WO2000041189A1 - Actionneur electromagnetique equipe de moyens d'ajustement de la position de son element polaire mobile - Google Patents
Actionneur electromagnetique equipe de moyens d'ajustement de la position de son element polaire mobile Download PDFInfo
- Publication number
- WO2000041189A1 WO2000041189A1 PCT/FR1999/003238 FR9903238W WO0041189A1 WO 2000041189 A1 WO2000041189 A1 WO 2000041189A1 FR 9903238 W FR9903238 W FR 9903238W WO 0041189 A1 WO0041189 A1 WO 0041189A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- movable
- polar
- electromagnetic actuator
- fixed stator
- pole
- 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.)
- Ceased
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01V—GEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
- G01V1/00—Seismology; Seismic or acoustic prospecting or detecting
- G01V1/16—Receiving elements for seismic signals; Arrangements or adaptations of receiving elements
- G01V1/18—Receiving elements, e.g. seismometer, geophone or torque detectors, for localised single point measurements
- G01V1/181—Geophones
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F7/00—Magnets
- H01F7/06—Electromagnets; Actuators including electromagnets
- H01F7/08—Electromagnets; Actuators including electromagnets with armatures
- H01F7/081—Magnetic constructions
Definitions
- the field of the invention is that of electromagnetic actuators and in particular those forming part of accelerometers intended for geophone applications.
- Geophones allow very detailed analysis of the nature of the earth's layers in order to detect possible petroleum sources.
- Sources of excitation send mechanical waves into the ground which act on the accelerometer, its response provides information on the nature of the terrestrial layers encountered by mechanical waves.
- the actuator operates with a stroke of very small amplitude and must have very high precision.
- An electromagnetic actuator has a fixed stator element coupled to a magnet, a coil and a movable pole element. The actuator is intended to move an external member, integral with the movable pole element.
- the external mobile member is a mobile mass, coupled to a servo system with means for detecting its position.
- the servo system delivers a servo current to the coil to compensate by electromagnetic induction phenomena a displacement of the mass under the effect of external conditions, for example seismic movements.
- the value of the acceleration undergone by the mass is deducted from the value of the servo current flowing in the coil which is necessary to prevent the displacement of the mass.
- the electromagnetic actuator can be used in other applications in which its operation is similar, for example, the external member to be moved can be a valve needle that the movable polar element must move from an initial position to a final working position.
- Means for detecting the position of the needle or of the movable polar element are provided for controlling the supply of the coil by a servo current which allows displacement by electromagnetic induction of the movable polar element. In this application very high precision in movement is also required.
- FIG. 1 schematically illustrates an example of an accelerometer incorporating an electromagnetic actuator of known type.
- the electromagnetic actuator referenced 10 comprises a fixed stator element 12 comprising a permanent magnet 5 radially magnetized.
- the magnet 5 surrounds a coil 6 inside which is a movable pole element 14 secured to a mass 2 to be moved.
- the fixed stator element 12 and the movable pole element 14 define between them at least two air gaps 51 and form a magnetic circuit.
- the magnet 5 creates lines of magnetic field in the magnetic circuit through the air gaps.
- the fixed stator element 12 is in the form of an enclosure represented as a cylinder of revolution and the magnet is represented as a ring.
- the mass 2 is suspended from a peripheral frame 3 by arms 80, 81.
- the peripheral frame 3 is fixed to the fixed stator element 12.
- a servo system 7 for the position of the mass 2 to move and therefore from the position of the movable pole element 14 generates a servo current in the coil 6 as long as the mass 2 to be moved is not in a reference position.
- This servo system has the effect of preventing any displacement of the mass 2 under the effect of external conditions, for example seismic movements. More specifically, the servo system 7 comprises means 82, 83 for detecting the position of the mobile mass 2 and therefore of the mobile pole element 14 and means 70 for circulating a servo current in the coil 6 , when the mass leaves a so-called reference position so as to move the movable polar element 14 by electromagnetic induction phenomena until the mass 2 returns to its reference position.
- the movable pole element 14 compensates for the displacement that the mass 2 undergoes under the effect of the external conditions.
- the means for detecting the position of the mass can be gauges 82, 83 of piezoelectric stresses placed on the arms 80, 81 for suspending the mass 2.
- the movable pole element 14 When the coil 6 is not supplied, the movable pole element 14 is subjected to different magnetic fields represented by arrows in FIG. 1. These arrows relate to the magnetic fields created by the permanent magnet 5.
- the element pole 14 is in an unstable equilibrium and tends to move along an axis YY 'perpendicular to the median plane of the magnet 5 and leaves a median position represented by the axis AA' and by the same moves the mobile mass 2 In this middle position, the movable pole element 14 is placed symmetrically with respect to the permanent magnet 5.
- the parts of the actuator must be perfectly sized and also positioned relative to the mass, the peripheral frame and the strain gauges before starting a series of measures.
- the rib chains which enter into the production of the parts of the actuator can only ensure an accuracy of 10 micrometers if one does not want to inconsiderately increase the cost of production of these parts.
- the present invention proposes to include in the actuator a polar element for adjusting the position of the movable polar element by compared to that of the fixed stator element. We can then perform an adjustment operation before operating the electromagnetic actuator.
- the subject of the invention is an electromagnetic actuator intended to move an external member, comprising a fixed stator element associated with a mobile pole element which can be joined to the external member, the fixed stator element and the mobile pole element forming a magnetic circuit and defining between them at least two air gaps, a magnet helping to create magnetic field lines in the magnetic circuit, a coil for controlling the movement of the movable polar element by electromagnetic induction phenomena, characterized in that 'it further comprises a polar adjustment element which cooperates with the fixed stator element pqur put the movable polar element in an adjusted position relative to that of the fixed stator element by deflecting the magnetic field lines.
- the polar adjustment element can be inserted into an opening of the fixed stator element, the depression of the polar adjustment element causing the movable polar element to move from a given initial position to the detected adjusted position by a position sensor, in the initial position the movable pole member being closer to the opening than in the adjusted position.
- the polar adjustment element will preferably be given the shape of an ankle. In order to keep the polar adjustment element in place after adjustment, it may include a longitudinally striated portion which cooperates with the opening, the edge of which is smooth.
- the striated portion may be followed by a conical portion, itself followed by an active portion which penetrates first into the opening, the active portion being of diameter smaller than that of the striated portion.
- the polar adjustment element can be produced from a soft ferromagnetic material such as an iron-nickel alloy.
- the position sensor detects the position of the external member secured to the movable polar element and therefore gives the position of the movable polar element, it can be used during adjustment but also when the actuator works.
- a system for controlling the position of the movable polar element is associated with the position sensor, this system supplying a servo current to the coil.
- the invention also relates to an electromagnetic accelerometer comprising a mobile mass suspended from a peripheral frame and associated with strain gauges and which incorporates an electromagnetic actuator mentioned above and in which the external member is the mobile mass, the position sensor the gauges constraints, the fixed stator pole element being fixed to the peripheral frame. In the adjusted position of the movable pole piece, the movable mass and the peripheral frame are substantially in the same plane.
- the present invention also relates to a method for adjusting the position of a movable polar element of an electromagnetic actuator, the electromagnetic actuator comprising a fixed stator element associated with the movable polar element, the fixed stator element and the element mobile pole forming a magnetic circuit and defining between them at least two air gaps, a magnet helping to create magnetic field lines in the magnetic circuit, a coil for controlling by movement of electromagnetic induction a movement of the mobile pole element, characterized in that it comprises the following stages:
- FIG. 1 schematically illustrates an example of an accelerometer incorporating an electromagnetic actuator of known type
- FIG. 2a, 2b cross sections of an example of an accelerometer incorporating an electromagnetic actuator according to the invention in which the movable pole member is respectively in its initial position and in its desired adjusted position;
- FIG. 3 a three-dimensional view of an accelerometer according to the invention in which a sector has been removed;
- FIG. 4a, 4b views in longitudinal and cross section of a pole member for adjusting the position of a movable pole member of an electromagnetic actuator according to the invention.
- FIGS. 2a, 2b show, in cross section, an example of an electromagnetic actuator according to the invention, respectively before and Figures 2a, 2b show, in cross section, an example of an electromagnetic actuator according to the invention, respectively before and after, the adjustment of the position of its movable pole member.
- Figure 3 is a three-dimensional view of the same actuator with a removed sector. This actuator is comparable to that of Figure 1 which illustrates the prior art but Figures 2 are less schematic.
- the fixed stator element 12 is assembled to the peripheral frame 3 in the accelerometer application and coupled to the magnet 5, the coil 6 and the movable pole element 14 defining with the fixed stator element 12 at least two air gaps 51
- the fixed stator element 12 is in the form of a chamber of revolution with an axis YY ′ but other configurations are possible, in particular the fixed stator element could be flat.
- the coil 6 is held in the enclosure 12 by a non-magnetic wedge 60.
- the coil is connected to contacts 61 allowing its electrical supply.
- the servo system is not shown completely as in FIG. 1, but the strain gauges 82, 83 are seen on the arms which hold the mass 2.
- the annular permanent magnet 5 is placed, in the example, in the internal diameter of the coil 6. The reverse would be possible.
- the magnet 5 is held in the enclosure 12 using a non-magnetic wedge 50.
- the mobile pole element 14 which is produced by a piece of soft magnetic material, is itself in the internal diameter of the magnet 5. It can move along the axis YY '.
- the air gaps 51 are arranged on either side of the median plane of the magnet 5 substantially perpendicular to the axis YY '.
- the fixed stator element 12 has two openings 121, 122 in planes substantially perpendicular to the axis YY '.
- the first 121 situated in the example at the base of the fixed stator element 12, on the side of the peripheral frame 3, allows the mobile pole element 14 to be fixed to the mobile mass 2 by means of an intermediate piece 140 non-magnetic which can be made of glass for example.
- One of the faces of this intermediate piece 140 can be glued to the movable mass 2 and the opposite face is fixed to the movable pole element 14.
- the intermediate piece 140 moves in translation through the first opening 121.
- the second opening 122 situated in the example, at the top of the fixed stator element 12, allows the introduction of a pole element for adjusting 15 the position of the movable pole element 14 relative to that of the fixed stator element 12.
- This polar adjustment element 15 is introduced into the magnetic circuit formed by the fixed stator element 12 and the movable polar element 14.
- the introduction of the polar adjustment element 15 into the enclosure through the opening 122 has the effect of deflecting the magnetic field lines, due in particular to the magnet 5, which are established in the magnetic circuit in crossing the air gaps 51.
- the introduction of the polar adjustment element 15 therefore has the action of electromagnetically moving the mobile polar element 14 relative to the fixed stator element 12.
- the actuator according to the invention associated with a mass 2 to be moved is at a stage of adjustment.
- the electromagnetic actuator was mounted having taken care to place its movable pole element 14 in an initial position at a distance d1 from the second opening 122.
- the adjusting pole element 15 is not introduced into the second opening 122.
- the movable pole element 14 is closer to the second opening 122 than when it is in a desired adjusted position shown in FIG. 2b.
- the mass 2 which it is intended to move is not in its reference position and the strain gauges 82, 83 are stressed.
- the position of the movable pole element 14 can be adjusted relative to that of the fixed stator element 12 by switching on the electromagnetic actuator and pressing the adjustment pole element 15 into the opening 122. These actions have the effect of electromagnetically displacing the movable pole element 14 away from the opening 122. It stops pushing the adjustment pole element 15 into the opening 122 when the pole element mobile 14 has reached the desired adjusted position, this position having been detected by the position detection means 82, 83.
- FIG. 2b illustrates the actuator according to the invention with its movable pole element 14 in its desired adjusted position. It is now located at a distance d2 from the opening 122 for the polar adjusting element 15. The distance d2 is greater than the distance d1.
- the position of the mass 2 corresponds to an "electrical zero”
- the movable polar element 14 is in a "mechanical zero” position with respect to the fixed stator element 12 and in the position of "magnetic zero” whatever the tolerances of the parts entering into the composition of the actuator.
- the adjustment pole member 15 contributes to the movable pole member 14 being in its "magnetic zero" position.
- the actuator according to the invention given as an example is seen in three dimensions and a sector has been removed which makes it possible to see the movable pole element 14, the coil 6, the magnet 5 and the polar adjustment element 15 inside the fixed stator element 12 forming an enclosure.
- the polar adjustment element 15 is in the form of an ankle. It is assumed that the adjustment has just been made and that the movable pole element is in the desired adjusted position.
- the opening 122 for the polar adjustment element 15 has smooth walls and the polar adjustment element 15 has a portion 15.1 striated longitudinally.
- the diameter of the dowel 15 at the bottom of the ridges is substantially the same as that of the opening 122.
- a certain resistance appears and this resistance makes it possible in particular to keep the dowel in place after adjustment.
- the dimensions of such actuators do not exceed ten cubic centimeters and these dimensions impose a polar adjustment element 15 with a magnetically active part which enters the opening 122 having a diameter less than a millimeter and a length of the order of a millimeter .
- this dowel will be configured with several consecutive portions 15.1, 15.2, 15.3 including the striated portion 15.1 on one side, the magnetically portion active 15.3, of smaller diameter, on the other, and between the two portions a conical portion 15.2.
- Figures 4a, 4b illustrate such an anchor.
- a differential screw 16 causing a translation of the pin 15 of the order of a few micrometers per revolution, typically 5 micrometers per revolution.
- a soft ferromagnetic material such as an iron nickel alloy, in particular that known under the name SUPRANHUSTER 50 from IMPHY SA, may be chosen for the polar adjustment element 15.
- the intermediate element 140 ensuring the connection between the mobile polar element 14 and the mass 2 has its face connected to the mass 2 in the same plane as the outer face of the fixed stator element 12 which has the first opening 121.
- the accelerometer is ready to operate and the actuator can then be used in a working mode.
- the present invention also relates to a method for adjusting the position of the movable pole element of an electromagnetic actuator relative to that of its fixed stator element.
- the mobile pole element is given an initial position relative to that of the fixed stator element and in this initial position, it is closer to the opening for the pole adjustment element than in the desired adjusted position.
- the electromagnetic actuator is oriented so that the displacement of the movable pole element can be made substantially perpendicular to gravity.
- the electromagnetic actuator is energized.
- the polar adjusting element is inserted into the opening of the fixed stator element. This insertion is carried out until the movable pole element reaches the desired adjusted position, this position being detected by the position sensor. In the initial position, the movable pole element is closer to the opening than in the desired final position.
- the travel of the movable polar element is greater than 0 microns and less than 20 microns.
- the adjustment is made in combination with the servo.
- the electromagnetic actuator is capable of operating with the high precision required.
- the production of the parts of a known actuator and their assembly even with the greatest possible care and therefore at high cost cannot ensure such an adjustment of the positioning of the movable pole element relative to the fixed stator element. This positioning is practically done with a micrometer and it is impossible to obtain it by taking care of the sides of the parts and their respective positioning.
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- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Life Sciences & Earth Sciences (AREA)
- Electromagnetism (AREA)
- Geology (AREA)
- Environmental & Geological Engineering (AREA)
- General Life Sciences & Earth Sciences (AREA)
- General Physics & Mathematics (AREA)
- Geophysics (AREA)
- Acoustics & Sound (AREA)
- Power Engineering (AREA)
- Reciprocating, Oscillating Or Vibrating Motors (AREA)
Abstract
Description
Claims
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| MXPA01006637A MXPA01006637A (es) | 1998-12-30 | 1999-12-21 | Activador electromagnetico equipado con medios para ajustar la posicion de su elemento polar movil. |
| US09/857,212 US6556114B1 (en) | 1998-12-30 | 1999-12-21 | Electromagnetic actuator equipped with means for adjusting its mobile polar element |
| AU16658/00A AU1665800A (en) | 1998-12-30 | 1999-12-21 | Electromagnetic actuator equipped with means for adjusting its mobile polar element |
| BR9916689-5A BR9916689A (pt) | 1998-12-30 | 1999-12-21 | Atuador eletromagnético equipado com meios para o ajuste da posição de seu elemento polar móvel |
| CA002358209A CA2358209A1 (fr) | 1998-12-30 | 1999-12-21 | Actionneur electromagnetique equipe de moyens d'ajustement de la position de son element polaire mobile |
| NO20013266A NO20013266D0 (no) | 1998-12-30 | 2001-06-29 | Elektromagnetisk styreelement utstyrt med midler for å justere posisjonen til dets bevegelige polare element |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR9816659A FR2788163B1 (fr) | 1998-12-30 | 1998-12-30 | Actionneur electromagnetique equipe de moyens d'ajustement de la position de son element polaire mobile |
| FR98/16659 | 1998-12-30 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2000041189A1 true WO2000041189A1 (fr) | 2000-07-13 |
Family
ID=9534701
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/FR1999/003238 Ceased WO2000041189A1 (fr) | 1998-12-30 | 1999-12-21 | Actionneur electromagnetique equipe de moyens d'ajustement de la position de son element polaire mobile |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US6556114B1 (fr) |
| AU (1) | AU1665800A (fr) |
| BR (1) | BR9916689A (fr) |
| CA (1) | CA2358209A1 (fr) |
| FR (1) | FR2788163B1 (fr) |
| MX (1) | MXPA01006637A (fr) |
| NO (1) | NO20013266D0 (fr) |
| WO (1) | WO2000041189A1 (fr) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2001030125A2 (fr) * | 2000-11-20 | 2001-05-03 | HELAYEL, Emile | Procede de detection d'un mouvement relatif de deux systemes et detecteur utilise a cet effet |
| US7227440B2 (en) * | 2005-03-03 | 2007-06-05 | Pratt & Whitney Canada Corp. | Electromagnetic actuator |
| US8184974B2 (en) | 2006-09-11 | 2012-05-22 | Lumexis Corporation | Fiber-to-the-seat (FTTS) fiber distribution system |
| JP5596145B2 (ja) | 2009-08-06 | 2014-09-24 | ルメクシス・コーポレーション | 直列ネットワーキングファイバーツーザシート機内エンターテイメントシステム |
| WO2011020071A1 (fr) | 2009-08-14 | 2011-02-17 | Lumexis Corp. | Dispositif de connexion d'unité d'affichage vidéo pour un système fibre à l'écran de divertissement à bord |
| US8416698B2 (en) | 2009-08-20 | 2013-04-09 | Lumexis Corporation | Serial networking fiber optic inflight entertainment system network configuration |
| KR101592271B1 (ko) * | 2014-06-30 | 2016-02-11 | 현대중공업 주식회사 | 전자접촉기 |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS57166526A (en) * | 1981-04-07 | 1982-10-14 | Mitsubishi Electric Corp | Seismometer |
| EP0110431A1 (fr) * | 1982-06-08 | 1984-06-13 | Terra Dynamics B.V. | Géophone sensible aux accélérations |
| EP0258569A2 (fr) * | 1986-08-02 | 1988-03-09 | BBC Brown Boveri AG | Dispositif de positionnement électromagnétique |
| EP0441737A1 (fr) * | 1990-02-05 | 1991-08-14 | United Technologies Corporation | Réglage du gain magnétique pour moteur à force linéaire, magnétisé axialement ayant une armature entourée par un corps extérieur |
| US5153472A (en) * | 1991-07-19 | 1992-10-06 | International Business Machines Corporation | Probe positioning actuator |
| US5202658A (en) * | 1991-03-01 | 1993-04-13 | South Bend Controls, Inc. | Linear proportional solenoid |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4933515A (en) * | 1989-03-09 | 1990-06-12 | Automotive Systems Laboratory, Inc. | Accelerometer with dual-magnet sensing mass |
| FR2737610B1 (fr) | 1995-08-01 | 1997-09-12 | Sextant Avionique | Micro-capteur capacitif a faible capacite parasite |
| FR2742231B1 (fr) | 1995-12-12 | 1998-01-02 | Sextant Avionique | Accelerometre electromagnetique |
| FR2742230B1 (fr) | 1995-12-12 | 1998-01-09 | Sextant Avionique | Accelerometre et procede de fabrication |
| FR2776064B1 (fr) | 1998-03-10 | 2000-05-26 | Crouzet Automatismes | Dispositif de mesure de position angulaire utilisant un capteur magnetique |
| FR2784745B1 (fr) | 1998-10-16 | 2001-01-05 | Crouzet Automatismes | Detecteur de position a cellule de detection micro-usinee |
-
1998
- 1998-12-30 FR FR9816659A patent/FR2788163B1/fr not_active Expired - Fee Related
-
1999
- 1999-12-21 BR BR9916689-5A patent/BR9916689A/pt not_active IP Right Cessation
- 1999-12-21 CA CA002358209A patent/CA2358209A1/fr not_active Abandoned
- 1999-12-21 WO PCT/FR1999/003238 patent/WO2000041189A1/fr not_active Ceased
- 1999-12-21 MX MXPA01006637A patent/MXPA01006637A/es not_active Application Discontinuation
- 1999-12-21 AU AU16658/00A patent/AU1665800A/en not_active Abandoned
- 1999-12-21 US US09/857,212 patent/US6556114B1/en not_active Expired - Fee Related
-
2001
- 2001-06-29 NO NO20013266A patent/NO20013266D0/no not_active Application Discontinuation
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS57166526A (en) * | 1981-04-07 | 1982-10-14 | Mitsubishi Electric Corp | Seismometer |
| EP0110431A1 (fr) * | 1982-06-08 | 1984-06-13 | Terra Dynamics B.V. | Géophone sensible aux accélérations |
| EP0258569A2 (fr) * | 1986-08-02 | 1988-03-09 | BBC Brown Boveri AG | Dispositif de positionnement électromagnétique |
| EP0441737A1 (fr) * | 1990-02-05 | 1991-08-14 | United Technologies Corporation | Réglage du gain magnétique pour moteur à force linéaire, magnétisé axialement ayant une armature entourée par un corps extérieur |
| US5202658A (en) * | 1991-03-01 | 1993-04-13 | South Bend Controls, Inc. | Linear proportional solenoid |
| US5153472A (en) * | 1991-07-19 | 1992-10-06 | International Business Machines Corporation | Probe positioning actuator |
Non-Patent Citations (1)
| Title |
|---|
| PATENT ABSTRACTS OF JAPAN vol. 007, no. 006 (P - 167) 11 January 1983 (1983-01-11) * |
Also Published As
| Publication number | Publication date |
|---|---|
| MXPA01006637A (es) | 2003-03-27 |
| FR2788163A1 (fr) | 2000-07-07 |
| NO20013266L (no) | 2001-06-29 |
| AU1665800A (en) | 2000-07-24 |
| NO20013266D0 (no) | 2001-06-29 |
| US6556114B1 (en) | 2003-04-29 |
| BR9916689A (pt) | 2001-09-25 |
| CA2358209A1 (fr) | 2000-07-13 |
| FR2788163B1 (fr) | 2001-03-16 |
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