GB2342504A - A bistable and monostable electromagnetic drive arrangement - Google Patents

A bistable and monostable electromagnetic drive arrangement Download PDF

Info

Publication number
GB2342504A
GB2342504A GB9914330A GB9914330A GB2342504A GB 2342504 A GB2342504 A GB 2342504A GB 9914330 A GB9914330 A GB 9914330A GB 9914330 A GB9914330 A GB 9914330A GB 2342504 A GB2342504 A GB 2342504A
Authority
GB
United Kingdom
Prior art keywords
armature
flux
magnetic
drive
travel
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.)
Granted
Application number
GB9914330A
Other versions
GB2342504B (en
GB9914330D0 (en
Inventor
Wladyslaw Wygnanski
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from GBGB9821842.3A external-priority patent/GB9821842D0/en
Priority claimed from GBGB9912518.9A external-priority patent/GB9912518D0/en
Application filed by Individual filed Critical Individual
Publication of GB9914330D0 publication Critical patent/GB9914330D0/en
Priority to GB0229887A priority Critical patent/GB2380064B/en
Priority to GB0229888A priority patent/GB2380065B/en
Priority to DE1999619557 priority patent/DE69919557T2/en
Priority to EP04015857A priority patent/EP1479956A3/en
Priority to US09/807,043 priority patent/US6598621B1/en
Priority to PT99949174T priority patent/PT1119723E/en
Priority to EP04015856A priority patent/EP1482227A1/en
Priority to EP99949174A priority patent/EP1119723B1/en
Priority to GB9923744A priority patent/GB2342782B/en
Priority to AU62159/99A priority patent/AU6215999A/en
Priority to EP04015111A priority patent/EP1482226A1/en
Priority to PCT/GB1999/003327 priority patent/WO2000020786A1/en
Priority to JP2000574861A priority patent/JP4359395B2/en
Priority to AT99949174T priority patent/ATE274162T1/en
Priority to ES99949174T priority patent/ES2228111T3/en
Publication of GB2342504A publication Critical patent/GB2342504A/en
Publication of GB2342504B publication Critical patent/GB2342504B/en
Application granted granted Critical
Priority to US10/449,486 priority patent/US7021603B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00Actuating devices; Operating means; Releasing devices
    • F16K31/02Actuating devices; Operating means; Releasing devices electric; magnetic
    • F16K31/06Actuating devices; Operating means; Releasing devices electric; magnetic using a magnet, e.g. diaphragm valves, cutting off by means of a liquid
    • F16K31/08Actuating devices; Operating means; Releasing devices electric; magnetic using a magnet, e.g. diaphragm valves, cutting off by means of a liquid using a permanent magnet
    • F16K31/082Actuating devices; Operating means; Releasing devices electric; magnetic using a magnet, e.g. diaphragm valves, cutting off by means of a liquid using a permanent magnet using a electromagnet and a permanent magnet
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00Actuating devices; Operating means; Releasing devices
    • F16K31/003Actuating devices; Operating means; Releasing devices operated without a stable intermediate position, e.g. with snap action
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00Actuating devices; Operating means; Releasing devices
    • F16K31/02Actuating devices; Operating means; Releasing devices electric; magnetic
    • F16K31/06Actuating devices; Operating means; Releasing devices electric; magnetic using a magnet, e.g. diaphragm valves, cutting off by means of a liquid
    • F16K31/0682Actuating devices; Operating means; Releasing devices electric; magnetic using a magnet, e.g. diaphragm valves, cutting off by means of a liquid with an articulated or pivot armature
    • 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
    • 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
    • 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
    • H01F7/121Guiding or setting position of armatures, e.g. retaining armatures in their end position
    • H01F7/122Guiding or setting position of armatures, e.g. retaining armatures in their end position by permanent magnets
    • 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
    • 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
    • H01F7/1615Armatures or stationary parts of magnetic circuit having permanent magnet
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F7/00Magnets
    • H01F7/06Electromagnets; Actuators including electromagnets
    • H01F7/08Electromagnets; Actuators including electromagnets with armatures
    • H01F7/16Rectilinearly-movable armatures
    • H01F7/1638Armatures not entering the winding
    • H01F7/1646Armatures or stationary parts of magnetic circuit having permanent magnet
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H51/00Electromagnetic relays
    • H01H51/22Polarised relays
    • H01H51/2209Polarised relays with rectilinearly movable armature
    • 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
    • H01F2007/1669Armatures actuated by current pulse, e.g. bistable actuators
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H1/00Contacts
    • H01H1/50Means for increasing contact pressure, preventing vibration of contacts, holding contacts together after engagement, or biasing contacts to the open position
    • H01H2001/506Fail safe contacts, i.e. the contacts being kept in a safe position, usually in an open circuit position, at end of life time of switch
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H11/00Apparatus or processes specially adapted for the manufacture of electric switches
    • H01H11/0006Apparatus or processes specially adapted for the manufacture of electric switches for converting electric switches
    • H01H2011/0043Apparatus or processes specially adapted for the manufacture of electric switches for converting electric switches for modifying the number or type of operating positions, e.g. momentary and stable

Landscapes

  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Magnetically Actuated Valves (AREA)

Abstract

An electromagnetic actuator comprises permanent magnet means 12, 14, an armature 10 and at least one electromagnet 36, 38. The actuator is arranged to operate in a bistable manner. The magnetic field produced by the permanent magnet means 12, 14 may be arranged to traverse gaps at either end of the actuator. The permanent magnetic field in respective gaps is in opposite directions such that when the electromagnet 36, 38 is energised a magnetic field is generated which boosts the field in one direction and reduces the field in the other direction. The electromagnet 36, 38 creates a stronger magnetic field in one of the gaps which will tend to attract the armature 10 towards it. The armature 10 is latched into position by the permanent magnetic field which prevents the armature moving when the electromagnet is de-energised. A magnetic shunt member 40 may be applied across one of the gaps to convert the actuator from bistable to monostable operation. The actuator may be used in arrangements for operating valves or electric relays and the magnetic shunt 40 may be introduced to the actuator via various means to provide a fail-safe operation.

Description

Title: Magnetic drives Field of invention This invention concerns magnetic drives, particularly but not exclusively for valves for controlling gas flow or fluid flow and for opening and closing electrical switch contacts.
Background to the invention UK Application No. 9821842.3 describes valves for controlling gas flow and examples are given of devices which when operated repetitively will produce sound waves, and magnetic drives for such valves. However the disclosure is not limited to sound producing devices and according to one of the aspects of the invention described in Application No. 9821842.3 a valve for controlling gas flow comprises: -a chamber to which gas is supplied under pressure to maintain a substantially constant pressure differential between the interior and exterior of the chamber, -an opening (orifice) in a wall of the chamber, -a closure member cooperatively associated with the opening, -bistable electromagnetic drive means associated with the closure member and adapted to hold the closure member either in a first position, in which it blocks the openina and prevents the passage of gas, or in a second position, in which the opening is unblocked, thereby allowing the passage of gas to and from the chamber, and -an electrical current supply means for supplying an appropriate electric current pulse to the electromagnetic drive means to cause it to shift from its present state into the other of its bistable states and open or close the valve accordingly.
Such a valve can be used as a low power bistable flow control valve for interrupting or enabling a flow of gas or fluid, with energy only being required to effect the transition from its open to closed, or from its closed to open condition.
Such a flow control valve will be referred to as a bistable valve as aforesaid.
Whilst double acting or bistable valves of this type are suitable for many applications, there are some applications in which a monostable device is to be preferred, particularly where the valve needs to automatically revert to a closed condition in the event of electrical power failure or other emergency conditions.
Such valves are normally necessary for the purpose of controlling the flow of inflammable or poisonous gases or fluids, so that the valve operates in a so-called fail-safe mode in the event of a power failure. By fail-safe is meant that the valve will revert to a closed condition in the event that there is an electrical power failure.
One object of the present invention is to provide a drive having a bistable or a monostable characteristic, and which if bistable can be readily modified tc revert to one condition (typically the closed state) in the event of a power failure.
It is another object of the invention to provide a mechanical device for aitering the characteristics of a bistable magnetic drive, to those of a monostable magnetic drive.
It is a further object of the invention to provide an improved construction of bistable magnetic drive for a valve such as described in UK Application 9821842.3.
It is a further object of the invention to provide a digital gas flow controlling valve.
A further object of the invention is to provide a digitally controllable gas flow control valve with a safety characteristic which reverts to a closed state in the event of the failure of a monitored source of energy such as electrical power or heat or light.
Summary of the invention According to one aspect of the present invention in a bistable magnetic drive comprising magnet means producing first and second magnetic fields, the polarity of the first and second fields being opposite, and a magnetisable armature mounted for movement between the two said fields, the armature being magnetised South/North or North/South depending on which of the two fields it occupies and requiring considerable force acting perpendicular to the magnetic flux lines to shift the armature out of the influence of either field once it is aligned therewith, a magnetic or magnetisable shunt is provided which is movable into a position in which the magnetic flux of one of the first and second fields becomes diverted therethrough, so as to cause the armature to either remain in the unaffected field or immediately to move, under the influence of the unaffected magnetic field flux, so as to occupy the unaffected field.
Shifting the armature from one end to the other of the drive normally can be achieved by reinforcing the flux at the said other end by causing an electric current to flow in one or more energising windings, to flow which is/are located so as to influence the flux in the two fields.
A magnetic drive as aforesaid may serve to control a pneumatic or hydraulic valve or provide the movement necessary to open and close electrical contacts of an electrical switch.
If the magnetic shunt is permanently in position then it can be arranged that either the additional flux provided by the energising winding will be sufficient to overcome non-shunted field at the other end of the drive, or not to do so. If the induced flux is sufficient to move the armature from the nonshunted field into the shunted field, it will be seen that as soon as the energy current is removed or significantly reduced, the armature will return to the non-shunted field end.
A more preferred arrangement is one in which an additional electro-magnetic device is provided at the shunted field end of the drive, with which the armature makes contact when moved into the shunted field. Preferably the additional device includes a magnetic core and the contact with the armature means that there is no air gap to reduce the flux density after contact is made. By providing a complete magnetic path without an air gap, the flux density is magnified many times in manner known per se. The preferred arrangement therefore enables the armature to be attracted away from the non-shunted field by a high electric current flowing in the additional device, which can be reduced to a low current once the armature and device core make contact to hold the armature at the shunted field end.
Such an arrangement has a fail-safe characteristic in that if the small holding electric current fails, the residual flux gradient present in the drive will be such as to cause the armature immediately to move to occupy the non-shunted field where the static flux is highest.
The additional electromagnetic device may be a solenoid having a large number of turns on a magnetic core-eg a core of ferromagnetic material.
A valve employing a drive as aforesaid may be used to control the flow of inflammable gas to a burner or jet, if in manner known per se, a small thermocouple is located adjacent the burner or jet so as to be heated by a flame emanating from the burner or jet, to cause electric current to flow in any circuit connected to the thermocouple. Thus if the latter either produces, or controls the production of, a current for the holding solenoid at the shunted field end, the solenoid will produce a magnetic flux sufficient to retain the armature in contact therewith at the shunted field end provided the thermocouple remains heated by the flame. In the event of flame failure for any reason, the thermocouple cools, the holding current collapses and with it the magnetic flux linking the holding solenoid to the armature, thereby releasing the latter to move to the higher flux concentration at the other end of its travel.
An alternative arrangement which has similar fail-safe characteristics involves mounting the flux short circuiting device on a movable element, the position of which relative to the drive is controlled by the passage of an electric current or is dependent upon a particular voltage being present, or a gas or fluid pressure being exerted against the movable element, or any other physical parameter which changes in the event of some failure (such as flame failure in a gas burner) which will result in the movable element shifting the flux shunting device from a position in which a relatively large air gap exists between it and the magnetic flux at one end of the drive, into a position in which the shunting element diverts most or all the said flux to significantly reduce the flux density at that end of the armature travel and cause the armature either to move to the other end of the drive to where the magnetic flux remains unaffected, or to remain at that other end.
Preferred forms of movable element are a bimetal strip, a piezo bender, a spring, a diaphragm or other device which will move under increasing or decreasing pressure.
In addition or instead of movement in relation to failure of a flame or other physical event, the mechanism which determines the instantaneous position of the flux shunting element can be adapted to respond to an increase in a monitored parameter such as temperature or pressure as well as a decrease. Thus the flux shunting device may be moved into position so as to direct the flux at one end of the drive, either in response to flame failure (in the case of a gas burner) or in the event of excess temperature.
Where a holding solenoid is to be provided, this may be located to advantage within the drive at the end which is to be affected by the flux shunting element.
The armature is generally formed from magnetisable material, typically a ferro-magnetic material, and in order to reduce its mass, a split form of construction may be employed in which ferro-magnetic poles are located at opposite ends of the drive with a relatively small gap between opposed magnetic pole faces at each end of the drive, and the movable section of the armature (also formed from magnetisable material) is such as to just fit in the small gaps between the opposed pole faces at the opposite ends of the drive, the movable element itself being secured to one end of a connecting rod which extends through one end of the magnetic drive to terminate externally of the drive in a valve closure member.
By constructing the armature in this way, the mass of the armature can be reduced to little more than the mass of the connecting rod, which itself can be hollowed so as to reduce its mass, and the solid piece of ferro-magnetic material forming the movable part of the armature is simply a small cross-section but solid extension, of the connecting rod.
The connecting rod is preferably formed from non-magnetic material.
By reducing the mass of the armature in this way, the operating speed of the device (and any valve associated therewith) can be increased considerably relatively to an arrangement in which a more massive armature has to be moved from one end of the drive to the other under the influence of the same magnetic field gradient.
A magnetic drive as described is typically combined with a chamber to or from which fluid can flow depending on the position of a valve closure member relative to a valve seating surrounding an opening, which in one position of the armature is closed by the valve closure member, and in the other end position of the armature, is unobstructed by the valve closure member.
It is important that in such arrangements it may be necessary to ensure that there is no chance of leakage of the fluid which may be gas or liquid into the drive. This is particularly important where a flammable or explosive gas or liquid is involved. To this end the opening through which the connecting rod extends between the magnetic drive and the valve closure member may be sealed with one or more seals to prevent the escape of fluid gas or liquid from the chamber.
More preferably a diaphragm seal may be provided, instead of or in addition to sealing means surrounding the connecting rod, and the diaphragm material is selected so as to be impervious to the fluid to be controlled and is sufficiently flexible to permit linear movement of the connecting rod in response to movement of the magnetic armature.
In a preferred arrangement the diaphragm is generally circular in shape, includes a corrugated annular region to provide fiexibility and displaceability of its central region relative to the circumference thereof and is centrally perforated to allow the connecting rod to extend therethrough, but is sealed around the connecting rod, typically to a collar on the rod, the collar forming an integral part of or being sealingly fitted to the rod, and the periphery of the diaphragm is likewise bonded or otherwise sealingly joined to a larger diameter collar which is sealingly joined or integrally formed with an end wall of the magnetic drive assembly, which forms at least part of one wall of the fluid chamber into which the connecting rod and valve closure member extends.
Where a flux shunting element is provided at one end of the drive, typically the end thereof remote from the fluid chamber, a button operated setting/resetting device may be provided, proximate to the flux shunting element for holding the latter away from the magnet assembly while the bimetal strip, piezo bender, or other mechanism which will normally holds the flux shunting away from the magnetic field, establishes a sufficient force to stand off the flux shunting element after the button is released.
In addition or alternatively, an emergency button may be provided for forcing the flux shunting device into contact with the magnet components of the drive to cause the valve to flip into its closed condition as a consequence of the collapse of the magnetic flux, in one of the fields.
Typically the collapse occurs in the field remote from the fluid chamber containing the valve closure device.
The invention also lies in a plurality of bistable flow control valves arranged in parallel, each having orifices which differ in size and are selected in such a manner that by opening different ones of the orifices, either alone, or in combination with other orifices, different effective overall orifice sizes can be obtained, so as to regulate the flow of fluid through the valves, the overall open orifice area determining the rate of flow for a given pressure differential.
Preferably the different overall orifice areas which can be obtained thereby, constitute each of a sequence of area values such that a progression from zero area to the maximum area (when all valves are open) can be effected in a series of known steps.
The invention also lies in a magnetic drive formed from a permanent magnet means generating magnetic flux, an armature which can occupy either a first air gap in which the flux is in one direction, or a second air gap in which the flux is in the opposite direction, with a region of flux cancellation between the two air gaps, at least one electromagnet winding to which current can be supplied to produce a magnetic flux in one direction or the other, depending on the direction of the current, the flux from the winding increasing the flux density in one of the air gaps and reducing the flux density in the other air gap, thereby effectively shifting the flux cancellation region towards or into one of the two air gaps, so as to produce a flux density gradient extending from one air gap to the other which will cause the armature to move towards (or remain in) the air gap having the higher flux density when the current flows in the winding.
The invention also lies in a magnetic drive as aforesaid which further includes low reluctance flux concentrating means external to the electromagnet winding which provides a low reluctance external path for returning flux from one end to the other thereof when the winding is energised, thereby to increase the flux produced by the winding when energised, so as to magnify the magnetic flux available to effect movement of the armature.
The external flux concentrating means conveniently comprises at least one elongate member of magnetisable material which extends parallel to the magnetic flux in the air gap and generally perpendicular to the direction of movement of the armature and beyond the extent of its travel.
The external flux concentrating means may be combined with other magnetic drive enhancement in particular one in which four similar elongate magnetisable pole pieces are arranged symmetrically in pairs, each pair occupying one of the two magnetic fields, and the air gap between the pole pieces in each pair defining the air gaps at the two extremes of the armature travel, the two pairs of pole pieces serving to concentrate the internal magnetic flux into the two air gaps at opposite ends of the armature travel.
The combination of internal and external flux concentrating elements assists in defining the two stable positions of the armature and also assists in effecting the movement of the armature from one end to the other.
A pair of electrical contacts may be provided at one end of the armature travel which are electrically joined by being bridged by the armature, or by conductive means or a coating on the armature, when the latter is located at that end of its travel.
Likewise a pair of electrical contacts may be provided at the other end of the travel as well, and if required second conductive means or a coating is provided on the armature to ensure that the said other contacts are also bridged when the armature is at the other end of its travel.
By providing electrical contacts at either one or both ends of the armature travel, the drive is converted into an electrical switch in which one pair of contacts are bridged when the armature is at one end of its travel and the other pair are bridged when it is at the other end of its travel. The converted drive is therefore equivalent to an electromagnetic relay or contactor.
A drive as aforesaid may be contained within a sealed chamber and where electrical contacts are involved, at least part of the wall of the chamber is formed from electrical insulating material to provide a region for conductive feedthroughs to terminals external of the chamber to allow electrical connection to be made to the contacts therein which, when the armature is in an appropriate position, are bridged thereby.
Typically the chamber is formed from plastics or glass or quartz.
A drive as aforesaid may include a further flux concentrator which is movable relative to the drive, so as to adopt a first position relatively close to the drive to reduce the flux density at one end of the armature travel, thereby causing the device to assume a monostable characteristic when the further concentrator is in that position, and is movable out of the first position onto a second position where it has little or no influence on the flux density in the drive to reinstate the bistable characteristic of the drive.
In an alternative arrangement, the said further flux concentrator may be permanently located very close to one end of the armature travel so as to produce a drive having a permanent monostable characteristic.
In one embodiment of the invention, a single permanent magnet may be employed at one end of an electromagnetic coil having located internally thereof two pairs of aligned, spaced apart pole pieces, defining air gaps at opposite ends of the armature travel, with or without external flux concentrating elements for increasing the flux density attributable to a current flowing in the electromagnetic coil, and instead of a second permanent magnet being located at the opposite end of the coil, an elongate member of magnetisable material is provided formed from material similar to that from which the pole pieces are formed, such that flux issuing from one of the two nearer internal pole pieces passes into and through the magnetisable material to issue from the other end thereof and pass into the other of two nearer internal pole pieces. The length oi magnetisable material thus provides a return path for the flux and maintains the flux direction at each end of the armature travel in the same way as a second permanent magnet would have done.
Further flux concentration can be obtained by providing filed focussing pole pieces at opposite ends of the permanent magnet and magnetisable elements at the opposite end of the coil (or at each end of the two permanent magnets where permanent magnets are located at both ends of the coil), wherein the pole pieces extend laterally of each magnet or length of magnetisable material and extend towards the pole pieces and flux concentrating elements located externally of the coil where provided.
In such an arrangement, any said further concentrator which is employed to produce a monostable characteristic in the drive, may also include pole pieces for fitting with small air gaps, between the said field focussing pole pieces and any internal pole pieces, and/or any external concentrator (s), at opposite ends of the coil.
The invention will now be described by way of example, with reference to the accompanying drawings in which: Figure 1 is a cross-section through a magnetic drive which can be bistable or monostable depending on whether or not a flux short-circuiting element is in position; Figure 2 illustrates a similar arrangement to that of Figure 1, but in which the armature is split into a number of parts most of which are stationary so as to reduce the mass of the moving part of the armature; Figure 3 is a further cross-section through a device similar to that of Figure 1 in which electromagnetic means is provided for holding the movable armature in a position from it would normally move as a result of the reduction in magnetic flux by movement of the flux short-circuiting device; Figure 4 illustrates the arrangement of Figure 3 in which the electromagnetic holding device has been disabled allowing the armature to shift to the other end of the drive ; Figure 5 shows the magnetic flux pattern of two magnets without a flux short circuiting device bridging one end of the magnets; Figure 6 shows the effect of short circuiting the flux at one end of the magnet assembly, thereby creating only one stable position for a magnetisable armature located between the two magnets; Figure 7 is a schematic diagram of a drive for a fluid control valve, in which the device is a balanced magnetic drive having two stable equilibrium positions; Figure 8 illustrates how a number of such valves can be arranged to provide digital control of gas flow, in series with a monostable fail-safe valve; Figure 9 is a diagrammatic illustration of a bistable magnetic drive, which incorporates two magnets and which constitutes another embodiment of the invention ; Figure 10 is a similar illustration of a two-magnet bistable magnetic drive constructed as a further embodiment of the invention; Figures 11 and 12 are similar views of the embodiment shown in Figure 10, showing the armature in its two bistable positions wherein the armature short-circuits pairs of electrical contacts at opposite ends of its travel and converts the drive into a relay; Figure 13 is a similar view of another bistable embodiment of the invention, in which only a single element magnet is required, and wherein the armature is again shown cooperating with pairs of contact to perform the function of a relay; Figure 14 is a further bistable embodiment of the invention constructed so as to more precisely route the magnetic flux available from the permanent magnets; Figure 15 is a modification of the Figure 14 arrangement in that a flux concentrator is provided which if moved close enough to the balanced magnetic circuit, will introduce imbalance in the flux pattern so as to introduce optionally (for example in a power failure mode) monostability into the operating characteristics of the device; and Figure 16 is a further modification of the Figure 14 arrangement in which the flux concentrator is located permanently in a flux imbalancing position, to create a monostable drive device.
In Figure 1 an armature 10 is movable between the poles of a pair of magnets 12 and 14 arranged so as to produce two opposed fields at opposite ends of the travel of the armature. The latter is attached to a rod 16 to the upper end of which is attached a valve closure member 18. A diaphragm seal 20 extends between a collar 22 around the rod 16 and a second collar 24 attached to a wall 26 between the chamber 28 to which gas or liquid can be supplied via inlet opening 30 and which can exit when the valve closure member 18 is in the position shown displaced from a valve seat 32, by escaping through the outlet 34.
The armature 10 will attempt to align with one or the other of the two cross fields of the upper or lower end of the its travel and can be induced to move from one end to the other by passing a current through windings 36 and 38 in one direction or the other so as to either reinforce the flux at one end or reinforce the flux at the other.
Since reinforcement of magnetic flux in one of the cross fields will automatically reduce the flux in the other field, the effect of the current in the windings 36 and 38 will be to generate a flux gradient from one end of the armature travel to the other and the latter will tend to move towards the position of maximum flux density.
In accordance with the invention described in earlier Application No. 9821842.3, it is only necessary to supply a pulse of energy to the coils 36 and 38 to produce the flux gradient and therefore the transition of the armature from one end to the other, since, once the armature has moved into the position of maximum flux density, it will remain there even if the current ceases to flow in the windings 36 and 38 which reestablishes the two cross fields as they were. The reason for this is that there is no tendency for the armature to move across the region of lower flux density between the two cross fields and it will tend to remain in one or the other of the two extreme positions at the top or bottom of its travel.
As shown in Figure 1, the armature is actually mid-way between its two extreme positions.
In accordance with the present invention, a flux concentrator and therefore short circuiting device 40 is mounted on a piezo bender 42 or a bi-metal strip such that the supply of appropriate electrical energy (potential or current) to the device 42 will cause the latter to be bent in the manner shown in Figure 1 thereby holding the device 40 away from the end of the magnet 12 and 14.
In the event of the voltage or current failing, the piezo bender or bi-metal strip 42 will tend to straighten causing the device 40 to move closer to the two opposite poles of the magnets 12 and 14, and magnetic flux will tend to be attracted to two poles 42 and 44 and will be concentrated into the structure of the device 40 if the latter is formed from magnetisable material. Typically it is formed from a ferromagnetic material or other suitable magnetisable material.
The effect of the flux attraction will be to induce opposite magnetic poles in the poles 42 and 44 from those adjoining them in the magnets 12 and 14 causing attraction and closure of any gap between the device 40 and the magnets 12 and 14. The device 40 will therefore tend to clamp itself onto the lower end of the two magnets 12 and 14, and most of the flux which would normally extend between the two lower poles of the two magnets 12 and 14 will be concentrated into and extend through the device 40.
The net effect is that the magnetic flux density in the cross field at the lower end of the assembly of Figure 1 will collapse to a very low level and a flux gradient will exist between the lower end of the assembly and the upper end.
If the armature 10 is already at the upper end, there will be no tendency for it to move.
If however the armature is at the lower end, the armature will tend to move up the gradient to the upper end of the assembly where the flux density is highest and to remain in that position.
Figure 2 illustrates the same arrangement as shown in Figure 1, but here the armature has been divided into four stationary parts 46 and 48 at the upper end and 50 and 52 at the lower end of the armature travel and the latter has been reduced to a small element of magnetisable material 54 which will just fit with a small gap between the elements 46 and 48 when the armature is at the upper end and between 50 and 52 when it is at its lower end of its travel.
The elements 46 to 52 essentially comprise pole piece extensions of the magnets 12 and 14.
The remaining parts of the device are as described in relation to Figure 1.
Figures 3 and 4 illustrate a modification to the Figure 1 arrangement in which electromagnet 56 having a winding 58 is located at the lower end of the armature travel to engage the armature and provide a holding magnetic flux when the armature 10 is in its lowermost position as shown in Figure 3.
The holding flux will only exist whilst a current flows in the winding 58, and to this end a current source exists to supply an appropriate current in the winding 58. If the latter is made up of a large number of turns of thin wire, only a very small current is needed to generate sufficient flux to hold the armature 10 against the pole pieces of the solenoid 56 and provided no air gap is introduced between the pole pieces and the armature 10, the closed path provided for the magnetic flux will hold the armature in the lower position as shown in Figure 3.
In the event that the current flowing through winding 58 falls to a low value or collapses completely, the holding flux will also collapse and if a flux g position where the armature is held at the lower end by virtue of a small current flowing in the coil 58.
Transition between the home position and the latched position is effected in the manner described in relation to Figure 1 by means of a pulse of current of appropriate polarity flowing in the windings 36 and 38 so as to reinforce the field which is otherwise reduced by the effect of the short circuiting device 40 to cause the armature to move towards the solenoid 58. Once in contact therewith, the low current flowing in the solenoid winding 58 will maintain the armature in its lower position and the device is fail-safe in that if the current in the winding 58 collapses or simply reduces considerably, the armature will be free to move back up the flux gradient to the stable home position.
In each case the stable home position corresponds to the valve closure member 18 being firmly positioned against the valve seat 32 thereby closing off the exit from the chamber 28.
Figures 5 and 6 show the flux lines between the magnets 12 and 14 with the short circuiting magnetisable concentrate 40 displaced from the assembly in Figure 5 and close to if not in contact with the assembly as shown in Figure 6.
Figure 7 shows the essential parts of a bi-stable valve constructed essentially as shown in Figure 1, with seals 60 and 62 between the hollow rod 64 which terminates in the upper end with a valve closure device 66. A concentrator 40 may be located in the chamber 68 if desired so as to concentrate the flux into itself between the lower poles of the two magnets 12 and 14 as previously described to convert the device into a mcnostable valve. It will be seen that the concentrator 40 could be inverted and located in the other chamber 70 at the upper end of the assembly so as to reverse the flux gradient but in this event the device would not close in the event of power failure.
For the monostable operation to be successful, an additional electromagnetic device is necessary as described with reference to Figures 3 and 4 to hold the armature at the unstable end of its travel.
Figure 8 shows how three valves each having a different sized orifice can be arranged in parallel to provide digital control having eight discrete flow rates depending on which of the valves is open between a first chamber 72 and a second chamber 74. Each of the valves is operated by a drive similar to that shown in Figure 7 and fluid is supplied to chamber 72 via a monostable fail-safe valve such as is described in relation to Figures 3 and 4.
This valve is denoted by reference numeral 76.
The inlet to valve 76 may be gas pipe 78 supplying gas at moderate pressure for burning in a gas burner jet 80 which is supplied with gas from the second chamber 74. Depending on which of the valves A, B and C are opened, so the flow of gas to the burner 80 will be zero or maximum or any one of six different levels in between.
A small bleed pipe 82 feeds a pilot jet 84 from the chamber 72 and a bi-metal strip or other temperature sensitive device is located in the pilot flame to provide a holding current for the holding solenoid such as 56,58 of Figures 3 and 4 as employed in the valve 76.
In the event of flame failure at the pilot light, the current in the holding device collapses and valve 76 closes.
As a safety measure, circuit means may be provided sensing the current in the holding device for valve 76 such that if this current fails, a current pulse is supplied to each of valves A, B and C to close each of these valves off.
The features of the device are set out in the list of features in the lower part of Figure 8.
As observed on the drawing, any number of valves such as A, B, C may be employed, the more that are employed, the greater the number of possible intermediate steps which can be provided between the fully open gas flow mode and the fully closed gas flow mode of the valves.
The invention provides a simple digital gas flow control valve arrangement which contains no moving parts and can be arranged to fail safe in the event of power failure.
Figure 9 illustrates a magnetic drive formed from two permanent magnets 86 and 88, and elongate armature 90 which can either rest in the upper position as shown or in the lower position shown in dotted outline at 92. The two positions of the armature coincide with the regions of maximum flux density in the complex field between the two magnets.
It will be appreciated that approximately half way between the two positions 90 and 92, the flux density will be effectively zero and will increase sharply in the directions of arrows 94 and 96. Beyond the positions 90 and 92, the flux density will tend to fall away.
The two positions 90 and 92 are therefore positions of equilibrium, albeit relatively unstable equilibrium in that if the armature is in one position, and is moved towards the other position by external means, there will become a point in time in which the influence of the magnetic flux associated with the other position will exceed that of the field from which the : e armature is moving and the latter will be attracted into the said other position.
Movement of the armature can be effected magnetically by locating an electromagnetic winding 98 between the two magnets 86 and 88. Passing a current through the winding in one sense will increase the magnetic flux density in the upper field and reduce the flux density in the lower field thereby shifting the position of zero flux density towards the lower field if not into and beyond the lower field depending on the flux density produced by the electrical magnet. Reversing the direction of current flow will reverse the effect on the flux in the upper and lower fields and shift the position of zero flux to the region of the upper field if not beyond it.
The net effect is to create a flux gradient extending from one armature position to the other depending on the direction of the current flow in the electromagnet 98 and the armature will always tend towards the region of higher flux density.
Once the armature has been moved from one field position to the other field position, current is no longer required to flow in the electromagnet to maintain the armature in the new position since on the collapse of the current, the flux pattern between the two magnets will be restored and the position of zero flux will again be located approximately midway between the armature positions causing the armature to remain in the position into which it has been moved.
In accordance with the invention, the flux produced by the electromagnet 98 can be significantly enhanced by locating magnetic concentrators 100 and 102 externally of the electromagnet coil 98 to provide a lower reluctance path outside the coil thereby effectively matching the low reluctance path within the coil (caused by the presence of the armature) and thereby increasing the flux available within the electromagnet to influence the magnetic fields between the two magnets 86 and 88.
The external concentrators 100 and 102 also attract flux from the permanent magnets 86 and 88 and by virtue of the magnetisation of the armature and the concentrators 100 and 102 by the permanent magnet fields and the flux generated by the flow of current in the electromagnet 98, the flux gradient from one end of the armature travel to the other is significantly enhanced, thereby improving the changeover characteristic of the drive for a given flow of current in the electromagnet 98.
Figure 10 illustrates a further refinement of the arrangement shown in Figure 9 in which the armature 90 is now replaced by a shorter element 104 which as shown is in its midway position between the two ends of its travel denoted by the rectangular dotted outlines 106 and 108. The magnetic flux from the magnets 86 and 88 is concentrated into upper and lower air gaps at opposite ends of the armature travel by means of two pairs of pole pieces 110 and 112, and 114 and 116. In accordance with the preferred aspects of the invention, elongate concentrators 100 and 102 are also provided externally of the switching coil/electromagnet 98.
The device operates in exactly the same way as described in relation to Figure 9, except that the armature is now less massive and requires effectively less energy to shift it from position 106 to 108 and vice versa. This means that the flux required to be generated by the electromagnet 98 can be reduced or for a given electromagnet and current, the force acting on the armature is considerably greater than would otherwise be the case leading to a more reliable operation of the drive or enabling greater force to be exerted from the armature to an external element which is driven by the armature.
Pole pieces 110 to 116 serve to concentrate flux in the two fields between the two permanent magnets into the upper and lower central air gaps and serve to better define the position of zero flux midway between those two air gaps in the nonenergised condition of the coil 98.
The external flux concentrators 100 and 102 serve to enhance the flux available on energisation of the electromagnet coil 98 as previously described.
Either of the arrangements shown in Figures 9 and 10 can be adapted to form an electrical switch by providing electrical contact adjacent one or both of the positions of the armature and by forming the armature from electrically conductive material or mounting on or coating on the armature electrically conductive material which completes an electrical circuit between the contacts when the armature occupies the position adjacent the contacts.
Contacts may be provided at both ends of the armature travel so that two different electrical circuits are made depending on whether the armature is at one end or the other of its travel.
Figures 11 and 12 illustrate the Figure 10 arrangement in which the armature 104 has conductive elements 118 and 120 located on opposite faces for making contact with a first pair of contacts 122,124 at the lower end of its travel and a second pair of contacts 126,128 at the upper end of its travel.
The armature 104 is shown in its upper position in Figure 11 and in its lower position in Figure 12.
It is to be understood that two permanent magnets such as 86 and 88 are not required and a drive can be constructed from single magnet such as 86 and a flux return member 130 as shown in Figure 13. This comprises the arrangement of Figure 12 in which the magnet 88 is replaced by the flux returning member 130. With no current flowing in coil 98, the flux from permanent magnet 86 will induce North and South poles as shown in the various magnetisable elements making up the circuit and armature 120 will remain in the lower position as shown.
Introducing a current of sufficient magnitude into the coil 98 will enhance the flux density between the upper pole pieces 110 and 112 and reduce if not eliminate flux between the pole pieces 114 and 116 causing the armature 120 to shift from the lower position shown to the upper position such as is designated in Figure 11.
It will be seen that the second magnet 88 serves no purpose other than to reinforce the flux density in the air gaps between the pole pieces at opposite ends of the armature travel, and by providing a low reluctance path as by an elongate magnetisable member 130 in place of the second magnet 88, the flux pattern within and operation of the drive remains unchanged.
Although an arrangement incorporating a single magnet is shown in conjunction with an armature having conductive 118 and 120 for cooperating with contacts as described in relation to Figures 11 and 12, it is to be understood that the single magnet drive is applicable to any arrangement including monostable arrangements as described herein.
Since the flux emanating from the magnets 86 and 88 will tend to issue from the end faces of the magnets, a practical arrangement preferably includes pole pieces at the ends of the magnets (or in the case of a single magnet arrangement, at the end of the magnet 86 and at the end of the flux returning device 130) which extend laterally towards the armature and pole piece assembly within the electromagnet as shown in Figures 14,15 and 16.
For simplicity a two magnet drive is shown based on the Figure 11 arrangement and the armature shown at 104 is in its upper rest position at one end of its travel. An outline position at 105 denotes the other stable position for the armature.
Similar reference numerals have been incorporated as used in Figures 10,11 and 12 to denote the same items.
In accordance with this aspect of the invention, laterally extending pole pieces 132 and 134 are provided at the opposite ends of the magnet 86 and similar pole pieces 136 and 138 are provided at opposite ends of the other magnet 88. The pole pieces provide a low reluctance path for flux linking the magnets 86 and 88 with the other magnetisable members of the magnetic drive and this increases the flux density available to the drive from any given pair of magnets 86 and 88 (or single magnet 86).
The arrangement shown in Figure 14 is a bistable arrangement since it is wholly symmetrical and the armature will remain in either the upper position at 106 or the lower position 108 as described in relation to Figure 10, until triggered to move from one position to the other by an appropriate current flow in the electromagnetic coil 98.
The arrangement shown in Figure 15 is a bistable drive which can be modified in an emergency to adopt a monostable characteristic by introduction of an external flux concentrating element 140 having pole pieces 142 and 144 which can be introduced between the pole pieces 134 and 138 and the external flux concentrating element 102 so as to significantly concentrate most of the flux which would otherwise link the armature (if in position 108 as shown), and lower pole pieces 114 and 116, whilst leaving the flux linking the other pole pieces 110 and 112 virtually unchanged. The flux gradient so produced will accelerate the armature 108 into the upper position 106 shown in Figure 14 and the armature will tend tc remain in that position all the time element 140 is located with its pole pieces 142 and 144 between the two magnets.
Passing an appropriate current through the electromagnetic coil 98 can overcome the flux short-circuiting effect of the element 140 to enable the armature 108 to be moved to the lower position while the current flows, but it will be seen that as soon as the current fails, the armature 108 will revert to the upper position for the reasons indicated above.
Figure 16 shows the element 140 located in its proximate position between the poles 134 and 138, and demonstrates how the armature will normally adopt the upper position 106 when the element 140 is so positioned.

Claims (35)

  1. CLAIMS 1. A magnetic drive formed from a permanent magnet means generating magnetic flux, an armature which can occupy either a first air gap in which the flux is in one direction, or a second air gap in which the flux is in the opposite direction, with a region of flux cancellation between the two air gaps and at least one electromagnet winding to which current can be supplied and adapted when energised to produce a magnetic flux in one direction or the other, depending on the direction of the current, the flux from the winding increasing the flux density in one of the air gaps and reducing the flux density in the other air gap, thereby effectively shifting the flux cancellation region towards or into one of the two air gaps so as to produce a flux density gradient extending from one air gap to the other which will cause the armature to move into (or remain in) the air gap having the higher flux density, and continue to remain in that air gap after the current flow ceases.
  2. 2. A magnetic drive as claimed in claim 1, which further includes low reluctance flux concentrating means external to the electromagnet winding which provides a low reluctance external path for returning flux from one end to the other thereof when the winding is energised, thereby to increase the flux produced by the winding when energised, so as to magnify the magnetic flux available to effect movement of the armature.
  3. 3. A magnetic drive as claimed in claim 2, wherein the external flux concentrating means comprises at least one elongate member of magnetisable material which extends parallel to the magnetic flux in the air gap and generally perpendicular to the direction of movement of the armature and beyond the extent of its travel.
  4. 4. A magnetic drive as claimed in any of claims 1 to 3, in which four similar elongate magnetisable pole pieces are arranged symmetrically in pairs, each pair occupying one of the two magnetic fields, and the air gap between the pole pieces in each pair defines the air gap at each of the two extremes of the armature travel, the two pairs of pole pieces serving to concentrate the internal magnetic flux into the two said air gaps.
  5. 5. A drive as claimed in any of claims 1 to 4, wherein a flux concentrator is located close to one end of the armature travel so as to produce a drive having a monostable characteristic.
  6. 6. A drive as claimed in any of claims 1 to 4, wherein a flux concentrator is movable relative to the drive, so as to adopt a first position relatively close to the drive to reduce the flux density at one end of the armature travel, thereby causing the device to assume a monostable characteristic and is movable out of the first position onto a second position where it has little or no influence on the flux density in the drive, so as to reinstate the bistable characteristic of the drive.
  7. 7. A drive as claimed in any of claims 1 to 6, wherein a single permanent magnet is employed at one end of an electromagnetic coil having located internally thereof two pairs of aligned, spaced apart pole pieces, defining air gaps at opposite ends of the armature travel, and an elongate member cf magnetisable material is provided at the opposite end of the coil formed from material similar to that from which the pole pieces are formed, such that flux issuing from one of the two nearer internal pole pieces passes into and through the magnetisable material to issue from the other end thereof and pass into the other of two nearer internal pole pieces, the elongate member of magnetisable material thus providing a return path for the flux to maintain the flux direction at each end of the armature travel in the same way as a second permanent magnet in place of the elongate member would do.
  8. 8. A drive as claimed in any of claims 1 to 7, further comprising field focussing pole pieces at opposite ends of the magnetic elements at opposite ends of the coil, wherein the pole pieces extend laterally of each magnetic element and extend towards the internal pole pieces and any flux concentrating elements located externally of the coil so as to further concentrate the magnetic flux.
  9. 9. A magnetic switch comprising a drive as claimed in any one of claims 1 to 8, wherein a pair of electrical contacts is provided at one end of the armature travel which are electrically joined by being bridged by conductive means moved into contact therewith by armature movement.
  10. 10. A magnetic switch as claimed in claim 9, wherein a pair of electrical contacts is also provided at the other end of the armature travel, for bridging by conductive means when the armature moves in an opposite sense.
  11. 11. A magnetic switch as claimed in claim 9 or 10, wherein the armature comprises the conductive means or the conductive means is a conductive layer or conductive member carried by the armature.
  12. 12. A magnetic switch as claimed in claim 9 or 10, wherein the contacts which are closed by movement of the armature to one end of its travel and the contacts are situated at the same end of the armature travel into which it has moved to close same.
  13. 13. A drive or switch as claimed in any of the preceding claims when within a sealed chamber.
  14. 14. A switch as claimed in claim 13, wherein at least part of the wall of the chamber is formed from electrical insulating material to provide a region for conductive feedthroughs to terminals external of the chamber to allow electrical connection to be made to the contacts therein.
  15. 15. A switch as claimed in claim 13 or 14, wherein the chamber is formed from plastics or glass or quartz.
  16. 16. A bistable magnetic drive as claimed in claim 1, comprising magnet means producing first and second magnetic fields, the polarity of the first and second fields being opposite, and a magnetisable armature mounted for movement between the two said fields, the armature being magnetised South/North or North/South depending on which of the two fields it occupies and requiring considerable force acting perpendicular to the magnetic flux lines to shift the armature out of the influence of either field once it is aligned therewith, wherein a magnetic or magnetisable shunt is provided which is movable into a position in which the magnetic flux of one of the first and second fields becomes diverted therethrough, so as to cause the armature to either remain in the unaffected field or immediately to move, under the influence of the unaffected magnetic field flux, so as tc occupy the unaffected field.
  17. 17. A magnetic drive as claimed in claim 16, wherein the magnetic shunt is permanently in position and the additional flux provided by the energising winding is selected to be sufficient to overcome the non-shunted field at the other end of the drive, whereby the induced flux is sufficient to move the armature from the non-shunted field into the shunted field, but as soon as the energy current is removed or significantly reduced, the armature will return to the non-shunted field end.
  18. 18. A magnetic drive as claimed in claim 16, wherein an additional electro-magnetic device is provided at the shunted field end of the drive, with which the armature makes contact when moved into the shunted field.
  19. 19. A magnetic drive as claimed in claim 18, wherein the additional device includes a magnetic core and the contact with the armature is such that there is no air gap to reduce the flux density after contact is made, which thereby enables the armature to be attracted away from the non-shunted field by a high electric current flowing in the additional device for a short period of time, but which can be reduced to a low holding current once the armature and device core make contact to hold the armature in contact with the core at the shunted field end.
  20. 20. A magnetic device as claimed in claim 19, which includes a fail-safe characteristic in that if the low holding electric current fails, the residual flux gradient present in the drive will be such as to cause the armature immediately to move to occupy the non-shunted field end where the static flux is highest.
  21. 21. A magnetic drive as claimed in claim 19 or 20, wherein the additional electromagnetic device is a solenoid having a large number of turns on a magnetic core, typically a core of ferromagnetic material.
  22. 22. A magnetic drive as claimed in any of the preceding claims, adapted to control a pneumatic or hydraulic valve or provide the movement necessary to open and close electrical contacts of an electrical switch.
  23. 23. A magnetic drive as claimed in any of claims 17 to 21, wherein a holding solenoid'is located within the drive at the end which is to be affected by the flux shunting element.
  24. 24. A magnetic drive as claimed in any of claims 17 to 20 in combination with a valve adapted to control the flow of an inflammable gas to a burner or jet.
  25. 25. A magnetic drive and valve combination as claimed in claim 24, further comprising a thermocouple located adjacent the burner or jet so as to be heated by a flame emanating therefrom to cause electric current to flow in any circuit connected to the thermocouple, and wherein the latter either produces, or controls the production of, the holding current for the solenoid at the shunted field end, and is such as to produce a magnetic flux sufficient to retain the armature in contact therewith at the shunted field end provided the thermocouple remains heated by the flame, whereby in the event of flame failure, the thermocouple cools, the holding current collapses and with it the magnetic flux linking the holding solenoid to the armature, thereby releasing the latter and enabling it to move to the higher flux concentration at the other end of its travel.
  26. 26. A magnetic drive and valve combination as claimed in claim 24, having a fail-safe characteristic in that the flux short circuiting device is mounted on a movable element, the position of which relative to the drive is controlled by a physical parameter which changes in the event of some failure (such as flame failure in a gas burner) which will result in the movable element shifting the flux shunting device from a position in which a relatively large air gap exists between it and the magnetic flux at one end of the drive, into a position in which the shunting element diverts most or all the said flux to significantly reduce the flux density at that end of the armature travel and cause the armature either to move to the other end of the drive to where the magnetic flux remains unaffected, or to remain at that said other end.
  27. 27. A magnetic drive and valve combination as claimed in claim 26, wherein the position of the movable element is controlled by the passage of an electric current, or is dependent upon a particular voltage being present, or a gas or fluid pressure being exerted against the movable element.
  28. 28. A magnetic drive and valve combination as claimed in claim 26 or 27, wherein the movable element is a bimetal strip, a piezo bender, a spring, a diaphragm or other device which will move under increasing or decreasing pressure.
  29. 29. A magnetic drive and valve combination as claimed in claim 26 or 27 in which the mechanism which determines the instantaneous position of the flux shunting element is adapted to respond to an increase in a monitored parameter such as temperature or pressure as well as or instead of a decrease, so that the flux shunting device can be moved into position so as to divert the flux at one end of the drive, either in response to flame failure (in the case of a gas burner) or in the event of excess temperature.
  30. 30. A magnetic drive as claimed in any of claims 1 to 24, wherein the armature is formed from magnetisable material, and in order to reduce its mass, magnetic poles are located at opposite ends of the drive with a relatively small gap between the two pairs of opposed magnetic pole faces, and the magnetisable part of the armature is reduced in size so as to just fit in the small gap between the pair of opposed pole faces at opposite ends of the drive, the said magnetisable part of the armature being secured to one end of a low mass connecting rod which extends through one or both ends of the magnetic drive to terminate externally thereof.
  31. 31, A magnetic drive as claimed in claim 30, wherein the connecting rod is formed from non-magnetic material.
  32. 32. A magnetic drive as claimed in any of claims 1 to 24, or 30 or 31, when combined with a chamber to or from which fluid can flow depending on the position of a valve closure member relative to a valve seating surrounding an opening in the chamber wall, which in one end position of the armature is closed by the closure member, and in the other end position of the armature, is unobstructed by the closure member.
  33. 33. A magnetic drive and chamber as claimed in claim 32, wherein a diaphragm seal is provided around the connecting rod, and the diaphragm material is selected so as to be impervious to the fluid in the chamber and is sufficiently flexible to permit linear movement of the connecting rod in response to movement of the magnetic armature.
    34. A magnetic drive and chamber as claimed in claim 33, wherein the diaphragm is generally circular in shape, includes a corrugated annular region to provide flexibility and displaceability of its central region relative to the circumference thereof, and is centrally perforated to allow the connecting rod to extend therethrough, but is sealed to the connecting rod, typically to a collar on the rod, the collar forming an integral part of or being sealingly fitted to the rod, and the periphery of the diaphragm is likewise bonded or otherwise sealingly joined to a larger diameter collar which is sealingly joined or integrally formed with an end wall of the magnetic drive assembly, which may form at least part of one wall of the fluid chamber into which the connecting rod and valve closure member extends.
  34. 34. A magnetic drive and chamber combination as claimed in claim 32,33 or 34, when combined with a plurality of similar said combinations, wherein the chambers are arranged in parallel and communicate with a common manifold and the orifices differ in size, and the drives are selected in such a manner that by opening different ones of the orifices, either alone, or in combination with other orifices, different effective overall orifice sizes can be obtained, so as to regulate the flow of fluid through the valves from the manifold, the overall open orifice area determining the rate of flow from the manifold for a given pressure differential.
  35. 35. A plural magnetic drive and chamber combination as claimed in claim 34, wherein the different overall orifice areas which can be obtained, constitute each of a sequence of area values such that a progression from zero to a maximum area (when all valves are open) can be effected in a series of known steps.
GB9914330A 1998-04-01 1999-06-21 Magnetic drives Expired - Lifetime GB2342504B (en)

Priority Applications (16)

Application Number Priority Date Filing Date Title
AT99949174T ATE274162T1 (en) 1998-10-08 1999-10-07 MAGNETIC DRIVE
ES99949174T ES2228111T3 (en) 1998-10-08 1999-10-07 MAGNETIC MOVEMENTS.
DE1999619557 DE69919557T2 (en) 1998-10-08 1999-10-07 MAGNETIC DRIVE
PCT/GB1999/003327 WO2000020786A1 (en) 1998-10-08 1999-10-07 Magnetic drives
GB0229887A GB2380064B (en) 1998-10-08 1999-10-07 Magnetic drives
EP04015857A EP1479956A3 (en) 1998-10-08 1999-10-07 Valve with magnetic drive
US09/807,043 US6598621B1 (en) 1998-04-01 1999-10-07 Magnetic drives
PT99949174T PT1119723E (en) 1998-10-08 1999-10-07 MAGNETIC UNITS
EP04015856A EP1482227A1 (en) 1998-10-08 1999-10-07 Magnetic drives
EP99949174A EP1119723B1 (en) 1998-10-08 1999-10-07 Magnetic drives
GB9923744A GB2342782B (en) 1998-10-08 1999-10-07 Magnetic drives
AU62159/99A AU6215999A (en) 1998-10-08 1999-10-07 Magnetic drives
EP04015111A EP1482226A1 (en) 1998-10-08 1999-10-07 Magnetic drive
GB0229888A GB2380065B (en) 1998-10-08 1999-10-07 Magnetic drives
JP2000574861A JP4359395B2 (en) 1998-10-08 1999-10-07 Magnetic drive
US10/449,486 US7021603B2 (en) 1998-10-08 2003-05-30 Electromagnetic actuator and integrated actuator and fluid flow control valve

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GBGB9821842.3A GB9821842D0 (en) 1998-10-08 1998-10-08 Valve for controlling gas flow
GBGB9907552.5A GB9907552D0 (en) 1998-10-08 1999-04-01 Valve for controlling gas flow
GBGB9912518.9A GB9912518D0 (en) 1999-05-29 1999-05-29 Magnetic drives

Publications (3)

Publication Number Publication Date
GB9914330D0 GB9914330D0 (en) 1999-08-18
GB2342504A true GB2342504A (en) 2000-04-12
GB2342504B GB2342504B (en) 2003-04-23

Family

ID=27269504

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9914330A Expired - Lifetime GB2342504B (en) 1998-04-01 1999-06-21 Magnetic drives

Country Status (1)

Country Link
GB (1) GB2342504B (en)

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2377555A (en) * 2001-04-24 2003-01-15 Camcon Ltd Electromagnetically operated valve
GB2387968A (en) * 2001-04-24 2003-10-29 Camcon Ltd Electromagnetically operated valve
WO2009147446A2 (en) 2008-06-07 2009-12-10 Camcon Limited Gas injection control devices and methods of operation thereof
US7665305B2 (en) 2005-12-29 2010-02-23 Delavan Inc Valve assembly for modulating fuel flow to a gas turbine engine
US7775052B2 (en) 2004-05-07 2010-08-17 Delavan Inc Active combustion control system for gas turbine engines
GB2480346A (en) * 2010-05-05 2011-11-16 Camcon Oil Ltd Electromagnetically operated valve
US8162287B2 (en) 2005-12-29 2012-04-24 Delavan Inc Valve assembly for modulating fuel flow to a gas turbine engine
WO2012052759A2 (en) 2010-10-20 2012-04-26 Camcon Oil Limited Fluid injection device
WO2012052760A2 (en) 2010-10-20 2012-04-26 Camcon Oil Limited Fluid injection device
WO2012069849A1 (en) 2010-11-26 2012-05-31 Camcon Oil Limited Lock assembly
US8200410B2 (en) 2008-03-12 2012-06-12 Delavan Inc Active pattern factor control for gas turbine engines
US8239114B2 (en) 2008-02-12 2012-08-07 Delavan Inc Methods and systems for modulating fuel flow for gas turbine engines
US8434310B2 (en) 2009-12-03 2013-05-07 Delavan Inc Trim valves for modulating fluid flow
EP2778485A1 (en) * 2013-03-13 2014-09-17 Kohler Mira Limited Valve
US9182047B2 (en) 2013-03-13 2015-11-10 Kohler Mira Limited Valve with fail-safe device
CN107068493A (en) * 2017-06-15 2017-08-18 南华大学 A kind of energy-saving electromagnetic switch
EP4122875A1 (en) * 2021-07-19 2023-01-25 Abb Schweiz Ag Robotized manifold system comprising a plurality of bistable valves

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108198732B (en) * 2016-07-30 2019-10-22 绍兴市逸晨医疗科技有限公司 A kind of stable method of gear unit in guard relay

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1513966A (en) * 1974-12-30 1978-06-14 Sds Elektro Gmbh Electromagnetic switching devices
GB2112212A (en) * 1981-04-30 1983-07-13 Matsushita Electric Works Ltd Polarized electromagnetic relay
GB2165096A (en) * 1984-03-05 1986-04-03 Mitsubishi Mining & Cement Co Electromagnetic actuator apparatus
GB2297429A (en) * 1993-09-11 1996-07-31 Mckean Brian Ass Ltd Bistable magnetic actuator

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1513966A (en) * 1974-12-30 1978-06-14 Sds Elektro Gmbh Electromagnetic switching devices
GB2112212A (en) * 1981-04-30 1983-07-13 Matsushita Electric Works Ltd Polarized electromagnetic relay
GB2165096A (en) * 1984-03-05 1986-04-03 Mitsubishi Mining & Cement Co Electromagnetic actuator apparatus
GB2297429A (en) * 1993-09-11 1996-07-31 Mckean Brian Ass Ltd Bistable magnetic actuator

Cited By (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2377555B (en) * 2001-04-24 2003-10-01 Camcon Ltd Electromagnetically operated valve
GB2387968A (en) * 2001-04-24 2003-10-29 Camcon Ltd Electromagnetically operated valve
GB2387968B (en) * 2001-04-24 2004-06-23 Camcon Ltd Electromagnetically operated valve
GB2377555A (en) * 2001-04-24 2003-01-15 Camcon Ltd Electromagnetically operated valve
US7775052B2 (en) 2004-05-07 2010-08-17 Delavan Inc Active combustion control system for gas turbine engines
US7665305B2 (en) 2005-12-29 2010-02-23 Delavan Inc Valve assembly for modulating fuel flow to a gas turbine engine
US8162287B2 (en) 2005-12-29 2012-04-24 Delavan Inc Valve assembly for modulating fuel flow to a gas turbine engine
US8239114B2 (en) 2008-02-12 2012-08-07 Delavan Inc Methods and systems for modulating fuel flow for gas turbine engines
US8200410B2 (en) 2008-03-12 2012-06-12 Delavan Inc Active pattern factor control for gas turbine engines
US8483931B2 (en) 2008-03-12 2013-07-09 Delavan Inc. Active pattern factor control for gas turbine engines
US8417434B2 (en) 2008-03-12 2013-04-09 Delavan Inc Active pattern factor control for gas turbine engines
WO2009147446A2 (en) 2008-06-07 2009-12-10 Camcon Limited Gas injection control devices and methods of operation thereof
EP2634364A1 (en) * 2008-06-07 2013-09-04 Camcon Oil Limited Gas injection control devices and methods of operation thereof
CN102057132B (en) * 2008-06-07 2014-11-05 卡姆肯石油有限公司 Gas injection control devices and methods of operation thereof
US8925638B2 (en) 2008-06-07 2015-01-06 Camcon Oil Limited Gas injection control devices and methods of operation thereof
CN102057132A (en) * 2008-06-07 2011-05-11 卡姆肯石油有限公司 Gas injection control devices and methods of operation thereof
EP2288787B1 (en) * 2008-06-07 2013-08-28 Camcon Oil Limited Gas injection control devices and methods of operation thereof
US8434310B2 (en) 2009-12-03 2013-05-07 Delavan Inc Trim valves for modulating fluid flow
GB2480346A (en) * 2010-05-05 2011-11-16 Camcon Oil Ltd Electromagnetically operated valve
US9046187B2 (en) 2010-05-05 2015-06-02 Camcon Oil Limited Electromagnetically operated switching devices and methods of actuation thereof
WO2012052759A2 (en) 2010-10-20 2012-04-26 Camcon Oil Limited Fluid injection device
WO2012052760A2 (en) 2010-10-20 2012-04-26 Camcon Oil Limited Fluid injection device
US9238452B2 (en) 2010-11-26 2016-01-19 Camcon Auto Limited Lock assembly
WO2012069849A1 (en) 2010-11-26 2012-05-31 Camcon Oil Limited Lock assembly
EP2778485A1 (en) * 2013-03-13 2014-09-17 Kohler Mira Limited Valve
US9182047B2 (en) 2013-03-13 2015-11-10 Kohler Mira Limited Valve with fail-safe device
US9644757B2 (en) 2013-03-13 2017-05-09 Kohler Mira Limited Valve with fail-safe device
US10443751B2 (en) 2013-03-13 2019-10-15 Kohler Mira Limited Valve with fail-safe device
CN107068493A (en) * 2017-06-15 2017-08-18 南华大学 A kind of energy-saving electromagnetic switch
CN107068493B (en) * 2017-06-15 2019-06-11 南华大学 A kind of energy-saving electromagnetic switch
EP4122875A1 (en) * 2021-07-19 2023-01-25 Abb Schweiz Ag Robotized manifold system comprising a plurality of bistable valves
WO2023001796A1 (en) * 2021-07-19 2023-01-26 Abb Schweiz Ag Robotized manifold system comprising a plurality of bistable valves

Also Published As

Publication number Publication date
GB2342504B (en) 2003-04-23
GB9914330D0 (en) 1999-08-18

Similar Documents

Publication Publication Date Title
US6598621B1 (en) Magnetic drives
GB2342504A (en) A bistable and monostable electromagnetic drive arrangement
US7021603B2 (en) Electromagnetic actuator and integrated actuator and fluid flow control valve
GB2380064A (en) Magnetic actuator
US4004258A (en) Position indicating pulse latching solenoid
US3212751A (en) Valve and permanent magnet
US4403765A (en) Magnetic flux-shifting fluid valve
US4538129A (en) Magnetic flux-shifting actuator
US20110001591A1 (en) Electromagnetic actuating mechanism
JPH04254306A (en) Magnetic apparatus
KR950002534B1 (en) Solenoid vlave
JPH0361777A (en) Solenoid valve using permanent magnet
KR19990063951A (en) Method and apparatus for manufacturing intake valve of plate type
US4114852A (en) Miniature reed-type valve
EP1381803B1 (en) Electromagnetically operated valve
RU2243441C1 (en) Solenoid valve
EP1479956A2 (en) Valve with magnetic drive
US602696A (en) Joseph denis cyprien chateau
GB2395362A (en) Improved electromagnetically operated device
JPS63231079A (en) Solenoid valve device
JP3251085B2 (en) solenoid valve
JPS57146970A (en) Gas flux control method by electromagnetic valve
JPS5872783A (en) Self holding solenoid valve
JP2765733B2 (en) Flow control valve with closing function
KR200407542Y1 (en) Directional valve for refrigerant

Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PE20 Patent expired after termination of 20 years

Expiry date: 20190620