EP0736882A1 - Control device for electromagnet with core without friction and application for valves with continuous control - Google Patents

Control device for electromagnet with core without friction and application for valves with continuous control Download PDF

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Publication number
EP0736882A1
EP0736882A1 EP96420115A EP96420115A EP0736882A1 EP 0736882 A1 EP0736882 A1 EP 0736882A1 EP 96420115 A EP96420115 A EP 96420115A EP 96420115 A EP96420115 A EP 96420115A EP 0736882 A1 EP0736882 A1 EP 0736882A1
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EP
European Patent Office
Prior art keywords
core
axial
blades
flexible
magnetic field
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EP96420115A
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German (de)
French (fr)
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EP0736882B1 (en
Inventor
Jean-Claude Maury
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APPAREILLAGES ELECTRO-MECANIQUES DU FAUCIGNY
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APPAREILLAGES ELECTRO-MECANIQUES DU FAUCIGNY
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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
    • H01F7/1607Armatures 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
    • H01F2007/083External yoke surrounding the coil bobbin, e.g. made of bent magnetic sheet

Definitions

  • the present invention relates to control devices of the electromechanical transducer type, in which an electromagnet transforms an electrical control signal into a displacement or a force applied to a sliding core.
  • the electromagnet comprises a fixed armature, integral with the frame of the device in which the electromagnet is inserted.
  • the armature made of material sensitive to the magnetic field, comprises an axial channel in which axially slides a generally cylindrical core made of material sensitive to the magnetic field.
  • the core slides in a first magnetic pole with a radial air gap, the second pole closing the axial channel and defining with the core a variable axial air gap.
  • An electrical coil connectable to an external source of electrical energy, generates in the armature, and in particular in the axial channel between the two poles of the armature, a magnetic field tending to drive the core in axial sliding in the channel axial along the longitudinal axis.
  • the core In its sliding, the core is guided by two elements with flexible radial blades comprising a peripheral part fixedly mounted on the fixed frame and connected by said flexible radial blades to a central part integral with the sliding core, to keep the core apart walls of the axial channel while allowing its axial displacement in an appropriate stroke between a first and a second extreme axial positions.
  • the two elements with flexible radial blades are arranged on the same side of the axial channel, or inside the axial channel. This results in a relatively complex construction, as well as a relatively small stroke of the sliding core between the extreme axial positions.
  • the problem proposed by the present invention is to design a new structure of control devices with electromagnet and sliding core, which is of simpler construction, which allows a greater axial stroke of the sliding core between its axial positions extremes, in order to better control the forces and strokes for better progressiveness of the control device as a function of the electric current flowing through the electric winding.
  • the axial guide means comprise two elements with flexible blades offset axially on the core, to the exclusion of any guide sliding in the axial channel.
  • the flexible blades have, in the first extreme axial position in the absence of a magnetic field produced by the fixed armature, a permanent deformation in bending in the direction of the axial displacement of the core in a first direction, the magnetic field causing the displacement of the core in the opposite direction to said first direction.
  • the flexible blades of at least one of the elements with flexible blades are substantially flat. This arrangement makes it possible to ensure better radial rigidity, to guarantee a more effective retention of the core in the position in which the magnetic field is maximum, preventing the magnetic forces from pressing the core radially against one of the magnetic poles.
  • a control device with an electromagnet and a sliding core comprises a fixed armature 1, provided with an electric coil 7 and an axial channel 3 which runs right through the electrical winding 7.
  • the fixed frame 1 is integral with the frame 2 of the device in which it is arranged.
  • a core 4 is slidably mounted in the axial channel 3.
  • the frame 1 made of a material sensitive to the magnetic field, is formed of a peripheral stirrup 9 the ends of which are folded radially inwards to form end flanges 10 and 11 each connecting to a first coaxial tubular element 5 and a second coaxial tubular element 6, respectively forming a first pole 5 and a second pole 6 of the armature 1.
  • the frame 1 may consist of one or more assembled parts, comprising for example two opposite side members forming a double stirrup 9 while being connected by the end flanges 10 and 11.
  • the poles 5 and 6 are shaped so that their respective inner faces 12 and 13 are opposite the core 4 and separated from the latter by a generally radial air gap of small thickness.
  • the winding 7 is adapted so that, when an electric current flows through it, it produces a magnetic field in the axial channel 3 between the poles 5 and 6. Under the action of the magnetic field, the core 4 tends to move axially sliding in the axial channel 3 in the direction producing the reduction of the air gaps.
  • the core 4 is made of a material sensitive to the magnetic field, and it is guided in sliding in the axial channel 3 by guide means capable of allowing its sliding without introducing friction opposing this sliding.
  • the guide means according to the invention comprise a first element 14 with flexible radial blades, and a second element 15 with flexible radial blades, arranged respectively on either side of the ends of the axial channel 3, at a sufficient distance from the armature 1 to allow the free bending of the flexible radial blades during the axial sliding of the core 4.
  • Each element with flexible radial blades such as the element 14 comprises a peripheral part 16 mounted fixed relative to the fixed frame 1, that is to say integral with either the fixed frame 1 or directly from the frame 2 of the 'apparatus.
  • the element 14 with flexible radial blades has a central part 17 integral with the sliding core 4.
  • the peripheral part 16 is connected to the central part 17 by flexible radial blades 18.
  • the flexible radial blades 18 are arranged to have great flexibility in the direction of axial sliding of the core as represented by arrow 19, and to simultaneously exhibit great rigidity in the direction of the radial movements of the core 4, so as to maintain the core 4 away from the walls of the axial channel 3, and in particular from the poles 5 and 6, while allowing its axial displacement along the axis II according to an appropriate stroke.
  • the flexibility of the blades 18 is chosen so that the appropriate stroke can be suitable for a possible displacement of the core 4 between two extreme axial control positions illustrated respectively in FIGS. 1 or 7 and 2 or 8.
  • the core 4 is held by the two elements 14 and 15 with flexible blades offset axially on the core 4, to the exclusion of any sliding guide in the axial channel 3.
  • At least three flexible blades are regularly provided at the periphery of the central part 17 of element 14.
  • the flexible blades 18 are flat blades, widened in the transverse plane, and of reduced thickness in the axial direction of the core 4.
  • the flexible blades comprise three blades, respectively 180, 181 and 182, having a general shape in a spiral around the longitudinal axis of the core.
  • each of the three flexible blades such as the blade 180 also comprises two portions in an arc of a circle, 184 and 185 respectively, connecting one to the other by the generally radial portion 188, and connecting respectively to the peripheral ring 16 by the generally radial portion 186 and to the central ring 17 by the generally radial portion 187.
  • the respective flexible blades 18 of the elements 14 and 15 with flexible blades are wound in the same direction around the longitudinal axis I-I of the device.
  • the flexible blades of the elements 14 and 15 impart to the core 4, simultaneously with its axial translation, a slight rotation around the longitudinal axis I-I, promoting a harmonious deformation of the flexible blades 18.
  • the elements with flexible blades such as the element 14 can be made from a flat disc of steel or other material, from which are cut openings to form the flexible blades as shown.
  • the elements 14 and 15 with flexible radial blades 18 can advantageously have a diameter significantly greater than that of the axial channel 3.
  • the peripheral ring 16 elements 14 and 15 can be fixed directly to the frame 2, thus having a diameter at least equal to the outside diameter of the frame 1. This thus favors the possibilities of bending of the flexible blades, in order to increase the admissible axial travel of the core 4.
  • Figures 1 and 7 illustrate a device according to the invention in a first extreme axial position.
  • the flexible blades 18 in the absence of a magnetic field produced by the fixed armature 1, the flexible blades 18 have a permanent bending deformation in the direction II of axial displacement of the core 4 in a first direction 20.
  • the core 4 is relatively far from the second pole 6 of the frame 1.
  • the permanent bending deformation of the flexible blades 18 in the first extreme axial position can result from a preforming of the flexible blades 18.
  • the permanent bending deformation of the flexible blades 18 in the first extreme axial position may result from the thrust of an axial spring 31 urging the core 4 towards its first extreme axial position.
  • the core 4 moves axially in the direction 19 opposite to said first direction 20 until in a second extreme axial position as illustrated on Figures 2 and 8, position in which the core 4 has approached the second pole 6 of the frame 1.
  • the elements 14 and 15 with flexible blades are deformed as illustrated in Figure 2, by bending flexible blades 18 of each element. It is noted that, between the two extreme positions illustrated in FIGS. 1 or 7 and 2 or 8, the core 4 can move while remaining permanently away from the poles 5 and 6 of the armature 1, so that 'No friction disturbs the axial movement of the core 4.
  • the flexible blades 18 of at least one of the elements 14 and 15 with flexible blades are substantially flat, that is to say in a plane generally perpendicular to axis II of the device.
  • the two elements 14 and 15 are substantially flat. This improves the radial rigidity of the blades in this second extreme axial position where the core undergoes maximum mechanical stress under the effect of the maximum magnetic field generated by the coil 7.
  • the first end of the core 4 is cylindrical, and slides in the first pole 5 whose respective inner surface 12 is cylindrical.
  • the first pole 5 defines with the core 4 a first constant radial air gap, independent of the axial position of the core 4 in the axial channel 3.
  • the second end of the core 4 is shaped as a cone 22, to cooperate with a corresponding conical part 23 of the second pole 6 in which it engages.
  • the second pole 6 thus defines with the core 4 a second radial air gap which decreases as a function of the axial displacement of the core 4 from the first to the second extreme axial position.
  • the axial displacement of the core 4 progressively modifies the air gap 21 between the cone 22 of the core 4 and the conical part 23 of the pole 6. It is thus possible to produce a progressive movement of the core in the presence of the magnetic field generated by the coil 7.
  • the first pole 5 also has a cylindrical interior surface defining a first constant air gap, as in the previous embodiments.
  • the second pole 6 has a cylindrical interior surface, and cooperates with a portion of core 4 of variable diameter, defining a second variable radial air gap.
  • Another alternative may consist in the presence of two poles 5 and 6 with cylindrical interior surfaces opposite cylindrical parts of core 4, defining two constant radial air gaps independent of the axial position of core 4.
  • the control device can be associated with shutter means, to constitute a continuously electrically controlled valve.
  • the core 4 carries or constitutes by itself a closure element making it possible to modify the open section of a fluid conduction channel as a function of the axial position of the core 4 in the frame 1.
  • FIG. 3 represents an embodiment of such a continuously electrically controlled valve, comprising an electromagnet control device identical to that of FIGS. 1 and 2, in which the same elements have been identified by the same reference numerals .
  • FIGS. 7 and 8 show another embodiment of such a continuously electrically controlled valve.
  • the core 4 carries a shutter element 24 coaxial of revolution which is received in the opening 25 of a seat 26 coaxial with a fluid conduction conduit.
  • the closure element 24 advantageously has a shape of revolution tapering progressively towards its end 27, so that the closure element 24 produces a continuous variation of the open section of the fluid conduction conduit as a function of the position axial of the core 4 and of the closure element 24 in the seat 26.
  • An elastomer seal 28 can be interposed between a front facet 29 of the seat 26 and a front facet 30 of the closure element 24, to ensure a sealed closure when the device is in the first extreme axial position illustrated in FIGS. 1, 3 and 7.
  • the core 4 is biased in axial translation by elastic means such as a compression spring 31, pushing it towards its first extreme axial position shown in FIGS. 1, 3 and 7, against the bias exerted by the field magnetic generated by the winding 7.
  • the spring 31 must have a return force greater than the axial force possibly exerted by the elements 14 and 15 with flexible blades, and less than the axial stress produced on the core by the magnetic field generated by the winding 7.
  • the core 4 made of magnetic material occupies only part of the length of the axial channel 3. Its first end, fixed to the first element 14 with flexible blades, has an axial extension 40 force-fitted in a corresponding axial bore of the part forming the closure element 24.
  • the second end of the axial core 4 has a diameter which is slightly reduced, and comprises a threaded axial bore 41 into which a tie rod 42 for connection with the second element 15 with flexible blades.
  • a barrel 43 is engaged on the tie rod 42 between the second end of the axial core 4 and a first face of the central part of the second element 15 with flexible blades.
  • a nut 44 is screwed onto the end of the tie rod 42 and comes to bear on the other face of the central part of the second element 15 with elastic blades.
  • the spring 31 is a compression spring engaged between the nut 44 and an end flange 45 of the frame 2.
  • the invention finds in particular applications in the control of gas flow.

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  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Magnetically Actuated Valves (AREA)
  • Reciprocating, Oscillating Or Vibrating Motors (AREA)
  • Valve Device For Special Equipments (AREA)
  • Vehicle Body Suspensions (AREA)

Abstract

The electromagnetic transducer drives an inner hub (4) laterally. The hub has a rear chamfer with shoulders on the armature channel holding it in place in the rest position. The armature (2) has electrical winding mounted coaxially around the hub centre. The hub is attached to a front and rear flexible section (14,15) covering the front and rear of the armature. The magnetic field moves the hub forward, displacing the flexible section.

Description

La présente invention concerne les dispositifs de commande de type transducteur électromécanique, dans lesquels un électroaimant transforme un signal électrique de commande en un déplacement ou une force s'appliquant sur un noyau coulissant.The present invention relates to control devices of the electromechanical transducer type, in which an electromagnet transforms an electrical control signal into a displacement or a force applied to a sliding core.

On connaît de tels dispositifs de commande à électroaimant à noyau coulissant, tels que ceux décrits dans les documents US-A-4 954 799, FR-A-1 053 825, US-A-4 463 332. Dans un tel dispositif, l'électroaimant comprend une armature fixe, solidaire du bâti de l'appareil dans lequel est inséré l'électroaimant. L'armature, en matériau sensible au champ magnétique, comprend un canal axial dans lequel coulisse axialement un noyau généralement cylindrique en matériau sensible au champ magnétique. Le noyau coulisse dans un premier pôle magnétique avec un entrefer radial, le second pôle obturant le canal axial et définissant avec le noyau un entrefer axial variable. Un bobinage électrique, connectable à une source extérieure d'énergie électrique, génère dans l'armature, et en particulier dans le canal axial entre les deux pôles de l'armature, un champ magnétique tendant à entraîner le noyau en coulissement axial dans le canal axial le long de l'axe longitudinal.Such control devices with a sliding core electromagnet are known, such as those described in the documents US-A-4,954,799, FR-A-1,053,825, US-A-4,463,332. In such a device, the electromagnet comprises a fixed armature, integral with the frame of the device in which the electromagnet is inserted. The armature, made of material sensitive to the magnetic field, comprises an axial channel in which axially slides a generally cylindrical core made of material sensitive to the magnetic field. The core slides in a first magnetic pole with a radial air gap, the second pole closing the axial channel and defining with the core a variable axial air gap. An electrical coil, connectable to an external source of electrical energy, generates in the armature, and in particular in the axial channel between the two poles of the armature, a magnetic field tending to drive the core in axial sliding in the channel axial along the longitudinal axis.

Dans son coulissement, le noyau est guidé par deux éléments à lames radiales flexibles comportant une partie périphérique montée fixe sur l'armature fixe et reliée par lesdites lames radiales flexibles à une partie centrale solidaire du noyau coulissant, pour maintenir le noyau à l'écart des parois du canal axial tout en autorisant son déplacement axial selon une course appropriée entre une première et une seconde positions axiales extrêmes. Dans ces documents antérieurs, par le fait que le second pôle obture le canal axial, les deux éléments à lames radiales flexibles sont disposés d'un même côté du canal axial, ou à l'intérieur du canal axial. Il en résulte une construction relativement complexe, ainsi qu'une course relativement réduite du noyau coulissant entre les positions axiales extrêmes.In its sliding, the core is guided by two elements with flexible radial blades comprising a peripheral part fixedly mounted on the fixed frame and connected by said flexible radial blades to a central part integral with the sliding core, to keep the core apart walls of the axial channel while allowing its axial displacement in an appropriate stroke between a first and a second extreme axial positions. In these previous documents, by the fact that the second pole closes the axial channel, the two elements with flexible radial blades are arranged on the same side of the axial channel, or inside the axial channel. This results in a relatively complex construction, as well as a relatively small stroke of the sliding core between the extreme axial positions.

Le problème proposé par la présente invention est de concevoir une nouvelle structure de dispositifs de commande à électroaimant et noyau coulissant, qui soit de construction plus simple, qui autorise une course axiale plus importante du noyau coulissant entre ses positions axiales extrêmes, afin de mieux maîtriser les efforts et les courses pour une meilleure progressivité du dispositif de commande en fonction du courant électrique traversant le bobinage électrique.The problem proposed by the present invention is to design a new structure of control devices with electromagnet and sliding core, which is of simpler construction, which allows a greater axial stroke of the sliding core between its axial positions extremes, in order to better control the forces and strokes for better progressiveness of the control device as a function of the electric current flowing through the electric winding.

Pour atteindre ces objets ainsi que d'autres, un dispositif de commande à électroaimant à noyau coulissant selon l'invention comprend :

  • une armature fixe, munie d'un bobinage électrique et d'un canal axial, générant dans ledit canal axial, entre un premier pôle et un second pôle, un champ magnétique lors du passage d'un courant électrique dans son bobinage,
  • un noyau mobile sensible au champ magnétique, entraîné en coulissement axial dans ledit canal axial par ledit champ magnétique et guidé par au moins deux éléments à lames radiales flexibles comportant une partie périphérique montée fixe par rapport à l'armature fixe et reliée par lesdites lames radiales flexibles à une partie centrale solidaire du noyau coulissant, pour maintenir le noyau à l'écart des parois du canal axial tout en autorisant son déplacement axial selon une course appropriée entre une première et une seconde positions axiales extrêmes ; en outre :
  • le canal axial traverse de part en part le bobinage électrique,
  • les éléments à lames radiales flexibles sont disposés respectivement de part et d'autre des extrémités du canal axial.
To achieve these and other objects, a sliding-core electromagnet control device according to the invention comprises:
  • a fixed armature, provided with an electric coil and an axial channel, generating in said axial channel, between a first pole and a second pole, a magnetic field during the passage of an electric current in its coil,
  • a movable core sensitive to the magnetic field, driven in axial sliding in said axial channel by said magnetic field and guided by at least two elements with flexible radial blades comprising a peripheral part mounted fixed relative to the fixed frame and connected by said radial blades flexible to a central part integral with the sliding core, to keep the core away from the walls of the axial channel while allowing its axial displacement according to an appropriate stroke between a first and a second extreme axial positions; in addition :
  • the axial channel runs right through the electrical winding,
  • the elements with flexible radial blades are disposed respectively on either side of the ends of the axial channel.

De préférence, les moyens de guidage axial comprennent deux éléments à lames flexibles décalés axialement sur le noyau, à l'exclusion de tout guidage glissant dans le canal axial.Preferably, the axial guide means comprise two elements with flexible blades offset axially on the core, to the exclusion of any guide sliding in the axial channel.

De préférence, les lames flexibles présentent, en première position axiale extrême en l'absence de champ magnétique produit par l'armature fixe, une déformation permanente en flexion dans la direction du déplacement axial du noyau dans un premier sens, le champ magnétique provoquant le déplacement du noyau dans le sens opposé audit premier sens.Preferably, the flexible blades have, in the first extreme axial position in the absence of a magnetic field produced by the fixed armature, a permanent deformation in bending in the direction of the axial displacement of the core in a first direction, the magnetic field causing the displacement of the core in the opposite direction to said first direction.

Selon un mode de réalisation avantageux, en seconde position axiale extrême, les lames flexibles de l'un au moins des éléments à lames flexibles sont sensiblement plates. Cette disposition permet d'assurer une meilleure rigidité radiale, pour garantir un maintien plus efficace du noyau dans la position dans laquelle le champ magnétique est maximum, évitant que les forces magnétiques viennent plaquer le noyau radialement contre l'un des pôles magnétiques.According to an advantageous embodiment, in the second extreme axial position, the flexible blades of at least one of the elements with flexible blades are substantially flat. This arrangement makes it possible to ensure better radial rigidity, to guarantee a more effective retention of the core in the position in which the magnetic field is maximum, preventing the magnetic forces from pressing the core radially against one of the magnetic poles.

Selon une première application, le noyau porte un élément d'obturation mobile logé dans l'ouverture d'un siège fixe d'un conduit de conduction de fluide pour modifier la section ouverte dudit conduit de conduction de fluide en fonction de la position axiale de l'élément d'obturation dans ledit siège. On réalise ainsi une vanne à commande électrique.According to a first application, the core carries a movable closure element housed in the opening of a fixed seat of a duct fluid conduction to modify the open section of said fluid conduction conduit as a function of the axial position of the closure element in said seat. An electrically operated valve is thus produced.

D'autres objets, caractéristiques et avantages de la présente invention ressortiront de la description suivante de modes de réalisation particuliers, faite en relation avec les figures jointes, parmi lesquelles:

  • la figure 1 illustre, en vue de côté en coupe longitudinale, une structure de dispositif de commande à électroaimant selon un mode de réalisation de la présente invention, en première position axiale extrême;
  • la figure 2 illustre, en vue de côté en coupe longitudinale, le dispositif de la figure 1 en seconde position axiale extrême ;
  • la figure 3 illustre, en vue de côté, le dispositif des figures 1 et 2 associé à un élément d'obturation ;
  • les figures 4 à 6 illustrent trois modes de réalisation des éléments à lames radiales élastiquement flexibles selon l'invention ;
  • la figure 7 illustre, en vue de côté en coupe longitudinale, un dispositif de commande selon un second mode de réalisation de la présente invention, en première position axiale extrême ;
  • la figure 8 illustre, en vue de côté en coupe longitudinale, le dispositif de la figure 7 en seconde position axiale extrême ; et
  • la figure 9 illustre, en vue de face, un autre mode de réalisation de l'élément à lames radiales élastiquement flexibles selon l'invention.
Other objects, characteristics and advantages of the present invention will emerge from the following description of particular embodiments, given in relation to the attached figures, among which:
  • FIG. 1 illustrates, in side view in longitudinal section, a structure of an electromagnet control device according to an embodiment of the present invention, in the first extreme axial position;
  • Figure 2 illustrates, in side view in longitudinal section, the device of Figure 1 in second extreme axial position;
  • Figure 3 illustrates, in side view, the device of Figures 1 and 2 associated with a closure element;
  • Figures 4 to 6 illustrate three embodiments of the elements with elastically flexible radial blades according to the invention;
  • FIG. 7 illustrates, in side view in longitudinal section, a control device according to a second embodiment of the present invention, in the first extreme axial position;
  • Figure 8 illustrates, in side view in longitudinal section, the device of Figure 7 in second extreme axial position; and
  • FIG. 9 illustrates, in front view, another embodiment of the element with elastically flexible radial blades according to the invention.

Dans les modes de réalisation illustrés sur les figures 1 à 3, 7 et 8, un dispositif de commande à électroaimant et noyau coulissant selon l'invention comprend une armature fixe 1, munie d'un bobinage électrique 7 et d'un canal axial 3 qui traverse de part en part le bobinage électrique 7. L'armature fixe 1 est solidaire du bâti 2 de l'appareil dans lequel elle est disposée. Un noyau 4 est monté à coulissement dans le canal axial 3.In the embodiments illustrated in FIGS. 1 to 3, 7 and 8, a control device with an electromagnet and a sliding core according to the invention comprises a fixed armature 1, provided with an electric coil 7 and an axial channel 3 which runs right through the electrical winding 7. The fixed frame 1 is integral with the frame 2 of the device in which it is arranged. A core 4 is slidably mounted in the axial channel 3.

L'armature 1, constituée d'un matériau sensible au champ magnétique, est formée d'un étrier périphérique 9 dont les extrémités sont repliées radialement vers l'intérieur pour former des flasques d'extrémités 10 et 11 se raccordant chacun respectivement à un premier élément tubulaire coaxial 5 et à un second élément tubulaire coaxial 6, formant respectivement un premier pôle 5 et un second pôle 6 de l'armature 1. L'armature 1 peut être constituée d'une ou plusieurs pièces assemblées, comprenant par exemple deux longerons opposés formant un double étrier 9 en étant reliés par les flasques d'extrémités 10 et 11. Les pôles 5 et 6 sont conformés de façon que leurs faces intérieures respectives 12 et 13 soient en regard du noyau 4 et séparées de celui-ci par un entrefer généralement radial de faible épaisseur.The frame 1, made of a material sensitive to the magnetic field, is formed of a peripheral stirrup 9 the ends of which are folded radially inwards to form end flanges 10 and 11 each connecting to a first coaxial tubular element 5 and a second coaxial tubular element 6, respectively forming a first pole 5 and a second pole 6 of the armature 1. The frame 1 may consist of one or more assembled parts, comprising for example two opposite side members forming a double stirrup 9 while being connected by the end flanges 10 and 11. The poles 5 and 6 are shaped so that their respective inner faces 12 and 13 are opposite the core 4 and separated from the latter by a generally radial air gap of small thickness.

Le bobinage 7 est adapté de façon que, lorsqu'un courant électrique le parcourt, il produit un champ magnétique dans le canal axial 3 entre les pôles 5 et 6. Sous l'action du champ magnétique, le noyau 4 tend à se déplacer axialement en coulissement dans le canal axial 3 dans le sens produisant la réduction des entrefers. Pour cela, le noyau 4 est réalisé en un matériau sensible au champ magnétique, et il est guidé en coulissement dans le canal axial 3 par des moyens de guidage aptes à permettre son coulissement sans introduire de frottement s'opposant à ce coulissement.The winding 7 is adapted so that, when an electric current flows through it, it produces a magnetic field in the axial channel 3 between the poles 5 and 6. Under the action of the magnetic field, the core 4 tends to move axially sliding in the axial channel 3 in the direction producing the reduction of the air gaps. For this, the core 4 is made of a material sensitive to the magnetic field, and it is guided in sliding in the axial channel 3 by guide means capable of allowing its sliding without introducing friction opposing this sliding.

Les moyens de guidage selon l'invention comprennent un premier élément 14 à lames radiales flexibles, et un second élément 15 à lames radiales flexibles, disposés respectivement de part et d'autre des extrémités du canal axial 3, à distance suffisante de l'armature 1 pour permettre la libre flexion des lames radiales flexibles lors du coulissement axial du noyau 4.The guide means according to the invention comprise a first element 14 with flexible radial blades, and a second element 15 with flexible radial blades, arranged respectively on either side of the ends of the axial channel 3, at a sufficient distance from the armature 1 to allow the free bending of the flexible radial blades during the axial sliding of the core 4.

Chaque élément à lames radiales flexibles tel que l'élément 14 comporte une partie périphérique 16 montée fixe par rapport à l'armature fixe 1, c'est-à-dire solidaire soit de l'armature fixe 1 soit directement du bâti 2 de l'appareil. L'élément 14 à lames radiales flexibles comporte une partie centrale 17 solidaire du noyau 4 coulissant. La partie périphérique 16 est reliée à la partie centrale 17 par des lames radiales flexibles 18.Each element with flexible radial blades such as the element 14 comprises a peripheral part 16 mounted fixed relative to the fixed frame 1, that is to say integral with either the fixed frame 1 or directly from the frame 2 of the 'apparatus. The element 14 with flexible radial blades has a central part 17 integral with the sliding core 4. The peripheral part 16 is connected to the central part 17 by flexible radial blades 18.

Les lames radiales flexibles 18 sont agencées pour présenter une grande flexibilité dans le sens du coulissement axial du noyau tel que représenté par la flèche 19, et pour présenter simultanément une grande rigidité dans le sens des déplacements radiaux du noyau 4, de façon à maintenir le noyau 4 à l'écart des parois du canal axial 3, et notamment des pôles 5 et 6, tout en autorisant son déplacement axial le long de l'axe I-I selon une course appropriée. La flexibilité des lames 18 est choisie de façon que la course appropriée puisse convenir pour un déplacement possible du noyau 4 entre deux positions axiales extrêmes de commande illustrées respectivement sur les figures 1 ou 7 et 2 ou 8.The flexible radial blades 18 are arranged to have great flexibility in the direction of axial sliding of the core as represented by arrow 19, and to simultaneously exhibit great rigidity in the direction of the radial movements of the core 4, so as to maintain the core 4 away from the walls of the axial channel 3, and in particular from the poles 5 and 6, while allowing its axial displacement along the axis II according to an appropriate stroke. The flexibility of the blades 18 is chosen so that the appropriate stroke can be suitable for a possible displacement of the core 4 between two extreme axial control positions illustrated respectively in FIGS. 1 or 7 and 2 or 8.

Ainsi, dans les modes de réalisation représentés, le noyau 4 est tenu par les deux éléments 14 et 15 à lames flexibles décalées axialement sur le noyau 4, à l'exclusion de tout guidage glissant dans le canal axial 3.Thus, in the embodiments shown, the core 4 is held by the two elements 14 and 15 with flexible blades offset axially on the core 4, to the exclusion of any sliding guide in the axial channel 3.

D'autres réalisations sont toutefois possibles, en prévoyant que le noyau est guidé en outre par un ou plusieurs paliers glissants.Other embodiments are however possible, by providing that the core is further guided by one or more sliding bearings.

On peut imaginer de nombreuses formes possibles pour les éléments 14 et 15 à lames flexibles.One can imagine many possible forms for the elements 14 and 15 with flexible blades.

Pour assurer une répartition égale de la résistance à la flexion radiale, assurant ainsi un bon maintien du noyau en alignement avec l'axe longitudinal I-I de l'armature 1, on prévoit au moins trois lames flexibles régulièrement réparties en périphérie de la partie centrale 17 de l'élément 14. Les lames flexibles 18 sont des lames plates, élargies dans le plan transversal, et d'épaisseur réduite dans la direction axiale du noyau 4.To ensure an equal distribution of the resistance to radial bending, thus ensuring good retention of the core in alignment with the longitudinal axis II of the frame 1, at least three flexible blades are regularly provided at the periphery of the central part 17 of element 14. The flexible blades 18 are flat blades, widened in the transverse plane, and of reduced thickness in the axial direction of the core 4.

Diverses formes peuvent être données aux lames flexibles 18, permettant notamment d'allonger leur longueur pour accroître les possibilités de flexion autorisant un coulissement axial du noyau 4.Various forms can be given to the flexible blades 18, making it possible in particular to lengthen their length to increase the possibilities of bending allowing axial sliding of the core 4.

Par exemple, dans les modes de réalisation des figures 4 et 9, les lames flexibles comprennent trois lames, respectivement 180, 181 et 182, ayant une forme générale en spirale autour de l'axe longitudinal du noyau.For example, in the embodiments of Figures 4 and 9, the flexible blades comprise three blades, respectively 180, 181 and 182, having a general shape in a spiral around the longitudinal axis of the core.

Dans le mode de réalisation de la figure 5, les lames flexibles comportent trois lames 180, 181 et 182 comportant chacune au moins une portion 184 sensiblement en arc de cercle centré sur l'axe longitudinal du noyau, et une ou plusieurs portions généralement radiales de raccordement : dans l'exemple représenté, la lame 180 comprend deux portions en arc de cercle 184 et 185, se raccordant respectivement à la couronne périphérique 16 par une portion généralement radiale 186 de raccordement, et à la couronne centrale 17 par une portion généralement radiale 187 de raccordement, et se raccordant l'une à l'autre par une troisième portion généralement radiale 188 de raccordement.In the embodiment of FIG. 5, the flexible blades comprise three blades 180, 181 and 182 each comprising at least one portion 184 substantially in an arc of circle centered on the longitudinal axis of the core, and one or more generally radial portions of connection: in the example shown, the blade 180 comprises two portions in an arc 184 and 185, connecting respectively to the peripheral ring 16 by a generally radial connection portion 186, and to the central ring 17 by a generally radial portion 187 of connection, and connecting to each other by a third generally radial portion 188 of connection.

Dans le mode de réalisation illustré sur la figure 6, chacune des trois lames flexibles telles que la lame 180 comporte également deux portions en arc de cercle respectivement 184 et 185, se raccordant l'une à l'autre par la portion généralement radiale 188, et se raccordant respectivement à la couronne périphérique 16 par la portion généralement radiale 186 et à la couronne centrale 17 par la portion généralement radiale 187.In the embodiment illustrated in FIG. 6, each of the three flexible blades such as the blade 180 also comprises two portions in an arc of a circle, 184 and 185 respectively, connecting one to the other by the generally radial portion 188, and connecting respectively to the peripheral ring 16 by the generally radial portion 186 and to the central ring 17 by the generally radial portion 187.

De préférence, les lames flexibles 18 respectives des éléments 14 et 15 à lames flexibles s'enroulent dans un même sens autour de l'axe longitudinal I-I du dispositif. Ainsi, lors du mouvement axial du noyau 4, les lames flexibles des éléments 14 et 15 impriment au noyau 4, simultanément à sa translation axiale, une légère rotation autour de l'axe longitudinal I-I, favorisant une déformation harmonieuse des lames flexibles 18.Preferably, the respective flexible blades 18 of the elements 14 and 15 with flexible blades are wound in the same direction around the longitudinal axis I-I of the device. Thus, during the axial movement of the core 4, the flexible blades of the elements 14 and 15 impart to the core 4, simultaneously with its axial translation, a slight rotation around the longitudinal axis I-I, promoting a harmonious deformation of the flexible blades 18.

On comprend que les éléments à lames flexibles tels que l'élément 14 peuvent être constitués à partir d'un disque plat en acier ou autre matériau, dans lequel sont découpées des lumières pour former les lames flexibles telles que représentées.It is understood that the elements with flexible blades such as the element 14 can be made from a flat disc of steel or other material, from which are cut openings to form the flexible blades as shown.

Grâce à leur position à l'extérieur du canal axial 3, les éléments 14 et 15 à lames radiales flexibles 18 peuvent avantageusement avoir un diamètre nettement supérieur à celui du canal axial 3. Par exemple, comme illustré sur les figures, la couronne périphérique 16 des éléments 14 et 15 peut être fixée directement au bâti 2, ayant ainsi un diamètre au moins égal au diamètre extérieur de l'armature 1. On favorise ainsi les possibilités de flexion des lames flexibles, pour augmenter la course axiale admissible du noyau 4.Thanks to their position outside the axial channel 3, the elements 14 and 15 with flexible radial blades 18 can advantageously have a diameter significantly greater than that of the axial channel 3. For example, as illustrated in the figures, the peripheral ring 16 elements 14 and 15 can be fixed directly to the frame 2, thus having a diameter at least equal to the outside diameter of the frame 1. This thus favors the possibilities of bending of the flexible blades, in order to increase the admissible axial travel of the core 4.

Les figures 1 et 7 illustrent un dispositif selon l'invention en une première position axiale extrême. De préférence, dans cette première position, en l'absence de champ magnétique produit par l'armature fixe 1, les lames flexibles 18 présentent une déformation permanente en flexion selon la direction I-I de déplacement axial du noyau 4 dans un premier sens 20. Dans cette position, le noyau 4 est relativement éloigné du second pôle 6 de l'armature 1.Figures 1 and 7 illustrate a device according to the invention in a first extreme axial position. Preferably, in this first position, in the absence of a magnetic field produced by the fixed armature 1, the flexible blades 18 have a permanent bending deformation in the direction II of axial displacement of the core 4 in a first direction 20. In this position, the core 4 is relatively far from the second pole 6 of the frame 1.

Selon une première possibilité, illustrée par la figure 1, la déformation permanente en flexion des lames flexibles 18 en première position axiale extrême peut résulter d'un préformage des lames flexibles 18.According to a first possibility, illustrated by FIG. 1, the permanent bending deformation of the flexible blades 18 in the first extreme axial position can result from a preforming of the flexible blades 18.

Selon une seconde possibilité, illustrée par les figures 3, 7 et 8, la déformation permanente en flexion des lames flexibles 18 en première position axiale extrême peut résulter de la poussée d'un ressort axial 31 sollicitant le noyau 4 vers sa première position axiale extrême.According to a second possibility, illustrated by FIGS. 3, 7 and 8, the permanent bending deformation of the flexible blades 18 in the first extreme axial position may result from the thrust of an axial spring 31 urging the core 4 towards its first extreme axial position.

Sous l'action d'un champ magnétique créé par le passage d'un courant électrique dans le bobinage 7, le noyau 4 se déplace axialement dans le sens 19 opposé audit premier sens 20 jusque dans une seconde position axiale extrême telle qu'illustrée sur les figures 2 et 8, position dans laquelle le noyau 4 s'est rapproché du second pôle 6 de l'armature 1. Lors de ce déplacement, les éléments 14 et 15 à lames flexibles se déforment comme illustré sur la figure 2, par fléchissement des lames flexibles 18 de chaque élément. On remarque que, entre les deux positions extrêmes illustrées sur les figures 1 ou 7 et 2 ou 8, le noyau 4 peut se déplacer tout en restant en permanence à l'écart des pôles 5 et 6 de l'armature 1, de sorte qu'aucun frottement ne vient perturber le déplacement axial du noyau 4.Under the action of a magnetic field created by the passage of an electric current in the winding 7, the core 4 moves axially in the direction 19 opposite to said first direction 20 until in a second extreme axial position as illustrated on Figures 2 and 8, position in which the core 4 has approached the second pole 6 of the frame 1. During this movement, the elements 14 and 15 with flexible blades are deformed as illustrated in Figure 2, by bending flexible blades 18 of each element. It is noted that, between the two extreme positions illustrated in FIGS. 1 or 7 and 2 or 8, the core 4 can move while remaining permanently away from the poles 5 and 6 of the armature 1, so that 'No friction disturbs the axial movement of the core 4.

De préférence, comme illustré sur la figure 8, dans la seconde position axiale extrême, les lames flexibles 18 de l'un au moins des éléments 14 et 15 à lames flexibles, sont sensiblement plates, c'est-à-dire dans un plan généralement perpendiculaire à l'axe I-I du dispositif. Sur la figure 2, les deux éléments 14 et 15 sont sensiblement plats. On améliore ainsi la rigidité radiale des lames dans cette seconde position axiale extrême où le noyau subit la contrainte mécanique maximale sous l'effet du champ magnétique maximal généré par la bobine 7.Preferably, as illustrated in FIG. 8, in the second extreme axial position, the flexible blades 18 of at least one of the elements 14 and 15 with flexible blades, are substantially flat, that is to say in a plane generally perpendicular to axis II of the device. In Figure 2, the two elements 14 and 15 are substantially flat. This improves the radial rigidity of the blades in this second extreme axial position where the core undergoes maximum mechanical stress under the effect of the maximum magnetic field generated by the coil 7.

Dans le mode de réalisation illustré sur les figures 1 à 3, la première extrémité du noyau 4 est cylindrique, et coulisse dans le premier pôle 5 dont la surface intérieure respective 12 est cylindrique. Ainsi, le premier pôle 5 définit avec le noyau 4 un premier entrefer radial constant, indépendant de la position axiale du noyau 4 dans le canal axial 3.In the embodiment illustrated in Figures 1 to 3, the first end of the core 4 is cylindrical, and slides in the first pole 5 whose respective inner surface 12 is cylindrical. Thus, the first pole 5 defines with the core 4 a first constant radial air gap, independent of the axial position of the core 4 in the axial channel 3.

Dans ce même mode de réalisation, la seconde extrémité du noyau 4 est conformée en cône 22, pour venir coopérer avec une partie correspondante conique 23 du second pôle 6 dans lequel elle vient s'engager. Le second pôle 6 définit ainsi avec le noyau 4 un second entrefer radial qui décroît en fonction du déplacement axial du noyau 4 de la première vers la seconde position axiale extrême. Le déplacement axial du noyau 4 modifie progressivement l'entrefer 21 entre le cône 22 du noyau 4 et la partie conique 23 du pôle 6. On peut ainsi réaliser une progressivité de déplacement du noyau en présence du champ magnétique généré par le bobinage 7.In this same embodiment, the second end of the core 4 is shaped as a cone 22, to cooperate with a corresponding conical part 23 of the second pole 6 in which it engages. The second pole 6 thus defines with the core 4 a second radial air gap which decreases as a function of the axial displacement of the core 4 from the first to the second extreme axial position. The axial displacement of the core 4 progressively modifies the air gap 21 between the cone 22 of the core 4 and the conical part 23 of the pole 6. It is thus possible to produce a progressive movement of the core in the presence of the magnetic field generated by the coil 7.

Dans le mode de réalisation des figures 7 et 8, le premier pôle 5 présente également une surface intérieure cylindrique définissant un premier entrefer constant, comme dans les modes de réalisation précédents. Par contre, le second pôle 6 présente une surface intérieure cylindrique, et coopère avec une portion de noyau 4 à diamètre variable, définissant un second entrefer radial variable.In the embodiment of Figures 7 and 8, the first pole 5 also has a cylindrical interior surface defining a first constant air gap, as in the previous embodiments. On the other hand, the second pole 6 has a cylindrical interior surface, and cooperates with a portion of core 4 of variable diameter, defining a second variable radial air gap.

Une autre alternative peut consister dans la présence de deux pôles 5 et 6 à surfaces intérieures cylindriques en face de parties cylindriques de noyau 4, définissant deux entrefers radiaux constants indépendants de la position axiale du noyau 4.Another alternative may consist in the presence of two poles 5 and 6 with cylindrical interior surfaces opposite cylindrical parts of core 4, defining two constant radial air gaps independent of the axial position of core 4.

Le dispositif de commande selon l'invention peut être associé à des moyens d'obturation, pour constituer une vanne à commande électrique en continu. Pour cela, le noyau 4 porte ou constitue par lui-même un élément d'obturation permettant de modifier la section ouverte d'un canal de conduction de fluide en fonction de la position axiale du noyau 4 dans l'armature 1.The control device according to the invention can be associated with shutter means, to constitute a continuously electrically controlled valve. For this, the core 4 carries or constitutes by itself a closure element making it possible to modify the open section of a fluid conduction channel as a function of the axial position of the core 4 in the frame 1.

Ainsi, la figure 3 représente un mode de réalisation d'une telle vanne à commande électrique en continu, comprenant un dispositif de commande à électroaimant identique à celui des figures 1 et 2, dans lequel les mêmes éléments ont été repérés par les mêmes références numériques. Il en est de même des figures 7 et 8, qui représentent un autre mode de réalisation d'une telle vanne à commande électrique en continu. Le noyau 4 porte un élément d'obturation 24 coaxial de révolution venant se loger dans l'ouverture 25 d'un siège 26 coaxial d'un conduit de conduction de fluide.Thus, FIG. 3 represents an embodiment of such a continuously electrically controlled valve, comprising an electromagnet control device identical to that of FIGS. 1 and 2, in which the same elements have been identified by the same reference numerals . The same is true of FIGS. 7 and 8, which show another embodiment of such a continuously electrically controlled valve. The core 4 carries a shutter element 24 coaxial of revolution which is received in the opening 25 of a seat 26 coaxial with a fluid conduction conduit.

L'élément d'obturation 24 présente avantageusement une forme de révolution se rétrécissant progressivement vers son extrémité 27, de sorte que l'élément d'obturation 24 produit une variation continue de la section ouverte du conduit de conduction de fluide en fonction de la position axiale du noyau 4 et de l'élément d'obturation 24 dans le siège 26.The closure element 24 advantageously has a shape of revolution tapering progressively towards its end 27, so that the closure element 24 produces a continuous variation of the open section of the fluid conduction conduit as a function of the position axial of the core 4 and of the closure element 24 in the seat 26.

Un joint en élastomère 28 peut être interposé entre une facette 29 frontale du siège 26 et une facette 30 frontale de l'élément d'obturation 24, pour assurer une obturation étanche lorsque le dispositif est en première position axiale extrême illustrée sur les figures 1, 3 et 7.An elastomer seal 28 can be interposed between a front facet 29 of the seat 26 and a front facet 30 of the closure element 24, to ensure a sealed closure when the device is in the first extreme axial position illustrated in FIGS. 1, 3 and 7.

Le noyau 4 est sollicité en translation axiale par des moyens élastiques tels qu'un ressort de compression 31, le repoussant vers sa première position axiale extrême représentée sur les figures 1, 3 et 7, à l'encontre de la sollicitation exercée par le champ magnétique généré par le bobinage 7. Le ressort 31 doit avoir une force de rappel supérieure à la force axiale éventuellement exercée par les éléments 14 et 15 à lames flexibles, et inférieure à la sollicitation axiale produite sur le noyau par le champ magnétique généré par le bobinage 7.The core 4 is biased in axial translation by elastic means such as a compression spring 31, pushing it towards its first extreme axial position shown in FIGS. 1, 3 and 7, against the bias exerted by the field magnetic generated by the winding 7. The spring 31 must have a return force greater than the axial force possibly exerted by the elements 14 and 15 with flexible blades, and less than the axial stress produced on the core by the magnetic field generated by the winding 7.

Dans la réalisation illustrée sur les figures 7 et 8, le noyau 4 en matériau magnétique occupe seulement une partie de la longueur du canal axial 3. Sa première extrémité, fixée au premier élément 14 à lames flexibles, comporte un prolongement axial 40 emmanché en force dans un alésage axial correspondant de la pièce formant l'élément d'obturation 24. La seconde extrémité du noyau axial 4 présente un diamètre qui se réduit légèrement, et comporte un alésage axial taraudé 41 dans lequel se visse un tirant 42 de liaison avec le second élément 15 à lames flexibles. Un canon 43 est engagé sur le tirant 42 entre la seconde extrémité du noyau axial 4 et une première face de la partie centrale du second élément 15 à lames flexibles. Un écrou 44 se visse sur l'extrémité du tirant 42 et vient porter sur l'autre face de la partie centrale du second élément 15 à lames élastiques. Le ressort 31 est un ressort de compression engagé entre l'écrou 44 et un flasque d'extrémité 45 du bâti 2.In the embodiment illustrated in FIGS. 7 and 8, the core 4 made of magnetic material occupies only part of the length of the axial channel 3. Its first end, fixed to the first element 14 with flexible blades, has an axial extension 40 force-fitted in a corresponding axial bore of the part forming the closure element 24. The second end of the axial core 4 has a diameter which is slightly reduced, and comprises a threaded axial bore 41 into which a tie rod 42 for connection with the second element 15 with flexible blades. A barrel 43 is engaged on the tie rod 42 between the second end of the axial core 4 and a first face of the central part of the second element 15 with flexible blades. A nut 44 is screwed onto the end of the tie rod 42 and comes to bear on the other face of the central part of the second element 15 with elastic blades. The spring 31 is a compression spring engaged between the nut 44 and an end flange 45 of the frame 2.

L'invention trouve en particulier des applications dans la commande de débit des gaz.The invention finds in particular applications in the control of gas flow.

La présente invention n'est pas limitée aux modes de réalisation qui ont été explicitement décrits, mais elle en inclut les diverses variantes et généralisations contenues dans le domaine des revendications ci-après.The present invention is not limited to the embodiments which have been explicitly described, but it includes the various variants and generalizations thereof contained in the field of claims below.

Claims (10)

Dispositif de commande à électroaimant à noyau coulissant (4), dans lequel : - une armature fixe (1), munie d'un bobinage électrique (7) et d'un canal axial (3), génère dans ledit canal axial (3), entre un premier pôle (5) et un second pôle (6), un champ magnétique lors du passage d'un courant électrique dans son bobinage (7), - un noyau (4) mobile sensible au champ magnétique est entraîné en coulissement axial dans ledit canal axial (3) par ledit champ magnétique et est guidé par au moins deux éléments (14, 15) à lames radiales flexibles (18) comportant une partie périphérique (16) montée fixe par rapport à l'armature fixe (1) et reliée par lesdites lames radiales (18) flexibles à une partie centrale (17) solidaire du noyau (4) coulissant, pour maintenir le noyau (4) à l'écart des parois du canal axial (3) tout en autorisant son déplacement axial selon une course appropriée entre une première et une seconde positions axiales extrêmes, caractérisé en ce que : - le canal axial (3) traverse de part en part le bobinage électrique (7), - les éléments (14, 15) à lames radiales flexibles (18) sont disposés respectivement de part et d'autre des extrémités du canal axial (3). Sliding core electromagnet control device (4), in which: - a fixed armature (1), provided with an electric winding (7) and an axial channel (3), generates in said axial channel (3), between a first pole (5) and a second pole (6) , a magnetic field during the passage of an electric current in its winding (7), - a movable core (4) sensitive to the magnetic field is driven in axial sliding in said axial channel (3) by said magnetic field and is guided by at least two elements (14, 15) with flexible radial blades (18) comprising a part peripheral (16) mounted fixed relative to the fixed frame (1) and connected by said flexible radial blades (18) to a central part (17) integral with the sliding core (4), to hold the core (4) at the separation of the walls of the axial channel (3) while allowing its axial displacement according to an appropriate stroke between a first and a second extreme axial positions, characterized in that: - the axial channel (3) passes right through the electric winding (7), - The elements (14, 15) with flexible radial blades (18) are disposed respectively on either side of the ends of the axial channel (3). Dispositif selon la revendication 1, caractérisé en ce que les moyens de guidage axial comprennent deux éléments (14, 15) à lames flexibles décalés axialement sur le noyau (4), à l'exclusion de tout guidage glissant dans le canal axial (3).Device according to claim 1, characterized in that the axial guide means comprise two elements (14, 15) with flexible blades offset axially on the core (4), to the exclusion of any guide sliding in the axial channel (3) . Dispositif selon l'une des revendications 1 ou 2, caractérisé en ce que les lames flexibles (18) présentent, en première position axiale extrême en l'absence de champ magnétique produit par l'armature fixe (1), une déformation permanente en flexion selon la direction de déplacement axial (I-I) du noyau (4) dans un premier sens (20), le champ magnétique provoquant le déplacement du noyau (4) dans le sens opposé (19) audit premier sens (20).Device according to one of claims 1 or 2, characterized in that the flexible blades (18) have, in the first extreme axial position in the absence of magnetic field produced by the fixed armature (1), a permanent deformation in bending in the direction of axial movement (II) of the core (4) in a first direction (20), the magnetic field causing the displacement of the core (4) in the opposite direction (19) to said first direction (20). Dispositif selon la revendication 3, caractérisé en ce que, en seconde position axiale extrême, les lames flexibles (18) de l'un au moins des éléments (14, 15) à lames flexibles sont sensiblement plates, pour présenter une meilleure rigidité radiale.Device according to claim 3, characterized in that, in the second extreme axial position, the flexible blades (18) of at least one of the elements (14, 15) with flexible blades are substantially flat, in order to have better radial rigidity. Dispositif selon l'une quelconque des revendications 1 à 4, caractérisé en ce que : - le premier pôle (5) définit avec le noyau (4) un premier entrefer radial constant indépendant de la position axiale du noyau (4) dans ledit canal axial (3), - le second pôle (6) définit avec le noyau (4) un second entrefer radial constant indépendant de la position axiale du noyau (4) dans ledit canal axial (3). Device according to any one of Claims 1 to 4, characterized in that: the first pole (5) defines with the core (4) a first constant radial air gap independent of the axial position of the core (4) in said axial channel (3), - The second pole (6) defines with the core (4) a second constant radial air gap independent of the axial position of the core (4) in said axial channel (3). Dispositif selon l'une quelconque des revendications 1 à 4, caractérisé en ce que : - le premier pôle (5) définit avec le noyau (4) un premier entrefer radial constant indépendant de la position axiale du noyau (4) dans ledit canal axial (3), - le second pôle (6) définit avec le noyau (4) un second entrefer radial qui décroît en fonction du déplacement axial du noyau (4) de la première position axiale extrême vers la seconde position axiale extrême. Device according to any one of Claims 1 to 4, characterized in that: the first pole (5) defines with the core (4) a first constant radial air gap independent of the axial position of the core (4) in said axial channel (3), - The second pole (6) defines with the core (4) a second radial air gap which decreases as a function of the axial displacement of the core (4) from the first extreme axial position towards the second extreme axial position. Dispositif selon l'une quelconque des revendications 1 à 6, caractérisé en ce que le noyau (4) porte un élément d'obturation (24) logé dans l'ouverture (25) d'un siège (26) d'un conduit de conduction de fluide pour modifier la section ouverte dudit conduit de conduction de fluide en fonction de la position axiale de l'élément d'obturation (24) dans ledit siège (26), constituant une vanne à commande électrique.Device according to any one of Claims 1 to 6, characterized in that the core (4) carries a closure element (24) housed in the opening (25) of a seat (26) of a duct for fluid conduction for modifying the open section of said fluid conduction conduit as a function of the axial position of the closure element (24) in said seat (26), constituting an electrically controlled valve. Dispositif selon l'une quelconque des revendications 1 à 7, caractérisé en ce que les lames flexibles (18) respectives des éléments (14, 15) à lames flexibles s'enroulent dans un même sens autour de l'axe longitudinal (I-I) du dispositif.Device according to any one of Claims 1 to 7, characterized in that the respective flexible blades (18) of the elements (14, 15) with flexible blades wind in the same direction around the longitudinal axis (II) of the device. Dispositif selon l'une quelconque des revendications 1 à 8, caractérisé en ce que le noyau (4) est sollicité en translation axiale par des moyens élastiques (31) le repoussant vers la première position axiale extrême à l'encontre de la sollicitation exercée par le champ magnétique généré par le bobinage (7).Device according to any one of Claims 1 to 8, characterized in that the core (4) is biased in axial translation by elastic means (31) pushing it towards the first extreme axial position against the bias exerted by the magnetic field generated by the coil (7). Dispositif selon l'une quelconque des revendications 1 à 9, caractérisé en ce que la partie périphérique (16) des éléments (14, 15) à lames radiales flexibles (18) est solidaire directement du bâti (2).Device according to any one of claims 1 to 9, characterized in that the peripheral part (16) of the elements (14, 15) with flexible radial blades (18) is directly attached to the frame (2).
EP96420115A 1995-04-07 1996-04-05 Control device for electromagnet with core without friction and application for valves with continuous control Expired - Lifetime EP0736882B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9504363 1995-04-07
FR9504363A FR2732814B1 (en) 1995-04-07 1995-04-07 CONTROL DEVICE WITH FRICTIONLESS CORE SOLENOID, AND APPLICATION TO CONTINUOUSLY CONTROLLED VALVES

Publications (2)

Publication Number Publication Date
EP0736882A1 true EP0736882A1 (en) 1996-10-09
EP0736882B1 EP0736882B1 (en) 2000-08-30

Family

ID=9478020

Family Applications (1)

Application Number Title Priority Date Filing Date
EP96420115A Expired - Lifetime EP0736882B1 (en) 1995-04-07 1996-04-05 Control device for electromagnet with core without friction and application for valves with continuous control

Country Status (8)

Country Link
EP (1) EP0736882B1 (en)
AT (1) ATE196032T1 (en)
DE (1) DE69610009T2 (en)
DK (1) DK0736882T3 (en)
ES (1) ES2151139T3 (en)
FR (1) FR2732814B1 (en)
GR (1) GR3034980T3 (en)
PT (1) PT736882E (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL1029504C2 (en) * 2005-07-13 2007-01-16 Univ Eindhoven Tech Actuator.
US9620274B2 (en) 2015-02-17 2017-04-11 Enfield Technologies, Llc Proportional linear solenoid apparatus
FR3081605A1 (en) * 2018-05-24 2019-11-29 Valeo Systemes De Controle Moteur ELECTROMAGNETIC DEVICE
WO2020186358A1 (en) * 2019-03-20 2020-09-24 The University Of British Columbia Solenoid apparatus and methods

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010037922A1 (en) 2010-10-01 2012-04-05 Contitech Vibration Control Gmbh actuator

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Publication number Priority date Publication date Assignee Title
FR1053825A (en) * 1950-03-01 1954-02-05 Bofors Ab Device for maintaining in relative position one or more axially movable bodies
US2858487A (en) * 1954-12-20 1958-10-28 Westinghouse Electric Corp Dust-tight d. c. solenoid assemblies
US4463332A (en) * 1983-02-23 1984-07-31 South Bend Controls, Inc. Adjustable, rectilinear motion proportional solenoid
DE3439378A1 (en) * 1984-10-27 1986-04-30 Heller Hydraulik GmbH, 7440 Nürtingen Pressure control valve and a method for producing such a pressure control valve
EP0284634A1 (en) * 1987-03-31 1988-10-05 MOOG GmbH Electromechanical positioning device
US4954799A (en) * 1989-06-02 1990-09-04 Puritan-Bennett Corporation Proportional electropneumatic solenoid-controlled valve
US5202658A (en) * 1991-03-01 1993-04-13 South Bend Controls, Inc. Linear proportional solenoid

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1053825A (en) * 1950-03-01 1954-02-05 Bofors Ab Device for maintaining in relative position one or more axially movable bodies
US2858487A (en) * 1954-12-20 1958-10-28 Westinghouse Electric Corp Dust-tight d. c. solenoid assemblies
US4463332A (en) * 1983-02-23 1984-07-31 South Bend Controls, Inc. Adjustable, rectilinear motion proportional solenoid
DE3439378A1 (en) * 1984-10-27 1986-04-30 Heller Hydraulik GmbH, 7440 Nürtingen Pressure control valve and a method for producing such a pressure control valve
EP0284634A1 (en) * 1987-03-31 1988-10-05 MOOG GmbH Electromechanical positioning device
US4954799A (en) * 1989-06-02 1990-09-04 Puritan-Bennett Corporation Proportional electropneumatic solenoid-controlled valve
US5202658A (en) * 1991-03-01 1993-04-13 South Bend Controls, Inc. Linear proportional solenoid

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL1029504C2 (en) * 2005-07-13 2007-01-16 Univ Eindhoven Tech Actuator.
WO2007008068A1 (en) * 2005-07-13 2007-01-18 Technische Universiteit Eindhoven Actuator
US8111121B2 (en) 2005-07-13 2012-02-07 Technische Universiteit Eindhoven Actuator
US9620274B2 (en) 2015-02-17 2017-04-11 Enfield Technologies, Llc Proportional linear solenoid apparatus
US9704636B2 (en) 2015-02-17 2017-07-11 Enfield Technologies, Llc Solenoid apparatus
FR3081605A1 (en) * 2018-05-24 2019-11-29 Valeo Systemes De Controle Moteur ELECTROMAGNETIC DEVICE
WO2020186358A1 (en) * 2019-03-20 2020-09-24 The University Of British Columbia Solenoid apparatus and methods
US11972899B2 (en) 2019-03-20 2024-04-30 The University Of British Columbia Solenoid apparatus and methods

Also Published As

Publication number Publication date
FR2732814B1 (en) 1997-05-09
PT736882E (en) 2001-02-28
DE69610009T2 (en) 2001-05-03
EP0736882B1 (en) 2000-08-30
FR2732814A1 (en) 1996-10-11
ATE196032T1 (en) 2000-09-15
ES2151139T3 (en) 2000-12-16
DE69610009D1 (en) 2000-10-05
GR3034980T3 (en) 2001-02-28
DK0736882T3 (en) 2001-01-02

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