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EP2686853B1 - Electromagnetic actuator device - Google Patents

Electromagnetic actuator device Download PDF

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Publication number
EP2686853B1
EP2686853B1 EP12714594.4A EP12714594A EP2686853B1 EP 2686853 B1 EP2686853 B1 EP 2686853B1 EP 12714594 A EP12714594 A EP 12714594A EP 2686853 B1 EP2686853 B1 EP 2686853B1
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EP
European Patent Office
Prior art keywords
yoke
armature
unit
section
flux
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Not-in-force
Application number
EP12714594.4A
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German (de)
French (fr)
Other versions
EP2686853A1 (en
Inventor
Raphael BORY
Jonas BOLL
Daniela HÄRTER
Robert STEYER
Philipp TERHORST
Thomas Schiepp
Markus Laufenberg
Oliver Thode
Viktor Raff
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ETO Magnetic GmbH
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ETO Magnetic GmbH
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Publication date
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Priority to EP17165459.3A priority Critical patent/EP3211645A1/en
Publication of EP2686853A1 publication Critical patent/EP2686853A1/en
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Publication of EP2686853B1 publication Critical patent/EP2686853B1/en
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F7/00Magnets
    • H01F7/06Electromagnets; Actuators including electromagnets
    • H01F7/08Electromagnets; Actuators including electromagnets with armatures
    • H01F7/16Rectilinearly-movable armatures
    • H01F7/1638Armatures not entering the winding
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F7/00Magnets
    • H01F7/06Electromagnets; Actuators including electromagnets
    • H01F7/08Electromagnets; Actuators including electromagnets with armatures
    • H01F7/081Magnetic constructions

Definitions

  • the present invention relates to an electromagnetic actuator device according to the preamble of the main claim.
  • Such a device is for example from the JP 2000 170951 A is known and relates to an electromagnetic actuator device for implementing a 3-way valve, in which, in departure from the usual and beyond known as vortex actuator technologies, the coil winding does not surround the armature (or the associated working air gap), but the coil winding, in the Type of "outsourced coil” is offset laterally relative to an armature movement longitudinal axis (or an associated air gap) and a magnetic flux transfer to the armature unit or to the air gap by means of suitable flux-conducting portions of the yoke.
  • JP 2000 170951 A in a very special technical context, which in particular makes a transfer to other, generic actuating tasks (or else to other valve drives) only possible to a very limited extent.
  • the known from this prior art device requires a not inconsiderable space, in addition, a heat dissipation from the known device is not without problems.
  • the DE 20 2008 015980 U1 the applicant and the EP1 288 487 A2 and the DE 101 46 899 A1 each disclosing an electromagnetic actuator device according to the preamble of claim 1. Further electromagnetic actuator devices are in US4633209 and DE 20 2008 015 303 U1 disclosed.
  • Object of the present invention is therefore to provide an electromagnetic actuator according to the preamble of the main claim, wherein a Bestrombare coil unit encloses a first yoke portion of a stationary yoke unit and relative to the yoke unit movably guided, cooperating with a control partner and drivable for performing an actuating armature anchor second yoke portions of the yoke unit to form working air gaps cooperate, with regard to to improve a more compact, in particular also more flexible, mechanical realization, in particular to be able to separate the coil unit from the working air gap, and to create the possibility of realizing improved heat dissipation or localized heat (and thus less concentrated on one location) let develop.
  • the object is achieved by the electromagnetic actuator device having the features of the main claim; advantageous developments of the invention are described in the subclaims.
  • the working air gaps are formed outside the first yoke section, that is to say they are not enclosed by a coil unit (which is typically cylindrical or rectangular in design), but laterally displaced in the sense discussed above.
  • a magnetic flux resistance of flux guide is at least one of the magnetic flux circuits in response to a flowing therein magnetic flux variable.
  • presetting or predetermined influencing of the movement behavior of the plurality of anchor units is to design the air gaps differently (in each case based on a predetermined, comparable anchor position, for example a stop position of the anchor units).
  • Another way to influence the switching or movement behavior of a respective armature unit of the anchor means is to associate this armature spring means or the like power storage and about further education to store one or more of the armature units against a restoring force of such a spring or lead (where in turn further education by different configurations such as the spring forces then the respective switching or movement behavior of the associated anchor units can be influenced in a predetermined manner).
  • the electromagnetic actuator device according to the invention is indeed preferably for the realization of hydraulic or pneumatic valve solutions, especially in the vehicle sector, but is not limited to these applications.
  • the present invention can be used favorably and suitably configured for virtually any field of application in which structural or spatial flexibility can be used in conjunction with flexibly configurable magnetic flux guides or flow paths within the respective flux guide circuits.
  • the Fig. 1 illustrates in the schematic longitudinal sectional view of an electromagnetic actuator device for driving two anchor units 10, 12 by means of a common, centrally located (centrally) between them on a yoke section 13 coil unit 14. More specifically, as schematically with reference to the graph of Fig. 1 recognizable, the elongated armature units 10 and 12 shown axially movably guided (in a movement and drive direction perpendicular in the plane), wherein the armature units 10 and 12 cooperate with stationary yoke sections 15 and 16 and, for the realization thereof, together by the coil unit 14 extending flow control circuits, which are guided over flow-conducting connection sections 18 to 24. Accordingly arise for the anchor units 10 and 12 effective air gaps 26 and 28 respectively.
  • the Fig. 2 to 4 illustrate various operating conditions in response to energization of the coil unit 14: So shows about the Fig. 3 two flow paths in the flux guide circuits running through the respective armatures 10 and 12, respectively, on the basis of the arrowheads 30 and 32, these magnetic fluxes flowing through the yoke section 13 ("first yoke section") associated with the coil unit 14, as symbolized by the arrowhead 34. Is against it, as in the Fig. 2 As shown by a shortened air gap 28, an effective flow resistance in the right flow circuit (ie relative to the armature unit 12) is reduced relative to the other branch, the magnetic flux concentrates as indicated by the arrowhead 36 in FIG Fig.
  • a first variant illustrates the Fig. 5 in the perspective view: on both sides of an axially movable armature 40 and a stationary yoke portion 42 having central arrangement, a pair of individual coils 44 and 46 is provided such that armature 40 and stator 42 are framed on both sides of the individual coils 44, 46.
  • a magnetic flux (resulting when the coils are energized) of the coils 44 and 46, respectively, is fed into the armature 40 or the stator 42 via common elongated plate-shaped flux conducting elements 48 and 50, the elements 48 and 50 additionally being used for a mechanical connection the overall arrangement (with an outlet opening 52 for the anchor unit) provide.
  • two flux guide circuits are formed, wherein a respective one of the flux circuits runs through one of the individual coils 44 and 46 and both flux circuits then flow together through the armature-stator arrangement 40, 42 (insofar the flow path corresponds analogously of the Fig. 3 but with a provision of a central armature-stator arrangement and two external individual coils).
  • This basic configuration of the Fig. 5 is, however, not limited to two individual coils, nor about the symmetrical arrangement shown; Rather, by varying the geometry of the elements 48, 50, a change in distance it can also, as in the Fig. 6 to 8 illustrates, compared to the elongated elements 48, 50 suitably kinked configuration are present, or it can be provided around one (or even more) common armature-stator assembly (s) around more than two individual coils: So describes about the Fig. 6 in plan view, a variation of the elements 48 and 50, such that now two legs 54, 56, angled away from each other by an angle 58 of about 135 °, extend and end, compare Fig.
  • FIG. 7 A comparison arrangement of the presupposed as known, traditional type in the representation of Fig. 7 illustrates the resulting installation space or geometry advantage: namely, in order to produce a magnetic flux behavior comparable to the pair of individual coils 44, 46, a single coil of a winding cross-section 60, as in FIG Fig. 7 indicated to be present, but possibly in a limited installation space (adapted to the configuration of Fig. 6, 8 ) not possible.
  • a further advantage of the example with a plurality of individual coils provided adjacent to an armature-stator arrangement with an adding or overlapping flow profile, such as in FIG Fig. 5 respectively. 6 and 8 shown, is that possible lateral forces are reduced (to the anchor) compared to a solution with only one adjacent the anchor unit outsourced coil (as far as a mutual compensation takes place, see for example the flowchart of Fig. 3 in analogous application to an arrangement with two external individual coils).
  • a reduction of the lateral forces on the anchor has a favorable effect on wear and therefore an effective service life.
  • the present invention allows numerous practical advantages: For example, arranging the anchor means in a use as a valve offers much more flexible connection possibilities in the configuration according to the invention adjacent to the coil unit for example, compared to the known state of the art, in which typically the elongated armature unit is surrounded by the coil unit (typically cylindrical-radial). Accordingly, the working air gap can be made more flexible (and suitable for a particular application).
  • advantageous is provided adapted to respective installation and room conditions, not to provide the cylindrical winding, but to provide approximately rectangular or other coil cross-sections. This is especially true in cooperation with flux-conducting elements, which are realized by means of (typically produced by punching) sheets and further advantageously present in suitable stacking configurations.

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  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Electromagnets (AREA)

Description

Die vorliegende Erfindung betrifft eine elektromagnetische Aktuatorvorrichtung nach dem Oberbegriff des Hauptanspruchs.The present invention relates to an electromagnetic actuator device according to the preamble of the main claim.

Eine derartige Vorrichtung ist beispielsweise aus der JP 2000 170951 A bekannt und betrifft eine elektromagnetische Aktuatorvorrichtung zur Realisierung eines 3-Wege-Ventils, bei welcher, in Abkehr von üblichen und darüber hinaus als bekannt vorauszusetzenden Aktuatortechnologien, die Spulenwicklung nicht den Anker (bzw. den zugehörigen Arbeitsluftspalt) umschließt, vielmehr die Spulenwicklung, in der Art einer "ausgelagerten Spule", gegenüber einer Anker-Bewegungslängsachse (bzw. einem zugehörigen Luftspalt) lateral versetzt ist und eine magnetische Flussübertragung zur Ankereinheit bzw. zum Luftspalt mittels geeigneter flussleitender Abschnitte des Jochs erfolgt.Such a device is for example from the JP 2000 170951 A is known and relates to an electromagnetic actuator device for implementing a 3-way valve, in which, in departure from the usual and beyond known as vorzusetzenden actuator technologies, the coil winding does not surround the armature (or the associated working air gap), but the coil winding, in the Type of "outsourced coil" is offset laterally relative to an armature movement longitudinal axis (or an associated air gap) and a magnetic flux transfer to the armature unit or to the air gap by means of suitable flux-conducting portions of the yoke.

Allerdings erfolgt die Offenbarung gemäß JP 2000 170951 A in einem sehr speziellen technischen Kontext, der insbesondere eine Übertragung auf andere, generische Stellaufgaben (oder aber auf andere Ventilantriebe) nur sehr begrenzt möglich macht. Zudem benötigt auch die aus diesem Stand der Technik bekannte Vorrichtung einen nicht unbeträchtlichen Bauraum, wobei zusätzlich eine Wärmeabfuhr von der bekannten Vorrichtung nicht unproblematisch ist. Zum weiteren Stand der Technik werden die DE 20 2008 015980 U1 der Anmelderin sowie die EP1 288 487 A2 und die DE 101 46 899 A1 genannt, die jeweils eine elektromagnetische Aktuatorvorrichtung nach dem Oberbegriff von Anspruch 1 offenbaren. Weitere elektromagnetische Aktuatorvorrichtungen sind in US4633209 und DE 20 2008 015 303 U1 offenbart. Aufgabe der vorliegenden Erfindung ist es daher, eine elektromagnetische Aktuatorvorrichtung nach dem Oberbegriff des Hauptanspruchs zu schaffen, bei welcher eine bestrombare Spuleneinheit einen ersten Jochabschnitt einer stationären Jocheinheit umschließt und relativ zur Jocheinheit bewegbar geführte, mit einem Stellpartner zusammenwirkende und zum Ausführen einer Stellbewegung antreibbare Ankermittel mit zweiten Jochabschnitten der Jocheinheit unter Ausbildung von Arbeitsluftspalten zusammenwirken, im Hinblick auf eine kompaktere, insbesondere auch flexiblere mechanische Realisierung zu verbessern, dabei insbesondere die Möglichkeit zu schaffen, die Spuleneinheit vom Arbeitsluftspalt zu separieren, und die Möglichkeit zu schaffen, eine verbesserte Wärmeabfuhr zu realisieren bzw. Wärme lokal verteilt (und damit weniger auf einen Ort konzentriert) entstehen zu lassen.However, the disclosure is according to JP 2000 170951 A in a very special technical context, which in particular makes a transfer to other, generic actuating tasks (or else to other valve drives) only possible to a very limited extent. In addition, the known from this prior art device requires a not inconsiderable space, in addition, a heat dissipation from the known device is not without problems. For further prior art, the DE 20 2008 015980 U1 the applicant and the EP1 288 487 A2 and the DE 101 46 899 A1 , each disclosing an electromagnetic actuator device according to the preamble of claim 1. Further electromagnetic actuator devices are in US4633209 and DE 20 2008 015 303 U1 disclosed. Object of the present invention is therefore to provide an electromagnetic actuator according to the preamble of the main claim, wherein a Bestrombare coil unit encloses a first yoke portion of a stationary yoke unit and relative to the yoke unit movably guided, cooperating with a control partner and drivable for performing an actuating armature anchor second yoke portions of the yoke unit to form working air gaps cooperate, with regard to to improve a more compact, in particular also more flexible, mechanical realization, in particular to be able to separate the coil unit from the working air gap, and to create the possibility of realizing improved heat dissipation or localized heat (and thus less concentrated on one location) let develop.

Die Aufgabe wird durch die elektromagnetische Aktuatorvorrichtung mit den Merkmalen des Hauptanspruchs gelöst; vorteilhafte Weiterbildungen der Erfindung sind in den Unteransprüchen beschrieben. Erfindungsgemäss sind die Arbeitsluftspalte außerhalb des ersten Jochabschnitts gebildet, mithin also nicht von einer (weiterbildungsgemäß typischerweise zylindrisch oder rechteckförmig ausgebildeten) Spuleneinheit umschlossen ist, sondern im vorstehend diskutierten Sinne lateral ausgelagert ist.The object is achieved by the electromagnetic actuator device having the features of the main claim; advantageous developments of the invention are described in the subclaims. According to the invention, the working air gaps are formed outside the first yoke section, that is to say they are not enclosed by a coil unit (which is typically cylindrical or rectangular in design), but laterally displaced in the sense discussed above.

In besonders bevorzugter Ausgestaltung der Erfindung mit einer Mehrzahl von magnetische Flussleitkreisen in der Jocheinheit, wobei jeder der Flussleitkreise durch den (die gemeinsame Spule tragenden) ersten Jochabschnitt sowie über einen jeweiligen einer der Mehrzahl der Ankereinheiten zugeordneten Luftspalte verläuft, ist ein magnetischer Flusswiderstand von Flussleitmitteln mindestens eines der magnetischen Flussleitkreise in Abhängigkeit von einem darin fließenden magnetischen Fluss veränderlich. Dies geschieht insbesondere dadurch, dass durch geeignete Ausgestaltung eines wirksamen Flussleitquerschnittes dieser Flussleitmittel ab einer vorbestimmten magnetischen Flussdichte eine Sättigung auftritt, mithin ab dieser Schwelle der magnetische Flusswiderstand erhöht ist. Konsequenz dieses Effektes ist, dass dann ein Magnetfluss vom betreffenden Flussleitkreis in einen anderen der Flussleitkreise verdrängt wird, insoweit dann eine Ankerbewegung ausgelöst oder beeinflusst werden kann.In a particularly preferred embodiment of the invention with a plurality of magnetic flux circuits in the yoke unit, wherein each of the flux circuits extends through the (youtube carrying the first coil yoke portion and via a respective one of the plurality of anchor units associated air gaps, a magnetic flux resistance of flux guide is at least one of the magnetic flux circuits in response to a flowing therein magnetic flux variable. This happens in particular in that saturation occurs as a result of suitable design of an effective flux-conducting cross-section of these flux-conducting means above a predetermined magnetic flux density, and therefore the magnetic flux resistance is increased from this threshold. The consequence of this effect is that a magnetic flux is then displaced from the relevant flux circuit into another of the flux circuits, insofar as an armature movement can then be triggered or influenced.

Weitere Möglichkeiten zur Voreinstellung bzw. vorbestimmten Beeinflussung des Bewegungsverhaltens der Mehrzahl der Ankereinheiten (in den jeweiligen Jochzweigen) besteht darin, die Luftspalte unterschiedlich auszugestalten (jeweils bezogen auf eine vorbestimmte, vergleichbare Ankerposition, etwa eine Anschlagposition der Ankereinheiten). Dabei ist es insbesondere weiterbildungsgemäß bevorzugt, den wirksamen Luftspalt in einem jeweiligen Jochzweig zu variieren bzw., entsprechend einem beabsichtigten Bewegungsverhalten (etwa einer beabsichtigten Reihenfolge einer Aktivierung), unterschiedlich einzurichten.Further possibilities for presetting or predetermined influencing of the movement behavior of the plurality of anchor units (in the respective yoke branches) is to design the air gaps differently (in each case based on a predetermined, comparable anchor position, for example a stop position of the anchor units). In this case, it is preferred in particular according to the invention to vary the effective air gap in a respective yoke branch or, corresponding to an intended movement behavior (such as an intended order of activation) to set up differently.

Eine weitere Möglichkeit, das Schalt- bzw. Bewegungsverhalten einer jeweiligen Ankereinheit der Ankermittel zu beeinflussen, liegt darin, dieser Ankereinheit Federmittel oder dergleichen Kraftspeicher zuzuordnen und etwa weiterbildungsgemäß eine oder mehrere der Ankereinheiten gegen eine Rückstellkraft einer derartigen Feder zu lagern bzw. zu führen (wobei wiederum weiterbildungsgemäß durch unterschiedliche Ausgestaltungen etwa der Federkräfte dann das jeweilige Schalt- bzw. Bewegungsverhalten der zugeordneten Ankereinheiten vorbestimmt beeinflusst werden kann). Im Rahmen weiterer bevorzugter Ausführungsformen der Erfindung ist vorgesehen, die Jocheinheit mittels geeigneter blechförmiger, weiter bevorzugt durch Stanzen hergestellter Flussleitelemente, ggf. geeignet gestapelt, zu realisieren, um auch hier, neben Vorteilen in der Herstellung, Wirbelströme zu reduzieren.Another way to influence the switching or movement behavior of a respective armature unit of the anchor means is to associate this armature spring means or the like power storage and about further education to store one or more of the armature units against a restoring force of such a spring or lead (where in turn further education by different configurations such as the spring forces then the respective switching or movement behavior of the associated anchor units can be influenced in a predetermined manner). In the context of further preferred embodiments of the invention, it is provided to realize the yoke unit by means of suitable sheet-shaped, more preferably by punching produced Flußleitelemente, possibly suitably stacked to reduce eddy currents here, in addition to advantages in the production.

Im Rahmen bevorzugter Weiterbildungen der Erfindung liegt es ferner, die Spuleneinheit im Rahmen der Erfindung mit beliebigen Umfangskonturen bzw. Querschnitten zu versehen, um insoweit wiederum die baulich-konstruktiven Optimierungsmöglichkeiten zu nutzen; neben zylindrischen Außenkonturen ist es dabei insbesondere vorteilhaft und weiterbildungsgemäß beansprucht, die Spuleneinheit querschnittlich rechteckig auszugestalten.In the context of preferred developments of the invention, it is also to provide the coil unit in the context of the invention with any circumferential contours or cross-sections, in order to turn to use the constructional-constructive optimization possibilities; In addition to cylindrical outer contours, it is claimed in particular advantageous and weiterbildungsgemäß to design the coil unit cross-sectionally rectangular.

Im Ergebnis eignet sich die erfindungsgemäße elektromagnetische Aktuatorvorrichtung zwar bevorzugt zur Realisierung von Hydraulik- oder Pneumatikventillösungen, insbesondere im Fahrzeugbereich, ist jedoch nicht auf diese Anwendungsgebiete beschränkt. Vielmehr lässt sich die vorliegende Erfindung günstig für nahezu beliebige Anwendungsgebiete nutzen und geeignet konfigurieren, bei welchen bauliche bzw. räumliche Flexibilität in Verbindung mit flexibel gestaltbaren magnetischen Flussführungen bzw. Flussverläufen innerhalb der jeweiligen Flussleitkreise genutzt werden können.As a result, the electromagnetic actuator device according to the invention is indeed preferably for the realization of hydraulic or pneumatic valve solutions, especially in the vehicle sector, but is not limited to these applications. On the contrary, the present invention can be used favorably and suitably configured for virtually any field of application in which structural or spatial flexibility can be used in conjunction with flexibly configurable magnetic flux guides or flow paths within the respective flux guide circuits.

Weitere Vorteile, bevorzugte Merkmale und Einzelheiten der Erfindung ergeben sich aus der nachfolgenden Beschreibung bevorzugter Ausführungsbeispiele sowie anhand der Zeichnungen; diese zeigen in:

Fig. 1:
eine Prinzipdarstellung einer elektromagnetischen Aktuatorvorrichtung gemäß einer ersten Ausführungsform der Erfindung zum Verdeutlichen des prinzipiellen Zusammenwirkens der verschiedenen Funktionskomponenten;
Fig. 2 - Fig. 4:
verschiedene Betriebs- bzw. Magnetfluss- und Schaltzustände der Vorrichtung gemäß Fig. 1, verdeutlicht durch einen jeweiligen Magnetfluss symbolisierende Pfeilschaaren;
Fig. 5:
eine Perspektivansicht einer Ausführungsform der elektromagnetischen Aktuatorvorrichtung welche nicht Teil der vorliegenden Erfindung ist
Fig. 6 - Fig. 8:
konstruktive Varianten der Ausgestaltung eines Flussleitelements in weiteren nicht Teil der Erfindung seienden Beispielen gegenüber dem Beispiel der Fig. 5.
Further advantages, preferred features and details of the invention will become apparent from the following description of preferred embodiments and from the drawings; these show in:
Fig. 1:
a schematic diagram of an electromagnetic actuator device according to a first embodiment of the invention to illustrate the basic interaction of the various functional components;
2 - Fig. 4:
various operating or magnetic flux and switching states of the device according to Fig. 1 , illustrates by a respective magnetic flux symbolizing arrow heads;
Fig. 5:
a perspective view of an embodiment of the electromagnetic actuator device which is not part of the present invention
Fig. 6 - Fig. 8:
constructive variants of the embodiment of a flux-conducting in further not part of the invention, be examples compared to the example of Fig. 5 ,

Die Fig. 1 verdeutlicht in der schematischen Längsschnittansicht eine elektromagnetische Aktuatorvorrichtung zum Antreiben zweier Ankereinheiten 10, 12 mittels einer gemeinsamen, zentral (mittig) zwischen diesen auf einem Jochabschnitt 13 vorgesehenen Spuleneinheit 14. Genauer gesagt sind, wie schematisch anhand des Schaubilds der Fig. 1 erkennbar, die langgestreckt dargestellten Ankereinheiten 10 bzw. 12 axial beweglich geführt (in einer Bewegungs- und Antriebsrichtung senkrecht in der Zeichnungsebene), wobei die Ankereinheiten 10 und 12 zusammenwirken mit stationären Jochabschnitten 15 bzw. 16 und, zur Realisierung entsprechender, gemeinsam durch die Spuleneinheit 14 verlaufender Flussleitkreise, die über flussleitende Verbindungsabschnitte 18 bis 24 geführt sind. Entsprechend entstehen für die Ankereinheiten 10 bzw. 12 wirksame Luftspalte 26 bzw. 28.The Fig. 1 illustrates in the schematic longitudinal sectional view of an electromagnetic actuator device for driving two anchor units 10, 12 by means of a common, centrally located (centrally) between them on a yoke section 13 coil unit 14. More specifically, as schematically with reference to the graph of Fig. 1 recognizable, the elongated armature units 10 and 12 shown axially movably guided (in a movement and drive direction perpendicular in the plane), wherein the armature units 10 and 12 cooperate with stationary yoke sections 15 and 16 and, for the realization thereof, together by the coil unit 14 extending flow control circuits, which are guided over flow-conducting connection sections 18 to 24. Accordingly arise for the anchor units 10 and 12 effective air gaps 26 and 28 respectively.

Die Fig. 2 bis 4 verdeutlichen verschiedene Betriebszustände als Reaktion auf eine Bestromung der Spuleneinheit 14: So zeigt etwa die Fig. 3 zwei Flussverläufe in den durch die jeweiligen Anker 10 bzw. 12 verlaufenden Flussleitkreise anhand der Pfeilschaaren 30 bzw. 32, wobei diese Magnetflüsse durch den der Spuleneinheit 14 zugeordneten Jochabschnitt 13 ("ersten Jochabschnitt") fließen, wie durch die Pfeilschaar 34 symbolisiert. Ist dagegen, wie in der Fig. 2 gezeigt, durch einen verkürzten Luftspalt 28 ein wirksamer Flusswiderstand im rechten Flussleitkreis (d.h. bezogen auf die Ankereinheit 12) gegenüber dem anderen Zweig vermindert, konzentriert sich der Magnetfluss, wie durch die Pfeilschaar 36 in Fig. 2 gezeigt, auf diesen rechten Bereich, mit der Wirkung, dass primär eine Antriebswirkung auf die Ankereinheit 12 in Richtung auf das statische Element 16 entsteht, entsprechend dieser Luftspalt dann geschlossen wird (Darstellung der Fig. 4). Durch diese Wirkung und eine entsprechende (Querschnitt-) Dimensionierung im rechtseitigen Flussleitkreis (z.B. der flussleitenden Komponenten 16, 20, 24 bzw. 12) tritt dann jedoch eine Sättigung in diesem Flussleitkreis auf, mit der Wirkung, dass durch den dadurch wiederum erhöhten Flusswiderstand ein Teil des Magnetflusses in den linken Flussleitkreis, wirksam für die Ankereinheit 10, verdrängt wird. Entsprechend kommt es durch diesen verdrängten Fluss 38 zu einer Kraftbeaufschlagung der Ankereinheit 10, welche darauffolgend den Luftspalt 30 schließt. Mithin verdeutlicht die gezeigte asymmetrische Konfiguration (ausgehend von der Fig. 2), wie etwa ein unterschiedliches, hier zeitlich aufeinanderfolgendes, Bewegungs- bzw. Schaltverhalten der Ankereinheiten provoziert werden kann.The Fig. 2 to 4 illustrate various operating conditions in response to energization of the coil unit 14: So shows about the Fig. 3 two flow paths in the flux guide circuits running through the respective armatures 10 and 12, respectively, on the basis of the arrowheads 30 and 32, these magnetic fluxes flowing through the yoke section 13 ("first yoke section") associated with the coil unit 14, as symbolized by the arrowhead 34. Is against it, as in the Fig. 2 As shown by a shortened air gap 28, an effective flow resistance in the right flow circuit (ie relative to the armature unit 12) is reduced relative to the other branch, the magnetic flux concentrates as indicated by the arrowhead 36 in FIG Fig. 2 shown on this right area, with the effect that primarily a driving effect on the armature unit 12 is formed in the direction of the static element 16, according to this air gap is then closed (representation of Fig. 4 ). Due to this effect and a corresponding (cross-sectional) dimensioning in the right-hand flux circuit (eg the flux-conducting components 16, 20, 24 and 12), however, saturation then occurs in this flux circuit, with the effect that this in turn increases the flow resistance Part of the magnetic flux in the left Flußleitkreis, effective for the anchor unit 10, is displaced. Accordingly, it comes through this displaced flow 38 to a force applied to the armature unit 10, which subsequently closes the air gap 30. Thus, the asymmetric configuration shown (starting from the Fig. 2 ), such as a different, here temporally successive, movement or switching behavior of the anchor units can be provoked.

Alternativ kann eine derartige Wirkung auch durch geeignet an den Ankereinheiten vorzusehende Federmittel (mit entsprechend verschiedenen Federkräften) realisiert werden, wiederum ergänzend oder alternativ mittels vorbestimmt eingestellter und dann entsprechend eine Sättigung erreichender wirksamer magnetischer Flussquerschnitte der beteiligten flussleitenden Komponenten.Alternatively, such an effect can also be realized by suitably provided on the anchor units spring means (with correspondingly different spring forces), again in addition or alternatively by means of predetermined adjusted and then corresponding saturation reaching effective magnetic flux cross sections of the flux-conducting components involved.

Mechanisch befinden sich bei dem Ausführungsbeispiel der Fig. 1 bis 4 beide Ankereinheiten 10 bzw. 12 unmittelbar am Spulenumfang bzw. diesem benachbart, sodass in potentiell einen Spulenwirkungsgrad erhöhender Weise eine optimierte Feldlinienbündelung über beide Anker und damit beidseits der Spuleneinheit erfolgt, vergleiche die Fig. 3. Eine geometrisch-mechanische Unsymmetrie, etwa durch Variation der jeweiligen Ankerabstände von der mittleren Spule, gestattet dann hier wiederum das Einrichten geeigneter abweichender Flussverläufe bzw. davon bestimmter Ankerbewegungen. Nicht Teil der Erfindung ist ein Beispiel, welches in in den Figuren nicht gezeigter Weise lediglich eine Ankereinheit mit einem zugehörigen zweiten Jochabschnitt, bevorzugt seitlich beabstandet bzw. benachbart zur Spuleneinheit, vorsieht. Auch dieses einfachste Beispiel realisiert bereits das Prinzip des ausgelagerten Ankers, nämlich eines im Rahmen eines Flusskreiszweiges vorgesehenen und seitlich bzw. benachbart angeordneten Ankers (samt zugehörigem Luftspalt), so dass eine Ankerbewegungsrichtung zwar weiterbildungsgemäß achsparallel zu einer Erstreckungsrichtung der Spuleneinheit (bzw. des zugehörigen ersten Jochabschnitts) erfolgen kann, diese Achsen jedoch nicht mehr koaxial verlaufen.Mechanically located in the embodiment of the Fig. 1 to 4 both anchor units 10 and 12 directly adjacent to the coil circumference or this, so that in potentially a coil efficiency increasing manner an optimized field line bundling over both armatures and thus takes place on both sides of the coil unit, compare the Fig. 3 , A geometric-mechanical asymmetry, such as by variation of the respective anchor distances from the central coil, then in turn permits the setting up of suitable deviating flow courses or anchor movements determined therefrom. Not part of the invention is an example which, in a manner not shown in the figures, only provides an armature unit with an associated second yoke section, preferably laterally spaced apart or adjacent to the coil unit. Even this simplest example already realizes the principle of the outsourced armature, namely a provided in the context of a flow circle branch and laterally or adjacent armature (and associated air gap), so that an armature movement direction while continuing education paraxial to an extension direction of the coil unit (or the associated first Jochabschnitts) can take place, but these axes are no longer coaxial.

Anhand der Fig. 5 bis 8 wird nachfolgend ein Aspekt, der nicht Teil der vorliegenden Erfindung ist, anhand eines weiteren Beispiels beschrieben. Eine erste Variante verdeutlicht die Fig. 5 in der perspektivischen Ansicht: Beidseits einer einen axial beweglichen Anker 40 sowie einen stationären Jochabschnitt 42 aufweisenden mittleren Anordnung ist ein Paar von Einzelspulen 44 bzw. 46 vorgesehen, dergestalt, dass Anker 40 bzw. Stator 42 beidseits von den Einzelspulen 44, 46 umrahmt sind. Ein (bei Bestromung der Spulen entstehender) Magnetfluss der Spulen 44 bzw. 46 wird über gemeinsame, langgestreckt-plattenförmige Flussleitelemente 48 bzw. 50 in den Anker 40 bzw. den Stator 42 eingetragen, wobei die Elemente 48 bzw. 50 zusätzlich für eine mechanische Verbindung der Gesamtanordnung (mit einer Austrittsöffnung 52 für die Ankereinheit) sorgen.Based on Fig. 5 to 8 Hereinafter, an aspect not part of the present invention will be described by way of further example. A first variant illustrates the Fig. 5 in the perspective view: on both sides of an axially movable armature 40 and a stationary yoke portion 42 having central arrangement, a pair of individual coils 44 and 46 is provided such that armature 40 and stator 42 are framed on both sides of the individual coils 44, 46. A magnetic flux (resulting when the coils are energized) of the coils 44 and 46, respectively, is fed into the armature 40 or the stator 42 via common elongated plate-shaped flux conducting elements 48 and 50, the elements 48 and 50 additionally being used for a mechanical connection the overall arrangement (with an outlet opening 52 for the anchor unit) provide.

Im Hinblick auf eine Flussführung in dieser Vorrichtung sind wiederum zwei Flussleitkreise ausgebildet, wobei ein jeweiliger der Flussleitkreise durch eine der Einzelspulen 44 bzw. 46 verläuft und beide Flussleitkreise dann gemeinsam durch die Anker-Stator-Anordnung 40, 42 fließen (insoweit entspricht der Flussverlauf analog der Fig. 3, jedoch bei einem Vorsehen einer mittleren Anker-Stator-Anordnung und zwei außenliegenden Einzelspulen).With regard to a flow guide in this device, in turn, two flux guide circuits are formed, wherein a respective one of the flux circuits runs through one of the individual coils 44 and 46 and both flux circuits then flow together through the armature-stator arrangement 40, 42 (insofar the flow path corresponds analogously of the Fig. 3 but with a provision of a central armature-stator arrangement and two external individual coils).

Diese prinzipielle Konfiguration der Fig. 5 ist gleichwohl weder auf zwei Einzelspulen, noch etwa die gezeigte symmetrische Anordnung beschränkt; vielmehr kann, etwa durch Variation der Geometrie der Elemente 48, 50, eine Abstandsänderung erfolgen, es kann auch, wie in den Fig. 6 bis 8 verdeutlicht, eine gegenüber den langgestreckten Elementen 48, 50 geeignet abgeknickte Konfiguration vorliegen, oder aber es können mehr als zwei Einzelspulen um eine (oder aber auch um mehrere) gemeinsame Anker-Stator-Anordnung(en) herum vorgesehen sein: So beschreibt etwa die Fig. 6 in der Draufsicht eine Variation der Elemente 48 bzw. 50, dergestalt, dass nunmehr zwei Schenkel 54, 56, voneinander um einen Winkel 58 von ca. 135° abgewinkelt, sich erstrecken und endseitig, vergleiche Fig. 8, mit den Einzelspulen 44 bzw. 46 flussleitend verbunden sind. Eine Vergleichsanordnung der als bekannt vorausgesetzten, traditionellen Art in der Darstellung der Fig. 7 verdeutlicht den dadurch realisierten Einbauraum- bzw. Geometrievorteil: Um nämlich ein dem Paar von Einzelspulen 44, 46 vergleichbares magnetisches Flussverhalten zu erzeugen, müsste eine Einzelspule eines Wicklungsquerschnitts 60, wie in Fig. 7 angedeutet, vorhanden sein, was aber möglicherweise in einem beschränkten Einbauraum (angepasst an die Konfiguration der Fig. 6, 8) nicht möglich ist.This basic configuration of the Fig. 5 is, however, not limited to two individual coils, nor about the symmetrical arrangement shown; Rather, by varying the geometry of the elements 48, 50, a change in distance it can also, as in the Fig. 6 to 8 illustrates, compared to the elongated elements 48, 50 suitably kinked configuration are present, or it can be provided around one (or even more) common armature-stator assembly (s) around more than two individual coils: So describes about the Fig. 6 in plan view, a variation of the elements 48 and 50, such that now two legs 54, 56, angled away from each other by an angle 58 of about 135 °, extend and end, compare Fig. 8 , 44 are connected to the individual coils 44 and 46, respectively. A comparison arrangement of the presupposed as known, traditional type in the representation of Fig. 7 illustrates the resulting installation space or geometry advantage: namely, in order to produce a magnetic flux behavior comparable to the pair of individual coils 44, 46, a single coil of a winding cross-section 60, as in FIG Fig. 7 indicated to be present, but possibly in a limited installation space (adapted to the configuration of Fig. 6, 8 ) not possible.

Ein weiterer Vorteil des Beispiels mit einer Mehrzahl von benachbart einer Anker-Stator-Anordnung vorgesehener Einzelspulen mit sich addierendem bzw. überlagerndem Flussverlauf, etwa der in Fig. 5 bzw. Fig. 6 und 8 gezeigten Art, liegt darin, dass mögliche Querkräfte (auf den Anker) im Vergleich zu einer Lösung mit lediglich einer benachbart der Ankereinheit ausgelagerten Spule verringert sind (da insoweit eine gegenseitige Kompensation stattfindet, vergleiche etwa das Flussdiagramm der Fig. 3 bei analoger Anwendung auf eine Anordnung mit zwei außenliegenden Einzelspulen). Gerade bei Produkten mit hohen Lebensdaueranforderungen, wie etwa im Ventilbereich, wirkt sich eine derartige Verringerung der Querkräfte auf den Anker günstig auf einen Verschleiß und mithin eine wirksame Nutzungsdauer aus.A further advantage of the example with a plurality of individual coils provided adjacent to an armature-stator arrangement with an adding or overlapping flow profile, such as in FIG Fig. 5 respectively. 6 and 8 shown, is that possible lateral forces are reduced (to the anchor) compared to a solution with only one adjacent the anchor unit outsourced coil (as far as a mutual compensation takes place, see for example the flowchart of Fig. 3 in analogous application to an arrangement with two external individual coils). Especially for products with high service life requirements, such as in the valve area, such a reduction of the lateral forces on the anchor has a favorable effect on wear and therefore an effective service life.

Die vorliegende Erfindung, unabhängig von den gezeigten oder weiteren möglichen Ausführungsformen, ermöglicht zahlreiche praktische Vorteile: So bietet etwa das Anordnen der Ankermittel in einer Verwendung als Ventil deutlich flexiblere Anschlussmöglichkeiten in der erfindungsgemäßen Konfiguration benachbart der Spuleneinheit etwa gegenüber dem bekannten Stand der Technik, bei welchem typischerweise die langgestreckte Ankereinheit von der Spuleneinheit (typischerweise zylindrisch-radial) umgeben ist. Entsprechend kann der Arbeitsluftspalt flexibler (und geeignet für einen jeweiligen Anwendungsfall) ausgestaltet werden. Zusätzlich weiterbildungsgemäß vorteilhaft ist vorgesehen, angepasst an jeweilige Einbau- und Raumbedingungen, die nicht mit zylindrischer Wicklung zu versehen, sondern etwa rechteckige oder andere Spulenquerschnitte vorzusehen. Dies gilt insbesondere im Zusammenwirken mit flussleitenden Elementen, welche mithilfe von (typischerweise durch Stanzen hergestellten) Blechen realisiert sind und weiter vorteilhaft in geeigneten Stapelkonfigurationen vorliegen.The present invention, regardless of the embodiments shown or other possible, allows numerous practical advantages: For example, arranging the anchor means in a use as a valve offers much more flexible connection possibilities in the configuration according to the invention adjacent to the coil unit for example, compared to the known state of the art, in which typically the elongated armature unit is surrounded by the coil unit (typically cylindrical-radial). Accordingly, the working air gap can be made more flexible (and suitable for a particular application). In addition, according to further education advantageous is provided adapted to respective installation and room conditions, not to provide the cylindrical winding, but to provide approximately rectangular or other coil cross-sections. This is especially true in cooperation with flux-conducting elements, which are realized by means of (typically produced by punching) sheets and further advantageously present in suitable stacking configurations.

Damit lässt sich auch für die vorliegende Erfindung der Vorteil einer Wirbelstromreduktion (gerade für höhere Frequenzen) geblechter Flussleitelemente nutzen.This also makes it possible to use the advantage of an eddy-current reduction (especially for higher frequencies) of flat flux-conducting elements for the present invention.

Claims (9)

  1. An electromagnetic actuator device with a coil unit (14) which encloses a first yoke section (13) of a stationary yoke unit of the actuator device and which can be activated by being energised;
    and with armature elements (10, 12) which can be guided so as to be moveable relative to the yoke unit and which interact with an output-side actuating partner and which can be driven to perform such an actuating movement, the armature elements interacting with a second yoke section (15, 16) of the yoke unit by forming air gaps (26, 28) for the magnetic flux produced by the activated coil unit,
    characterised in that the armature elements are provided radially externally adjacent to an outer casing of the coil unit, and in that at this point a plurality of second yoke sections (15, 16) are formed for interacting with a plurality of separately movably guided armature units (10, 12) of the armature elements, in such a way
    that a plurality of magnetic flux conducting circuits is created in the yoke unit by forming a plurality of air gaps associated with a respective armature unit and radially externally formed adjacent to the outer casing outside the first yoke section,
    wherein each of the flux conducting circuits passes through the first yoke section, the respective one of the second yoke sections, the respective one of the armature units as well as over the respective air gap, and a change in the respective one of the air gaps due to an actuating position and/or a movement of an associated armature unit, effects a change in a flux conducting circuit of another one of the armature units.
  2. The device according to claim 1, characterised in that the yoke unit has flux conducting means which are formed in such a way that their magnetic flux resistance is adjustable, in particular by forming a predetermined maximally effective flux cross-section, in particular in that it rises above a threshold value determined by the flux cross-section.
  3. The device according to claim 2, characterised in that the flux conducting means, which are realised as a magnetically conductive material, form a number of yoke branches corresponding to the number of armature units, which are joined to the first yoke section.
  4. The device according to claim 3, characterised in that a respective one of the yoke branches forms one of the said air gaps which is influenced by an actuating position of the armature unit with an associated one of the armature units.
  5. The device according to one of claims 1 to 4, characterised in that the respective air gaps configured for a stop position of the plurality of armature units, are of different dimensions, in particular having different effective distances between air gaps.
  6. The device according to one of claims 1 to 5, further comprising spring elements, wherein at least one of the armature units is mounted or guided against a restoring force of the spring elements.
  7. The device according to claim 6, characterised in that the restoring force operating on the plurality of armature units, is configured differently for at least two of the armature units.
  8. The device according to one of claims 1 to 7, characterised in that the yoke unit and/or the first yoke section and/or the second yoke section and/or a flux conducting section between the first and the second yoke section is realised as a sheet metal element, in particular a stackable sheet metal element, and/or as a layered structure made of a plurality of sheet metal elements.
  9. A use of the electromagnetic actuator device according to one of claims 1 to 8 for realising a pneumatic or hydraulic valve, in particular for a motor vehicle.
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Families Citing this family (2)

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Publication number Priority date Publication date Assignee Title
DE102018117074A1 (en) * 2018-07-13 2020-01-16 Svm Schultz Verwaltungs-Gmbh & Co. Kg Electromagnetic actuator with armature disk
CN113562203B (en) * 2021-07-02 2022-12-13 哈尔滨工业大学 Electromagnetic actuator with redundant air gaps

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202008015303U1 (en) * 2008-11-19 2009-03-26 Bürkert Werke GmbH & Co. KG Lifting armature drive

Family Cites Families (80)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4157520A (en) * 1975-11-04 1979-06-05 Westinghouse Electric Corp. Magnetic flux shifting ground fault trip indicator
US4164721A (en) * 1975-12-11 1979-08-14 Minolta Camera Kabushiki Kaisha Magnetic actuator for a shutter mechanism
DE2816555A1 (en) * 1977-04-18 1978-10-19 Francaise App Elect Mesure MAGNETIC CIRCUIT FOR AN ELECTROMAGNET FOR ONE WITH A PERMANENT MAGNET AS ANCHOR
GB1591471A (en) * 1977-06-18 1981-06-24 Hart J C H Electromagnetic actuators
US4127835A (en) * 1977-07-06 1978-11-28 Dynex/Rivett Inc. Electromechanical force motor
US4217507A (en) * 1979-01-08 1980-08-12 The Singer Company Linear motor
US4306207A (en) * 1980-05-07 1981-12-15 Hosiden Electronics Co., Ltd. Self-sustaining solenoid
JPH0134326Y2 (en) * 1981-04-22 1989-10-19
JPS5829754U (en) * 1981-08-21 1983-02-26 日立金属株式会社 Actuator for door lock
FR2520152B1 (en) * 1982-01-20 1986-02-28 Telemecanique Electrique ELECTRO-MAGNET WITH MOBILE EQUIPMENT WITH PERMANENT MAGNET WITH MONOSTABLE OPERATION
US4524797A (en) * 1982-02-25 1985-06-25 Robert Bosch Gmbh Solenoid valve
US4550302A (en) * 1982-11-09 1985-10-29 Matsushita Electric Industrial Co., Ltd. Solenoid
JPS59171314U (en) * 1983-04-28 1984-11-16 オムロン株式会社 electromagnet device
EP0130423A3 (en) * 1983-06-30 1985-09-18 EURO-Matsushita Electric Works Aktiengesellschaft Polarized electromagnet and its use in a polarized electromagnetic relay
DE3334159A1 (en) * 1983-09-21 1985-04-04 Sauer, Otto, 6800 Mannheim MAGNETIC VALVE
US4797645A (en) * 1984-03-05 1989-01-10 Mitsubishi Mining & Cement Co., Ltd. Electromagnetic actuator
JPS60261111A (en) * 1984-06-08 1985-12-24 Mitsubishi Mining & Cement Co Ltd Electromagnetic actuator
FR2568402B1 (en) * 1984-07-24 1987-02-20 Telemecanique Electrique DIRECT CURRENT ELECTROMAGNET, PARTICULARLY FOR ELECTRIC SWITCHING APPARATUS
CN1003822B (en) * 1984-10-09 1989-04-05 三菱矿业水泥株式会社 Electromagnetic actuator
GB8514544D0 (en) * 1985-06-08 1985-07-10 Lucas Ind Plc Electromagnetic actuator
US4679017A (en) * 1986-03-19 1987-07-07 Synchro-Start Products, Inc. Emergency manual actuation mechanism for a solenoid
US4835503A (en) * 1986-03-20 1989-05-30 South Bend Controls, Inc. Linear proportional solenoid
US4751487A (en) * 1987-03-16 1988-06-14 Deltrol Corp. Double acting permanent magnet latching solenoid
US4868695A (en) * 1988-03-30 1989-09-19 Magnetic Peripherals Inc. Head/arm lock mechanism for a disk drive
US4903578A (en) * 1988-07-08 1990-02-27 Allied-Signal Inc. Electropneumatic rotary actuator having proportional fluid valving
US5268662A (en) * 1988-08-08 1993-12-07 Mitsubishi Mining & Cement Co., Ltd. Plunger type electromagnet
US5388086A (en) * 1989-06-13 1995-02-07 Kabushiki Kaisha Toshiba Electro-magnetic actuator for driving an objective lens
US4994776A (en) * 1989-07-12 1991-02-19 Babcock, Inc. Magnetic latching solenoid
DE19646243C1 (en) * 1996-11-08 1997-10-23 Siemens Ag Electromagnetic difference current circuit-breaker release
US5032812A (en) * 1990-03-01 1991-07-16 Automatic Switch Company Solenoid actuator having a magnetic flux sensor
US5257014A (en) * 1991-10-31 1993-10-26 Caterpillar Inc. Actuator detection method and apparatus for an electromechanical actuator
JP3294382B2 (en) * 1992-10-30 2002-06-24 株式会社デンソー Flow control valve
US5303012A (en) * 1993-02-10 1994-04-12 Honeywell Inc. Single magnet latch valve with position indicator
JP2607670Y2 (en) * 1993-10-21 2002-03-04 エスエムシー株式会社 Self-holding solenoid valve
US5453724A (en) * 1994-05-27 1995-09-26 General Electric Flux shifter assembly for circuit breaker accessories
US5523684A (en) * 1994-11-14 1996-06-04 Caterpillar Inc. Electronic solenoid control apparatus and method with hall effect technology
US6836201B1 (en) * 1995-12-01 2004-12-28 Raytheon Company Electrically driven bistable mechanical actuator
US5809157A (en) * 1996-04-09 1998-09-15 Victor Lavrov Electromagnetic linear drive
US5969589A (en) * 1996-08-28 1999-10-19 Ferrofluidics Corporation Quiet ferrofluid solenoid
DE19712669C2 (en) * 1997-03-26 2000-03-30 Daimler Chrysler Ag Electromagnetically controlled valve
JP2000170951A (en) 1998-10-02 2000-06-23 Pacific Ind Co Ltd Self holding type three-way solenoid valve
US6242994B1 (en) * 1999-03-16 2001-06-05 Ferrofluidics Corporation Apparatus to reduce push back time in solenoid valves
DE19914372B4 (en) * 1999-03-30 2007-05-16 Pierburg Gmbh Device for monitoring the valve lift of an electromagnetically driven valve
US6293516B1 (en) * 1999-10-21 2001-09-25 Arichell Technologies, Inc. Reduced-energy-consumption actuator
US6265956B1 (en) * 1999-12-22 2001-07-24 Magnet-Schultz Of America, Inc. Permanent magnet latching solenoid
WO2001063626A2 (en) * 2000-02-22 2001-08-30 Bergstrom Gary E An improved system to determine solenoid position and flux without drift
US6305662B1 (en) * 2000-02-29 2001-10-23 Arichell Technologies, Inc. Reduced-energy-consumption actuator
US6948697B2 (en) * 2000-02-29 2005-09-27 Arichell Technologies, Inc. Apparatus and method for controlling fluid flow
US20070241298A1 (en) * 2000-02-29 2007-10-18 Kay Herbert Electromagnetic apparatus and method for controlling fluid flow
US6501357B2 (en) * 2000-03-16 2002-12-31 Quizix, Inc. Permanent magnet actuator mechanism
US6401976B1 (en) * 2000-03-23 2002-06-11 Nordson Corporation Electrically operated viscous fluid dispensing apparatus and method
DE10033923A1 (en) * 2000-07-12 2002-01-24 Lsp Innovative Automotive Sys Sensorless detecting of velocity and position in drives of electromagnetic adjustment systems, involves measuring current and voltage in excitation circuit and measuring characteristic line field
CN1234135C (en) * 2001-01-18 2005-12-28 株式会社日立制作所 Electromagnetic and operating mechanism of switch using said electromagnet
JP3842990B2 (en) * 2001-08-13 2006-11-08 Smc株式会社 Movable iron core for solenoid valve and method for manufacturing the same
US6856222B1 (en) * 2001-08-31 2005-02-15 Caterpillar Inc. Biarmature solenoid
DE10146899A1 (en) 2001-09-24 2003-04-10 Abb Patent Gmbh Electromagnetic actuator, in particular electromagnetic drive for a switching device
WO2003056579A1 (en) * 2001-12-27 2003-07-10 Nok Corporation Solenoid
JP3927089B2 (en) * 2002-07-16 2007-06-06 日本電産サンキョー株式会社 Linear actuator, pump device and compressor device using the same
US7352268B2 (en) * 2002-09-26 2008-04-01 Engineering Matters, Inc. High intensity radial field magnetic actuator
US7280019B2 (en) * 2003-08-01 2007-10-09 Woodward Governor Company Single coil solenoid having a permanent magnet with bi-directional assist
JP2006108615A (en) * 2004-09-07 2006-04-20 Toshiba Corp Electromagnetic actuator
CN1291433C (en) * 2005-09-09 2006-12-20 刘津平 Low power consumption digital controlled contact device and control system thereof
CA2622425C (en) * 2005-09-13 2012-04-10 Armour Magnetic Components, Inc. Solenoid actuator and method for making and using same
JP2009521074A (en) * 2005-12-22 2009-05-28 シーメンス アクチエンゲゼルシヤフト Switching device operating method and operating device
FR2895594B1 (en) * 2005-12-22 2008-03-07 Sagem Defense Securite DEVICE FOR LINEAR DISPLACEMENT OF A BODY BETWEEN TWO PREDETERMINED POSITIONS
FR2896615A1 (en) * 2006-01-20 2007-07-27 Areva T & D Sa MAGNETIC ACTUATOR WITH PERMANENT MAGNET WITH REDUCED VOLUME
US20070210653A1 (en) * 2006-03-13 2007-09-13 Scanlon Matthew J Moving magnet actuator with counter-cogging end-ring and asymmetrical armature stroke
DE102007004377A1 (en) * 2007-01-29 2008-08-07 Diener Precision Pumps Ltd. Electromagnetically actuated valve
US8106734B2 (en) * 2007-04-25 2012-01-31 Saia-Burgess, Inc. Adjustable mid air gap magnetic latching solenoid
DE102007028600B4 (en) * 2007-06-19 2011-06-22 ETO MAGNETIC GmbH, 78333 Electromagnetic actuator
DE202007013709U1 (en) * 2007-10-01 2007-12-20 Bürkert Werke GmbH & Co. KG Arrangement of stringed magnet drives
DE202009010495U1 (en) * 2008-08-01 2009-12-17 Eto Magnetic Gmbh Electromagnetic actuator
US7864008B2 (en) * 2008-10-22 2011-01-04 Deltrol Controls Solenoid assembly with shock absorbing feature
US7969772B2 (en) * 2008-11-18 2011-06-28 Seagate Technology Llc Magnetic mechanical switch
DE202008015980U1 (en) * 2008-12-03 2010-04-29 Eto Magnetic Gmbh Electromagnetic actuator device
KR200451951Y1 (en) * 2008-12-31 2011-01-25 엘에스산전 주식회사 Monostable Permanent Magnet Actuator with Laminated Core
DE202009006940U1 (en) * 2009-04-16 2010-09-02 Eto Magnetic Gmbh Electromagnetic camshaft adjusting device
US8581682B2 (en) * 2009-10-07 2013-11-12 Tyco Electronics Corporation Magnet aided solenoid for an electrical switch
DE202010010371U1 (en) * 2010-07-16 2011-10-17 Eto Magnetic Gmbh Electromagnetic actuator
DE102011014193A1 (en) * 2011-03-16 2012-10-04 Eto Magnetic Gmbh actuator

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202008015303U1 (en) * 2008-11-19 2009-03-26 Bürkert Werke GmbH & Co. KG Lifting armature drive

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WO2012123538A1 (en) 2012-09-20
CN103443877A (en) 2013-12-11
CN103443877B (en) 2017-06-09
EP3211645A1 (en) 2017-08-30
EP2686853A1 (en) 2014-01-22
US9117583B2 (en) 2015-08-25
US20140125437A1 (en) 2014-05-08
DE202011004021U1 (en) 2012-07-09

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