EP1455372B1 - Relay with core having partly enlarged cross section - Google Patents

Relay with core having partly enlarged cross section Download PDF

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Publication number
EP1455372B1
EP1455372B1 EP03005059A EP03005059A EP1455372B1 EP 1455372 B1 EP1455372 B1 EP 1455372B1 EP 03005059 A EP03005059 A EP 03005059A EP 03005059 A EP03005059 A EP 03005059A EP 1455372 B1 EP1455372 B1 EP 1455372B1
Authority
EP
European Patent Office
Prior art keywords
core
yoke
relay
cross
bobbin
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP03005059A
Other languages
German (de)
French (fr)
Other versions
EP1455372A1 (en
Inventor
Rudolf Mikl
Leopold Mader
Bernd Adrian
Johannes Helmreich
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.)
Tyco Electronics Austria GmbH
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Tyco Electronics Austria GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to ES03005059T priority Critical patent/ES2266657T3/en
Application filed by Tyco Electronics Austria GmbH filed Critical Tyco Electronics Austria GmbH
Priority to EP03005059A priority patent/EP1455372B1/en
Priority to AT03005059T priority patent/ATE328359T1/en
Priority to DE50303564T priority patent/DE50303564D1/en
Priority to US10/786,407 priority patent/US7026896B2/en
Priority to JP2004052797A priority patent/JP4462536B2/en
Priority to CNB2004100077175A priority patent/CN100367434C/en
Publication of EP1455372A1 publication Critical patent/EP1455372A1/en
Application granted granted Critical
Publication of EP1455372B1 publication Critical patent/EP1455372B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H50/00Details of electromagnetic relays
    • H01H50/16Magnetic circuit arrangements
    • H01H50/36Stationary parts of magnetic circuit, e.g. yoke
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H50/00Details of electromagnetic relays
    • H01H50/16Magnetic circuit arrangements
    • H01H50/163Details concerning air-gaps, e.g. anti-remanence, damping, anti-corrosion

Definitions

  • the invention relates to a relay with a bobbin, a core passing through the bobbin and a yoke, wherein the cross-sectional area of the core in the region of the transition to the yoke and at the yoke facing away from the end of the core is greater than in the surrounding of the bobbin center region of the core.
  • a safety valve is described with a U-shaped Kemjoch having a core and a yoke leg, wherein the core leg is arranged in a bobbin.
  • the bobbin, the core and the yoke form a magnet system which causes a switching action when the coil is energized.
  • a magnetic switching force is generated, which moves an armature.
  • the movement of the armature is transferred to a contact spring, which then closes or opens contacts.
  • a disadvantage of the known from the prior art relays are in part only low switching forces or at high switching forces large designs.
  • the invention is therefore based on the object to improve a relay of the type mentioned so that large switching forces can be achieved with a small volume.
  • the core is formed from at least two core elements.
  • the center region of the core surrounded by the bobbin has a reduced cross-section, which provides room for additional coil windings, so that the coil can generate a higher magnetic force.
  • the cross-section is made widened, so that a high magnetic flux can be conducted from the core to the yoke.
  • the core is formed according to the invention from at least two core elements.
  • the surface area of the pole face according to the invention be greater than the cross-sectional area in the central region of the core. Due to the enlarged pole surface, a high magnetic flux acts on the armature, which ensures high switching forces and fast switching operations.
  • the core can also be tapered in a development in the region of the bobbin, so that at both ends of the core large cross-sectional areas for a line of magnetic flux with low losses are available and at the same time in the region of the taper space for additional windings of the bobbin held by the coil is provided.
  • the assembly of the core in the bobbin can be simplified by a series of independent developments.
  • the core elements can be designed to be used successively in the track body, so that in spite of the cross-sectional widening a simple assembly is possible, even if the cross-sectional widening of the core engages behind the bobbin.
  • At least two core elements may have a cross-sectional widening towards the yoke; Furthermore, at least two core elements may have a cross-sectional widening to the pole face.
  • a core element can be inserted substantially in the bobbin be designed.
  • the core element can be fitted in inserted in already inserted in the bobbin further core element.
  • the assembly of the core element can be further facilitated by the fact that at least one core element is configured substantially free of undercuts or substantially cuboid-shaped. This configuration facilitates in particular the insertion of the core element in the bobbin.
  • the core may also consist of a plurality of transverse to the longitudinal extent of the bobbin juxtaposed core elements are minimized by the power loss when switching on and / or off the excitation current of the coil.
  • the core elements may be permanently pre-assembled in this embodiment.
  • the core or at least one core element may be integrally formed with the yoke to minimize the losses in the transition of the magnetic flux from the core to the yoke and to reduce assembly costs.
  • this core element can be designed to be insertable into the bobbin.
  • the module unit of bobbin and yoke is completed by simply inserting the yoke in the bobbin. Only the core element provided with the cross-sectional widening must be inserted into the bobbin before insertion of the core element on the yoke.
  • At least one core element can at least touch the yoke, so that the air gaps penetrated by the magnetic field are as small as possible or absent.
  • a relay 1 has a coil wound on a bobbin 2 (not shown in FIG. 1), a yoke 3 and a core passing through the bobbin 2 (not shown in FIG. 1).
  • the yoke 3 terminates in a pole face 4 which adjoins a working air gap 5 borders.
  • the pole face 4 may also be formed on the core.
  • the working air gap 5 is arranged between the pole face 4 and a movable armature 6.
  • the armature 6 is connected in a motion-transmitting manner with a contact spring 8 via a connecting element 7 guided along the bobbin 2, so that a movement of the armature 6 inevitably leads to a movement of the contact spring 8.
  • the contact spring 8 in turn is arranged between two mutually spaced in the direction of movement of the contact spring contacts 9, 10, wherein they can preferably only one of the two contacts 9, 10 touch.
  • the contact spring 8 is biased so that it rests in the power-free state against one of the contacts, for example the contact 10.
  • the contacts 9, 10 and the contact spring 8 are each provided with guided to outside the relay pins 11, 12, 13.
  • the contact pins 11, 12, 13 may each be present in pairs.
  • the contacts 11, 13 and 11, 12 are closed in dependence on the position of the contact spring 8.
  • the contacts 11 and 12 are connected to one another via the contact spring 8 and the contact 11.
  • contact pills 14, 15, 16 may be provided on the contacts 9, 10 and / or the contact spring 8.
  • FIG. 2 an embodiment of the bobbin 2 with the yoke 3 and the coil passing through the core 17 is shown, wherein the viewing direction is directed obliquely on the pole face 4.
  • the core 17 has two core elements 19, 20 which lie perpendicular to one another perpendicular to the coil direction.
  • the core 17 protrudes from the bobbin 2.
  • yoke 3 and the core 17 is shown in the perspective of FIG. 2 with the bobbin 2 removed.
  • both core elements 19, 20 terminate flush to form a substantially flat end face 21, which can also serve as a pole face 4.
  • the core element 20 formed integrally with the yoke is substantially cuboid and has no projections and / or undercuts.
  • the other, separate core element 19 is provided in the longitudinal direction L of the coil at the respective end faces with cross-sectional widenings 22, 23.
  • the cross-sectional widenings 22, 23 engage behind the bobbin 2.
  • the cross section of the core is reduced in relation to the two end regions located in the longitudinal direction of the bobbin. This results in a recess 25 which can be used as an additional winding space for the coil, so that the coil has a higher winding number and / or density.
  • the cross-sectional widening 23 can also be dispensed with, although this impairs the flow of the magnetic field from the core into the armature;
  • the pole face 4 formed by the yoke 3 may have a cross-sectional widening.
  • the dividing plane 26 extends between the two core elements 19, 20 in the longitudinal direction L of the coil parallel to the yoke 3.
  • the superposed surfaces are as flat and smooth as possible. This avoids air gaps in the transition areas and losses in the magnetic flux.
  • FIGS. 4 to 6 show further embodiments of the core element 20.
  • the cross-section at the two longitudinal ends 22, 23 is widened in a cross-sectional plane perpendicular to the longitudinal direction L of the coil.
  • the cross-sectional plane Q is shown schematically in FIG. 4 once in the middle region as a cross-sectional plane Q 1 and once in the end region as a cross-sectional plane Q 2 .
  • the surface area of the cross section Q 2 is greater than the area of the cross section Q 1 .
  • the core element 19 of FIG. 4 is efficiently manufactured in one piece and has bent ends 22, 23. By a over the entire width of the core member 19 extending recess 28 in the vicinity of the bending radius 29 of the bending process is facilitated.
  • a core member 19 is shown, which is composed of a plurality of individual elements 19a, 19b, ..., which are arranged side by side.
  • the number of juxtaposed and preferably touching core elements 19a, 19b,... Is arbitrary; in FIG. 5, four adjacent elements are shown by way of example only.
  • the cross-sectional areas or contours of the individual core elements 19a, 19b,... In a plane lying in the longitudinal direction L are the same.
  • the core elements 19a, 19b, ... integrally connected to each other, for example, glued, soldered or welded.
  • Fig. 6 is an embossed part of a metal material, in which the two cross-sectional extensions 22, 23 in the form of obliquely extending in the longitudinal direction L of the coil, embossed ramps are configured.
  • the core element 19 can also be produced by injection molding.
  • bobbin 2 is shown, wherein the core 17 and the yoke 3 are omitted.
  • the bobbin 2 has a passage 30 extending in the longitudinal direction L of the bobbin, which is open on both sides.
  • the clear cross section in a plane perpendicular to the longitudinal direction L of the passage 30 is reduced to make room for additional coil windings.
  • the shape of the region 32 is adapted to the shape of the respective cross-sectional widening 22, 23, so that the core element 19 with the cross-sectional widenings 22, 23 in the passage 30 can be included.
  • the cross-section of the passage 30 is dimensioned at its smallest point so that the cross-sectional widening 22 of the core element 19 can still be inserted through the passage 30. When inserted, the cross-sectional widenings 22, 23 engage behind the bobbin 2, so that the core element 19 is held substantially immovably by the bobbin.
  • the cross-sectional widening of the passage 30 at the two open ends can be designed differently, for example, at one end a flush termination of Kerns with the bobbin 2 and at the other end to allow the core 17 to protrude.
  • the passage 30 is designed so that when inserted core element 19 with cross-sectional extensions 22 and 23 extending through the bobbin 2 therethrough Free space 33 remains of substantially constant clear width.
  • the other core element 20 can be inserted 19 after insertion of the respective other core element.
  • the cross-sectional widenings 22, 23 the one core element 19 can no longer be removed from the passage 30 as long as the other core element 20 is inserted.
  • the core can be held firmly in the bobbin.
  • the cross section of the core element 20 is slightly larger than the cross section of the free space 33.
  • the core element 19 is used, which is provided with at least one cross-sectional widening 22, 23. As soon as the cross-sectional enlargements 22, 23 are received in the extension 32 of the passage assigned to it, the other core element 20 is inserted into the remaining free space 33.
  • the yoke 3 or the core element 19 is placed in the passage 30. Subsequently, the substantially quäderförmige core element 20 is inserted.

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  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Electromagnets (AREA)
  • Coils Or Transformers For Communication (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)

Abstract

A partition plane (26) extends between first (19) and second (20) core elements in a coil's lengthwise direction (L) parallel to a yoke (3). Interlayered surfaces are made as flat and smooth as possible on the parting plane as well as on a buffer surface (27) between a cross-sectional enlargement (22) and the yoke. This avoids air gaps in transitional areas and losses in magnetic flux.

Description

Die Erfindung betrifft ein Relais mit einem Spulenkörper, einem den Spulenkörper durchsetzenden Kern und einem Joch, wobei die Querschnittsfläche des Kerns im Bereich des Übergangs zum Joch und an der dem Joch abgewandten Stirnseite des Kerns größer ist als in dem vom Spulenkörper umgebenden Mittenbereich des Kerns.The invention relates to a relay with a bobbin, a core passing through the bobbin and a yoke, wherein the cross-sectional area of the core in the region of the transition to the yoke and at the yoke facing away from the end of the core is greater than in the surrounding of the bobbin center region of the core.

Relais mit diesen Merkmalen sind beispielsweise aus der EP-A-202 651, EP-B-363 976. EP-B-691 667 und der DE-C-42 32 228 bekannt.Relays with these features are known for example from EP-A-202 651, EP-B-363 976. EP-B-691 667 and DE-C-42 32 228.

Ein weiteres Relais ist in der US-A-3,497,845 beschrieben, das einen Spulenkörper, einen im Spulenkörper angeordneten Kern und ein Joch umfasst.Another relay is described in US-A-3,497,845, which comprises a bobbin, a core arranged in the bobbin, and a yoke.

In der WO-A-00 24019 ist ein Sicherheitsventil mit einem U-förmigen Kemjoch beschrieben, das einen Kern- und einen Jochschenkel aufweist, wobei der Kemschenkel in einem Spulenkörper angeordnet ist.In WO-A-00 24019 a safety valve is described with a U-shaped Kemjoch having a core and a yoke leg, wherein the core leg is arranged in a bobbin.

Bei allen diesen Relais bildet der Spulenkörper, der Kern und das Joch ein Magnetsystem, das bei Erregung der Spule einen Schaltvorgang bewirkt. Im Zuge des Schaltvorgangs, bei Erregung der Spule, wird eine magnetische Schaltkraft erzeugt, die einen Anker bewegt. Die Bewegung des Ankers wird auf eine Kontaktfeder übertragen, die daraufhin Kontakte schließt oder öffnet.In all these relays, the bobbin, the core and the yoke form a magnet system which causes a switching action when the coil is energized. In the course of the switching process, upon energization of the coil, a magnetic switching force is generated, which moves an armature. The movement of the armature is transferred to a contact spring, which then closes or opens contacts.

Nachteilig bei den aus dem Stand der Technik bekannten Relais sind die zum Teil nur niedrige Schaltkräfte bzw. die bei hohen Schaltkräften großen Bauformen.A disadvantage of the known from the prior art relays are in part only low switching forces or at high switching forces large designs.

Der Erfindung liegt daher die Aufgabe zugrunde, ein Relais der eingangs genannten Art so zu verbessern, dass bei kleinen Bauvolumen große Schaltkräfte erreicht werden.The invention is therefore based on the object to improve a relay of the type mentioned so that large switching forces can be achieved with a small volume.

Diese Aufgabe wird für das eingangs genannte Relais dadurch gelöst, dass der Kern aus wenigstens zwei Kernelementen gebildet ist.This object is achieved for the above-mentioned relay in that the core is formed from at least two core elements.

Diese Lösung ist konstruktiv einfach und führt zu kleineren Bauformen des Relais bei gleichbleibender hoher Schaltkraft.This solution is structurally simple and leads to smaller designs of the relay at a constant high switching force.

Entsprechend dem Oberbegriff des ersten Anspruchs weist der Mittenbereich des Kerns, der vom Spulenkörper umgeben ist, einen verringerten Querschnitt auf, der Raum für zusätzliche Spulenwicklungen bietet, so dass die Spule eine höhere Magnetkraft erzeugen kann. Im Übergangsbereich zwischen Joch und Kern und an der dem Joch abgewandten Stirnseite des Kerns ist dagegen der Querschnitt erweitert ausgestaltet, so dass ein hoher Magnetfluss vom Kern zum Joch geleitet werden kann. Beide Maßnahmen, die Querschnittserweiterung im Übergangsbereich zwischen Kern und Joch sowie die Querschnittsverminderung und der vermehrte Wicklungsraum für den Spulenkörper, ergänzen sich gegenseitig optimal bei der Erzeugung einer höheren Schaltkraft.According to the preamble of the first claim, the center region of the core surrounded by the bobbin has a reduced cross-section, which provides room for additional coil windings, so that the coil can generate a higher magnetic force. In contrast, in the transitional region between the yoke and the core and at the end face of the core facing away from the yoke, the cross-section is made widened, so that a high magnetic flux can be conducted from the core to the yoke. Both measures, the cross-sectional widening in the transition region between core and yoke and the reduction in cross-section and the increased winding space for the bobbin, complement each other optimally in generating a higher switching power.

Der Kern ist erfindungsgemäß aus wenigstens zwei Kernelementen gebildet.The core is formed according to the invention from at least two core elements.

Die Leistungsfähigkeit des solchermaßen verbesserten Relais kann durch verschiedene, voneinander unabhängig vorteilhafte Weiterbildungen gesteigert werden, wie sie im Folgenden erläutert sind.The performance of the thus improved relay can be increased by various, mutually independently advantageous developments, as explained below.

Falls beispielsweise die dem Joch abgewandte Stirnseite des Kerns eine Polfläche ausbildet, die mit einem beweglichen Anker zusammenwirkt, kann gemäß einer vorteilhaften Weiterbildung der Erfindung der Flächeninhalt der Polfläche erfindungsgemäß größer sein als die Querschnittsfläche im Mittenbereich des Kerns. Durch die vergrößerte Polfläche wirkt ein hoher Magnetfluss auf den Anker, was hohe Schaltkräfte und schnelle Schaltvorgänge gewährleistet.If, for example, the yoke facing away from the end face of the core forms a pole face, which cooperates with a movable armature, according to an advantageous embodiment of the invention, the surface area of the pole face according to the invention be greater than the cross-sectional area in the central region of the core. Due to the enlarged pole surface, a high magnetic flux acts on the armature, which ensures high switching forces and fast switching operations.

Der Kern kann auch in einer Weiterbildung im Bereich des Spulenkörpers verjüngt ausgebildet sein, so dass an beiden Enden der Kerns große Querschnittsflächen für eine Leitung des Magnetflusses mit geringen Verlusten zur Verfügung stehen und gleichzeitig im Bereich der Verjüngung Raum für zusätzliche Wicklungen der vom Spulenkörper gehaltenen Spule bereit gestellt ist.The core can also be tapered in a development in the region of the bobbin, so that at both ends of the core large cross-sectional areas for a line of magnetic flux with low losses are available and at the same time in the region of the taper space for additional windings of the bobbin held by the coil is provided.

Die Montage des Kerns im Spulenkörper kann durch eine Reihe von voneinander unabhängigen Weiterbildungen vereinfacht werden.The assembly of the core in the bobbin can be simplified by a series of independent developments.

Die Kernelemente können nacheinander in den Spurenkörper einsetzbar ausgestaltet sein, so dass trotz der Querschnittserweiterung eine einfache Montage möglich ist, selbst wenn die Querschnittserweiterung des Kerns den Spulenkörper hintergreift.The core elements can be designed to be used successively in the track body, so that in spite of the cross-sectional widening a simple assembly is possible, even if the cross-sectional widening of the core engages behind the bobbin.

Wenigstens zwei Kernelemente können eine Querschnittserweiterung zum Joch hin aufweisen; ferner können wenigstens zwei Kernelemente eine Querschnittserweiterung zur Polfläche aufweisen.At least two core elements may have a cross-sectional widening towards the yoke; Furthermore, at least two core elements may have a cross-sectional widening to the pole face.

Um die Montage des Kerns im Spulenkörper trotz der Querschnittserweiterung zu erleichtern, kann ein Kernelement im Wesentlichen in den Spulenkörper einschiebbar ausgestaltet sein. Insbesondere kann das Kernelement bei bereits in dem Spulenkörper eingelegtem weiteren Kernelement einschiebbar ausgestattet sein.In order to facilitate the assembly of the core in the bobbin despite the cross-sectional widening, a core element can be inserted substantially in the bobbin be designed. In particular, the core element can be fitted in inserted in already inserted in the bobbin further core element.

Die Montage des Kernelements kann ferner dadurch erleichtert werden, dass wenigstens ein Kernelement im Wesentlichen hinterschneidungsfrei ausgestaltet ist bzw. im Wesentlichen quaderförmig ausgestaltet ist. Diese Ausgestaltung erleichtert insbesondere das Einschieben des Kernelements in den Spulenkörper.The assembly of the core element can be further facilitated by the fact that at least one core element is configured substantially free of undercuts or substantially cuboid-shaped. This configuration facilitates in particular the insertion of the core element in the bobbin.

Der Kern kann auch aus einer Vielzahl von quer zur Längserstreckung des Spulenkörpers nebeneinander angeordneten Kernelementen bestehen, durch die Verlustleistungen beim Ein- und/oder Ausschalten des Erregerstroms der Spule minimiert werden. Die Kernelemente können bei dieser Ausgestaltung fest vormontiert sein.The core may also consist of a plurality of transverse to the longitudinal extent of the bobbin juxtaposed core elements are minimized by the power loss when switching on and / or off the excitation current of the coil. The core elements may be permanently pre-assembled in this embodiment.

Ferner kann der Kern oder wenigstens ein Kernelement einstückig mit dem Joch ausgestaltet sein, um die Verluste beim Übergang des magnetischen Flusses vom Kern auf das Joch möglichst gering zu halten und um den Montageaufwand zu verringern.Further, the core or at least one core element may be integrally formed with the yoke to minimize the losses in the transition of the magnetic flux from the core to the yoke and to reduce assembly costs.

Um Spulenkörper und Joch beim Montagevorgang möglichst effizient als einteiliges Modul zusammensetzen zu können, kann bei einem einstückig mit wenigstens einem Kernelement ausgebildeten Joch dieses Kernelement in den Spulenkörper einschiebbar ausgebildet sein. Durch diese Maßnahme wird die Moduleinheit aus Spulenkörper und Joch durch einfaches Einschieben des Jochs in den Spulenkörper fertiggestellt. Lediglich das mit der Querschnittserweiterung versehene Kernelement muss vor dem Einschieben des Kernelements am Joch in den Spulenkörper eingesetzt werden.In order to be able to assemble the bobbin and the yoke as efficiently as possible as a one-piece module during the assembly process, in the case of a yoke formed integrally with at least one core element, this core element can be designed to be insertable into the bobbin. By this measure, the module unit of bobbin and yoke is completed by simply inserting the yoke in the bobbin. Only the core element provided with the cross-sectional widening must be inserted into the bobbin before insertion of the core element on the yoke.

Um die Verluste beim Übergang des Magnetflusses vom Kern zum Joch zu minimieren, kann wenigstens ein Kernelement das Joch wenigstens berühren, so dass die vom Magnetfeld durchsetzten Luftspalte möglichst gering bzw. nicht vorhanden sind.In order to minimize the losses during the transition of the magnetic flux from the core to the yoke, at least one core element can at least touch the yoke, so that the air gaps penetrated by the magnetic field are as small as possible or absent.

Im Folgenden wird die Erfindung anhand verschiedener Ausführungsformen beispielhaft mit Bezug auf die beigefügten Zeichnungen erläutert. Die bei den einzelnen Ausführungsformen unterschiedlichen Merkmale können dabei unabhängig voneinander kombiniert werden, wie dies oben bei den einzelnen vorteilhaften Ausgestaltungen bereits dargelegt wurde.In the following, the invention will be explained with reference to various embodiments by way of example with reference to the accompanying drawings. The different features in the individual embodiments can be combined independently of each other, as has already been set out above in the individual advantageous embodiments.

Es zeigen:

Fig. 1
eine Ausführungsform eines Relais in einer schematischen Perspektivansicht;
Fig. 2
eine Ausführungsform eines Spulenkörpers mit Kern und Joch in einer schematischen Perspektivansicht;
Fig. 3
den Kern und das Joch der Ausführungsform der Fig. 2 in einer schematischen Perspektivansicht;
Fig. 4
eine Ausführungsform eines Kernelements in einer schematischen Perspektivansicht;
Fig. 5
eine weitere Ausführungsform eines Kernelements in einer schematischen Perspektivansicht;
Fig. 6
eine weitere Ausführungsform eines Kernelements in einer schematischen Perspektivansicht;
Fig. 7
eine Ausführungsform eines Spulenkörpers in einer schematischen Perspektivansicht;
Fig. 8
den Spulenkörper der Fig. 7 in einer Ansicht von Pfeil VIII; und
Fig. 9
eine Ausführungsform eines Spulenkörpers mit eingesetztem Kernelement in einer schematischen Perspektivansicht.
Show it:
Fig. 1
an embodiment of a relay in a schematic perspective view;
Fig. 2
an embodiment of a bobbin with core and yoke in a schematic perspective view;
Fig. 3
the core and the yoke of the embodiment of Figure 2 in a schematic perspective view.
Fig. 4
an embodiment of a core element in a schematic perspective view;
Fig. 5
a further embodiment of a core element in a schematic perspective view;
Fig. 6
a further embodiment of a core element in a schematic perspective view;
Fig. 7
an embodiment of a bobbin in a schematic perspective view;
Fig. 8
the bobbin of Figure 7 in a view of arrow VIII. and
Fig. 9
an embodiment of a bobbin with inserted core element in a schematic perspective view.

Zunächst wird der allgemeine Aufbau eines Relais mit Bezug auf die Fig. 1 beschrieben.First, the general structure of a relay will be described with reference to FIG.

Ein Relais 1 weist eine auf einem Spulenkörper 2 aufgewickelte Spule (in Fig. 1 nicht dargestellt), ein Joch 3 und einen den Spulenkörper 2 durchsetzenden Kern (in Fig. 1 nicht dargestellt) auf. Das Joch 3 endet in einer Polfläche 4, die an einen Arbeitsluftspalt 5 grenzt. In anderen Ausgestaltungen kann die Polfläche 4 auch am Kern ausgebildet sein.A relay 1 has a coil wound on a bobbin 2 (not shown in FIG. 1), a yoke 3 and a core passing through the bobbin 2 (not shown in FIG. 1). The yoke 3 terminates in a pole face 4 which adjoins a working air gap 5 borders. In other embodiments, the pole face 4 may also be formed on the core.

Der Arbeitsluftspalt 5 ist zwischen der Polfläche 4 und einem beweglichen Anker 6 angeordnet. Der Anker 6 ist über ein längs des Spulenkörpers 2 geführtes Verbindungselement 7 bewegungsübertragend mit einer Kontaktfeder 8 verbunden, so dass eine Bewegung des Ankers 6 zwangsläufig zu einer Bewegung der Kontaktfeder 8 führt.The working air gap 5 is arranged between the pole face 4 and a movable armature 6. The armature 6 is connected in a motion-transmitting manner with a contact spring 8 via a connecting element 7 guided along the bobbin 2, so that a movement of the armature 6 inevitably leads to a movement of the contact spring 8.

Die Kontaktfeder 8 wiederum ist zwischen zwei voneinander in Bewegungsrichtung der Kontaktfeder beabstandeten Kontakten 9, 10 angeordnet, wobei sie vorzugsweise jeweils nur einen der beiden Kontakte 9, 10 berühren kann. Üblicherweise ist die Kontaktfeder 8 so vorgespannt, dass sie im kraftfreien Zustand gegen einen der Kontakte, beispielsweise dem Kontakt 10, anliegt.The contact spring 8 in turn is arranged between two mutually spaced in the direction of movement of the contact spring contacts 9, 10, wherein they can preferably only one of the two contacts 9, 10 touch. Usually, the contact spring 8 is biased so that it rests in the power-free state against one of the contacts, for example the contact 10.

Wird ein Erregerstrom durch die Spule geleitet, entsteht an der Polfläche 4 eine Magnetkraft, die den Anker 6 anzieht und den Arbeitsluftspalt zu verkleinern sucht. Dadurch bewegt sich der Anker 6 aus seiner Ruhestellung. Über das Verbindungselement 7 wird diese Bewegung auf die Kontaktfeder 8 übertragen. Dadurch bewegt sich die Kontaktfeder 8 ebenfalls aus ihrer Ruhestellung heraus und wird gegen den Kontakt 9 gedrückt.If an exciting current is passed through the coil, a magnetic force is generated at the pole surface 4, which attracts the armature 6 and seeks to reduce the working air gap. As a result, the armature 6 moves from its rest position. About the connecting element 7, this movement is transmitted to the contact spring 8. As a result, the contact spring 8 also moves out of its rest position and is pressed against the contact 9.

Die Kontakte 9, 10 sowie die Kontaktfeder 8 sind jeweils mit nach außerhalb des Relais geführten Kontaktstiften 11, 12, 13 versehen. Die Kontaktstifte 11, 12, 13 können jeweils paarweise vorhanden sein.The contacts 9, 10 and the contact spring 8 are each provided with guided to outside the relay pins 11, 12, 13. The contact pins 11, 12, 13 may each be present in pairs.

Die Kontakte 11, 13 bzw. 11, 12 werden in Abhängigkeit von der Stellung der Kontaktfeder 8 geschlossen. Beispielsweise sind in der in Fig. 1 gezeigten Ruhestellung der Kontaktfeder 8 die Kontakte 11 und 12 über die Kontaktfeder 8 und den Kontakt 11 miteinander verbunden.The contacts 11, 13 and 11, 12 are closed in dependence on the position of the contact spring 8. For example, in the rest position of the contact spring 8 shown in FIG. 1, the contacts 11 and 12 are connected to one another via the contact spring 8 and the contact 11.

Um definierte Kontaktpunkte an den Kontakten 9, 10 und der Kontaktfeder 8 zu schaffen, können Kontaktpillen 14, 15, 16 an den Kontakten 9, 10 und/oder der Kontaktfeder 8 vorgesehen sein.In order to create defined contact points on the contacts 9, 10 and the contact spring 8, contact pills 14, 15, 16 may be provided on the contacts 9, 10 and / or the contact spring 8.

In Fig. 2 ist eine Ausführungsform des Spulenkörpers 2 mit dem Joch 3 und dem die Spule durchsetzenden Kern 17 dargestellt, wobei die Blickrichtung schräg auf die Polfläche 4 gerichtet ist.In Fig. 2, an embodiment of the bobbin 2 with the yoke 3 and the coil passing through the core 17 is shown, wherein the viewing direction is directed obliquely on the pole face 4.

Der Übersicht halber ist die Spule, die vom Spulenkörper 2 in der sich in Umfangsrichtung erstreckenden Ausnehmung 18 gehalten wird, in Fig. 2. weggelassen.For the sake of clarity, the coil which is held by the bobbin 2 in the circumferentially extending recess 18 is omitted in FIG.

Wie in Fig. 2 zu erkennen ist, weist der Kern 17 zwei Kernelemente 19, 20 auf, die quer zur Spulenrichtung senkrecht aufeinander liegen.As can be seen in FIG. 2, the core 17 has two core elements 19, 20 which lie perpendicular to one another perpendicular to the coil direction.

In Längsrichtung des Spulenkörpers 2 ragt der Kern 17 aus dem Spulenkörper 2 hervor.In the longitudinal direction of the bobbin 2, the core 17 protrudes from the bobbin 2.

In Fig. 3 ist das Joch 3 sowie der Kern 17 in der Perspektive der Fig. 2 bei entferntem Spulenkörper 2 dargestellt.In Fig. 3, the yoke 3 and the core 17 is shown in the perspective of FIG. 2 with the bobbin 2 removed.

Es ist zu erkennen, dass das eine Kernelement 20 einstückig mit dem Joch 3 ausgebildet ist, während das andere Kernelement 19 am Joch 3 und am Kern 20 anliegt. Zum Anker hin, an der Stirnfläche 21 des Kerns 17, schließen beide Kernelemente 19, 20 bündig ab, um eine im Wesentlichen ebene Stirnfläche 21 zu bilden, die auch als Polfläche 4 dienen kann.It can be seen that the one core element 20 is formed integrally with the yoke 3, while the other core element 19 rests against the yoke 3 and the core 20. Towards the armature, on the end face 21 of the core 17, both core elements 19, 20 terminate flush to form a substantially flat end face 21, which can also serve as a pole face 4.

Eines der Kernelemente 19, 20, bei der Ausführungsform der Fig. 3 das einstückig mit dem Joch ausgebildete Kernelement 20, ist im Wesentlichen quaderförmig und weist keine Vorsprünge und/oder Hinterschneidungen auf.One of the core elements 19, 20, in the embodiment of FIG. 3, the core element 20 formed integrally with the yoke, is substantially cuboid and has no projections and / or undercuts.

Das andere, separate Kernelement 19 ist in Längsrichtung L der Spule an den jeweiligen Endflächen mit Querschnittserweiterungen 22, 23 versehen. Die Querschnittserweiterungen 22, 23 hintergreifen den Spulenkörper 2.The other, separate core element 19 is provided in the longitudinal direction L of the coil at the respective end faces with cross-sectional widenings 22, 23. The cross-sectional widenings 22, 23 engage behind the bobbin 2.

Im Mittenbereich des Kerns 17, der vom Spulenkörper 2 umgeben ist, ist der Querschnitt des Kerns gegenüber den beiden in Längsrichtung des Spulenkörpers gelegenen Endbereichen verringert. Dadurch entsteht eine Ausnehmung 25, die als zusätzlicher Wickelraum für die Spule verwendet werden kann, so dass die Spule eine höhere Wicklungszahl und/oder -dichte aufweist.In the center region of the core 17, which is surrounded by the bobbin 2, the cross section of the core is reduced in relation to the two end regions located in the longitudinal direction of the bobbin. This results in a recess 25 which can be used as an additional winding space for the coil, so that the coil has a higher winding number and / or density.

Falls der Kern 17 nicht an den Arbeitsluftspalt 5 des Relais 1 grenzt, kann auch auf die Querschnittserweiterung 23 verzichtet werden, obwohl dadurch der Fluss des Magnetfeldes vom Kern in den Anker beeinträchtigt wird; natürlich kann auch die vom Joch 3 gebildete Polfläche 4 eine Querschnittserweiterung aufweisen.If the core 17 does not adjoin the working air gap 5 of the relay 1, the cross-sectional widening 23 can also be dispensed with, although this impairs the flow of the magnetic field from the core into the armature; Of course, the pole face 4 formed by the yoke 3 may have a cross-sectional widening.

Wie in Fig. 3 ferner zu erkennen ist, erstreckt sich die Trennebene 26 zwischen den beiden Kernelementen 19, 20 in Längsrichtung L der Spule parallel zum Joch 3. An der Trennebene 26, wie auch an der Anschlagsfläche 27 zwischen der Querschnittserweiterung 22 und dem Joch 3, sind die aufeinander liegenden Flächen möglichst plan und glatt ausgebildet. Dadurch werden Luftspalte in den Übergangsbereichen und Verluste im magnetischen Fluss vermieden.As can also be seen in FIG. 3, the dividing plane 26 extends between the two core elements 19, 20 in the longitudinal direction L of the coil parallel to the yoke 3. At the parting plane 26, as well as at the abutment surface 27 between the cross-sectional widening 22 and the yoke 3, the superposed surfaces are as flat and smooth as possible. This avoids air gaps in the transition areas and losses in the magnetic flux.

In den Figuren 4 bis 6 sind weitere Ausführungsformen des Kernelements 20 dargestellt. Bei all diesen Kernelementen 20 ist der Querschnitt an den beiden in Längsrichtung liegenden Enden 22, 23 in einer Querschnittsebene senkrecht zur Längsrichtung L der Spule erweitert.FIGS. 4 to 6 show further embodiments of the core element 20. In all of these core elements 20, the cross-section at the two longitudinal ends 22, 23 is widened in a cross-sectional plane perpendicular to the longitudinal direction L of the coil.

Die Querschnittsebene Q ist in Fig. 4 einmal im Mittenbereich als Querschnittsebene Q1 und einmal im Endbereich als Querschnittsebene Q2 schematisch eingezeichnet. Wie zu erkennen ist, ist der Flächeninhalt des Querschnitts Q2 größer als der Flächeninhalt des Querschnitts Q1.The cross-sectional plane Q is shown schematically in FIG. 4 once in the middle region as a cross-sectional plane Q 1 and once in the end region as a cross-sectional plane Q 2 . As can be seen, the surface area of the cross section Q 2 is greater than the area of the cross section Q 1 .

Das Kernelement 19 der Fig. 4 ist rationell aus einem Stück gefertigt und weist umgebogene Enden 22, 23 auf. Durch eine sich über die gesamte Breite des Kernelements 19 erstreckende Aussparung 28 in der Nähe des Biegeradius 29 wird der Biegevorgang erleichtert.The core element 19 of FIG. 4 is efficiently manufactured in one piece and has bent ends 22, 23. By a over the entire width of the core member 19 extending recess 28 in the vicinity of the bending radius 29 of the bending process is facilitated.

In Fig. 5 ist ein Kernelement 19 dargestellt, das aus mehreren Einzelelementen 19a, 19b, ..., die nebeneinander angeordnet sind, aufgebaut ist. Die Anzahl der nebeneinander angeordneten und sich vorzugsweise berührenden Kernelemente 19a, 19b, ... ist beliebig, in Fig. 5 sind lediglich beispielhaft vier nebeneinander liegende Elemente gezeigt. Die Querschnittsflächen bzw. Konturen der einzelnen Kernelemente 19a, 19b, ... in einer in Längsrichtung L liegenden Ebene sind gleich. Um das Kernelement 19 in der Ausführungsform der Fig. 5 einfach handhaben zu können, sind die Kernelemente 19a, 19b, ... miteinander einteilig verbunden, beispielsweise verklebt, verlötet oder verschweißt.In Fig. 5, a core member 19 is shown, which is composed of a plurality of individual elements 19a, 19b, ..., which are arranged side by side. The number of juxtaposed and preferably touching core elements 19a, 19b,... Is arbitrary; in FIG. 5, four adjacent elements are shown by way of example only. The cross-sectional areas or contours of the individual core elements 19a, 19b,... In a plane lying in the longitudinal direction L are the same. To the core element 19 in the 5 easy to handle embodiment, the core elements 19a, 19b, ... integrally connected to each other, for example, glued, soldered or welded.

Bei der Ausführungsform der Fig. 6 handelt es sich um ein geprägtes Teil aus einem Metallwerkstoff, bei dem die beiden Querschnittserweiterungen 22, 23 in Form von in Längsrichtung L der Spule schräg verlaufenden, eingeprägten Rampen ausgestaltet sind. Alternativ kann das Kernelement 19 auch durch Spritzguss hergestellt werden.In the embodiment of Fig. 6 is an embossed part of a metal material, in which the two cross-sectional extensions 22, 23 in the form of obliquely extending in the longitudinal direction L of the coil, embossed ramps are configured. Alternatively, the core element 19 can also be produced by injection molding.

In Fig. 7 ist der Spulenkörper 2 dargestellt, wobei der Kern 17 und das Joch 3 weggelassen sind. Der Spulenkörper 2 weist einen sich in Längsrichtung L der Spule erstreckenden Durchlass 30 auf, der an beiden Seiten offen ist.In Fig. 7, the bobbin 2 is shown, wherein the core 17 and the yoke 3 are omitted. The bobbin 2 has a passage 30 extending in the longitudinal direction L of the bobbin, which is open on both sides.

Im mittleren Bereich 31 des Spulenkörpers 2, der mit der Ausnehmung 18 für die Spule im Wesentlichen zusammenfällt, ist der lichte Querschnitt in einer Ebene senkrecht zur Längsrichtung L des Durchlasses 30 verringert, um Platz für zusätzliche Spulenwicklungen zu schaffen. Zu den beiden Enden des Spulenkörpers 2 hin erweitert sich der Durchlass 30 in einem Bereich 32. Die Form des Bereichs 32 ist dabei an die Form der jeweiligen Querschnittserweiterung 22, 23 angepasst, so dass das Kernelement 19 mit den Querschnittserweiterungen 22, 23 im Durchlass 30 aufgenommen werden kann. Der Querschnitt des Durchlasses 30 ist an seiner kleinsten Stelle so bemessen, dass die Querschnittserweiterung 22 des Kernelements 19 noch durch den Durchlass 30 hindurch gesteckt werden kann. Im eingesetzten Zustand hintergreifen die Querschnittserweiterungen 22, 23 den Spulenkörper 2, so dass das Kernelement 19 im Wesentlichen unverschieblich vom Spulenkörper gehalten ist.In the middle region 31 of the bobbin 2, which substantially coincides with the recess 18 for the coil, the clear cross section in a plane perpendicular to the longitudinal direction L of the passage 30 is reduced to make room for additional coil windings. The shape of the region 32 is adapted to the shape of the respective cross-sectional widening 22, 23, so that the core element 19 with the cross-sectional widenings 22, 23 in the passage 30 can be included. The cross-section of the passage 30 is dimensioned at its smallest point so that the cross-sectional widening 22 of the core element 19 can still be inserted through the passage 30. When inserted, the cross-sectional widenings 22, 23 engage behind the bobbin 2, so that the core element 19 is held substantially immovably by the bobbin.

Wie in Fig. 8, in der der Spulenkörper 2 der Fig. 7 in Blickrichtung VIII dargestellt ist, zu erkennen ist, kann die Querschnittserweiterung des Durchlasses 30 an den beiden offenen Enden unterschiedlich ausgestaltet sein, um beispielsweise an dem einen Ende einen bündigen Abschluss des Kerns mit dem Spulenkörper 2 und an dem anderen Ende ein Herausragen des Kerns 17 zu ermöglichen.As can be seen in Fig. 8, in which the bobbin 2 of Fig. 7 is shown in the direction of view VIII, the cross-sectional widening of the passage 30 at the two open ends can be designed differently, for example, at one end a flush termination of Kerns with the bobbin 2 and at the other end to allow the core 17 to protrude.

Der Durchlass 30 ist so ausgestaltet, dass bei eingelegtem Kernelement 19 mit Querschnittserweiterungen 22 bzw. 23 ein sich durch den Spulenkörper 2 hindurch erstreckender Freiraum 33 von im Wesentlichen konstanter lichter Weite verbleibt. In den Freiraum 33 kann das andere Kernelement 20 nach Einsetzen des jeweiligen anderen Kernelements 19 eingeschoben werden. Durch die Querschnittserweiterungen 22, 23 gehalten, kann das eine Kernelement 19 nicht mehr aus dem Durchlass 30 entfernt werden, solange das andere Kernelement 20 eingesetzt ist. Durch einen Presssitz des Kernelements 20 kann der Kern fest im Spulenkörper gehalten sein. Hierzu ist der Querschnitt des Kernelements 20 etwas größer als der Querschnitt des Freiraums 33.The passage 30 is designed so that when inserted core element 19 with cross-sectional extensions 22 and 23 extending through the bobbin 2 therethrough Free space 33 remains of substantially constant clear width. In the free space 33, the other core element 20 can be inserted 19 after insertion of the respective other core element. Held by the cross-sectional widenings 22, 23, the one core element 19 can no longer be removed from the passage 30 as long as the other core element 20 is inserted. By a press fit of the core member 20, the core can be held firmly in the bobbin. For this purpose, the cross section of the core element 20 is slightly larger than the cross section of the free space 33.

Im Folgenden wird kurz der Montagevorgang eines erfindungsgemäßen Relais beschrieben.In the following, the assembly process of a relay according to the invention will be briefly described.

Zunächst wird in das Relais das Kernelement 19 eingesetzt, das mit wenigstens einer Querschnittserweiterung 22, 23 versehen ist. Sobald die Querschnittserweiterungen 22, 23 in die ihm zugeordnete Erweiterung 32 des Durchlasses aufgenommen ist, wird das andere Kernelement 20 in den freibleibenden Raum 33 eingeschoben.First, in the relay, the core element 19 is used, which is provided with at least one cross-sectional widening 22, 23. As soon as the cross-sectional enlargements 22, 23 are received in the extension 32 of the passage assigned to it, the other core element 20 is inserted into the remaining free space 33.

Je nachdem, ob die Querschnittserweiterungen 22, 23 einstückig am Joch 3 oder am separaten Kernelement 19 ausgebildet sind, wird zunächst das Joch 3 oder das Kernelement 19 in den Durchlass 30 gesetzt. Anschließend wird das im Wesentlichen quäderförmige Kernelement 20 eingeschoben.Depending on whether the cross-sectional widenings 22, 23 are formed integrally on the yoke 3 or on the separate core element 19, first the yoke 3 or the core element 19 is placed in the passage 30. Subsequently, the substantially quäderförmige core element 20 is inserted.

Claims (11)

  1. A relay (1) having a coil former (2), a core (17) passing through the coil former (2) and a yoke (3), the cross-sectional area (Q2) of the core (17) being larger in the area of transition to the yoke (3) and at the end face of the core (17) remote from the yoke (3) than in the central area (31) of the core (17) surrounded by the coil former (2), characterised in that the core (17) is formed of at least two core elements (19, 20; 19a, 19b, ...).
  2. A relay (1) according to claim 1, characterised in that the core (17) is of tapered configuration in the area of the coil former (2).
  3. A relay (1) according to claim 1 or claim 2, characterised in that one core element (20) is configured to be substantially insertable into the coil former (2).
  4. A relay (1) according to any one of the preceding claims, characterised in that one core element (20) is configured to be substantially free of undercuts.
  5. A relay (1) according to any one of the preceding claims, characterised in that the yoke (3) is in one piece with one of the core elements (19, 20).
  6. A relay (1) according to any one of the preceding claims, characterised in that the core element (19, 20) provided in one piece on the yoke (3) is substantially cuboid in configuration.
  7. A relay (1) according to any one of the preceding claims, characterised in that the core element (19, 20) provided in one piece on the yoke (3) is configured to be insertable when a further core element (19, 20) has already been introduced into the coil former (2).
  8. A relay (1) according to any one of the preceding claims, characterised in that at least two core elements (19, 20; 19a, 19b, etc.) are provided, whose cross-section (Q2) is configured to widen towards the yoke (3).
  9. A relay (1) according to any one of the preceding claims, characterised in that at least two core elements (19, 20; 19a, 20a, etc.) are provided, whose cross-section (Q2) is configured to widen towards the pole face (4).
  10. A relay (1) according to any one of the preceding claims, characterised in that the at least one core element (19, 20) is in contact with the yoke (3).
  11. A relay (1) according to any one of the preceding claims, characterised in that the at least one cross-sectionally widened portion (22, 23) of the core (17) engages behind the coil former (2).
EP03005059A 2003-03-06 2003-03-06 Relay with core having partly enlarged cross section Expired - Lifetime EP1455372B1 (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
EP03005059A EP1455372B1 (en) 2003-03-06 2003-03-06 Relay with core having partly enlarged cross section
AT03005059T ATE328359T1 (en) 2003-03-06 2003-03-06 RELAY WITH EXTENDED CROSS SECTION CORE
DE50303564T DE50303564D1 (en) 2003-03-06 2003-03-06 Relay with cross-sectional widened core
ES03005059T ES2266657T3 (en) 2003-03-06 2003-03-06 RELAY WITH NUCLEO OF CROSS SECTION AGRANDADA.
US10/786,407 US7026896B2 (en) 2003-03-06 2004-02-25 Relay with a core having an enlarged cross-section
JP2004052797A JP4462536B2 (en) 2003-03-06 2004-02-27 relay
CNB2004100077175A CN100367434C (en) 2003-03-06 2004-03-05 Relays with cores with enlarged cross-section

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP03005059A EP1455372B1 (en) 2003-03-06 2003-03-06 Relay with core having partly enlarged cross section

Publications (2)

Publication Number Publication Date
EP1455372A1 EP1455372A1 (en) 2004-09-08
EP1455372B1 true EP1455372B1 (en) 2006-05-31

Family

ID=32798789

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Application Number Title Priority Date Filing Date
EP03005059A Expired - Lifetime EP1455372B1 (en) 2003-03-06 2003-03-06 Relay with core having partly enlarged cross section

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Country Link
US (1) US7026896B2 (en)
EP (1) EP1455372B1 (en)
JP (1) JP4462536B2 (en)
CN (1) CN100367434C (en)
AT (1) ATE328359T1 (en)
DE (1) DE50303564D1 (en)
ES (1) ES2266657T3 (en)

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Publication number Priority date Publication date Assignee Title
US7495535B2 (en) 2006-03-30 2009-02-24 Tyco Electronics Austria Gmbh Magnet system with H-shaped armature for a relay

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Publication number Priority date Publication date Assignee Title
DE102007048710B4 (en) * 2007-10-11 2014-02-13 Tyco Electronics Austria Gmbh Electrical cross connector
JP4803206B2 (en) * 2008-04-24 2011-10-26 パナソニック電工株式会社 Electromagnet for relay
DE102018109856B3 (en) * 2018-04-24 2019-08-01 Phoenix Contact Gmbh & Co. Kg relay
EP3570302B8 (en) * 2018-05-18 2021-08-04 Tyco Electronics Austria GmbH Yoke assembly for a magnetic switching device, such as a relay, magnetic assembly, and magnetic switching device

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US2539547A (en) * 1945-06-13 1951-01-30 Clare & Co C P Relay
FR1543930A (en) * 1966-10-13 1968-10-31 Soprotekel Method of fixing magnetic cores in relays or pole pieces
US4720694A (en) 1985-05-22 1988-01-19 Siemens Aktiengesellschaft Electromagnetic relay
EP0363176B1 (en) 1988-10-07 1996-02-14 International Business Machines Corporation Word organised data processors
CH677162A5 (en) * 1989-10-30 1991-04-15 Carlo Cavazzi Electromatic Ag
AT402579B (en) 1991-10-07 1997-06-25 Schrack Components Ag RELAY
AT410856B (en) 1994-07-08 2003-08-25 Tyco Electronics Austria Gmbh RELAY
AT410724B (en) * 1994-10-10 2003-07-25 Tyco Electronics Austria Gmbh RELAY
JP3333898B2 (en) * 1996-07-03 2002-10-15 富士電機株式会社 Electromagnetic contactor
DE19847831C2 (en) * 1998-10-16 2002-11-21 Tyco Electronics Austria Gmbh safety relay
CN1269167C (en) * 2002-08-21 2006-08-09 厦门宏发电声有限公司 Miniaturized great-power electromagnetic relay with upper and lower variable-section cavities

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Publication number Priority date Publication date Assignee Title
US7495535B2 (en) 2006-03-30 2009-02-24 Tyco Electronics Austria Gmbh Magnet system with H-shaped armature for a relay

Also Published As

Publication number Publication date
ATE328359T1 (en) 2006-06-15
DE50303564D1 (en) 2006-07-06
CN100367434C (en) 2008-02-06
ES2266657T3 (en) 2007-03-01
CN1551272A (en) 2004-12-01
JP2004342589A (en) 2004-12-02
JP4462536B2 (en) 2010-05-12
US7026896B2 (en) 2006-04-11
EP1455372A1 (en) 2004-09-08
US20040227600A1 (en) 2004-11-18

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