breite a des Anschlagabschnitts 68 entspricht, auch bei Verschleiß konstant bleibt, ist eine konstante Kontaktbreite während des Anschlagens von Kern 2 und Anker 27 über die gesamte Lebensdauer vorhanden, wodurch auch die hydraulischen Verhältnisse im Spalt zwischen dem Kern 2 und dem Anker 27 konstant bleiben, was einen besonderen Vorteil darstellt. Wie bereits erwähnt, kann zumindest die Oberfläche des Anschlagabschnittes 68 auch durch ein Härteverfahren verschleißfest gemacht werden, so daß keine zusätzliche Schicht 65 auf die Stirnfläche 67 aufgetragen werden muß.Since the stop surface width is that of the width a of the stop section 68 corresponds, constant even with wear remains, is a constant contact width during the Striking core 2 and anchor 27 over the entire Lifespan available, which also affects the hydraulic conditions in the gap between the core 2 and the armature 27 remain constant, which is a particular advantage. As already mentioned, at least the surface of the stop section 68 also wear-resistant thanks to a hardening process be made so that no additional Layer 65 must be applied to the end face 67.

Die gleichen Effekte sind ebenso erzielbar, wenn sowohl der Anker 27 als auch der Kern 2 vor dem Beschichten bzw. dem Erzeugen einer verschleißfesten Oberfläche mit Keilabschnitten 73 der Stirnflächen 67 versehen werden. Damit kann eine noch höhere Anschlagsicherheit bzw. Verhinderung des hydraulischen Klebens gewährleistet werden. Wenn es zweckmäßig ist, kann selbstverständlich das Anbringen eines Keilabschnitts der Stirnfläche auch nur am Kern 2 vorgenommen werden, wobei der Anker 27 beispielsweise eine plane Stirnfläche behält.The same effects can also be achieved if both the anchor 27 as well as the core 2 before coating or creating a wear-resistant surface with wedge sections 73 of the end faces 67 are provided. In order to can an even higher security against impact or prevention of hydraulic gluing can be guaranteed. If it is appropriate, of course, the attachment of a wedge section of the end face only on the core 2 be made, the anchor 27, for example, a flat end face.

Weitere Ausführungsbeispiele von erfindungsgemäß ausgebildeten Ankern 27 zeigen die Figuren 4 und 5. In der Figur 4 ist ein Anker 27 dargestellt, bei dem der Keilabschnitt 73 der Stirnfläche 67 geneigt nach außen ausgeführt ist.Further exemplary embodiments of those designed according to the invention Anchors 27 are shown in FIGS. 4 and 5. In FIG. 4 An anchor 27 is shown in which the wedge section 73 the end face 67 is inclined to the outside.

Ein erfindungsgemäßes Ausführungsbeispiel des Ankers 27, bei dem die Stirnfläche 67 nur durch den Keilabschnitt 73 gebildet wird, zeigt die Figur 5. Hierbei wird völlig auf den wenigstens eine geringe radiale Erstreckung aufweisenden Anschlagabschnitt 68 verzichtet; vielmehr liegt eine Keiligkeit an der gesamten Stirnfläche 67 vor, es besteht also kein senkrecht zur Ventil längsachse 10 verlaufender Bereich der Stirnfläche 67. Besonders bei sehr kleinen Winkeln des Keilabschnitts 73 liegt auch dann ein stabiler Anschlag vor, so daß auch bei Dauerbetrieb eine definierte Anschlagfläche bleibt. Neben der in Figur 5 gezeigten Möglichkeit des Verlaufs der Neigung des Keilabschnitts 73 in Richtung zu der Ventillängsachse 10 hin, ist auch ein Ausführungsbeispiel analog zu dem in der Figur 4 dargestellten Ausführungsbeispiel denkbar, bei dem sich der Keilabschnitt 73 in Richtung von der Ventillängsachse 10 weg erstreckt, also nach außen geneigt ausgeführt ist.An embodiment of the armature 27 according to the invention, in which the end face 67 only through the wedge section 73 is shown, Figure 5. This is completely on the one with at least a small radial extension Stop section 68 omitted; rather there is one Wedge on the entire face 67 before, there is So no longitudinal axis 10 perpendicular to the valve Area of the end face 67. Especially for very small ones Angles of the wedge section 73 are then more stable Stop before, so that even in continuous operation a defined The stop surface remains. In addition to the possibility shown in Figure 5 the slope of the wedge portion 73 in Direction to the valve longitudinal axis 10 is also an embodiment analogous to that shown in FIG. 4 Embodiment conceivable in which the wedge section 73 extends in the direction away from the valve longitudinal axis 10, is designed inclined outwards.

Da an wenigstens einer Stirnfläche 67 von Anker 27 und/oder Kern 2 bereits der Keilabschnitt 73 vorliegt, der bisher erst durch das Aufbringen von Chrom- oder Nickelschichten erzielt wurde, können nun, wie bereits erwähnt, auch andere Verfahren zur Qualitätserhöhung durch Verbesserung der Verschleißfestigkeit der Stirnfläche 67 zum Einsatz kommen. Durch den Einsatz von Härteverfahren, wie z.B. Plasmanitrieren, Gasnitrieren oder Carburieren, durch die die Oberflächenstruktur am Anker 27 und/oder Kern 2 verändert wird, kann sogar ganz auf Verfahren zur unmittelbaren Beschichtung verzichtet werden.Since at least one end face 67 of armature 27 and / or core 2 already has the wedge section 73 which so far only through the application of chrome or nickel layers has been achieved, as already mentioned, other methods of increasing quality through improvement the wear resistance of the end face 67 to Come into play. Through the use of hardening processes, such as e.g. Plasma nitriding, gas nitriding or carburizing the surface structure on anchor 27 and / or core 2 is changed, can even be entirely based on procedures for immediate Coating can be dispensed with.

Claims (9)

  1. Electromagnetically operable valve, in particular a fuel injection valve for fuel injection systems of internal-combustion engines, having a valve longitudinal axis, having a core made from ferromagnetic material, having a magnet coil, and an armature, which operates a valve closing member cooperating with a fixed valve seat and is drawn against a stop surface of the core when the magnet coil is excited, characterized in that at least one of the two end faces (67) of the components of armature (27) and core (2), which are each directed towards the other, opposite component, has at least one wedge section (73) extending obliquely relative to the valve longitudinal axis (10).
  2. Valve according to Claim 1, characterized in that at least one of the two end faces (67) of the components of armature (27) and core (2) is divided into a stop section (68) and the at least one wedge section (73) extending obliquely relative to the valve longitudinal axis (10), and the at least one stop section (68) has a defined width (a).
  3. Valve according to Claim 2, characterized in that the at least one stop section (68) on the armature (27) and/or core (2) has a width (a) which represents only a fraction of the diameter of the end face (67).
  4. Valve according to Claim 1, characterized in that the at least one wedge section (73) extending obliquely relative to the valve longitudinal axis (10) extends over the entire end face (67).
  5. Valve according to Claim 2 or 4, characterized in that the at least one wedge section (73) on the core (2) and/or armature (27) extends in an inclined fashion in the direction of the valve longitudinal axis (10).
  6. Valve according to Claim 2 or 4, characterized in that the at least one wedge section (73) on the core (2) and/or armature (27) extends in an inclined fashion away from the valve longitudinal axis (10).
  7. Valve according to Claim 1, characterized in that the core (2) and/or armature (27) are coated in the region of the end face (67).
  8. Valve according to Claim 7, characterized in that the layer (65) applied by coating is magnetic.
  9. Valve according to Claim 1, characterized in that the core (2) and/or armature (27) are treated in the region of the end face (67) by means of a hardening process.
EP95900661A 1993-12-09 1994-11-24 Electromagnetic valve Expired - Lifetime EP0683862B1 (en)

Applications Claiming Priority (5)

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DE4341961 1993-12-09
DE4341961 1993-12-09
DE4421935 1994-06-23
DE4421935A DE4421935A1 (en) 1993-12-09 1994-06-23 Electromagnetically operated valve esp. for IC engine fuel-injection valve - has one of facing end faces of armature or core elements having wedge section which is inclined to valve longitudinal axis
PCT/DE1994/001392 WO1995016126A1 (en) 1993-12-09 1994-11-24 Electromagnetic valve

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EP0683862B1 true EP0683862B1 (en) 1998-06-10

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JP (2) JP3742651B2 (en)
CN (1) CN1049951C (en)
BR (1) BR9406079A (en)
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WO2002095215A1 (en) 2001-05-21 2002-11-28 Robert Bosch Gmbh Fuel injection valve
DE102008053310A1 (en) 2008-10-27 2010-04-29 Vacuumschmelze Gmbh & Co. Kg Soft-magnetic workpiece with wear-resistant layer, used to make fuel injection- or solenoid valve, includes core of crystalline iron-cobalt alloy
DE102008031690B4 (en) * 2007-07-06 2011-06-16 AISAN KOGYO KABUSHIKI KAISHA, Obu-shi Fuel injection valve

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US5732888A (en) 1998-03-31
JP2005337266A (en) 2005-12-08
BR9406079A (en) 1996-01-16
EP0683862A1 (en) 1995-11-29
RU2131549C1 (en) 1999-06-10
WO1995016126A1 (en) 1995-06-15
JPH08506877A (en) 1996-07-23
ES2118531T3 (en) 1998-09-16
JP3742651B2 (en) 2006-02-08
CZ285156B6 (en) 1999-05-12
CN1049951C (en) 2000-03-01
CZ197795A3 (en) 1996-05-15
CN1116871A (en) 1996-02-14
JP3864175B2 (en) 2006-12-27

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