US3532121A - Latching valve - Google Patents

Latching valve Download PDF

Info

Publication number
US3532121A
US3532121A US3532121DA US3532121A US 3532121 A US3532121 A US 3532121A US 3532121D A US3532121D A US 3532121DA US 3532121 A US3532121 A US 3532121A
Authority
US
United States
Prior art keywords
valve
permanent magnet
valve head
magnetic
force
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
Inventor
Oded E Sturman
Salvatore A Sciortino
Abdul R Kassir
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.)
HR TEXTRON Inc A CORP OF DE
Bell Aerospace Corp
Original Assignee
Bell Aerospace Corp
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
Application filed by Bell Aerospace Corp filed Critical Bell Aerospace Corp
Application granted granted Critical
Publication of US3532121A publication Critical patent/US3532121A/en
Assigned to HR TEXTRON INC., A CORP. OF DE. reassignment HR TEXTRON INC., A CORP. OF DE. ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: TEXTRON, INC.,
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/8593Systems
    • Y10T137/86493Multi-way valve unit
    • Y10T137/86815Multiple inlet with single outlet

Definitions

  • the magnetic potential of the permanent magnet decreases whereby the suspension plate moves the valve head toward the opposite seat.
  • the other permanent magnet secures the valve head in that position until the application ofa voltage of polarity opposite to the polarity of the first-applied voltage.
  • the suspension plate also serves to isolate the magnetic circuit from the valve head-seat area.
  • Latching valves are utilized when there is a need to switch from one valve position to another upon receipt of a signal therefor and to maintain the new condition in the absence of a signal to switch back.
  • a valve can be switched open or closed, or flow can be switched from a primary inlet port to secondary inlet port, upon the receipt of an electrical voltage pulse.
  • latching valves having increased safety, reliability and responsiveness.
  • a valve comprising a valve assembly including a valve head, a seat for the valve head and a pair of permanent magnets for applying magnetic force on the valve assembly to bias the valve assembly to a particular position with respect to the seat.
  • the valve assembly includes mechanical means that are deformed to a first configuration when the valve head is in a particular position. However, the spring moment of the mechanical means is less than the magnetic force of the permanent magnet biasing the valve head in its position.
  • voltage means are series disposed in the permanent magnetic circuit flux path for decreasing the magnetic potential of the permanent magnet.
  • the magnetic force from the permanent magnet is decreased, whereby the mechanical means springs the valve head out of its position.
  • the second permanent magnet latches the valve head in its opposite position and deforms the mechanical means to an opposite configuration.
  • the spring moment of the mechanical means is insufficient to overcome the biasing force of the permanent magnet and in order to release the valve head another voltage pulse, of opposite polarity, must be applied.
  • the voltage means is also series disposed in the magnetic circuit flux path of this permanent magnet and upon the application of the opposite polarity voltage pulse, the magnetic force exerted by the second permanent magnet is decreased so that the resiliency of the mechanical means returns the valve head to its initial position to be latched thereat by the first permanent magnet.
  • the result is a latching valve that switches valve conditions upon the receipt of an appropriate electrical voltage pulse.
  • the mechanical means includes a suspension plate that supports the valve head on one side and an armature of magnetically permeable material on the other side movably associated with the valve head.
  • a coil is disposed on the armature and is in series with the magnetic flux paths of both permanent magnets. The coil is energizable to develop a magnetic potential in opposition to the potential of one of the permanent magnets upon the receipt ofa voltage pulse of a particular polarity, and is energizable to develop a magnetic potential in opposition to the other permanent magnet potential upon receipt of a voltage pulse of opposite polarity.
  • FIG. I is a schematic, cross-sectional representation of a valve constructed in accordance with the present invention.
  • FIG. 2 depicts a force-deflection plot for valves of this invention.
  • FIG. 3 depicts a typical demagnetization curve for an Alnico VIII permanent magnet.
  • a valve 10 having a housing 12 defining a chamber 14, primary and secondary inlet ports 16 and I8, respectively, and an outlet port (not shown).
  • One wall of the chamber 14 is defined by a circular suspension plate 20 that completely encloses the chamber 14 at that end thereof and isolates the chamber 14 from the magnetic circuit as more fully explained below.
  • a flapper 22 extends into the chamber 14 from the suspension plate 20 and carries a valve head 24 at its end.
  • a stem 26 is disposed on the other side of the suspension plate 20 as a continuation of the flapper 22.
  • the end of the stem 26 is encased in an armature sleeve 28 of magnetically permeable material and that end is disposed between a pair of magnetic poles 30 and 32.
  • Each pole 30 and 32 comprises upper and lower frames 34 and 36, respectively, of magnetically permeable material sandwiching an Alnico permanent magnets 38 and 39, respectively, but leaving a channel 40 adjacent the armature sleeve 28 between the upper and lower frames 34 and 36.
  • a coil 42 is disposed on the armature sleeve 28 and supported within the channel 40 between the upper and lower frames 34 and 36.
  • the poles 30 and 32 and permanent magnets 38 and 39 are secured to the housing 12 by means of screws (not shown) to provide a rigid assembly. Electrical leads (not shown) are provided for supplying energizing current to the coil 42.
  • the circular suspension plate 20 is deformable and serves both as a mechanical spring as well as to isolate the magnetic circuit from the chamber 14.
  • the suspension plate 20 is similar to a flat flexure diaphragm only in that it physically separates the chamber 14 from the upper areas of the valve and flexes in response to movement of the armature 28, but it is much thicker and has a spring moment of much greater magnitude than typical flexure diaphragms.
  • the thickness and spring rate of the suspension plate 20 is very important to the operation of the valve.
  • the suspension plate 20 must be deformable but thick enough to withstand fluid pressures and have the mechanical strength to return the valve head 24.
  • the suspension plate 20 can be constructed, as shown, as a separate member secured between the housing l2 and the underside of the poles 30 and 32, or it can be a part of the housing 12 itself, i.e., an integral wall thereof formed thin enough to be deformable; the bottom wall 50 of the housing 12 can then be separable from the remainder of the housing 12 and threadable therein to form the enclosed chamber 14.
  • valve head 24 is provided with a centrally disposed cylindrical aperture 25 for receipt therein, in ball and socket fashion, of the knob end 27 of the flapper 22.
  • the valve head 24 is supported by a pin member 29 straddling the bottom of the valve chamber 14 and having its end embedded in opposite walls thereof.
  • the valve head 24 carries an ultra hard tungsten carbide tip 52 on each port-facing side thereof. Mating tungsten carbide seats 54 and 55 are retained within the ports 16 and 18.
  • the ports 16 and 18 are provided with annular grooves 56 and 58 midway thereof.
  • Retaining rings 60 and 61 are disposed within the grooves 56 and 58 and in opposing annular grooves 62 and 63 in the tungsten carbide seats 54 and 55, respectively.
  • the retaining rings 60 and 61 abut annular flanges 64 and 65 on the seats 54 and 55, respectively, to thereby secure the seats within the ports.
  • the magnetic attraction of the stem 26, via the magnetically permeable sleeve 28, to the permanent magnet 39 on the right side pre-loads the valve head 24 against the primary inlet port seat 54, preventing fluid flow therethrough and fluid flows through the secondary inlet port 18.
  • the parts are sized so that the valve head 24 is pressed firmly against its seat 54 while the armature 28 barely contacts the right side pole 32.
  • the Alnico magnets 38 and 39 are arranged with opposite polarities in the same direction, e.g., the permanent magnet 38 on the left hand side has its north pole facing upwardly whereas the permanent magnet 39 on the right hand side has its north pole facing downwardly.
  • the coil 42 In order to release the valve head from its latched position, the coil 42 must be energized with a voltage of polarity and magnitude such as to oppose the permanent magnet 39 potential. Sufficient opposite magnetic potential must be generated to reduce the permanent magnet 39 force on the armature 28 enough to allow the spring moment of the deformed suspension plate 20 to move the armature-flapper-valve head assembly 28-262224-52 out of its seat 54.
  • the opposite permanent magnet 38 has sufficient magnetic potential, particularly in combination with the magnetic flux generated by the coil 42 current, so that at this point the armature 28 is magnetically attracted to the other permanent magnet 38 and latched thereat, even in the absence of the coil current 42.
  • the result is that the valve head 24 is swept across the valve chamber 14 to seat against the secondary inlet port seat 55 and allow fluid to flow from the primary inlet port 16.
  • FIG. 2 depicts changes in magnetic and spring moment with changes in deflection of the suspension plate 20 (pressure of the fluid is assumed as zero for simplicity of explanation).
  • the valve is normally closed by a pre-loading permanent magnet 39 force exerted by the flapper 22 on the valve head 24.
  • the pro-loading permanent magnetic force is at its maximum since, with no air gap, the reluctance of the magnetic circuit thereat is at its minimum.
  • the suspension plate acting as a spring is unstressed when the valve head is positioned midway between the primary and secondary ports 16 and 18, but exerts a force opposing the permanent magnet 39 moment when the valve head 24 is seated.
  • the pre-loading force is equal to the moment generated by the magnetic force of the permanent magnet 39 minus the moment required to bend the suspension plate 20 per unit length of the flapper 22 minus the moment generated by the opposite permanent magnet 38.
  • the pole 32 is sized so that it is substantially saturated by the permanent magnet.
  • FIG. 3 depicts the energy product curves and major A and minor B hysteresis loop curves of an Alnico VIII permanent magnet. Importantly, demagnetization occurs on the minor hysteresis loop B as illustrated by conditions l4 thereof.
  • the permanent magnet 39 potential is decreased to 37.5 force units.
  • the coil 42 potential also generates magnetic flux about the left side pole 30 loop at all positions throughout the air gap thereat of, say, 3.3 force units.
  • the permanent magnet 38 thereat also generates magnetic flux about the left side pole loop of, say, 8.0 units on the armature sleeve 28 at the present position.
  • the magnetic potential of the permanent magnet 39 is only 9.4 units which is opposed by a magnetic potential of the current enhanced permanent magnet ofabout 65.6 units for a total net moment of minus 56.2 units to accelerate the armatureflapper-valve head assembly 28-26-22-24-52 past the null point.
  • the left side pole 30 is sized so that it is not saturated by the permanent magnet 38 thereat. However, upon application of the enhancing coil potential, a saturation condition obtains to impart a force on the armature 28 when thereat of 212.5 force units.
  • the magnetic moment due to the coil 42 ceases; however, the left hand permanent magnet 38 still has a magnetic attraction force of units which opposes the opposite permanent magnet 39 magnetic attraction of 8.0 units and the spring moment of 75 units for a total net force of minus 67 units to latch the valve head 24 against the secondary port seat 55.
  • the foregoing described latching valve utilizes differently sized poles and is particularly useful when a large difference in pressure differential is encountered in different latching directions.
  • the description is analogously applicable to symmetrically formed valves; for example, the force-deflection diagram of FIG. 2 can apply to operation in either direction of a symmetrical valve.
  • the suspension plate 20 not only acts as a mechanical spring but also isolates the magnetic circuits from the fluid in the chamber 14. Further, magnetically permeable material is utilized only in the vicinity of the magnetic circuit so that the fluid chamber 14 area is unaffected by generated magnetic fields.
  • a latching valve comprising:
  • valve assembly including a valve head
  • first permanent magnet means for applying a first predetermined magnetic force on said valve assembly to bias said valve head to a first position with respect to said seat;
  • valve assembly including mechanical means that are deformed to a first configuration when said valve head is in said first position to urge said valve head toward a second position, with respect to said seat, with a spring moment less than said first predetermined magnetic force;
  • second permanent magnet means for applying a second predetermined magnetic force on said valve assembly of polarity opposite to said first magnetic force to bias said valve head to said second position;
  • said mechanical means being deformed to a second configuration when said valve head is in said second position to urge said valve head toward said first position with a spring moment less than said second predetermined magnetic force
  • said voltage means being series disposed in the second permanent magnet flux path for decreasing the magnetic potential of said second permanent magnet upon the application of voltage of polarity opposite to said first voltage to thereby decrease said second magnetic force whereby said mechanical means can move said valve head toward said first position.
  • valve of claim 1 including means isolating said magnetic potentials from said seat.
  • valve assembly comprises a magnetically permeable member supported between said first and second permanent magnets on one side of said mechanical means and said valve head supported on another side thereof, said mechanical means being shaped and disposed to isolate said magnetic potentials from said seat.
  • valve assembly comprises an armature of magnetically permeable material, spaced from said valve head but movably associated therewith and subject to said magnetic forces, and said voltage means comprises a coil on said armature energizable to selectively oppose one or the other of said magnetic potentials.
  • valve of claim 1 wherein said seat is disposed at said first position and including a second valve head seat at said second position, said valve head having opposite surfaces engageable with respective ones of said seats.
  • each seat defines a port of said valve, said valve defining an additional port communicating with one seat when the valve is in one latched condition and with the other seat when said valve is in an opposite latched condition.
  • a latching valve comprising:
  • a housing defining a chamber having first and second ports and at least one deformable wall
  • valve head at each of said ports, said valve head having opposite surfaces engageable with respective ones of said seats;
  • a first permanent magnet operative with a first magnetic force to magnetically attract said armature to bias said valve head to one of said seats and deform said wall to be a first configuration
  • a second permanent magnet operative with a magnetic force of opposite polarity to said first magnetic force to magnetically attract said armature when said coil is energized with said voltage of first polarity to bias said valve head to the other of said seats and deform said wall to a second configuration
  • said coil being series disposed in second permanent magnet flux path and energizable with a voltage of polarity opposite to said first polarity to oppose the magnetic potential of said second permanent magnet to thereby decrease its magnetic attraction.
  • said deformable wall has sufficient spring moment to carry said valve head out of its seated position when said coil is appropriately energized.

Description

Unite States atent [54] LATCHING VALVE 8 Claims, 3 Drawing Figs.
[52] U.S. Cl l37/625.4, 251/65, 251/129, 251/75 [51] lnt.Cl r F16k 31/08 [50] Field of Search 251/65,
[56] References Cited UNITED STATES PATENTS 3,368,788 2/1968 Padula t. 251/65 3,379,214 4/1968 Weinberg 251/65X Boonshaft et a1 251/77X ABSTRACT: A latching valve containing two separate magnetic circuits of opposite polarity with a common armature and coil thereon. Each magnetic circuit consists of a permanent magnet in series with the coil. A resilient suspension plate, with high spring moment, carries a valve head on one side thereof and the armature on the other side to constitute an integrated assembly. The valve head has opposite surfaces engageable with oppositely disposed valve seats. Initially, one of the permanent magnets biases the valve head to one of these seats, with resultant deformation of the suspension plate. Upon application of a voltage of appropriate polarity, the magnetic potential of the permanent magnet decreases whereby the suspension plate moves the valve head toward the opposite seat. The other permanent magnet then secures the valve head in that position until the application ofa voltage of polarity opposite to the polarity of the first-applied voltage. The suspension plate also serves to isolate the magnetic circuit from the valve head-seat area.
Patented Oct. 1970 3,532,121
LATCHING VALVE BACKGROUND OF THE INVENTION 1. Field of the Invention The fields of art to which the invention pertains include the fields of fluid handling, valve and valve actuation.
2. Description of the Prior Art Latching valves are utilized when there is a need to switch from one valve position to another upon receipt of a signal therefor and to maintain the new condition in the absence of a signal to switch back. By such means a valve can be switched open or closed, or flow can be switched from a primary inlet port to secondary inlet port, upon the receipt of an electrical voltage pulse. There is a need for latching valves having increased safety, reliability and responsiveness.
SUMMARY OF THE INVENTION The present invention represents a new generation of latching valves. The valves provided herein are superior to present latching valves in that they are more reliable, more responsive, safer and consume less power. Specifically, a valve is provided comprising a valve assembly including a valve head, a seat for the valve head and a pair of permanent magnets for applying magnetic force on the valve assembly to bias the valve assembly to a particular position with respect to the seat. The valve assembly includes mechanical means that are deformed to a first configuration when the valve head is in a particular position. However, the spring moment of the mechanical means is less than the magnetic force of the permanent magnet biasing the valve head in its position. In order to release the valve head, voltage means are series disposed in the permanent magnetic circuit flux path for decreasing the magnetic potential of the permanent magnet. Upon the application of voltage of appropriate polarity, the magnetic force from the permanent magnet is decreased, whereby the mechanical means springs the valve head out of its position. The second permanent magnet latches the valve head in its opposite position and deforms the mechanical means to an opposite configuration. Here also, the spring moment of the mechanical means is insufficient to overcome the biasing force of the permanent magnet and in order to release the valve head another voltage pulse, of opposite polarity, must be applied. The voltage means is also series disposed in the magnetic circuit flux path of this permanent magnet and upon the application of the opposite polarity voltage pulse, the magnetic force exerted by the second permanent magnet is decreased so that the resiliency of the mechanical means returns the valve head to its initial position to be latched thereat by the first permanent magnet. The result is a latching valve that switches valve conditions upon the receipt of an appropriate electrical voltage pulse.
In particular embodiments, the mechanical means includes a suspension plate that supports the valve head on one side and an armature of magnetically permeable material on the other side movably associated with the valve head. A coil is disposed on the armature and is in series with the magnetic flux paths of both permanent magnets. The coil is energizable to develop a magnetic potential in opposition to the potential of one of the permanent magnets upon the receipt ofa voltage pulse of a particular polarity, and is energizable to develop a magnetic potential in opposition to the other permanent magnet potential upon receipt of a voltage pulse of opposite polarity.
Improved reliability is obtained as a result of design simplicity and complete magnetic circuit isolation. Design simplicity is accomplished by the use ofa mechanism containing only one moving part, the armature-flapper assembly. A fast dynamic response is obtained as a result of a greatly reduced number of ampere turns, typically a reduction of 16 to l. The reduction in ampere turns is allowed because (a) the required coil flux density to generate a given output force is reduced due to the presence of the permanent magnet fields; (b) the reluctance of the magnetic circuit is reduced because no air gaps are required at the closed positions; and (c) a reduction of the magnetic circuit reluctance results in a decrease in the number of magnetic leakage lines. Since the time constant is directly proportional to the square of the number of coil turns, response time is dramatically decreased. Power consumption is improved since that is proportional to the square of the input current, reduced with the reduction in ampere turns. Safety is improved since the present construction readily allows designing for pre-load forces larger than necessary to meet leakage requirements, allows the force available to open the valve to be made larger than the pressure force, and allows the flow area to be made larger than required.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. I is a schematic, cross-sectional representation of a valve constructed in accordance with the present invention;
FIG. 2 depicts a force-deflection plot for valves of this invention; and
FIG. 3 depicts a typical demagnetization curve for an Alnico VIII permanent magnet.
DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring to FIG. 1, a valve 10 is shown having a housing 12 defining a chamber 14, primary and secondary inlet ports 16 and I8, respectively, and an outlet port (not shown). One wall of the chamber 14 is defined by a circular suspension plate 20 that completely encloses the chamber 14 at that end thereof and isolates the chamber 14 from the magnetic circuit as more fully explained below. A flapper 22 extends into the chamber 14 from the suspension plate 20 and carries a valve head 24 at its end. A stem 26 is disposed on the other side of the suspension plate 20 as a continuation of the flapper 22. The end of the stem 26 is encased in an armature sleeve 28 of magnetically permeable material and that end is disposed between a pair of magnetic poles 30 and 32. Each pole 30 and 32 comprises upper and lower frames 34 and 36, respectively, of magnetically permeable material sandwiching an Alnico permanent magnets 38 and 39, respectively, but leaving a channel 40 adjacent the armature sleeve 28 between the upper and lower frames 34 and 36. A coil 42 is disposed on the armature sleeve 28 and supported within the channel 40 between the upper and lower frames 34 and 36. The poles 30 and 32 and permanent magnets 38 and 39 are secured to the housing 12 by means of screws (not shown) to provide a rigid assembly. Electrical leads (not shown) are provided for supplying energizing current to the coil 42.
The circular suspension plate 20 is deformable and serves both as a mechanical spring as well as to isolate the magnetic circuit from the chamber 14. The suspension plate 20 is similar to a flat flexure diaphragm only in that it physically separates the chamber 14 from the upper areas of the valve and flexes in response to movement of the armature 28, but it is much thicker and has a spring moment of much greater magnitude than typical flexure diaphragms. The thickness and spring rate of the suspension plate 20 is very important to the operation of the valve. The suspension plate 20 must be deformable but thick enough to withstand fluid pressures and have the mechanical strength to return the valve head 24. The suspension plate 20 can be constructed, as shown, as a separate member secured between the housing l2 and the underside of the poles 30 and 32, or it can be a part of the housing 12 itself, i.e., an integral wall thereof formed thin enough to be deformable; the bottom wall 50 of the housing 12 can then be separable from the remainder of the housing 12 and threadable therein to form the enclosed chamber 14.
Referring to the valve head-seat area, the valve head 24 is provided with a centrally disposed cylindrical aperture 25 for receipt therein, in ball and socket fashion, of the knob end 27 of the flapper 22. The valve head 24 is supported by a pin member 29 straddling the bottom of the valve chamber 14 and having its end embedded in opposite walls thereof.
The valve head 24 carries an ultra hard tungsten carbide tip 52 on each port-facing side thereof. Mating tungsten carbide seats 54 and 55 are retained within the ports 16 and 18. The ports 16 and 18 are provided with annular grooves 56 and 58 midway thereof. Retaining rings 60 and 61 are disposed within the grooves 56 and 58 and in opposing annular grooves 62 and 63 in the tungsten carbide seats 54 and 55, respectively. The retaining rings 60 and 61 abut annular flanges 64 and 65 on the seats 54 and 55, respectively, to thereby secure the seats within the ports.
In operation, the magnetic attraction of the stem 26, via the magnetically permeable sleeve 28, to the permanent magnet 39 on the right side, (in the drawing) pre-loads the valve head 24 against the primary inlet port seat 54, preventing fluid flow therethrough and fluid flows through the secondary inlet port 18. To allow maximum transfer of force to the valve head-seat area, the parts are sized so that the valve head 24 is pressed firmly against its seat 54 while the armature 28 barely contacts the right side pole 32.
The Alnico magnets 38 and 39 are arranged with opposite polarities in the same direction, e.g., the permanent magnet 38 on the left hand side has its north pole facing upwardly whereas the permanent magnet 39 on the right hand side has its north pole facing downwardly. In order to release the valve head from its latched position, the coil 42 must be energized with a voltage of polarity and magnitude such as to oppose the permanent magnet 39 potential. Sufficient opposite magnetic potential must be generated to reduce the permanent magnet 39 force on the armature 28 enough to allow the spring moment of the deformed suspension plate 20 to move the armature-flapper-valve head assembly 28-262224-52 out of its seat 54. The opposite permanent magnet 38 has sufficient magnetic potential, particularly in combination with the magnetic flux generated by the coil 42 current, so that at this point the armature 28 is magnetically attracted to the other permanent magnet 38 and latched thereat, even in the absence of the coil current 42. The result is that the valve head 24 is swept across the valve chamber 14 to seat against the secondary inlet port seat 55 and allow fluid to flow from the primary inlet port 16.
Referring to the operation of the valve R in more detail, FIG. 2 depicts changes in magnetic and spring moment with changes in deflection of the suspension plate 20 (pressure of the fluid is assumed as zero for simplicity of explanation). The valve is normally closed by a pre-loading permanent magnet 39 force exerted by the flapper 22 on the valve head 24. At the initial position, the pro-loading permanent magnetic force is at its maximum since, with no air gap, the reluctance of the magnetic circuit thereat is at its minimum. The suspension plate acting as a spring is unstressed when the valve head is positioned midway between the primary and secondary ports 16 and 18, but exerts a force opposing the permanent magnet 39 moment when the valve head 24 is seated. Accordingly, the pre-loading force is equal to the moment generated by the magnetic force of the permanent magnet 39 minus the moment required to bend the suspension plate 20 per unit length of the flapper 22 minus the moment generated by the opposite permanent magnet 38. With reference to FIG. 2, the pre-loading force is equal to Fmo, minus Fsp minus Fmo. (I5075 8.0)=67 units of force. The pole 32 is sized so that it is substantially saturated by the permanent magnet.
When the coil 42 is energized, magnetic potential is developed across the armature sleeve 28. This potential opposes the permanent magnet 39 potential, thereby decreasing the force due to the permanent magnet 39. This effect can be illustrated with reference to FIG. 3 which depicts the energy product curves and major A and minor B hysteresis loop curves of an Alnico VIII permanent magnet. Importantly, demagnetization occurs on the minor hysteresis loop B as illustrated by conditions l4 thereof.
Referring back to FIG. 2, when the coil 42 is energized as described, the permanent magnet 39 potential is decreased to 37.5 force units. The coil 42 potential also generates magnetic flux about the left side pole 30 loop at all positions throughout the air gap thereat of, say, 3.3 force units. The permanent magnet 38 thereat also generates magnetic flux about the left side pole loop of, say, 8.0 units on the armature sleeve 28 at the present position. The result is that the net magnetic moment (in FIG. 1, the right side minus the left side moments) is equal to Fmiminus Fmi+ (37.5 l1.3) =26.2 force units which is opposed by the spring bending moment of the suspension plate 20 of 75 units minus the pressure moment of the fluid between the ports 16 and 18 (here zero). This results in a total net force of 48.8 units to move the armature-flappervalve head assembly 28-2622-24-52 from the primary port seat 54 toward the secondary port seat 55.
At the spring null position of the spring plate 20, the magnetic potential of the permanent magnet 39 is only 9.4 units which is opposed by a magnetic potential of the current enhanced permanent magnet ofabout 65.6 units for a total net moment of minus 56.2 units to accelerate the armatureflapper-valve head assembly 28-26-22-24-52 past the null point. In this example, the left side pole 30 is sized so that it is not saturated by the permanent magnet 38 thereat. However, upon application of the enhancing coil potential, a saturation condition obtains to impart a force on the armature 28 when thereat of 212.5 force units. With the valve head 24 seated against the secondary port seat 55, and with the coil 42 still energized, the current enhanced left hand permanent magnet 38 force potential of 212.5 units opposes the right hand permanent magnet 39 current limited potential of 4.7 units and a spring moment of 75 units for a total net force of minus 132.8 units to bias the valve head 24 against the secondary port seat 55. When the current to the coil 42 is removed, the magnetic moment due to the coil 42 ceases; however, the left hand permanent magnet 38 still has a magnetic attraction force of units which opposes the opposite permanent magnet 39 magnetic attraction of 8.0 units and the spring moment of 75 units for a total net force of minus 67 units to latch the valve head 24 against the secondary port seat 55. To release the valve head 24 from the secondary port seat 55 and switch it back into latching engagement with the primary port seat 54, one need merely energize the coil 42 with a similar voltage pulse of opposite polarity. The force-deflection diagram of FIG. 2 would again apply, but with the magnitudes appropriate to reverse operation. An inspection of the force-deflection diagram of FIG. 2 reveals that there are static moments available at all armature positions to accelerate the valve head from one seat into latching engagement with the other seat.
The foregoing described latching valve utilizes differently sized poles and is particularly useful when a large difference in pressure differential is encountered in different latching directions. The description is analogously applicable to symmetrically formed valves; for example, the force-deflection diagram of FIG. 2 can apply to operation in either direction of a symmetrical valve.
The suspension plate 20 not only acts as a mechanical spring but also isolates the magnetic circuits from the fluid in the chamber 14. Further, magnetically permeable material is utilized only in the vicinity of the magnetic circuit so that the fluid chamber 14 area is unaffected by generated magnetic fields.
We Claim:
1. A latching valve, comprising:
a valve assembly including a valve head;
a seat for said valve head;
first permanent magnet means for applying a first predetermined magnetic force on said valve assembly to bias said valve head to a first position with respect to said seat;
said valve assembly including mechanical means that are deformed to a first configuration when said valve head is in said first position to urge said valve head toward a second position, with respect to said seat, with a spring moment less than said first predetermined magnetic force;
voltage means series disposed in the first permanent magnet flux path for decreasing the magnetic potential of said first permanent magnet upon the application of first voltage of appropriate polarity to thereby decrease said first magnetic force whereby said mechanical means can move said valve head toward said second position;
second permanent magnet means for applying a second predetermined magnetic force on said valve assembly of polarity opposite to said first magnetic force to bias said valve head to said second position;
said mechanical means being deformed to a second configuration when said valve head is in said second position to urge said valve head toward said first position with a spring moment less than said second predetermined magnetic force; and
said voltage means being series disposed in the second permanent magnet flux path for decreasing the magnetic potential of said second permanent magnet upon the application of voltage of polarity opposite to said first voltage to thereby decrease said second magnetic force whereby said mechanical means can move said valve head toward said first position.
2. The valve of claim 1 including means isolating said magnetic potentials from said seat.
3. The valve of claim 1 wherein said valve assembly comprises a magnetically permeable member supported between said first and second permanent magnets on one side of said mechanical means and said valve head supported on another side thereof, said mechanical means being shaped and disposed to isolate said magnetic potentials from said seat.
4. The valve of claim 1 wherein said valve assembly comprises an armature of magnetically permeable material, spaced from said valve head but movably associated therewith and subject to said magnetic forces, and said voltage means comprises a coil on said armature energizable to selectively oppose one or the other of said magnetic potentials.
5. The valve of claim 1 wherein said seat is disposed at said first position and including a second valve head seat at said second position, said valve head having opposite surfaces engageable with respective ones of said seats.
6. The valve of claim 5 wherein each seat defines a port of said valve, said valve defining an additional port communicating with one seat when the valve is in one latched condition and with the other seat when said valve is in an opposite latched condition.
7. A latching valve, comprising:
a housing defining a chamber having first and second ports and at least one deformable wall;
a member carrying a valve head between said ports on one side of said deformable wall;
a seat for said valve head at each of said ports, said valve head having opposite surfaces engageable with respective ones of said seats;
an armature of magnetically permeable material carried on the opposite side of said deformable wall;
a first permanent magnet operative with a first magnetic force to magnetically attract said armature to bias said valve head to one of said seats and deform said wall to be a first configuration;
a coil on said armature series disposed in the first permanent magnet flux path and energizable with a voltage of appropriate first polarity to oppose the magnetic potential of said first permanent magnet to thereby decrease its magnetic attraction;
a second permanent magnet operative with a magnetic force of opposite polarity to said first magnetic force to magnetically attract said armature when said coil is energized with said voltage of first polarity to bias said valve head to the other of said seats and deform said wall to a second configuration; and
said coil being series disposed in second permanent magnet flux path and energizable with a voltage of polarity opposite to said first polarity to oppose the magnetic potential of said second permanent magnet to thereby decrease its magnetic attraction. 8. The valve of claim 7 wherein said deformable wall has sufficient spring moment to carry said valve head out of its seated position when said coil is appropriately energized.
US3532121D 1969-01-15 1969-01-15 Latching valve Expired - Lifetime US3532121A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US79129069A 1969-01-15 1969-01-15

Publications (1)

Publication Number Publication Date
US3532121A true US3532121A (en) 1970-10-06

Family

ID=25153249

Family Applications (1)

Application Number Title Priority Date Filing Date
US3532121D Expired - Lifetime US3532121A (en) 1969-01-15 1969-01-15 Latching valve

Country Status (1)

Country Link
US (1) US3532121A (en)

Cited By (68)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3790127A (en) * 1972-11-03 1974-02-05 Vapor Corp Hydraulic valve
DE2511152A1 (en) * 1975-03-14 1976-09-23 Daimler Benz Ag ELECTROMAGNETIC CONTROL VALVE, ESPECIALLY FOR AUTOMATICALLY SWITCHING MOTOR VEHICLE TRANSMISSIONS
US3982562A (en) * 1974-10-04 1976-09-28 Allied Chemical Corporation Pressure control apparatus
US4127360A (en) * 1976-12-16 1978-11-28 Carpenter Clarence W Bumpless pump apparatus adjustable to meet slave system needs
US4208361A (en) * 1976-04-15 1980-06-17 Nissan Motor Company, Limited Automobile with altitude compensated fuel feed means
EP0040909A1 (en) * 1980-05-16 1981-12-02 Westinghouse Brake And Signal Company Limited Fluid pressure control valves
US4385642A (en) * 1981-01-19 1983-05-31 Hydraulic Servocontrols Corporation Bi-stable electrically operated valve
FR2552196A1 (en) * 1983-09-21 1985-03-22 Lorch & Co Kg J ELECTROMAGNETIC VALVE
US4561632A (en) * 1983-09-21 1985-12-31 J. Lorch Gesellschaft & Co. Kg Solenoid valve
EP0177944A2 (en) * 1984-10-12 1986-04-16 H. Kuhnke GmbH KG Bistable solenoid valve
EP0235451A1 (en) * 1985-11-29 1987-09-09 Fujikura Rubber Ltd. Directional control valve
US4794843A (en) * 1986-09-24 1989-01-03 Poling Denzil C Hydraulic valve for controlling single-acting cylinder
US4988074A (en) * 1988-05-17 1991-01-29 Hi-Ram, Inc. Proportional variable force solenoid control valve
EP0493843A1 (en) * 1990-12-03 1992-07-08 Koninklijke Philips Electronics N.V. Device for interrupting a material flow
US5161578A (en) * 1986-01-06 1992-11-10 Carrier Corporation Warm-up/changeover valve or proximity switch
US5407131A (en) * 1994-01-25 1995-04-18 Caterpillar Inc. Fuel injection control valve
US5421521A (en) * 1993-12-23 1995-06-06 Caterpillar Inc. Fuel injection nozzle having a force-balanced check
US5449119A (en) * 1994-05-25 1995-09-12 Caterpillar Inc. Magnetically adjustable valve adapted for a fuel injector
US5470043A (en) * 1994-05-26 1995-11-28 Lockheed Idaho Technologies Company Magnetic latching solenoid
US5474234A (en) * 1994-03-22 1995-12-12 Caterpillar Inc. Electrically controlled fluid control valve of a fuel injector system
US5479901A (en) * 1994-06-27 1996-01-02 Caterpillar Inc. Electro-hydraulic spool control valve assembly adapted for a fuel injector
US5488340A (en) * 1994-05-20 1996-01-30 Caterpillar Inc. Hard magnetic valve actuator adapted for a fuel injector
US5494220A (en) * 1994-08-08 1996-02-27 Caterpillar Inc. Fuel injector assembly with pressure-equalized valve seat
US5494219A (en) * 1994-06-02 1996-02-27 Caterpillar Inc. Fuel injection control valve with dual solenoids
WO1996011350A1 (en) * 1994-10-07 1996-04-18 Ian Malcolm Chatwin Solenoid actuated bi-stable pilot valve
US5597118A (en) * 1995-05-26 1997-01-28 Caterpillar Inc. Direct-operated spool valve for a fuel injector
US5605289A (en) * 1994-12-02 1997-02-25 Caterpillar Inc. Fuel injector with spring-biased control valve
US5628293A (en) * 1994-05-13 1997-05-13 Caterpillar Inc. Electronically-controlled fluid injector system having pre-injection pressurizable fluid storage chamber and direct-operated check
US5673669A (en) * 1994-07-29 1997-10-07 Caterpillar Inc. Hydraulically-actuated fluid injector having pre-injection pressurizable fluid storage chamber and direct-operated check
US5687693A (en) * 1994-07-29 1997-11-18 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US5697342A (en) * 1994-07-29 1997-12-16 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US5720318A (en) * 1995-05-26 1998-02-24 Caterpillar Inc. Solenoid actuated miniservo spool valve
US5826562A (en) * 1994-07-29 1998-10-27 Caterpillar Inc. Piston and barrell assembly with stepped top and hydraulically-actuated fuel injector utilizing same
US5850850A (en) * 1994-12-29 1998-12-22 Millipore Corporation Flow controller, parts of flow controller, and related method
US6082332A (en) * 1994-07-29 2000-07-04 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US6085991A (en) * 1998-05-14 2000-07-11 Sturman; Oded E. Intensified fuel injector having a lateral drain passage
US6116571A (en) * 1997-04-14 2000-09-12 Burkert Werke Gmbh & Co. Straight valve
US6148778A (en) * 1995-05-17 2000-11-21 Sturman Industries, Inc. Air-fuel module adapted for an internal combustion engine
US6161770A (en) * 1994-06-06 2000-12-19 Sturman; Oded E. Hydraulically driven springless fuel injector
US6257499B1 (en) 1994-06-06 2001-07-10 Oded E. Sturman High speed fuel injector
US6367767B2 (en) * 1998-11-06 2002-04-09 Festo Ag & Co. Control member for a piezo-valve
US6425375B1 (en) 1998-12-11 2002-07-30 Caterpillar Inc. Piston and barrel assembly with stepped top and hydraulically-actuated fuel injector utilizing same
US6575137B2 (en) 1994-07-29 2003-06-10 Caterpillar Inc Piston and barrel assembly with stepped top and hydraulically-actuated fuel injector utilizing same
US20030168619A1 (en) * 2002-02-28 2003-09-11 Jansen Harvey B. Active combustion fuel valve
US20050269543A1 (en) * 2001-04-18 2005-12-08 Fisher Controls International Llc Stem arrangement for pivot actuated sleeve valve
US20060219968A1 (en) * 2002-02-28 2006-10-05 Jansen's Aircraft Systems Control., Inc. Pattern factor control valve
US20070151252A1 (en) * 2005-12-29 2007-07-05 Delavan Inc. Valve assembly for modulating fuel flow to a gas turbine engine
US20070245982A1 (en) * 2006-04-20 2007-10-25 Sturman Digital Systems, Llc Low emission high performance engines, multiple cylinder engines and operating methods
US20080264393A1 (en) * 2007-04-30 2008-10-30 Sturman Digital Systems, Llc Methods of Operating Low Emission High Performance Compression Ignition Engines
US20090026398A1 (en) * 2005-12-29 2009-01-29 Delavan Inc Valve assembly for modulating fuel flow to a gas turbine engine
US20090077945A1 (en) * 2007-08-24 2009-03-26 Delavan Inc Variable amplitude double binary valve system for active fuel control
US20090183699A1 (en) * 2008-01-18 2009-07-23 Sturman Digital Systems, Llc Compression Ignition Engines and Methods
US20090204306A1 (en) * 2008-02-12 2009-08-13 Delavan Inc Methods and systems for modulating fuel flow for gas turbine engines
US20090234555A1 (en) * 2008-03-12 2009-09-17 Williams Brandon P Active pattern factor control for gas turbine engines
US7775052B2 (en) 2004-05-07 2010-08-17 Delavan Inc Active combustion control system for gas turbine engines
US7954472B1 (en) 2007-10-24 2011-06-07 Sturman Digital Systems, Llc High performance, low emission engines, multiple cylinder engines and operating methods
US20110131947A1 (en) * 2009-12-03 2011-06-09 Delavan Inc. Trim valves for modulating fluid flow
US8123196B1 (en) * 2009-10-07 2012-02-28 Chernoff Larry J Integrated valve system
US20120068095A1 (en) * 2010-09-17 2012-03-22 Woodward Hrt, Inc. Torque motor linearization
US20130087223A1 (en) * 2011-10-10 2013-04-11 In-Lhc Method of detecting failure of a servo-valve, and a servo-valve applying the method
US20130087726A1 (en) * 2010-05-05 2013-04-11 Camcon Oil Limited Electromagnetically Operated Switching Devices And Methods Of Actuation Thereof
US8596230B2 (en) 2009-10-12 2013-12-03 Sturman Digital Systems, Llc Hydraulic internal combustion engines
US8887690B1 (en) 2010-07-12 2014-11-18 Sturman Digital Systems, Llc Ammonia fueled mobile and stationary systems and methods
US9206738B2 (en) 2011-06-20 2015-12-08 Sturman Digital Systems, Llc Free piston engines with single hydraulic piston actuator and methods
US9464569B2 (en) 2011-07-29 2016-10-11 Sturman Digital Systems, Llc Digital hydraulic opposed free piston engines and methods
US20180017179A1 (en) * 2016-07-15 2018-01-18 Glen A. Robertson Dual acting solenoid valve using bi-stable permanent magnet activation for energy efficiency and power versatility
US20200025219A1 (en) * 2018-07-20 2020-01-23 Hamilton Sundstrand Corporation Servo valve
US11118702B2 (en) * 2018-07-23 2021-09-14 Buerkert Werke Gmbh & Co. Kg Valve with energy-saving electrodynamic actuator

Cited By (96)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3790127A (en) * 1972-11-03 1974-02-05 Vapor Corp Hydraulic valve
US3982562A (en) * 1974-10-04 1976-09-28 Allied Chemical Corporation Pressure control apparatus
DE2511152A1 (en) * 1975-03-14 1976-09-23 Daimler Benz Ag ELECTROMAGNETIC CONTROL VALVE, ESPECIALLY FOR AUTOMATICALLY SWITCHING MOTOR VEHICLE TRANSMISSIONS
US4120481A (en) * 1975-03-14 1978-10-17 Daimler-Benz Aktiengesellschaft Electromagnetic control valve, especially for automatically shifting change-speed transmissions
US4208361A (en) * 1976-04-15 1980-06-17 Nissan Motor Company, Limited Automobile with altitude compensated fuel feed means
US4127360A (en) * 1976-12-16 1978-11-28 Carpenter Clarence W Bumpless pump apparatus adjustable to meet slave system needs
EP0040909A1 (en) * 1980-05-16 1981-12-02 Westinghouse Brake And Signal Company Limited Fluid pressure control valves
US4385642A (en) * 1981-01-19 1983-05-31 Hydraulic Servocontrols Corporation Bi-stable electrically operated valve
FR2552196A1 (en) * 1983-09-21 1985-03-22 Lorch & Co Kg J ELECTROMAGNETIC VALVE
US4561632A (en) * 1983-09-21 1985-12-31 J. Lorch Gesellschaft & Co. Kg Solenoid valve
EP0177944A3 (en) * 1984-10-12 1987-06-24 H. Kuhnke GmbH KG Bistable solenoid valve
EP0177944A2 (en) * 1984-10-12 1986-04-16 H. Kuhnke GmbH KG Bistable solenoid valve
US4621660A (en) * 1984-10-12 1986-11-11 H. Kuhne Gmbh Kg Bistable magnetic valve
EP0235451A1 (en) * 1985-11-29 1987-09-09 Fujikura Rubber Ltd. Directional control valve
US4765370A (en) * 1985-11-29 1988-08-23 Fujikura Rubber Ltd. Directional control valve
US5161578A (en) * 1986-01-06 1992-11-10 Carrier Corporation Warm-up/changeover valve or proximity switch
US4794843A (en) * 1986-09-24 1989-01-03 Poling Denzil C Hydraulic valve for controlling single-acting cylinder
US4988074A (en) * 1988-05-17 1991-01-29 Hi-Ram, Inc. Proportional variable force solenoid control valve
EP0493843A1 (en) * 1990-12-03 1992-07-08 Koninklijke Philips Electronics N.V. Device for interrupting a material flow
US5158262A (en) * 1990-12-03 1992-10-27 U.S. Philips Corporation Device for interrupting a material flow
US5421521A (en) * 1993-12-23 1995-06-06 Caterpillar Inc. Fuel injection nozzle having a force-balanced check
US5407131A (en) * 1994-01-25 1995-04-18 Caterpillar Inc. Fuel injection control valve
US5474234A (en) * 1994-03-22 1995-12-12 Caterpillar Inc. Electrically controlled fluid control valve of a fuel injector system
US5628293A (en) * 1994-05-13 1997-05-13 Caterpillar Inc. Electronically-controlled fluid injector system having pre-injection pressurizable fluid storage chamber and direct-operated check
US5488340A (en) * 1994-05-20 1996-01-30 Caterpillar Inc. Hard magnetic valve actuator adapted for a fuel injector
US5752308A (en) * 1994-05-20 1998-05-19 Caterpillar Inc. Method of forming a hard magnetic valve actuator
US5449119A (en) * 1994-05-25 1995-09-12 Caterpillar Inc. Magnetically adjustable valve adapted for a fuel injector
US5470043A (en) * 1994-05-26 1995-11-28 Lockheed Idaho Technologies Company Magnetic latching solenoid
US5494219A (en) * 1994-06-02 1996-02-27 Caterpillar Inc. Fuel injection control valve with dual solenoids
US6161770A (en) * 1994-06-06 2000-12-19 Sturman; Oded E. Hydraulically driven springless fuel injector
US6257499B1 (en) 1994-06-06 2001-07-10 Oded E. Sturman High speed fuel injector
US5479901A (en) * 1994-06-27 1996-01-02 Caterpillar Inc. Electro-hydraulic spool control valve assembly adapted for a fuel injector
US5826562A (en) * 1994-07-29 1998-10-27 Caterpillar Inc. Piston and barrell assembly with stepped top and hydraulically-actuated fuel injector utilizing same
US5673669A (en) * 1994-07-29 1997-10-07 Caterpillar Inc. Hydraulically-actuated fluid injector having pre-injection pressurizable fluid storage chamber and direct-operated check
US5687693A (en) * 1994-07-29 1997-11-18 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US5697342A (en) * 1994-07-29 1997-12-16 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US5738075A (en) * 1994-07-29 1998-04-14 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US6575137B2 (en) 1994-07-29 2003-06-10 Caterpillar Inc Piston and barrel assembly with stepped top and hydraulically-actuated fuel injector utilizing same
US6065450A (en) * 1994-07-29 2000-05-23 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US6082332A (en) * 1994-07-29 2000-07-04 Caterpillar Inc. Hydraulically-actuated fuel injector with direct control needle valve
US5494220A (en) * 1994-08-08 1996-02-27 Caterpillar Inc. Fuel injector assembly with pressure-equalized valve seat
WO1996011350A1 (en) * 1994-10-07 1996-04-18 Ian Malcolm Chatwin Solenoid actuated bi-stable pilot valve
US5605289A (en) * 1994-12-02 1997-02-25 Caterpillar Inc. Fuel injector with spring-biased control valve
US5850850A (en) * 1994-12-29 1998-12-22 Millipore Corporation Flow controller, parts of flow controller, and related method
US6173685B1 (en) 1995-05-17 2001-01-16 Oded E. Sturman Air-fuel module adapted for an internal combustion engine
US6148778A (en) * 1995-05-17 2000-11-21 Sturman Industries, Inc. Air-fuel module adapted for an internal combustion engine
US5720318A (en) * 1995-05-26 1998-02-24 Caterpillar Inc. Solenoid actuated miniservo spool valve
US5597118A (en) * 1995-05-26 1997-01-28 Caterpillar Inc. Direct-operated spool valve for a fuel injector
US6116571A (en) * 1997-04-14 2000-09-12 Burkert Werke Gmbh & Co. Straight valve
US6085991A (en) * 1998-05-14 2000-07-11 Sturman; Oded E. Intensified fuel injector having a lateral drain passage
US6367767B2 (en) * 1998-11-06 2002-04-09 Festo Ag & Co. Control member for a piezo-valve
US6425375B1 (en) 1998-12-11 2002-07-30 Caterpillar Inc. Piston and barrel assembly with stepped top and hydraulically-actuated fuel injector utilizing same
US20050269543A1 (en) * 2001-04-18 2005-12-08 Fisher Controls International Llc Stem arrangement for pivot actuated sleeve valve
US7178785B2 (en) * 2001-04-18 2007-02-20 Fisher Controls International, Inc. Stem arrangement for pivot actuated sleeve valve
US6918569B2 (en) * 2002-02-28 2005-07-19 Jansen's Aircraft Systems Controls, Inc. Active combustion fuel valve
US20050224738A1 (en) * 2002-02-28 2005-10-13 Jansen Harvey B Active combustion fuel valve
US7004449B2 (en) 2002-02-28 2006-02-28 Jansen's Aircraft Systems Controls, Inc. Active combustion fuel valve
US20060219968A1 (en) * 2002-02-28 2006-10-05 Jansen's Aircraft Systems Control., Inc. Pattern factor control valve
US7137613B2 (en) * 2002-02-28 2006-11-21 Jansen's Aircraft Systems Controls, Inc. Pattern factor control valve
US20030168619A1 (en) * 2002-02-28 2003-09-11 Jansen Harvey B. Active combustion fuel 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
US20090026398A1 (en) * 2005-12-29 2009-01-29 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
US20070151252A1 (en) * 2005-12-29 2007-07-05 Delavan Inc. Valve assembly for modulating fuel flow to a gas turbine engine
US20070245982A1 (en) * 2006-04-20 2007-10-25 Sturman Digital Systems, Llc Low emission high performance engines, multiple cylinder engines and operating methods
US7793638B2 (en) 2006-04-20 2010-09-14 Sturman Digital Systems, Llc Low emission high performance engines, multiple cylinder engines and operating methods
US20080264393A1 (en) * 2007-04-30 2008-10-30 Sturman Digital Systems, Llc Methods of Operating Low Emission High Performance Compression Ignition Engines
US20090077945A1 (en) * 2007-08-24 2009-03-26 Delavan Inc Variable amplitude double binary valve system for active fuel control
US7954472B1 (en) 2007-10-24 2011-06-07 Sturman Digital Systems, Llc High performance, low emission engines, multiple cylinder engines and operating methods
US7958864B2 (en) * 2008-01-18 2011-06-14 Sturman Digital Systems, Llc Compression ignition engines and methods
US20090183699A1 (en) * 2008-01-18 2009-07-23 Sturman Digital Systems, Llc Compression Ignition Engines and Methods
US8239114B2 (en) 2008-02-12 2012-08-07 Delavan Inc Methods and systems for modulating fuel flow for gas turbine engines
US20090204306A1 (en) * 2008-02-12 2009-08-13 Delavan Inc Methods and systems for modulating fuel flow for gas turbine engines
US20090234555A1 (en) * 2008-03-12 2009-09-17 Williams Brandon P Active pattern factor control for gas turbine engines
US8200410B2 (en) 2008-03-12 2012-06-12 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
US8483931B2 (en) 2008-03-12 2013-07-09 Delavan Inc. Active pattern factor control for gas turbine engines
US8123196B1 (en) * 2009-10-07 2012-02-28 Chernoff Larry J Integrated valve system
US8596230B2 (en) 2009-10-12 2013-12-03 Sturman Digital Systems, Llc Hydraulic internal combustion engines
US8434310B2 (en) 2009-12-03 2013-05-07 Delavan Inc Trim valves for modulating fluid flow
US20110131947A1 (en) * 2009-12-03 2011-06-09 Delavan Inc. Trim valves for modulating fluid flow
JP2013525713A (en) * 2010-05-05 2013-06-20 カムコン・オイル・リミテッド Electromagnetic operation switch device and operation method thereof
US9046187B2 (en) * 2010-05-05 2015-06-02 Camcon Oil Limited Electromagnetically operated switching devices and methods of actuation thereof
US20130087726A1 (en) * 2010-05-05 2013-04-11 Camcon Oil Limited Electromagnetically Operated Switching Devices And Methods Of Actuation Thereof
US8887690B1 (en) 2010-07-12 2014-11-18 Sturman Digital Systems, Llc Ammonia fueled mobile and stationary systems and methods
US8522821B2 (en) * 2010-09-17 2013-09-03 Woodward Hrt, Inc. Torque motor linearization
US20120068095A1 (en) * 2010-09-17 2012-03-22 Woodward Hrt, Inc. Torque motor linearization
US9206738B2 (en) 2011-06-20 2015-12-08 Sturman Digital Systems, Llc Free piston engines with single hydraulic piston actuator and methods
US9464569B2 (en) 2011-07-29 2016-10-11 Sturman Digital Systems, Llc Digital hydraulic opposed free piston engines and methods
US20130087223A1 (en) * 2011-10-10 2013-04-11 In-Lhc Method of detecting failure of a servo-valve, and a servo-valve applying the method
US9897116B2 (en) * 2011-10-10 2018-02-20 In-Lhc Method of detecting failure of a servo-valve, and a servo-valve applying the method
US20180017179A1 (en) * 2016-07-15 2018-01-18 Glen A. Robertson Dual acting solenoid valve using bi-stable permanent magnet activation for energy efficiency and power versatility
US10024453B2 (en) * 2016-07-15 2018-07-17 Glen A. Robertson Dual acting solenoid valve using bi-stable permanent magnet activation for energy efficiency and power versatility
US20200025219A1 (en) * 2018-07-20 2020-01-23 Hamilton Sundstrand Corporation Servo valve
US11118702B2 (en) * 2018-07-23 2021-09-14 Buerkert Werke Gmbh & Co. Kg Valve with energy-saving electrodynamic actuator

Similar Documents

Publication Publication Date Title
US3532121A (en) Latching valve
US3570807A (en) Electromechanical control valve
US3570806A (en) Balanced electromechanical control valve
US4779582A (en) Bistable electromechanical valve actuator
US3379214A (en) Permanent magnet valve assembly
US7021603B2 (en) Electromagnetic actuator and integrated actuator and fluid flow control valve
CA1037343A (en) Pressure control valve
US8567440B2 (en) Solenoid operated valve
US20200018418A1 (en) Fluid servo valve and fluid servo apparatus
US3040217A (en) Electromagnetic actuator
KR101272724B1 (en) Fluid control valve
ATE46020T1 (en) PROPORTIONAL SOLENOID VALVE.
EP2115336B1 (en) Solenoid valve having a two piece moving valve element
US4299252A (en) Permanent magnet boosted electromagnetic actuator
US3861643A (en) Saturating magnetic control valve
KR950002534B1 (en) Solenoid vlave
GB1603036A (en) Pressure operated pilot controlled shut-off valve
US4638830A (en) High sensitivity magnetic actuator
US4114852A (en) Miniature reed-type valve
US3758071A (en) Magnetically-actuated fluid control valve
US3523677A (en) Fast acting electromagnetic gas valve
US6328279B1 (en) Miniature electrically operated diaphragm valve
JPH08270827A (en) Pilot kick type solenoid valve
US3246662A (en) Flux-actuated fluid logic device
US4759528A (en) Valve actuator

Legal Events

Date Code Title Description
AS Assignment

Owner name: HR TEXTRON INC., 25200 WEST RYE CANYON RD. VALENCI

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:TEXTRON, INC.,;REEL/FRAME:003978/0747

Effective date: 19820222