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EP3833865B1 - Valve of a fuel injector - Google Patents

Valve of a fuel injector Download PDF

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Publication number
EP3833865B1
EP3833865B1 EP19768811.2A EP19768811A EP3833865B1 EP 3833865 B1 EP3833865 B1 EP 3833865B1 EP 19768811 A EP19768811 A EP 19768811A EP 3833865 B1 EP3833865 B1 EP 3833865B1
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EP
European Patent Office
Prior art keywords
armature
damping element
valve
accordance
opening
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.)
Active
Application number
EP19768811.2A
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German (de)
French (fr)
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EP3833865A1 (en
Inventor
Richard Pirkl
Razvan-Sorin STINGHE
Martin Seidl
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.)
Liebherr Components Deggendorf GmbH
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Liebherr Components Deggendorf GmbH
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Publication of EP3833865A1 publication Critical patent/EP3833865A1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/0012Valves
    • F02M63/007Details not provided for in, or of interest apart from, the apparatus of the groups F02M63/0014 - F02M63/0059
    • F02M63/0075Stop members in valves, e.g. plates or disks limiting the movement of armature, valve or spring
    • 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
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/0012Valves
    • F02M63/0014Valves characterised by the valve actuating means
    • F02M63/0015Valves characterised by the valve actuating means electrical, e.g. using solenoid
    • F02M63/0017Valves characterised by the valve actuating means electrical, e.g. using solenoid using electromagnetic operating means
    • F02M63/0019Valves characterised by the valve actuating means electrical, e.g. using solenoid using electromagnetic operating means characterised by the arrangement of electromagnets or fixed armatures

Definitions

  • the present invention relates to a valve for a fuel injector.
  • Fuel injectors also called injection nozzles, are an essential component of every internal combustion engine, as they introduce the required amount of combusting fuel into the combustion chamber. For clean combustion, it is extremely important to maintain the rapid opening and closing of the injector throughout its entire service life in order to continuously deliver a precise amount of fuel.
  • a valve is provided to transition the injector from a closed to an open state. This valve separates a high-pressure fuel region from a low-pressure region. When the regions are connected by the valve transitioning to its open position, this leads to a fuel injection process through the injector via a hydraulic-mechanical chain of action.
  • a solenoid valve In a closed state, a A magnetizable part, the armature, is subjected to a preload force by means of a spring element, which presses the armature in the axial direction away from the magnet towards a seat plate which has an opening. By pressing the armature onto the seat plate, the armature closes the opening, thus closing a connection extending through the opening between the high-pressure area and the low-pressure area of the fuel.
  • This is typically achieved by a sealing plate of the armature facing the seat plate closing the opening in the seat plate, so that the high-pressure area is separated from a low-pressure area.
  • the high-pressure area corresponds to the system pressure with which the fuel is injected into the combustion chamber.
  • the area with lower pressure corresponds to the tank pressure or even the ambient pressure.
  • the connection between the high-pressure and low-pressure areas is released via the opening in the seat plate by an axial movement of the armature toward the magnet, allowing fuel to flow from the high-pressure area to the low-pressure area.
  • the hydraulic-mechanical chain of action briefly mentioned above at least one fuel inlet from the injector into the combustion chamber is opened, allowing fuel to enter the combustion chamber.
  • the US2014/0367595 A1 shows a valve for controlling a fuel-gas mixture, which has several asymmetrically formed damping elements spaced radially from the central axis of an armature.
  • the EP 1 970 557 A2 discloses a valve for fuel injectors in which a valve element is fixedly connected to an armature, the valve being in an open state when the armature or valve element is in an intermediate position in which the armature is neither completely repelled nor completely attracted by an electromagnet.
  • the WO 2017/158788 discloses a solenoid valve in which, in order to reduce the impact noise of a metal armature, the latter is provided with a thick, rubber-elastic body.
  • the aim of the present invention is to minimize armature bounce when the armature strikes the magnet, so that the associated disadvantages can be mitigated or overcome.
  • the valve of a fuel injector for selectively separating a high-pressure region from a low-pressure region of a fuel comprises an opening in a seat plate, an armature configured to close the opening of the seat plate, a spring element that biases the armature toward a position closing the opening, and an electromagnet for lifting the armature from the position closing the opening into a position releasing the opening.
  • the valve according to the invention is characterized in that it further comprises an elastically compressible damping element for limiting an armature stroke when the armature is lifted from the seat plate into the releasing position.
  • This elastically compressible damping element dampens when the magnet is activated and the armature is attracted as a result away from the opening, the movement of the armature is reduced, so that the bouncing between the magnet and the armature is prevented or reduced.
  • the damping element is a soft, elastic damping element.
  • a soft, elastic design of the damping element is particularly well suited to suppressing the oscillating vibration of the armature, which occurs when the damping element impacts with a continuous magnetic attraction force away from the opening.
  • the stiffness of the damping element is smaller than the stiffness of the anchor.
  • the damping element is a damping pin with a substantially cylindrical shape, which preferably has a cross-sectional reduction between its two end faces.
  • One of the two end faces is designed to serve as a stop surface for the armature.
  • the pin is arranged in a recess in the magnet.
  • the cross-sectional reduction can be a groove running around the outer circumference of the pin, which preferably runs completely around the outer circumference.
  • the circumferential groove has an arc shape when viewed in cross-section, which is rounded at the groove transitions.
  • the damping element has a spherical section on its contact surface with the armature in order to minimize a contact surface with the armature.
  • the advantage of this is that the magnetic flux across the contact surface is as low as possible. Furthermore, the spherical contact surface ensures that the contact area between the damping element and the armature is always the same, even if the damping element is misaligned due to tolerances.
  • the poles of the electromagnet and the end face of the damping element contacting the armature lie in a common plane when the damping element is in a relaxed state.
  • the end sections of the poles facing the armature and the end face of the damping element contacting the armature are arranged in a common plane when the armature is in its relaxed state and is not attracted by the magnet.
  • the damping element is designed separately from a housing of a fuel injector.
  • the damping element is mounted and held in position by a press fit.
  • the press fit can be implemented, for example, by providing a recess in the magnet into which the damping element is received.
  • the invention can provide for the preload force of the spring element to be adjustable, preferably via adjusting discs for changing the position of the spring element relative to the damping element and/or the armature. This allows the spring preload force to be precisely adjusted, even in the presence of an undesired deviation of the spring force from the expected spring force value.
  • the end face of the damping element facing away from the armature is designed as a flat seat. It can be provided that the flat seat is arranged in the magnet.
  • the armature has a raised portion on its surface facing the damping element, with which the armature contacts the damping element. Therefore, in the attracted state, i.e., when the magnet is active and the armature is in the release position, a gap can be provided between the pole cores of the magnet and a non-raised end face of the armature. This prevents contact between the armature and the magnet.
  • the anchor can be designed in several parts, so that it comprises an anchor part and a seat part or consists of these parts.
  • the spring element is a spiral spring, which preferably extends spirally around the damping element or winds spirally around the damping element.
  • the damping element is thus partially or completely accommodated in the space defined by the spiral shape of the spring element.
  • the invention provides that the armature only comes into contact with the damping element during the transition from the position closing the opening to the position releasing it.
  • the armature contacts the seat plate with a sealing surface and also the spring element, which exerts a spring force toward the opening.
  • the structure of the valve is rotationally symmetrical or rotationally symmetrical to a rotation axis, which is preferably identical to a rotation axis of the damping element.
  • the invention also relates to a fuel injector with a valve according to one of the variants listed above, in particular a diesel fuel injector.
  • the present invention makes it possible to accelerate the switch-off times of the solenoid valve due to the lower remanence force between the armature and the contact on the damping element. This is because, due to the reduced contact area between the damping element and the armature, a smaller magnetic flux flows through the damping element than would be the case with a larger contact area, as is typically found in the prior art.
  • Figure 1 shows a half sectional view of the valve 1 according to the invention.
  • This opening 2 is closed by an armature 4, which seals the opening 2 with its sealing surface 15 in its closed state.
  • the armature 4 can be lifted from this position when the magnet 6 is activated and thus pulls the armature 4 away from the opening 2.
  • a spiral spring 5 ensures that the armature 4 is pressed with its sealing surface 15 against the opening 2.
  • the magnet 6 has a coil 61 and a coil casing 62, so that a magnetic force can be generated by current flowing through the coil 61.
  • a damping element 7 is arranged in the space delimited by the spiral spring 5, which corresponds to a damping pin in the illustration shown.
  • This damping pin 7 has a first end face 8 that faces the armature 4.
  • the end face 8 is rounded in this case or corresponds to a section of a sphere, so that when the armature 4 impacts the damping element 7, only the smallest possible contact area is created between the armature 4 and the damping element 7.
  • the damping element 7 has a recess 14 in its circumference, which ensures lower rigidity and thus a certain elasticity of the damping element 7.
  • This recess 14 can be rounded, as can be seen from the reference numeral 12.
  • the damping element 7 can be held in the magnet 6 by a press fit.
  • an adjusting disk 11 can be provided to adjust the preload force of the spring element 5, with which the spring can be moved in its position in the axial direction.
  • the armature 4 can have a raised portion 13 with which the armature 4 strikes the contact surface 8 of the damping element 7.
  • An armature guide 16 is provided to guide the armature during a transition from its sealing position to the position that releases the opening 2.
  • a spacer ring 17 shields the armature 4 from the housing 10 of a fuel injector.
  • Reference numeral 9 designates the magnetic poles of the magnet 6.
  • the axis of symmetry 13 shows that the valve 1 is constructed with mirror symmetry and/or rotational symmetry.
  • a magnetizable part guided in the armature guide 16, here the armature 4 is subjected to a force defined by the adjusting disc 11, the preload force, by means of the spring element 5, which closes the armature 4 in the axial direction away from the magnet 6 toward a sealing part of the seat plate 3.
  • the seat plate 3 separates a high-pressure area from a low-pressure area of the fuel.
  • the connection between the high-pressure area and the low-pressure area is released via the opening 2 in the seat plate 3 by an axial movement of the armature 4 in the direction of the magnet 6, so that fuel is discharged from the Fig. 1 high pressure area below into the low pressure area, which is in the Fig. 1 arranged above the seat plate 3.
  • a hydraulic-mechanical chain of action at least one fuel inlet is released from the injector into the combustion chamber and fuel is supplied to the combustion chamber.
  • a voltage source To open the solenoid valve 1, i.e., the transition between a closed and an open state, a voltage source generates current that flows through the windings of the coil 61.
  • the windings of the coil 61 are surrounded by a coil sheath 62, which in turn is surrounded radially inward and outward by a ferromagnetic core 6, which serves to amplify the magnetic field induced by the current in the coil 61.
  • the armature 4 is continuously accelerated by the attractive magnetic force, which increases with decreasing distance, until the armature 4 comes into contact with the damping element 7.
  • the armature 4 then strikes a contact surface 8 of the damping element 7, which is formed by a pin projecting therefrom.
  • the damping pin 7 acts like a very hard spring, but has comparatively low stiffness compared to the armature 4.
  • the stiffness of the damping pin or damping element can be less than 70%, preferably less than 50%, and most preferably less than 30% of the stiffness of the armature 4.
  • the damping pin 7 completely brakes the armature 4, whereby the damping pin 7 is elastically compressed. Apart from the contact between the armature 4 and the pin 7, there is no further mechanical contact between the armature 4 and the magnet 6.
  • the restoring force of the spring 5 and the pin 7 causes the pin 7 to expand in the direction of the opening 2 of the seat plate 3.
  • the pin 7 is deformed to a degree at which the sum of the forces acting on the armature 4 (the attractive magnetic force and the repulsive restoring force by spring 5 and pin deformation) cancel each other out in the force equilibrium.
  • Fig. 3 shows this vibration behavior of the armature based on the armature stroke h in comparison with different elasticities of the damping element 7.
  • a solid line shows a hard elasticity
  • a dashed line shows a soft elasticity of the damping element 7.

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

Description

Die vorliegende Erfindung betrifft ein Ventil eines Kraftstoffinjektors. Kraftstoffinjektoren, die auch Einspritzdüsen genannt werden, sind wesentlicher Bestandteil einer jeden Brennkraftmaschine, da hierüber die erforderliche Menge des verbrennenden Kraftstoffes in den Brennraum eingeleitet wird. Für eine saubere Verbrennung ist es dabei von hoher Wichtigkeit, über die gesamte Lebensdauer eines Injektors ein möglichst rasches Öffnen und Schließen des Injektors beizubehalten, um fortwährend eine exakte Menge eines Kraftstoffes zuführen zu können.The present invention relates to a valve for a fuel injector. Fuel injectors, also called injection nozzles, are an essential component of every internal combustion engine, as they introduce the required amount of combusting fuel into the combustion chamber. For clean combustion, it is extremely important to maintain the rapid opening and closing of the injector throughout its entire service life in order to continuously deliver a precise amount of fuel.

Dem Fachmann ist bekannt, dass für einen Übergang von einem geschlossenen in einen geöffneten Zustand des Injektors ein Ventil vorhanden ist, das einen Hochdruckbereich des Kraftstoffs von einem Bereich mit Niederdruck trennt. Werden die Bereiche miteinander verbunden, indem das Ventil in seine geöffnete Stellung übergeht, führt dies über eine hydraulisch-mechanische Wirkkette zu einem Einspritzvorgang von Kraftstoff durch den Injektor.Those skilled in the art know that a valve is provided to transition the injector from a closed to an open state. This valve separates a high-pressure fuel region from a low-pressure region. When the regions are connected by the valve transitioning to its open position, this leads to a fuel injection process through the injector via a hydraulic-mechanical chain of action.

Nach dem Stand der Technik wird dabei typischerweise ein Magnetventil verwendet. In einem geschlossenen Zustand wird ein in einer Führung geführtes, magnetisierbares Teil, der Anker, mittels eines federnden Elements mit einer Vorspannkraft beaufschlagt, welche den Anker in axialer Richtung vom Magneten weg hin zu einer Sitzplatte drückt, die eine Öffnung aufweist. Durch das Drücken des Ankers hin auf die Sitzplatte, verschließt der Anker die Öffnung, sodass eine sich durch die Öffnung erstreckende Verbindung von Hochdruckbereich und Niederdruckbereich des Kraftstoffs geschlossen wird. Typischerweise wird dies dadurch erreicht, dass eine der Sitzplatte zugewandte Dichtplatte des Ankers die Öffnung in der Sitzplatte verschließt, sodass der unter Hochdruck stehende Bereich von einem Bereich mit Niederdruck getrennt ist. Der unter Hochdruck stehende Bereich entspricht dabei dem Systemdruck mit dem der Kraftstoff in den Brennraum eingespritzt wird. Der Bereich mit niedrigerem Druck entspricht dabei dem Tankdruck oder auch dem Umgebungsdruck.According to the state of the art, a solenoid valve is typically used. In a closed state, a A magnetizable part, the armature, is subjected to a preload force by means of a spring element, which presses the armature in the axial direction away from the magnet towards a seat plate which has an opening. By pressing the armature onto the seat plate, the armature closes the opening, thus closing a connection extending through the opening between the high-pressure area and the low-pressure area of the fuel. This is typically achieved by a sealing plate of the armature facing the seat plate closing the opening in the seat plate, so that the high-pressure area is separated from a low-pressure area. The high-pressure area corresponds to the system pressure with which the fuel is injected into the combustion chamber. The area with lower pressure corresponds to the tank pressure or even the ambient pressure.

In einem offenen Zustand wird die Verbindung zwischen Hochdruckbereich und Niederdruckbereich über die Öffnung in der Sitzplatte durch eine axiale Bewegung des Ankers in Richtung des Magneten freigegeben, sodass Kraftstoff von Hochdruckbereich in den Niederdruckbereich fließen kann. Über die bereits kurz erwähnte hydraulisch-mechanische Wirkkette wird mindestens ein Kraftstoffeinlass vom Injektor in den Brennraum freigegeben, sodass Kraftstoff in den Brennraum eintritt.In the open state, the connection between the high-pressure and low-pressure areas is released via the opening in the seat plate by an axial movement of the armature toward the magnet, allowing fuel to flow from the high-pressure area to the low-pressure area. Via the hydraulic-mechanical chain of action briefly mentioned above, at least one fuel inlet from the injector into the combustion chamber is opened, allowing fuel to enter the combustion chamber.

Beim Ausheben des Ankers aus dem geschlossenen in den offenen Zustand ist es nach dem Stand der Technik üblich, dass der Anker gegen eine Anschlagfläche des Magneten anschlägt und dabei an der Anschlagfläche prellt, was eine hohe Abnutzung des Ankers hervorruft. Weiter nachteilhaft ist das Prellen auch deswegen, da das Prellen die Schaltzeiten des Ankers stark beeinträchtigt.When lifting the armature from the closed to the open position, it is common practice in the state of the art for the armature to strike a stop surface of the magnet and bounce off the stop surface, causing significant wear on the armature. This bouncing is also disadvantageous because it severely impairs the armature's switching times.

Die US2014/0367595 A1 zeigt ein Ventil zur Steuerung eines Kraftstoff-GasGemisches, das mehrere asymmetrisch gebildete und radial von der Mittelachse eines Ankers beabstandete Dämpfungselemente aufweist.The US2014/0367595 A1 shows a valve for controlling a fuel-gas mixture, which has several asymmetrically formed damping elements spaced radially from the central axis of an armature.

Die EP 1 970 557 A2 offenbart ein Ventil für Kraftstoffinjektoren, bei dem ein Ventilelement fest mit einem Anker verbunden ist, wobei das Ventil in einem geöffneten Zustand ist, wenn sich der Anker bzw. des Ventilelement in einer Zwischenstellung befindet, bei der der Anker durch einen Elektromagneten weder vollständig abgestoßen noch vollständig angezogen ist.The EP 1 970 557 A2 discloses a valve for fuel injectors in which a valve element is fixedly connected to an armature, the valve being in an open state when the armature or valve element is in an intermediate position in which the armature is neither completely repelled nor completely attracted by an electromagnet.

Die WO 2017/158788 offenbart ein Magnetventil, bei dem zum Vermindern eines Schlaggeräusches eines metallenen Ankers dieser mit einem dicken, gummielastischen Körper versehen ist.The WO 2017/158788 discloses a solenoid valve in which, in order to reduce the impact noise of a metal armature, the latter is provided with a thick, rubber-elastic body.

Demnach ist es das Ziel der vorliegenden Erfindung, das Ankerprellen beim Anschlagen des Ankers am Magneten zu minimieren, sodass die damit einhergehenden Nachteile abgemildert oder überwunden werden können.Accordingly, the aim of the present invention is to minimize armature bounce when the armature strikes the magnet, so that the associated disadvantages can be mitigated or overcome.

Dies gelingt mithilfe eines Ventils eines Kraftstoffinjektors, das sämtliche Merkmale des Anspruchs 1 aufweist. Vorteilhafte Ausgestaltungen dieses Ventils finden sich dabei in den abhängigen Ansprüchen.This is achieved by means of a valve of a fuel injector having all the features of claim 1. Advantageous embodiments of this valve can be found in the dependent claims.

Nach der Erfindung umfasst das Ventil eines Kraftstoffinjektors zum wahlweisen Trennen eines Hochdruckbereichs von einem Niederdruckbereich eines Kraftstoffs eine Öffnung in einer Sitzplatte, einen Anker, der dazu ausgelegt ist, die Öffnung der Sitzplatte zu verschließen, ein Federelement, dass den Anker in Richtung einer die Öffnung verschließenden Position vorspannt und einen Elektromagnet zum Abheben des Ankers aus der die Öffnung verschließenden Position in eine die Öffnung freigebende Position. Das erfindungsgemäße Ventil zeichnet sich dadurch aus, dass es ferner ein elastisch stauchbares Dämpfungselement zum Begrenzen eines Ankerhubs beim Abheben des Ankers von der Sitzplatte in die freigebende Position umfasst.According to the invention, the valve of a fuel injector for selectively separating a high-pressure region from a low-pressure region of a fuel comprises an opening in a seat plate, an armature configured to close the opening of the seat plate, a spring element that biases the armature toward a position closing the opening, and an electromagnet for lifting the armature from the position closing the opening into a position releasing the opening. The valve according to the invention is characterized in that it further comprises an elastically compressible damping element for limiting an armature stroke when the armature is lifted from the seat plate into the releasing position.

Dieses elastisch stauchbare Dämpfungselement dämpft demnach bei einem Aktivieren des Magneten und einem hieraus resultierenden Anziehen des Ankers weg von der Öffnung die Bewegung des Ankers ab, sodass das Prellen zwischen Magnet und Anker verhindert oder abgeschwächt wird.This elastically compressible damping element dampens when the magnet is activated and the armature is attracted as a result away from the opening, the movement of the armature is reduced, so that the bouncing between the magnet and the armature is prevented or reduced.

Vorteilhaft hieran ist, wenn das Dämpfungselement ein weich elastisches Dämpfungselement ist. Wie später anhand der Figurenbeschreibung gezeigt wird, ist eine weichelastische Ausführung des Dämpfungselements in Bezug auf die oszillierende Schwingungsbewegung des Ankers, die sich bei einem Auftreffen auf das Dämpfungselement bei fortwährender magnetischer Anzugskraft weg von der Öffnung ergibt, besonders gut geeignet die oszillierende Schwingung zu unterdrücken.It is advantageous if the damping element is a soft, elastic damping element. As will be shown later in the description of the figures, a soft, elastic design of the damping element is particularly well suited to suppressing the oscillating vibration of the armature, which occurs when the damping element impacts with a continuous magnetic attraction force away from the opening.

Nach einer optionalen Modifikation der vorliegenden Erfindung ist die Steifigkeit des Dämpfungselements kleiner als die Steifigkeit des Ankers.According to an optional modification of the present invention, the stiffness of the damping element is smaller than the stiffness of the anchor.

Weiterhin kann nach der Erfindung vorgesehen sein, dass das Dämpfungselement ein Dämpfungspin mit einer im Wesentlichen zylindrischen Form ist, der vorzugsweise zwischen seinen beiden Stirnflächen einer Querschnittsverminderung besitzt. Eine der beiden Stirnflächen ist dazu ausgelegt, als Anschlagfläche für den Anker zu dienen. Mit der anderen der beiden Stirnflächen kann vorgesehen sein, dass der Pin in einer Ausnehmung des Magneten angeordnet ist. Die Querschnittsverminderung kann dabei eine um den Außenumfang des Pins umlaufende Nut darstellen, die vorzugsweise vollständig um den Außenumfang umläuft. Für eine verbesserte Dauerhaltbarkeit kann vorgesehen sein, dass die umlaufende Nut im Querschnitt gesehen eine Bogenform aufweist, die in den Nutübergängen verrundet ausgeführt ist.Furthermore, according to the invention, it can be provided that the damping element is a damping pin with a substantially cylindrical shape, which preferably has a cross-sectional reduction between its two end faces. One of the two end faces is designed to serve as a stop surface for the armature. With the other of the two end faces, it can be provided that the pin is arranged in a recess in the magnet. The cross-sectional reduction can be a groove running around the outer circumference of the pin, which preferably runs completely around the outer circumference. For improved durability, it can be provided that the circumferential groove has an arc shape when viewed in cross-section, which is rounded at the groove transitions.

Nach der Erfindung weist das Dämpfungselement an seiner Kontaktfläche zum Anker einen kugelförmigen Abschnitt auf, um eine Kontaktfläche mit dem Anker zu minimieren.According to the invention, the damping element has a spherical section on its contact surface with the armature in order to minimize a contact surface with the armature.

Dadurch entsteht zum einen eine geringe Kontaktfläche mit dem Anker, was in Bezug auf eine möglichst geringere Remanenzkraft des Magneten wünschenswert ist.On the one hand, this creates a small contact area with the armature, which is desirable in terms of keeping the remanence force of the magnet as low as possible.

Vorteilhaft daran ist es, dass der magnetische Fluss über die Kontaktfläche möglichst gering ist. Zum anderen wird durch die kugelförmige Kontaktfläche vorteilhafterweise erreicht, dass bei toleranzbedingter Schiefstellung des Dämpfungselements eine immer gleiche Kontaktfläche zwischen Dämpfungselement und Anker wirkt.The advantage of this is that the magnetic flux across the contact surface is as low as possible. Furthermore, the spherical contact surface ensures that the contact area between the damping element and the armature is always the same, even if the damping element is misaligned due to tolerances.

Weiter kann vorgesehen sein, dass die Pole des Elektromagneten und die den Anker berührende Stirnseite des Dämpfungselements in einem entspannten Zustand des Dämpfungselements in einer gemeinsamen Ebene liegen. In anderen Worten sind also die dem Anker zugewandten Endabschnitte der Pole sowie die den Anker berührende Stirnseite des Dämpfungselements in einer gemeinsamen Ebene angeordnet, wenn sich der Anker in seinem entspannten Zustand befindet und er nicht durch den Magneten angezogen wird.Furthermore, it can be provided that the poles of the electromagnet and the end face of the damping element contacting the armature lie in a common plane when the damping element is in a relaxed state. In other words, the end sections of the poles facing the armature and the end face of the damping element contacting the armature are arranged in a common plane when the armature is in its relaxed state and is not attracted by the magnet.

Gemäß einer Fortbildung der Erfindung ist das Dämpfungselement separat zu einem Gehäuse eines Kraftstoffinjektors ausgeführt. So kann vorgesehen sein, dass das Dämpfungselement durch eine Presspassung montiert und in Position gehalten wird. Die Presspassung kann beispielsweise dadurch umgesetzt werden, indem in dem Magneten eine Ausnehmung vorgesehen ist, in die das Dämpfungselement aufgenommen wird.According to a further development of the invention, the damping element is designed separately from a housing of a fuel injector. Thus, it can be provided that the damping element is mounted and held in position by a press fit. The press fit can be implemented, for example, by providing a recess in the magnet into which the damping element is received.

Weiter kann nach der Erfindung vorgesehen sein, dass die Vorspannkraft des Federelements einstellbar ist, vorzugsweise über Einstellscheiben zum Verändern der Position des Federelements gegenüber dem Dämpfungselement und/oder dem Anker. So kann die Federvorspannkraft exakt eingestellt werden und dies auch bei Vorhandensein einer ungewünschten Abweichung der Federkraft von dem erwartetem Federkraftwert.Furthermore, the invention can provide for the preload force of the spring element to be adjustable, preferably via adjusting discs for changing the position of the spring element relative to the damping element and/or the armature. This allows the spring preload force to be precisely adjusted, even in the presence of an undesired deviation of the spring force from the expected spring force value.

Nach einer Fortbildung der Erfindung ist die dem Anker abgewandte Stirnseite des Dämpfungselements als Flachsitz ausgeführt. Dabei kann vorgesehen sein, dass der Flachsitz in dem Magneten angeordnet ist.According to a further development of the invention, the end face of the damping element facing away from the armature is designed as a flat seat. It can be provided that the flat seat is arranged in the magnet.

Nach einer optionalen Modifikation der vorliegenden Erfindung weist der Anker eine Erhebung in seiner dem Dämpfungselement zugewandten Fläche auf, mit der der Anker auf das Dämpfungselement trifft. So kann unter Umständen deswegen im angezogenen Zustand, also wenn der Magnet aktiv ist und der Anker sich in der freigebenden Position befindet, ein Abstand zwischen den Polkernen des Magneten und einer nicht mit einer Erhebung versehenen Stirnseite des Ankers vorgesehen sein. Dies verhindert den Kontakt zwischen Anker und Magnet.According to an optional modification of the present invention, the armature has a raised portion on its surface facing the damping element, with which the armature contacts the damping element. Therefore, in the attracted state, i.e., when the magnet is active and the armature is in the release position, a gap can be provided between the pole cores of the magnet and a non-raised end face of the armature. This prevents contact between the armature and the magnet.

Ferner kann der Anker mehrteilig ausgeführt sein, sodass dieser einen Ankerteil und einen Sitzteil umfasst oder aus diesen Teilen besteht.Furthermore, the anchor can be designed in several parts, so that it comprises an anchor part and a seat part or consists of these parts.

Nach einer weiteren bevorzugten Ausführung der Erfindung ist das Federelement eine Spiralfeder, die sich vorzugsweise um das Dämpfungselement herum spiralförmig erstreckt, bzw. um das Dämpfungselement herum spiralförmig windet. Das Dämpfungselement ist also in dem durch die Spiralform des Federelements abgegrenzten Raum teilweise oder vollständig aufgenommen.According to a further preferred embodiment of the invention, the spring element is a spiral spring, which preferably extends spirally around the damping element or winds spirally around the damping element. The damping element is thus partially or completely accommodated in the space defined by the spiral shape of the spring element.

Weiter ist nach der Erfindung vorgesehen, dass der Anker beim Übergang aus der die Öffnung verschließenden Position in die die Öffnung freigebenden Position nur mit dem Dämpfungselement in Berührung kommt. Selbstverständlich berührt der Anker in einem noch dichten Zustand mit einer Dichtflächen die Sitzplatte und auch das Federelement, das eine in Richtung Öffnung ausübende Federkraft ausübt. Jedoch kommt es zu keinem direkten Kontakt zwischen dem Magneten oder einer durch den Magneten gebildeten Anschlagsfläche.Furthermore, the invention provides that the armature only comes into contact with the damping element during the transition from the position closing the opening to the position releasing it. Naturally, while still sealed, the armature contacts the seat plate with a sealing surface and also the spring element, which exerts a spring force toward the opening. However, there is no direct contact between the magnet or a stop surface formed by the magnet.

Ferner kann vorgesehen sein, dass der Aufbau des Ventils rotationssymmetrisch oder drehsymmetrisch zu einer Rotationsachse ist, die vorzugsweise identisch zu einer Rotationsachse des Dämpfungselements ist.Furthermore, it can be provided that the structure of the valve is rotationally symmetrical or rotationally symmetrical to a rotation axis, which is preferably identical to a rotation axis of the damping element.

Die Erfindung betrifft zudem einen Kraftstoffinjektor mit einem Ventil nach einer vorstehend aufgeführten Varianten, insbesondere einen Dieselkraftstoffinjektor.The invention also relates to a fuel injector with a valve according to one of the variants listed above, in particular a diesel fuel injector.

Mithilfe der vorstehend beschriebenen Erfindung ist es möglich, das Ankerprellen beim Anschlag des Ankers am Magneten zu verringern und dadurch eine stabilere Einspritzmengenregelung zu erreichen. Ferner erlaubt das geringere Ankerprellen das Einstellen eines kleineren Ankerhubes, sodass der Anker beim Auftreffen auf das Dämpfungselements weniger Impuls besitzt, wodurch die Problematik des Ankerprellens erneut abgemildert werden kann. Diese positiven Auswirkungen führen im Ergebnis dazu, dass eine geringere Streuung der Einspritzmenge zwischen den verschiedenen Injektoren als auch zwischen verschiedenen Einspritzvorgängen eines Injektors erreicht werden kann. Zu guter Letzt ist es mithilfe der vorliegenden Erfindung möglich, die Abschaltzeiten des Magnetventils aufgrund der geringeren Remanenzkraft zwischen Anker und dem Kontakt am Dämpfungselements zu beschleunigen. Dies ist darin begründet, da aufgrund einer verringerten Kontaktfläche zwischen Dämpfungselement und Anker ein geringerer magnetischer Fluss durch das Dämpfungselement verläuft, als dies der Fall bei einer größeren Kontaktfläche, wie sie sich typischerweise im Stand der Technik wiederfindet, wäre.With the help of the invention described above, it is possible to reduce armature bounce when the armature strikes the magnet and thus achieve more stable injection quantity control. Furthermore, the reduced armature bounce allows the setting of a smaller armature stroke, so that the armature has less momentum when it hits the damping element, which can again mitigate the problem of armature bounce. These positive effects ultimately lead to a smaller dispersion of the injection quantity between the various injectors as well as between different injection processes of an injector. Last but not least, the present invention makes it possible to accelerate the switch-off times of the solenoid valve due to the lower remanence force between the armature and the contact on the damping element. This is because, due to the reduced contact area between the damping element and the armature, a smaller magnetic flux flows through the damping element than would be the case with a larger contact area, as is typically found in the prior art.

Weitere Merkmale, Einzelheiten und Vorteile der Erfindung werden anhand der nachfolgenden Figurenbeschreibung ersichtlich. Dabei zeigen:

Fig. 1:
eine hälftige Schnittansicht durch das erfindungsgemäße Ventil,
Fig. 2:
ein Kraftdiagramm beim Übergang des Ankers zwischen seinen beiden Positionen, und
Fig. 3:
eine Darstellung des Ankerhubes in Abhängigkeit verschiedener Elastizitäten des Dämpfungselements.
Further features, details, and advantages of the invention will become apparent from the following description of the figures. These show:
Fig. 1:
a half sectional view through the valve according to the invention,
Fig. 2:
a force diagram during the transition of the armature between its two positions, and
Fig. 3:
a representation of the armature stroke depending on different elasticities of the damping element.

Figur 1 zeigt dabei eine hälftige Schnittansicht des erfindungsgemäßen Ventils 1. Die Sitzplatte 3, die den Hochdruckbereich (an der Unterseite) von einem Niederdruckbereich (an der Oberseite) trennt, weist eine Öffnung 2 auf, die einen Hochdruckbereich und einen Niederdruckberiech von Kraftstoff miteinander verbinden kann. Diese Öffnung 2 ist dabei von einem Anker 4 verschlossen, der mit seiner Dichtfläche 15 die Öffnung 2 in seinem geschlossenen Zustand abdichtet. Der Anker 4 kann aus dieser Position abgehoben werden, wenn der Magnet 6 aktiviert wird und so den Anker 4 von der Öffnung 2 abzieht. In einem deaktivierten Zustand des Magneten 6 sorgt eine Spiralfeder 5 dafür, dass der Anker 4 mit seiner Dichtfläche 15 gegen die Öffnung 2 gedrückt wird. Der Magnet 6 weist eine Spule 61 sowie eine Spulenummantelung 62 auf, sodass durch ein Hindurchströmen von Strom durch die Spule 61 eine Magnetkraft erzeugbar ist. In dem von der Spiralfeder 5 abgegrenzten Raum ist ein Dämpfungselement 7 angeordnet, das in der gezeigten Darstellung einem Dämpfungspin entspricht. Dieser Dämpfungspin 7 besitzt eine erste Stirnseite 8, die dem Anker 4 zugewandt ist. Die Stirnseite 8 ist vorliegend abgerundet bzw. entspricht einem Abschnitt einer Kugel, sodass bei einem Auftreffen des Ankers 4 auf dem Dämpfungselement 7 nur ein möglichst kleiner Kontaktbereich zwischen Anker 4 und Dämpfungselement 7 entsteht. Weiter erkennt man, dass das Dämpfungselement 7 eine Ausnehmung 14 in seinem Umfang aufweist, die für eine geringere Steifigkeit und damit eine gewisse Elastizität des Dämpfungselements 7 sorgt. Diese Ausnehmung 14 kann dabei verrundet vorgesehen sein, wie dies am Bezugszeichen 12 ersichtlich ist. Das Dämpfungselement 7 kann durch Presspassung in dem Magnet 6 gehalten werden. Weiter kann zum Einstellen der Vorspannkraft des Federelements 5 eine Einstellscheibe 11 vorgesehen sein, mit der die Feder in ihrer Position in Axialrichtung verrückt werden kann. Figure 1 shows a half sectional view of the valve 1 according to the invention. The seat plate 3, which separates the high-pressure area (on the underside) from a low-pressure area (on the top), has an opening 2, which connects a high-pressure area and a low-pressure area of fuel with each other can connect. This opening 2 is closed by an armature 4, which seals the opening 2 with its sealing surface 15 in its closed state. The armature 4 can be lifted from this position when the magnet 6 is activated and thus pulls the armature 4 away from the opening 2. When the magnet 6 is deactivated, a spiral spring 5 ensures that the armature 4 is pressed with its sealing surface 15 against the opening 2. The magnet 6 has a coil 61 and a coil casing 62, so that a magnetic force can be generated by current flowing through the coil 61. A damping element 7 is arranged in the space delimited by the spiral spring 5, which corresponds to a damping pin in the illustration shown. This damping pin 7 has a first end face 8 that faces the armature 4. The end face 8 is rounded in this case or corresponds to a section of a sphere, so that when the armature 4 impacts the damping element 7, only the smallest possible contact area is created between the armature 4 and the damping element 7. It can also be seen that the damping element 7 has a recess 14 in its circumference, which ensures lower rigidity and thus a certain elasticity of the damping element 7. This recess 14 can be rounded, as can be seen from the reference numeral 12. The damping element 7 can be held in the magnet 6 by a press fit. Furthermore, an adjusting disk 11 can be provided to adjust the preload force of the spring element 5, with which the spring can be moved in its position in the axial direction.

Der Anker 4 kann dabei eine Erhebung 13 aufweisen, mit der der Anker 4 auf die Kontaktfläche 8 des Dämpfungselements 7 trifft.The armature 4 can have a raised portion 13 with which the armature 4 strikes the contact surface 8 of the damping element 7.

Damit der Anker während eines Übergangs von seiner dichtenden Position in die die Öffnung 2 freigebende Position geführt wird, ist eine Ankerführung 16 vorgesehen. Ein Distanzring 17 schirmt dabei den Anker 4 von dem Gehäuse 10 eines Kraftstoffinjektors ab. Mit dem Bezugszeichen 9 sind die Magnetpole des Magneten 6 bezeichnet.An armature guide 16 is provided to guide the armature during a transition from its sealing position to the position that releases the opening 2. A spacer ring 17 shields the armature 4 from the housing 10 of a fuel injector. Reference numeral 9 designates the magnetic poles of the magnet 6.

Die Symmetrieachse 13 zeigt, dass das Ventil 1 spiegelsymmetrisch und/oder rotationssymmetrisch aufgebaut ist.The axis of symmetry 13 shows that the valve 1 is constructed with mirror symmetry and/or rotational symmetry.

In einem geschlossenen Zustand wird ein in der Ankerführung 16 geführtes magnetisierbares Teil, hier der Anker 4, mittels des Federelements 5 mit einer über die Einstellscheibe 11 definierbaren Kraft, der Vorspannkraft, beaufschlagt, die den Anker 4 in axialer Richtung vom Magneten 6 weg hin zu einem Dichtteil der Sitzplatte 3 verschließt. Wie gesagt trennt die Sitzplatte 3 einen Hochdruckbereich von einem Niederdruckbereich des Kraftstoffes.In a closed state, a magnetizable part guided in the armature guide 16, here the armature 4, is subjected to a force defined by the adjusting disc 11, the preload force, by means of the spring element 5, which closes the armature 4 in the axial direction away from the magnet 6 toward a sealing part of the seat plate 3. As mentioned, the seat plate 3 separates a high-pressure area from a low-pressure area of the fuel.

In einem offenen Zustand wird die Verbindung zwischen Hochdruckbereich und Niederdruckbereich über die Öffnung 2 in der Sitzplatte 3 durch eine axiale Bewegung des Ankers 4 in Richtung des Magneten 6 freigegeben, sodass Kraftstoff vom in Fig. 1 unten angeordneten Hochdruckbereich in den Niederdruckbereich, der in der Fig. 1 oberhalb der Sitzplatte 3 angeordnet ist, fließen kann. Über eine hydraulisch-mechanische Wirkkette wird mindestens ein Kraftstoffeinlass vom Injektor in den Brennraum freigegeben und Kraftstoff dem Brennraum zugeführt.In an open state, the connection between the high-pressure area and the low-pressure area is released via the opening 2 in the seat plate 3 by an axial movement of the armature 4 in the direction of the magnet 6, so that fuel is discharged from the Fig. 1 high pressure area below into the low pressure area, which is in the Fig. 1 arranged above the seat plate 3. Via a hydraulic-mechanical chain of action, at least one fuel inlet is released from the injector into the combustion chamber and fuel is supplied to the combustion chamber.

Zum Öffnen des Magnetventils 1, also dem Übergang zwischen einem geschlossenem zu einem offenen Zustand, wird mittels einer Spannungsquelle Strom erzeugt, der durch die Windungen der Spule 61 fließt. Die Windungen der Spule 61 sind von einer Spulenummantelung 62 umgeben, welche wiederum radial nach Innen und Außen von einem ferromagnetischen Kern 6 umgeben ist, der zur Verstärkung des durch den Strom in der Spule 61 induzierten Magnetfeldes dient.To open the solenoid valve 1, i.e., the transition between a closed and an open state, a voltage source generates current that flows through the windings of the coil 61. The windings of the coil 61 are surrounded by a coil sheath 62, which in turn is surrounded radially inward and outward by a ferromagnetic core 6, which serves to amplify the magnetic field induced by the current in the coil 61.

Aufgrund des magnetischen Feldes wirkt eine Kraft zwischen dem Magnetpol 9 des Magneten 6 und dem Anker 4. Bei einem genügend starken Stromsignal und genügend langer Ansteuerdauer übersteigt die anziehende Magnetkraft zwischen dem Magnetpol 9 und dem Anker 4 die entgegengesetzte Vorspannkraft der Feder 5. Im Ergebnis wird dann der Anker in Richtung des Magneten 6 in axialer Richtung angezogen, sodass die Öffnung 2 in der Sitzplatte 3 freigegeben wird.Due to the magnetic field, a force acts between the magnetic pole 9 of the magnet 6 and the armature 4. With a sufficiently strong current signal and a sufficiently long activation duration, the attractive magnetic force between the magnetic pole 9 and the armature 4 exceeds the opposing preload force of the spring 5. As a result, the armature is then attracted towards the magnet 6 in the axial direction, so that the opening 2 in the seat plate 3 is released.

Der Anker 4 wird durch die mit abnehmendem Abstand zunehmende anziehende Magnetkraft stets weiter beschleunigt, bis es zum Anschlag des Ankers 4 am Dämpfungselement 7 kommt. Dabei trifft der Anker 4 auf eine Kontaktfläche 8 des Dämpfungselements 7, das vorstehend durch einen Pin ausgebildet ist.The armature 4 is continuously accelerated by the attractive magnetic force, which increases with decreasing distance, until the armature 4 comes into contact with the damping element 7. The armature 4 then strikes a contact surface 8 of the damping element 7, which is formed by a pin projecting therefrom.

Der Dämpfungspin 7 wirkt wie eine sehr harte Feder, besitzt aber im Vergleich zum Anker 4 eine vergleichsweise geringe Steifigkeit. Dabei kann vorgesehen sein, dass die Steifigkeit des Dämpfungspins bzw. des Dämpfungselements kleiner als 70%, vorzugsweise kleiner als 50% und bevorzugterweise kleiner als 30% der Steifigkeit des Ankers 4 ist. Der Dämpfungspin 7 bremst den Anker 4 vollständig ab, wobei der Dämpfungspin 7 elastisch gestaucht wird. Dabei kommt es bis auf den Kontakt zwischen Anker 4 und Pin 7 zu keinem weiteren mechanischem Kontakt zwischen Anker 4 und Magnet 6.The damping pin 7 acts like a very hard spring, but has comparatively low stiffness compared to the armature 4. The stiffness of the damping pin or damping element can be less than 70%, preferably less than 50%, and most preferably less than 30% of the stiffness of the armature 4. The damping pin 7 completely brakes the armature 4, whereby the damping pin 7 is elastically compressed. Apart from the contact between the armature 4 and the pin 7, there is no further mechanical contact between the armature 4 and the magnet 6.

Nach einer maximalen Stauchung des Pins 7 bewirkt die rückstellende Kraft der Feder 5 sowie des Pins 7 ein Ausdehnen des Pins 7 in Richtung Öffnung 2 der Sitzplatte 3. In einem oszillierenden Vorgang stellt sich eine Verformung des Pins 7 auf ein Maß ein, bei dem sich die Summe der auf den Anker 4 wirkende Kräfte (die anziehende Magnetkraft und die abstoßende Rückstellkraft durch Feder 5 und Pinverformung) im Kräftegleichgewicht gegenseitig aufheben.After a maximum compression of the pin 7, the restoring force of the spring 5 and the pin 7 causes the pin 7 to expand in the direction of the opening 2 of the seat plate 3. In an oscillating process, the pin 7 is deformed to a degree at which the sum of the forces acting on the armature 4 (the attractive magnetic force and the repulsive restoring force by spring 5 and pin deformation) cancel each other out in the force equilibrium.

Mit einem Abschalten der Spannungsquelle werden der elektrische Strom sowie das Magnetfeld wieder reduziert. Die den Anker 4 anziehende Magnetkraft lässt dadurch sehr schnell nach und kann die Rückstellkraft der Feder nicht mehr überwinden. Daraufhin wird der Anker von der Feder 5 zurück in den geschlossenen Zustand gedrückt, sodass die Öffnung 2 in der Sitzplatte 3 durch den Anker 4 verschlossen wird und der Hochdruckraum (unterhalb der Sitzplatte 3) vom Niederdruckraum (oberhalb der Sitzplatte 3) wieder getrennt ist, sodass über die hydraulisch-mechanische Wirkkette ein oder mehrere Kraftstoffeinlässe vom Injektor in den Brennraum wieder verschlossen werden und kein Kraftstoff mehr in den Brennraum eingeführt wird.When the voltage source is switched off, the electric current and the magnetic field are reduced again. The magnetic force attracting the armature 4 therefore decreases very quickly and can no longer overcome the restoring force of the spring. The armature is then pushed back into the closed position by the spring 5, so that the opening 2 in the seat plate 3 is closed by the armature 4 and the high-pressure chamber (below the seat plate 3) is again separated from the low-pressure chamber (above the seat plate 3). This means that one or more fuel inlets from the injector into the combustion chamber are closed again via the hydraulic-mechanical chain of action, and no more fuel is fed into the combustion chamber.

Wie Fig. 2 zeigt, führt die Realisierung des Anschlags des Ankers 4 an dem Dämpfungselement 7, der relativ weichelastisch ausgebildet ist, zu einem sehr vorteilhaften Verhalten des Ankers 4. Trifft der Anker 4 auf das Dämpfungselement 7 schwingt dieser nur mit einer sehr geringen Schwingungsamplitude für einen überschaubaren Zeitraum.How Fig. 2 shows, the realization of the stop of the armature 4 on the damping element 7, which is designed to be relatively soft and elastic, leads to a very advantageous behavior of the armature 4. If the armature 4 hits the damping element 7, it only oscillates with a very low oscillation amplitude for a manageable period of time.

Fig. 3 zeigt dieses Schwingungsverhalten des Ankers anhand des Ankerhubs h in Gegenüberstellung von verschiedenen Elastizitäten des Dämpfungselements 7. Mit durchgehender Linie ist dabei eine harte Elastizität gezeigt, wohingegen in gestrichelter Ausführung eine weiche Elastizität des Dämpfungselements 7 dargestellt ist. Man kann erkennen, dass die Schwingungsamplitude der weichelastischen Ausführung Δhwe kleiner ist als bei der hartelastischen Ausführung Δhhe . Dies ist darin begründet, da die Verformung des Dämpfungselements 7 beim Aufprall des Ankers dazu führt, dass der Abstand zwischen Magnet 6 und Anker 4 zunächst weiter auf einen Abstand reduziert wird, der kleiner ist als derjenige Abstand, der sich im statischen Kräftegleichgewicht einstellen würde. Dies führt dazu, dass die den Anker 4 anziehende Magnetkraft FMag zwischen Anker 4 und Magnet 6 überproportional im Vergleich zu einer linear zunehmenden Rückstellkraft FRück , hervorgerufen durch Feder und Dämpfungselement 7, zunimmt. Der überproportionale Kraftzuwachs dämpft die rückfedernde Wirkung des Dämpfungselements 7 stark ab, sodass das Prellen des Ankers beim Anschlag des Magneten reduziert wird. Fig. 3 shows this vibration behavior of the armature based on the armature stroke h in comparison with different elasticities of the damping element 7. A solid line shows a hard elasticity, whereas a dashed line shows a soft elasticity of the damping element 7. It can be seen that the vibration amplitude of the soft elastic version Δh we is smaller than that of the hard elastic version Δh he . This is because the deformation of the damping element 7 upon impact of the armature leads to the distance between magnet 6 and armature 4 initially being further reduced to a distance that is smaller than the distance that would occur in a static force equilibrium. This leads to the magnetic force F Mag attracting the armature 4 between armature 4 and magnet 6 increasing disproportionately compared to a linearly increasing restoring force F Rück , caused by the spring and damping element 7. The disproportionate increase in force strongly dampens the spring-back effect of the damping element 7, so that the bouncing of the armature when the magnet strikes is reduced.

Grafisch ist dies dargestellt in Fig. 2, bei der die durchgehende Linie den Betrag der Magnetkraft FMag und die gestrichelte Linie den Betrag der Rückstellkraft FRück darstellt. Wird der Anker 4 nun beispielsweise bei einer Ausführung mit einem hartelastischen Dämpfungselement aufgrund der Magnetkraft nur bis zum Abstand xA1 angezogen, so ist die dabei resultierende Magnetkraft FA1 wesentlich geringer als diejenige Magnetkraft FA2 , die beim Anziehen des Ankers 4 bis in die Position xA2 erreicht wird, die sich bei einer weichelastischen Dämpfungselementausführung ergibt.This is shown graphically in Fig. 2 , where the solid line represents the magnitude of the magnetic force F Mag and the dashed line represents the magnitude of the restoring force F Rück . If, for example, in a design with a hard-elastic damping element, the armature 4 is only attracted up to the distance x A1 due to the magnetic force, the resulting magnetic force F A1 is significantly lower than the magnetic force F A2 that is achieved when the armature 4 is attracted up to the position x A2 , which results in a soft-elastic damping element design.

Da jedoch bei der Ausführung mit einem weichelastischen Dämpfungselement insgesamt eine stärkere Kraft auf den Anker 4 wirkt, als dies bei der hartelastischen Ausführung der Fall wäre, wird das schwingende Verhalten des Ankers 4, das solange andauert, bis ein statisches Kräftegleichgewicht eingenommen worden ist, deutlich reduziert. Dadurch lässt sich eine stabilere Regelung der Einspritzmenge erreichen, was insgesamt zu einer Verbesserung eines Kraftstoffinjektors führt.However, since the design with a soft-elastic damping element exerts a stronger overall force on armature 4 than would be the case with the hard-elastic design, the oscillating behavior of armature 4, which continues until a static force equilibrium is reached, is significantly reduced. This allows for more stable control of the injection quantity, which leads to an overall improvement in the fuel injector.

Claims (13)

  1. Valve (1) of a fuel injector for a selective separation of a high pressure region from a low pressure region of a fuel comprising:
    an opening (2) in a seat plate (3);
    an armature (4) that is configured to close the opening (2) of the seat plate (3);
    a spring element (5) that preloads the armature (4) in the direction of a position closing the opening (2); and
    an electromagnet (6) for raising the armature (4) from the position closing the opening (2) into a position releasing the opening (2),
    an elastically compressible damping element (7) to bound an armature stroke on the raising of the armature (4) from the seat plate (3) into the releasing position,
    characterized in that
    the damping element (7) has a spherical section (8) at its contact surface to the armature (4) to minimize a contact surface with the armature (4), and
    the armature (4), except for the contact to the damping element (7), does not have any further mechanical contact with the electromagnet (6) or an abutment surface formed by the electromagnet on the transition from the position closing the opening (2) into the position releasing the opening (2), in which the armature (4) is completely braked by the damping element (7).
  2. Valve (1) in accordance with claim 1, wherein the damping element (7) is a soft-elastic damping element (7).
  3. Valve (1) in accordance with one of the preceding claims, wherein the stiffness of the damping element (7) is smaller than the stiffness of the armature (4).
  4. Valve (1) in accordance with one of the preceding claims, wherein the damping element (7) is a damping pin having a substantially cylindrical shape that preferably has a cross-sectional reduction (12) between its two end surfaces.
  5. Valve (1) in accordance with one of the preceding claims, wherein the poles (9) of the electromagnet (6) and an end side of the damping element (7) contacting the armature (4) are disposed in a common plane in a relaxed state of the damping element (7).
  6. Valve (1) in accordance with one of the preceding claims, wherein the damping element (7) is separate from a housing (10) of a fuel injector.
  7. Valve (1) in accordance with one of the preceding claims, wherein the preload force of the spring element (5) can be set, preferably via setting plates (11) to change the position of the spring element (5) with respect to the damping element (7) and/or the armature (4).
  8. Valve (1) in accordance with one of the preceding claims, wherein the end side of the damping element (7) remote from the armature (4) is designed as a flat seat.
  9. Valve (1) in accordance with one of the preceding claims, wherein the armature (4) has an elevated portion (13) in its surface facing the damping element (7) at which the armature (4) impacts the damping element (7).
  10. Valve (1) in accordance with one of the preceding claims, wherein the armature (4) is designed in multiple parts and comprises an armature part and a seat part or consists of these parts.
  11. Valve (1) in accordance with one of the preceding claims, wherein the spring element (5) is a spiral spring that extends in a spiral manner around the damping element (7).
  12. Valve (1) in accordance with one of the preceding claims, wherein the design of the valve (1) is rotationally symmetrical to an axis of rotation (13) that is identical to an axis of rotation of the damping element (7).
  13. Fuel injector having a valve (1) in accordance with one of the preceding claims, in particular a diesel fuel injector.
EP19768811.2A 2018-09-12 2019-09-12 Valve of a fuel injector Active EP3833865B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102018122250.5A DE102018122250A1 (en) 2018-09-12 2018-09-12 Fuel injector valve
PCT/EP2019/074420 WO2020053359A1 (en) 2018-09-12 2019-09-12 Valve of a fuel injector

Publications (2)

Publication Number Publication Date
EP3833865A1 EP3833865A1 (en) 2021-06-16
EP3833865B1 true EP3833865B1 (en) 2025-05-07

Family

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Application Number Title Priority Date Filing Date
EP19768811.2A Active EP3833865B1 (en) 2018-09-12 2019-09-12 Valve of a fuel injector

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US (1) US12146462B2 (en)
EP (1) EP3833865B1 (en)
CN (1) CN112771269A (en)
DE (1) DE102018122250A1 (en)
ES (1) ES3035007T3 (en)
WO (1) WO2020053359A1 (en)

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DE102021133281A1 (en) * 2021-12-15 2023-06-15 Liebherr-Components Deggendorf Gmbh Electromagnetic valve, in particular for switching a fuel injector

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Also Published As

Publication number Publication date
WO2020053359A1 (en) 2020-03-19
EP3833865A1 (en) 2021-06-16
US20210254590A1 (en) 2021-08-19
DE102018122250A1 (en) 2020-03-12
US12146462B2 (en) 2024-11-19
CN112771269A (en) 2021-05-07
ES3035007T3 (en) 2025-08-27

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