US3334642A - Electro-pneumatic transducer - Google Patents

Electro-pneumatic transducer Download PDF

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US3334642A
US3334642A US47993565A US3334642A US 3334642 A US3334642 A US 3334642A US 47993565 A US47993565 A US 47993565A US 3334642 A US3334642 A US 3334642A
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Prior art keywords
armature
nozzle
relay
electro
torque motor
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Paul G Borthwick
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Fisher Governor Co
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Fisher Governor Co
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Priority to US47993565 priority Critical patent/US3334642A/en
Priority to FR45697A priority patent/FR1467313A/en
Priority to DE19661523496 priority patent/DE1523496A1/en
Priority to GB2235866A priority patent/GB1117794A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B5/00Transducers converting variations of physical quantities, e.g. expressed by variations in positions of members, into fluid-pressure variations or vice versa; Varying fluid pressure as a function of variations of a plurality of fluid pressures or variations of other quantities
    • F15B5/003Transducers converting variations of physical quantities, e.g. expressed by variations in positions of members, into fluid-pressure variations or vice versa; Varying fluid pressure as a function of variations of a plurality of fluid pressures or variations of other quantities characterised by variation of the pressure in a nozzle or the like, e.g. nozzle-flapper system
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B5/00Transducers converting variations of physical quantities, e.g. expressed by variations in positions of members, into fluid-pressure variations or vice versa; Varying fluid pressure as a function of variations of a plurality of fluid pressures or variations of other quantities
    • F15B5/006Transducers converting variations of physical quantities, e.g. expressed by variations in positions of members, into fluid-pressure variations or vice versa; Varying fluid pressure as a function of variations of a plurality of fluid pressures or variations of other quantities with electrical means, e.g. electropneumatic transducer
    • 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
    • Y10T137/2278Pressure modulating relays or followers
    • Y10T137/2409With counter-balancing pressure feedback to the modulating device

Definitions

  • This invention relates to an electro-pneumatic transducer and, more particularly, to an improved electropneum-atic transducer for use in electrical control loops in which the final control element is pneumatically operated.
  • An object of the present invention is to provide an improved electro-pneumatic transducer that can be readily mounted on a control valve or like pneumaticallyoperated Control element, such transducer receiving a direct current milliampere input signal and creating a pneumatic output pressure that is directly proportional to this input.
  • Another object of the present invention is to provide an improved electro-pneurnatic transducer comprising a torque motor assembly and a relay assembly that attaches to a common case without tubing.
  • a further object of this invention is to provide a novel electro-pneumatic transducer having an improved torque motor that includes adjustable coil and armature means for facilitating adjustment of the armature.
  • Still another object of the present invention is to provide an improved electro-pneumatic transducer having a torque motor constructed and arranged so as to interchangeably receive a plurality of feedback bellows (one for every output range).
  • Yet another object of this invention is to provide an improved electro-pneumatic transducer, the torque motor of which includes a relatively simple temperature compensating means.
  • FIGURE 1 is a perspective view illustrating an electro-pneumatic transducer which embodies the principles of the present invention mounted on a control valve and showing an air set and pressure gauge for use therewith;
  • FIGURE 2 is a top view of the electro-pneumatic transducer with the cover of the housing removed to show the torque motor assembly;
  • FIGURE 3 is a sectional view of the electro-pneumatic transducer illustrating the torque motor and the relay;
  • FIGURE 4 is an end view of the torque motor assembly
  • FIGURE 5 is a cross-sectional view of the torque motor assembly taken generally along the line 55 of FIG- URE 6;
  • FIGURE 7 is a perspective view of the armature and coil support bracket
  • FIGURE 9 is a detail view taken along line 99 of FIGURE 8 illustrating the connection of the relay to the housing for the transducer.
  • FIGURE 10 is a schematic illustration of the electropneumatic transducer of this invention.
  • the pneumatic output from the transducer 10 is fed to the actuator of the control valve 14 or other device to be controlled pneumatically by means of a conduit 20.
  • the actuator of the control valve may be either a diaphragm or a piston.
  • the transducer is comprised basically of a torque motor 22 enclosed within a housing 11 defined by a case 24 and a cover 26 threadedly connected to the case 24 and a relay 28 that is connected directly to the case 24 without the necessity for ancillary tubing.
  • the transducer 19 is used in electrical control loops in which the final control element is pneumatically operated. It receives a direct current milliampere input signal and creates a pneumatic output pressure that is directly prop0rtional to this input.
  • the torque motor assembly 22 includes an armature and coil support assembly having bracket means 42 for carrying electrical coils 44 and 45 thereon and for supporting an armature 46 for pivotable movement within the housing means.
  • the end 46a of the armature 46 cooperates with the opening Stla from nozzle 50 (that is threadedly connected to a tapped opening in the bottom pole piece plate 34 to cover or uncover the nozzle opening 5%) to control the flow of air therefrom.
  • the armature 46 pivots about a centrally located torsion bar means 52 that is fixed at its ends to the plate members 54 and 56 of the bracket means 42.
  • the torsion rod 52 comprises a pair of rod members 52a and 52b which are each rigidly afiixed at one end to the block 58 and extend therefrom.
  • the other ends of rod members 52a and 52b, respectively, are connected to plate members 54 and 56, respectively.
  • the armature 46 extends through the bracket means 42 between the coils 44 and 45 and is connected to the block 58 by means of suitable fastening means, as for example, machine screw 60.
  • the armature 46 pivots about the axis of centrally located torsion bar 52 with a change in input signal to cover or uncover the nozzle 50.
  • the direction of cur- 44 and 45 determines the Therefore, reversing the input leads to the coils will provide reverse action.
  • a baffie 62 (FIG. 3) is provided on the end 46a of the armature 46 to serve as an adjustable extension of the armature to insure that the covering of the nozzle opening 50a (to obtain proper restriction of air flow) is accomplished with the armature 46 centered between the pole pieces.
  • the exterior of the stud-like portion of baffle 62 is threaded for cooperation with a threaded opening in the end 46a of the armature.
  • a lock nut 63 is provided to retain the baffle 62 in selected adjusted position.
  • Spring means are provided for biasing the armature end 46a toward nozzle covering position.
  • the spring 66 acts between the armature 46 and the retainer member 68 which is threadedly engaged with an adjusting screw 70 to provide for selective adjustment of the spring bias force upon the armature.
  • the stem 71 of the adjusting screw 70 which is rotatably journaled in pole piece plate 30, has external threads thereon which engage with a threaded opening through the retaining member 68.
  • the adjustment provided by the change of bias force on the spring 66 is referred to as the Zero adjustment.
  • the zero adjustment provides a means of setting the initial output pressure at the desired value of input signal.
  • Feedback means are provided for urging the armature 46 in a direction in opposition to the bias of the spring means 66.
  • the feedback bellows assembly 75 which in.- cludes the feedback bellows 76 operatively connected at its ends to a base 77 and a cap '78, is removably afiixed between the armature end 46b and the top pole piece plate 30 so as to permit ready replacement of the feedback bellows assembly 75. This is necessary for a different feedback bellows assembly is required for every selected output range.
  • the feedback bellows assembly 75 is readily removed by first loosening the lock nut 79 which engages with a stud portion 80 on the end of the base 77 that extends through an opening in the armature 46. Upon removal of lock screw 82, which extends through an opening in the top pole piece plate 30 into threaded engagement with the top cap 78, the feedback bellows assembly may be slid from position. It is noted from FIGURE that the end 46b of armature 46 is provided with a slot 46c to permit the stud 80 to be easily slid outwardly from the armature. O-ring seal means 84 are provided between the top pole piece plate 30 and the top cap 78 to prevent loss of feedback air from within the feedback bellows assembly 75 during use.
  • Another important feature of this invention is the provision of a span adjustment for providing a means of obtaining a full change in output pressure for a full change in input signal.
  • the span adjustment is accomplished by moving a piece of magnetic material 90 (FIG- URES 5 and 6) toward or away from the permanent magnet 32 to shunt away or add to the magnetic flux in the armature air gap. The result is a change in the amount of torque produced.
  • the bar of magnetic material 90 is carried at one end on the pole piece plate 34 by means of an angle bracket 91 affixed to one end of bar 90 by screw means 92 and aflixed at its other end to the pole piece plate 34 by screw means 93.
  • the bracket 91 has resiliency and will normally function to bias the upper end of the bar 90 toward the permanent magnet 32.
  • Adjustment screw 94 which is adapted to bear at its end against the pole piece 31, may be rotated to suitably adjust the position of the bar 90 with respect to the permanent magnet 32.
  • Lock nut means 96 are provided to lock the adjustment screw in its selected adjusted position.
  • the support bracket 42 for the armature 46 and the coils 44 and 45 comprises a pair of plate members 54 and 56 joined together by the ends of torsion rod means 52.
  • Each plate member includes inwardly extending arms 54a and 56a, respectively, having elongated recesses 54b and 56]), respectively, therein.
  • downwardly depending legs 54c and 560 are provided on the plate members 54 and 56.
  • the slot-like openings 54d and 56d provide for adjustment of the bracket means 42 with respect to the bottom pole piece plate 34 to adjust the position of armature 46 between the pole pieces 31 and 35, as will be more clearly understood hereafter.
  • the two identical coils 44 and 45 are mounted to the armature and coil support assembly 42 by screw means 102.
  • the armature 46 is inserted through the two coils 44 and 45 and is fastened to the assembly 42 by the screw means 60, which preferably comprises a hexagonal socket head screw.
  • the coil and armature assembly 42 is adjustable by virtue of the slotted holes 54d and 56d, respectively, in the plate members 54 and 56.
  • the assembly 42 is mounted on the bottom pole piece plate 34 by means of screw means 104, which may be hexagonal socket head screws. Before the four screws 104 are tightened, the armature 46 is centered between the two pole pieces 31 and 35.
  • the four slotted mounting holes 54d and 56d, respectively, in the plate members 54 and 56 facilitate this adjustment.
  • the terminal mounting bracket assembly 105 is mounted directly on the torque motor.
  • the terminal mounting bracket assembly comprises a terminal strip 106 and terminal strip mounting bracket 107 which is manufactured from a material whose magnetic permeability change with temperature change is the opposite from the permeability change of the pole pieces 31, 35 and the armature 46.
  • Bracket 107 is affixed to the pole piece plates 30 and 34 by suitable fastening means 107a, for example, machine screws.
  • the bracket 107 is positioned with respect to the permanent magnet 32 in such manner that part of the magnetic flux created from the permanent magnet is carried through the bracket. By virtue of this orientation of components, temperature compensation is provided for the bracket assembly 105.
  • the relay 28 is connected directly to the case 24 by fastening means 25, such as elongated screws, without the necessity for ancillary tubing.
  • the O-ring seal 110 is provided between the case 24 and the housing portion 112 of the relay 28 to seal the chamber 109.
  • Air may be exhausted from within the housing means 11 defined by cover 26 and case 24 through the exhaust opening 114 in the case 24 which communicates directly with the exhaust opening 116 in the relay 28 through the passage 118.
  • An O-ring seal 119 is disposed about the passage 118 between the case 24 and the relay 28 to prevent escape of air from passage 118.
  • the opening 120 in the relay 28 communicates directly with the passage 122 in the case 24 that is connected with the nozzle 50.
  • An O-ring 124 is provided about the opening 120 to prevent the undesired loss of pressure.
  • porous stainless steel flame arresters 126 and 128 are provided in the air passages between the case 24 and the relay 28.
  • the use of the flame arresters in cooperation with the housing means provides for an explosion-proof housing.
  • Filter screen 129 is provided in vent opening 116 to prevent dirt from entering relay 28.
  • Valve means comprising an inlet valve 150 and an exhaust valve 152 are interconnected for cooperation within the relay 28 to control the flow of air therethrough.
  • Inlet valve 150 is biased toward closed position by spring 151, which operates between the valve 150 and plate 149 fixed in chamber 109.
  • Spring 153 normally biases the spacer 140 away from exhaust valve 152 to exhaust air from chamber 141 through the exhaust passage through spacer 140 as will be more fully explained later.
  • Passage 162 permits a constant bleed of air from the compartment 109 through compartment 142 to the atmosphere. This allows a small clearance between the exhaust valve 152 and the exhaust valve seat (defined by the extension of spacer 14-13) to revent dead band.
  • the operation of the electro-pneumatic transducer of the present invention will best be understood by reference to FIGURE 10.
  • the transducer which comprises basically torque motor 22 and relay 28 is utilized in electrical control loops in which the final control element is pneumatically operated.
  • the transducer receives a direct current milliampere input signal and creates a pneumatic output pressure that is directly proportional to this input.
  • the torque motor 22 is the first stage in the conversion of the electrical input signal to a pneumatic output pressure.
  • the second stage in the conversion from the electrical input to the pneumatic output takes place in the relay 28.
  • the pole piece means are already polarized by the permanent magnet 32.
  • the armature polarity in this case will be as shown in FIGURE 10, for example, with the top pole means 29 comprising a north pole and the bottom pole means 33 comprising a south pole.
  • the magnetic attraction will, therefore, be downward at the nozzle end 46a of the armature 46 and upward at the feedback bellows end 46b, resulting in a torque that rotates the armature 46 about the fixed torsion rod 52 to cover the nozzle opening 511a.
  • the resulting restriction of the nozzle opening 50a of nozzle 50 produces an increased pressure in the nozzle, in the chamber 143 of the relay and in the feedback bellows '75.
  • the feedback bellows 75 communicates with nozzle 51) and passage 145 in relay 28 via line 41.
  • the relay 28 responds to the increase in nozzle pressure to increase the output pressure to the control valve.
  • the increased pressure in the feedback bellows 75 creates a force that acts on the armature 46 to move it back to the equilibrium position. In this way, the new nozzle pressure is compared to the input current by the force balance principle.
  • Reverse-acting transducers operate in a similar manner except that when the D-C input signal increases, the output pressure from the relay decreases. Conversely, a decreasing input signal increases the output pressure.
  • an improved electro-pneumatic transducer comprising a torque motor which is the first stage in the conversion of the electrical input signal to a pneumatic output pressure and a relay which is the second stage in the conversion from the electrical input to the pneumatic output.
  • the twostage design with each stage possessing its own feedback loop allows for uniformly high stability for any output load.
  • An overall feedback loop was purposely avoided by the present invention in order to maintain stability that was completely independent of the output load.
  • the high capacity relay will amplify the torque motor nozzle pressure into the output pressure by a three to one ratio.
  • the relay output pressure changes 12 p.s.i., the span for a standard 3 to 15 p.s.i. range.
  • the high loop gain, the high torque output, and the torsion rod suspension of the armature result in high static performance.
  • the back of the case or housing for the transducer is designed to mate with a plug-in relay so that the relay may be readily serviced without disturbing the electrical or pneumatic connections.
  • the case and the cover thread together and are gasketed to form an explosion-proof housing which is preserved by the use of porous stainless steel flame arresters in the air passages between the case and the relay.
  • an electro-pneumatic transducer the combination of housing means, a torque motor assembly removably mounted in said housing means, said torque motor assembly including permanent magnet means and pole pieces associated therewith, an armature and coil assembly including a support bracket carrying electrical coils and pivotally supporting an armature thereon, the armature being movable between the pole pieces in response to electrical energization of said coils, said permanent magnet means and said pole pieces being removable from the torque motor assembly separately from the armature and coil assembly, a bleed nozzle on said housing means operatively associated with said armature, said armature being biased toward the bleed nozzle for restricting the discharge of air from said nozzle, a feedback member operatively associated with said armature and acting on said armature to increase the discharge of air from said bleed nozzle, means for supplying a direct current input signal to said coils to energize said coils and produce a magnetic field having a strength that changes proportionately with the change in input signal, the magnetic attraction between the armature and pole
  • a terminal mounting bracket assembly is provided within said housing means for mounting on said torque motor assembly, said mounting bracket assembly including a mounting bracket disposed adjacent the permanent magnet means, the mounting bracket being made from a material whose magnetic permeability change with temperature change is the opposite from the magnetic permeability change of the pole pieces and armature so as to provide for temperature compensation.
  • An electro-pneumatic transducer as in claim 1 wherein a piece of magnetic material is adjustably posi tioned with respect to said permanent magnet to shunt away or add to the magnetic flux in the air gap between the armature and the pole pieces.
  • housing means a torque motor assembly removably mounted in said housing means, said torque motor assembly including permanent magnet means and pole pieces connected to form a subassembly, armature and coil means operatively associated with said pole pieces, said armature and coil means including a support frame fixed with respect to said pole pieces and carrying electrical coils thereon, an armature supported on said support frame for movement between the pole pieces about an axis transverse to the length of said armature, said permanent magnet means and said pole pieces being removable from the torque motor assembly separately from said armature and coil means, nozzle means in said housing means adjacent one end of said armature, said nozzle means being operatively connected to a pneumatic relay by conduit means, said one end of said armature being movable to regulate the discharge of air from said nozzle means, means for biasing the armature toward the nozzle means, a feedback member operative on the other end of said armature in opposition to said biasing means, said feedback bellows
  • said support frame includes a pair of generally parallel plate members having inwardly bent tabs thereon for supporting said coil means.
  • said support frame includes a pair of generally parallel plate members joined together by torsion rod means afiixed at its ends to the plate members, said armature being fixedly connected intermediate the ends thereof to said torsion rod means.
  • An electro-pneumatic transducer as in claim 9 wherein said plate members are adjustably supported in said housing means to provide centering adjustment of said armature between said pole pieces.
  • An electro-pneumatic transducer as in claim 8 wherein said housing means has an exhaust opening, a supply air opening and a nozzle connecting opening in one wall thereof and said pneumatic relay includes a housing having an exhaust opening complementary to the housing means exhaust opening, a supply air inlet cooperating with said supply air opening in said housing means, and an outlet opening cooperating With said nozzle connecting opening, and O-ring seal means provided about the respective complementary and cooperating openings, and means for connecting the relay to the housing means, whereby the necessity for separate conduit between the housing means and the relay is obviated.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supply Devices, Intensifiers, Converters, And Telemotors (AREA)

Description

g- 8, 3937 P. cs BORTHWICK 3,334,642
ELECTRO-PNEUMATIC TRANSDUCER Filed Aug. 16, 1965 4 Sheets-Sheet l Aug. 8, 1%? P. G. BORTHWICK ELECTRO-PNEUMATIC TRANSDUCER 4 Sheets-Sheet 2 Filed Aug. 16, 1965 Aug. 8, 396 P. e. BORTHWICK ELECTRO-PNEUMATI C TRANSDUCER 4 Sheets-Sheet 5 Filed Aug. 16, 1965 r 4 ZZZ if may g- 9 17 P. (-3. BQRTHWIQK ELECTRO'PNEUMATIC TRANSDUCER 4 Sheets-Sheet 1;
Filed Aug. 16, 19 5 I JEQZZZ /gy United States Patent M 3,334,642 ELECTRO-PNEUMATIC TRANSDUCER Paul G. Borthwick, Marshalltown, Iowa, assignor to Fisher Governor Company, a corporation of Iowa Filed Aug. 16, 1965, Ser. No. 479,935
11 Claims. (Cl. 137-85) This invention relates to an electro-pneumatic transducer and, more particularly, to an improved electropneum-atic transducer for use in electrical control loops in which the final control element is pneumatically operated.
An object of the present invention is to provide an improved electro-pneumatic transducer that can be readily mounted on a control valve or like pneumaticallyoperated Control element, such transducer receiving a direct current milliampere input signal and creating a pneumatic output pressure that is directly proportional to this input.
Another object of the present invention is to provide an improved electro-pneurnatic transducer comprising a torque motor assembly and a relay assembly that attaches to a common case without tubing.
A further object of this invention is to provide a novel electro-pneumatic transducer having an improved torque motor that includes adjustable coil and armature means for facilitating adjustment of the armature.
Still another object of the present invention is to provide an improved electro-pneumatic transducer having a torque motor constructed and arranged so as to interchangeably receive a plurality of feedback bellows (one for every output range).
Yet another object of this invention is to provide an improved electro-pneumatic transducer, the torque motor of which includes a relatively simple temperature compensating means.
It is another object of this invention to provide an improved electro-pneumatic transducer having high loop gain, high torque output andtorsion rod suspension that combine to result in high static performance for the transducer. These and other objects of the present invention will become more apparent hereinafter.
The specific details of a presently preferred form of the present invention and their mode of operation will 'be made most manifest and particularly pointed out in clear, concise and exact terms in conjunction with the accompanying drawings, wherein:
FIGURE 1 is a perspective view illustrating an electro-pneumatic transducer which embodies the principles of the present invention mounted on a control valve and showing an air set and pressure gauge for use therewith;
FIGURE 2 is a top view of the electro-pneumatic transducer with the cover of the housing removed to show the torque motor assembly;
FIGURE 3 is a sectional view of the electro-pneumatic transducer illustrating the torque motor and the relay;
FIGURE 4 is an end view of the torque motor assembly;
FIGURE 5 is a cross-sectional view of the torque motor assembly taken generally along the line 55 of FIG- URE 6;
FIGURE 6 is a cross-sectional view of the torque motor assembly taken generally along the line 6-6 of FIG- URE 5;
FIGURE 7 is a perspective view of the armature and coil support bracket;
FIGURE 8 is a rear view of the transducer housing and relay;
FIGURE 9 is a detail view taken along line 99 of FIGURE 8 illustrating the connection of the relay to the housing for the transducer; and
FIGURE 10 is a schematic illustration of the electropneumatic transducer of this invention.
3,334,642 Patented Aug. 8, 1967 Referring now to the drawing, there is illustrated in FIGURE 1 an electro-pneumatic transducer 10 embodying the principles of the present invention and having a casing or housing 11 which is mounted on a bracket 12 that is suitably affixed to the casing of a control valve 14 for controlling the operation of such control valve. It will be understood that the electro-pneumatic transducer 10 can also be mounted on a stand pipe with a U- bolt connection.
If desired, an air set 16 and a pressure gauge 18 may be mounted on the electro-pneumatic transducer 10-.
The pneumatic output from the transducer 10 is fed to the actuator of the control valve 14 or other device to be controlled pneumatically by means of a conduit 20. The actuator of the control valve may be either a diaphragm or a piston.
Considering now FIGURES 2 and 3 of the drawing, it is seen that the transducer is comprised basically of a torque motor 22 enclosed within a housing 11 defined by a case 24 and a cover 26 threadedly connected to the case 24 and a relay 28 that is connected directly to the case 24 without the necessity for ancillary tubing. The transducer 19 is used in electrical control loops in which the final control element is pneumatically operated. It receives a direct current milliampere input signal and creates a pneumatic output pressure that is directly prop0rtional to this input.
The torque motor 22 is the first stage in the conversion an electrical input signal to a pneumatic output presstage in the conversion from the electrical input to the pneumatic output takes place in the relay 28.
The torque motor consists basically of a nozzle flapper signal amplifier and associated electro-mechanical elements. The torque motor 22, as seen in FIGURES 2-6, includes top pole means comprising a top pole piece plate 30 and a top pole piece 31, permanent magnet means 32 and bottom pole piece means comprising bottom pole piece plate 34 and bottom pole piece 35. The assembly pole pieces 31,
' means, as shown 1n the drawing by four round head screws 36.
The bottom pole piece plate 34 is rigidly affixed to the case 24 by means of suitable machine screws 38 (FIG. 2) to mount the torque motor 22 within the case 24.
The torque motor assembly 22 includes an armature and coil support assembly having bracket means 42 for carrying electrical coils 44 and 45 thereon and for supporting an armature 46 for pivotable movement within the housing means. The end 46a of the armature 46 cooperates with the opening Stla from nozzle 50 (that is threadedly connected to a tapped opening in the bottom pole piece plate 34 to cover or uncover the nozzle opening 5%) to control the flow of air therefrom.
The armature 46 pivots about a centrally located torsion bar means 52 that is fixed at its ends to the plate members 54 and 56 of the bracket means 42. The torsion rod 52 comprises a pair of rod members 52a and 52b which are each rigidly afiixed at one end to the block 58 and extend therefrom. The other ends of rod members 52a and 52b, respectively, are connected to plate members 54 and 56, respectively. The armature 46 extends through the bracket means 42 between the coils 44 and 45 and is connected to the block 58 by means of suitable fastening means, as for example, machine screw 60.
The armature 46 pivots about the axis of centrally located torsion bar 52 with a change in input signal to cover or uncover the nozzle 50. The direction of cur- 44 and 45 determines the Therefore, reversing the input leads to the coils will provide reverse action. The
armature and the pole pieces are preferably fabricated from magnetic materials which are chosen to reduce hysteresis and improve performance.
It is to be noted that a baffie 62 (FIG. 3) is provided on the end 46a of the armature 46 to serve as an adjustable extension of the armature to insure that the covering of the nozzle opening 50a (to obtain proper restriction of air flow) is accomplished with the armature 46 centered between the pole pieces. The exterior of the stud-like portion of baffle 62 is threaded for cooperation with a threaded opening in the end 46a of the armature. A lock nut 63 is provided to retain the baffle 62 in selected adjusted position.
Spring means are provided for biasing the armature end 46a toward nozzle covering position. The spring 66 acts between the armature 46 and the retainer member 68 which is threadedly engaged with an adjusting screw 70 to provide for selective adjustment of the spring bias force upon the armature. It is noted that the stem 71 of the adjusting screw 70, which is rotatably journaled in pole piece plate 30, has external threads thereon which engage with a threaded opening through the retaining member 68. The adjustment provided by the change of bias force on the spring 66 is referred to as the Zero adjustment. The zero adjustment provides a means of setting the initial output pressure at the desired value of input signal.
Feedback means are provided for urging the armature 46 in a direction in opposition to the bias of the spring means 66. The feedback bellows assembly 75, which in.- cludes the feedback bellows 76 operatively connected at its ends to a base 77 and a cap '78, is removably afiixed between the armature end 46b and the top pole piece plate 30 so as to permit ready replacement of the feedback bellows assembly 75. This is necessary for a different feedback bellows assembly is required for every selected output range.
The feedback bellows assembly 75 is readily removed by first loosening the lock nut 79 which engages with a stud portion 80 on the end of the base 77 that extends through an opening in the armature 46. Upon removal of lock screw 82, which extends through an opening in the top pole piece plate 30 into threaded engagement with the top cap 78, the feedback bellows assembly may be slid from position. It is noted from FIGURE that the end 46b of armature 46 is provided with a slot 46c to permit the stud 80 to be easily slid outwardly from the armature. O-ring seal means 84 are provided between the top pole piece plate 30 and the top cap 78 to prevent loss of feedback air from within the feedback bellows assembly 75 during use.
Another important feature of this invention is the provision of a span adjustment for providing a means of obtaining a full change in output pressure for a full change in input signal. The span adjustment is accomplished by moving a piece of magnetic material 90 (FIG- URES 5 and 6) toward or away from the permanent magnet 32 to shunt away or add to the magnetic flux in the armature air gap. The result is a change in the amount of torque produced.
The bar of magnetic material 90 is carried at one end on the pole piece plate 34 by means of an angle bracket 91 affixed to one end of bar 90 by screw means 92 and aflixed at its other end to the pole piece plate 34 by screw means 93. The bracket 91 has resiliency and will normally function to bias the upper end of the bar 90 toward the permanent magnet 32. Adjustment screw 94, which is adapted to bear at its end against the pole piece 31, may be rotated to suitably adjust the position of the bar 90 with respect to the permanent magnet 32. Lock nut means 96 are provided to lock the adjustment screw in its selected adjusted position.
The support bracket 42 for the armature 46 and the coils 44 and 45, as seen in FIGURE 7, comprises a pair of plate members 54 and 56 joined together by the ends of torsion rod means 52. Each plate member includes inwardly extending arms 54a and 56a, respectively, having elongated recesses 54b and 56]), respectively, therein. In addition, downwardly depending legs 54c and 560, respectively, are provided on the plate members 54 and 56. Within each of the legs 54c and 560, respectively, is an elongated slot-like opening 540. and 56d, respectively. The slot- like openings 54d and 56d provide for adjustment of the bracket means 42 with respect to the bottom pole piece plate 34 to adjust the position of armature 46 between the pole pieces 31 and 35, as will be more clearly understood hereafter.
As best seen in FIGURES 4 and 5, the two identical coils 44 and 45 are mounted to the armature and coil support assembly 42 by screw means 102. The armature 46 is inserted through the two coils 44 and 45 and is fastened to the assembly 42 by the screw means 60, which preferably comprises a hexagonal socket head screw.
The coil and armature assembly 42 is adjustable by virtue of the slotted holes 54d and 56d, respectively, in the plate members 54 and 56. The assembly 42 is mounted on the bottom pole piece plate 34 by means of screw means 104, which may be hexagonal socket head screws. Before the four screws 104 are tightened, the armature 46 is centered between the two pole pieces 31 and 35. The four slotted mounting holes 54d and 56d, respectively, in the plate members 54 and 56 facilitate this adjustment.
Referring to FIGURES 4, 5 and 6, it is noted that the terminal mounting bracket assembly 105 is mounted directly on the torque motor. The terminal mounting bracket assembly comprises a terminal strip 106 and terminal strip mounting bracket 107 which is manufactured from a material whose magnetic permeability change with temperature change is the opposite from the permeability change of the pole pieces 31, 35 and the armature 46. Bracket 107 is affixed to the pole piece plates 30 and 34 by suitable fastening means 107a, for example, machine screws. The bracket 107 is positioned with respect to the permanent magnet 32 in such manner that part of the magnetic flux created from the permanent magnet is carried through the bracket. By virtue of this orientation of components, temperature compensation is provided for the bracket assembly 105.
Considering FIGURES 3, 8 and 9, it is seen that the relay 28 is connected directly to the case 24 by fastening means 25, such as elongated screws, without the necessity for ancillary tubing. The inlet opening 108 in the case 24, which is connected to a suitable source of air supply, communicates with a chamber 109 defined between the case 24 and the housing of the relay 28. The O-ring seal 110 is provided between the case 24 and the housing portion 112 of the relay 28 to seal the chamber 109.
Air may be exhausted from within the housing means 11 defined by cover 26 and case 24 through the exhaust opening 114 in the case 24 which communicates directly with the exhaust opening 116 in the relay 28 through the passage 118. An O-ring seal 119 is disposed about the passage 118 between the case 24 and the relay 28 to prevent escape of air from passage 118. Similarly, the opening 120 in the relay 28 communicates directly with the passage 122 in the case 24 that is connected with the nozzle 50. An O-ring 124 is provided about the opening 120 to prevent the undesired loss of pressure.
It is noted that porous stainless steel flame arresters 126 and 128 are provided in the air passages between the case 24 and the relay 28. The use of the flame arresters in cooperation with the housing means provides for an explosion-proof housing. Filter screen 129 is provided in vent opening 116 to prevent dirt from entering relay 28.
Considering now the construction of the relay 28, it is seen that the relay housing is comprised of separate members 112, 130 and 132 operatively connected to one another and joined to the case 24. Provided within the relay 28 are a pair of diaphragms 134 and 136 which are peripherally connected to the relay housing so as to permit the central portions thereof to move longitudinally within the housing or casing of relay 28. Spacer member 140 is operatively connected to the diaphragms 134 and 136 for movement therewith. The diaphragms cooperate with the relay'housing to define compartments 141, 142 and 143 therewithin.
Valve means comprising an inlet valve 150 and an exhaust valve 152 are interconnected for cooperation within the relay 28 to control the flow of air therethrough. Inlet valve 150 is biased toward closed position by spring 151, which operates between the valve 150 and plate 149 fixed in chamber 109. Spring 153 normally biases the spacer 140 away from exhaust valve 152 to exhaust air from chamber 141 through the exhaust passage through spacer 140 as will be more fully explained later.
Air from a suitable source of supply will flow through the passage 108 into the chamber 1139 defined between the relay 28 and the case 24. From the chamber 199, air will flow through the fixed restriction 144 and through the passage 145 to the compartment or chamber 143 to exert a pressure on the spacer means in opposition to the pressure of spring 153. A portion of the air will pass from the restriction 144 through the opening 120 and passageway 122 to the nozzle 50 for discharge therethrough.
When the nozzle opening is restricted by bafi le 62 on armature 46, the pressure will build up within compartment 143 until it is sufficient to overcome the spring bias and move the inlet valve 150 away from the opening 150a to permit the passage of air through opening 161) to the control valve or other pneumatically operated device. The outlet pressure flowing through the opening 160 will continue to increase until the relay diaphragm assembly comprising the spacer means 140 and diaphragms 134 and 136 is pushed back by the force of the pressure acting on the smaller diaphragm 134 to its original position and the inlet valve 156 is closed. When the force derived from the pressure within the chamber 141 acting on diaphragm 134 coupled with the force of spring 153 is sufiicient to overcome the force derived from the pressure within the chamber 143 acting on diaphragm 136, the spacer means 140 will move away from the exhaust valve 152 to permit the exhaust of air from the compartment 141, through the exhaust passage in spacer 146, compartment 142, and the vent opening 116. It is to be noted at this time that air may be exhausted from within the housing means 11 through passage 114 which communicates via passage 118 with the exhaust opening 116 in relay 28.
Passage 162 permits a constant bleed of air from the compartment 109 through compartment 142 to the atmosphere. This allows a small clearance between the exhaust valve 152 and the exhaust valve seat (defined by the extension of spacer 14-13) to revent dead band.
The operation of the electro-pneumatic transducer of the present invention will best be understood by reference to FIGURE 10. The transducer which comprises basically torque motor 22 and relay 28 is utilized in electrical control loops in which the final control element is pneumatically operated. The transducer receives a direct current milliampere input signal and creates a pneumatic output pressure that is directly proportional to this input. The torque motor 22 is the first stage in the conversion of the electrical input signal to a pneumatic output pressure. The second stage in the conversion from the electrical input to the pneumatic output takes place in the relay 28.
Assuming that the transducer is direct-acting, an. increase in the D-C milliampere signal to coils 44 and 45 increases magnetic field around the coils. This increase in magnetic field increases the magnetic strength in the armature 46 and the magnetic attraction across the air gap between the armature and the pole piece means 29 and 33.
The pole piece means are already polarized by the permanent magnet 32. The armature polarity in this case will be as shown in FIGURE 10, for example, with the top pole means 29 comprising a north pole and the bottom pole means 33 comprising a south pole. The magnetic attraction will, therefore, be downward at the nozzle end 46a of the armature 46 and upward at the feedback bellows end 46b, resulting in a torque that rotates the armature 46 about the fixed torsion rod 52 to cover the nozzle opening 511a.
The resulting restriction of the nozzle opening 50a of nozzle 50 produces an increased pressure in the nozzle, in the chamber 143 of the relay and in the feedback bellows '75. The feedback bellows 75 communicates with nozzle 51) and passage 145 in relay 28 via line 41. The relay 28 responds to the increase in nozzle pressure to increase the output pressure to the control valve. The increased pressure in the feedback bellows 75 creates a force that acts on the armature 46 to move it back to the equilibrium position. In this way, the new nozzle pressure is compared to the input current by the force balance principle.
The nozzle pressure acts on the relay diaphragm 136 to force the spacer means 141) (operatively mounted between the two diaphragms 134 and 136) downward against the exhaust valve 152, closing the exhaust port and opening the inlet port a. Supply air then flows through the inlet port 150a and the opening from the chamber 141 through the conduit to the control valve. The output pressure continues to increase until the relay diaphragm assembly is pushed back by the force of the pressure acting on the diaphragm 134 to its original position and the exhaust valve 152 is closed again.
When a decreasing D-C signalis received, the magnetic attraction across the air gap is reduced. The armature 46 rotates or pivots about the axis of torsion rod 52 to uncover the nozzle opening 50a and decrease the pressure in the nozzle 50, relay 28 and feedback bellows 75. The relay diaphragm assembly moves upwardly, as viewed in FIGURE 10, and the exhaust port in the spacer means 140 is opened to bleed the output pressure to the atmosphere through compartment 142 and exhaust opening 116. The output decreases until the diaphragm assembly is forced back to its original position and the exhaust port is closed again. The reduced pressure in the feedback bellows 75 diminishes the force to return the armature 46 to the equilibrium position.
Reverse-acting transducers operate in a similar manner except that when the D-C input signal increases, the output pressure from the relay decreases. Conversely, a decreasing input signal increases the output pressure.
There has been provided by the present invention an improved electro-pneumatic transducer comprising a torque motor which is the first stage in the conversion of the electrical input signal to a pneumatic output pressure and a relay which is the second stage in the conversion from the electrical input to the pneumatic output. The twostage design with each stage possessing its own feedback loop allows for uniformly high stability for any output load. An overall feedback loop was purposely avoided by the present invention in order to maintain stability that was completely independent of the output load. In a presently preferred form of the invention, the high capacity relay will amplify the torque motor nozzle pressure into the output pressure by a three to one ratio. Thus, for a nozzle pressure change of 4 p.s.i., the relay output pressure changes 12 p.s.i., the span for a standard 3 to 15 p.s.i. range.
The high loop gain, the high torque output, and the torsion rod suspension of the armature result in high static performance.
The back of the case or housing for the transducer is designed to mate with a plug-in relay so that the relay may be readily serviced without disturbing the electrical or pneumatic connections. The case and the cover thread together and are gasketed to form an explosion-proof housing which is preserved by the use of porous stainless steel flame arresters in the air passages between the case and the relay.
While there has been shown and described a particular embodiment of this invention, it will be obvious to those skilled in the art that various changes and modifications may be made therein without departing from the invention. Therefore, it is intended in the appended claims to cover all such changes and modifications as fall within the true spirit and scope of the invention.
I claim:
1. In an electro-pneumatic transducer, the combination of housing means, a torque motor assembly removably mounted in said housing means, said torque motor assembly including permanent magnet means and pole pieces associated therewith, an armature and coil assembly including a support bracket carrying electrical coils and pivotally supporting an armature thereon, the armature being movable between the pole pieces in response to electrical energization of said coils, said permanent magnet means and said pole pieces being removable from the torque motor assembly separately from the armature and coil assembly, a bleed nozzle on said housing means operatively associated with said armature, said armature being biased toward the bleed nozzle for restricting the discharge of air from said nozzle, a feedback member operatively associated with said armature and acting on said armature to increase the discharge of air from said bleed nozzle, means for supplying a direct current input signal to said coils to energize said coils and produce a magnetic field having a strength that changes proportionately with the change in input signal, the magnetic attraction between the armature and pole pieces causing movement of the armature to vary the position of the armature with respect to the nozzle opening for controlling the discharge of air from said nozzle, the feedback member cooperating with the nozzle in a force balance relationship.
2. An electro-pneumatic transducer as in claim 1 wherein said feedback member comprises a bellows removably affixed to the armature so as to provide for interchangeability of bellows to accommodate a wide output range.
3. An electro-pneumatic transducer as in claim 1 wherein said armature is provided with adjustable baffle means for covering the nozzle to obtain proper restriction of air flow from the nozzle when the armature is centered between the pole pieces.
4. An electro-pneumatic transducer as in claim 1 wherein a terminal mounting bracket assembly is provided within said housing means for mounting on said torque motor assembly, said mounting bracket assembly including a mounting bracket disposed adjacent the permanent magnet means, the mounting bracket being made from a material whose magnetic permeability change with temperature change is the opposite from the magnetic permeability change of the pole pieces and armature so as to provide for temperature compensation.
5. An electro-pneumatic transducer as in claim 1 wherein a piece of magnetic material is adjustably posi tioned with respect to said permanent magnet to shunt away or add to the magnetic flux in the air gap between the armature and the pole pieces.
6. An electro-pneumatic transducer as in claim 1 wherein the support bracket is adjustably supported in the permanent magnet means for facilitating centering of the armature between the pole pieces.
7. In an electro-pneumatic transducer, the combination of housing means, a torque motor assembly removably mounted in said housing means, said torque motor assembly including permanent magnet means and pole pieces connected to form a subassembly, armature and coil means operatively associated with said pole pieces, said armature and coil means including a support frame fixed with respect to said pole pieces and carrying electrical coils thereon, an armature supported on said support frame for movement between the pole pieces about an axis transverse to the length of said armature, said permanent magnet means and said pole pieces being removable from the torque motor assembly separately from said armature and coil means, nozzle means in said housing means adjacent one end of said armature, said nozzle means being operatively connected to a pneumatic relay by conduit means, said one end of said armature being movable to regulate the discharge of air from said nozzle means, means for biasing the armature toward the nozzle means, a feedback member operative on the other end of said armature in opposition to said biasing means, said feedback bellows communicating with said conduit means, means for supplying a direct current input signal to said coil means to energize said coil means, the magnetic attraction between the armature and the pole pieces causing movement of said armature at its pivot axis to vary the position of said one end with respect to the nozzle means for controlling the discharge of air from said nozzle mean, the feedback member cooperating with the nozzle means in a force balance relationship.
8. An electro-pneumatic transducer as in claim 7 wherein said support frame includes a pair of generally parallel plate members having inwardly bent tabs thereon for supporting said coil means.
9. An electro-pneumatic transducer as in claim 7 wherein said support frame includes a pair of generally parallel plate members joined together by torsion rod means afiixed at its ends to the plate members, said armature being fixedly connected intermediate the ends thereof to said torsion rod means.
It). An electro-pneumatic transducer as in claim 9 wherein said plate members are adjustably supported in said housing means to provide centering adjustment of said armature between said pole pieces.
11. An electro-pneumatic transducer as in claim 8 wherein said housing means has an exhaust opening, a supply air opening and a nozzle connecting opening in one wall thereof and said pneumatic relay includes a housing having an exhaust opening complementary to the housing means exhaust opening, a supply air inlet cooperating with said supply air opening in said housing means, and an outlet opening cooperating With said nozzle connecting opening, and O-ring seal means provided about the respective complementary and cooperating openings, and means for connecting the relay to the housing means, whereby the necessity for separate conduit between the housing means and the relay is obviated.
References Cited UNITED STATES PATENTS 2,844,158 7/1958 Carson 137-85 X 2,954,794 10/1960 Paine 13785 X 3,058,038 10/1962 Stedman 335237 X 3,155,104 11/1964 Hilgert 13785 3,165,262 1/1965 Olliver 13785 X 3,194,998 7/1965 Marfut 335217 ALAN COHAN, Primary Examiner.

Claims (1)

1. IN AN ELECTRO-PNEUMATIC TRANSDUCER, THE COMBINATION OF HOUSING MEANS, A TORQUE MOTOR ASSEMBLY REMOVABLY MOUNTED IN SAID HOUSING MEANS, SAID TORQUE MOTOR ASSEMBLY INCLUDING PERMANENT MAGNET MEANS AND POLE PIECES ASSOCIATED THEREWITH, AN ARMATURE AND COIL ASSEMBLY INCLUDING A SUPPORT BRACKET CARRYING ELECTRICAL COILS AND PIVOTALLY SUPPORTING AN ARMATURE THEREON, THE ARMATURE BEING MOVABLE BETWEEN THE POLE PIECES IN RESPONSE TO ELECTRICAL ENERGIZATION OF SAID COILS, SAID PERMANENT MAGNET MEANS AND SAID POLE PIECES BEING REMOVABLE FROM THE TORQUE MOTOR ASSEMBLY SEPARATELY FROM THE ARMATURE AND COIL ASSEMBLY, A BLEED NOZZLE ON SAID HOUSING MEANS OPERATIVELY ASSOCIATED WITH SAID ARMATURE, SAID ARMATURE BEING BIASED TOWARD THE BLEED NOZZLE FOR RESTRICTING THE DISCHARGE OF AIR FROM SAID NOZZLE, A FEEDBACK MEMBER OPERATIVELY ASSOCIATED WITH SAID ARMATURE AND ACTING ON SAID
US47993565 1965-08-16 1965-08-16 Electro-pneumatic transducer Expired - Lifetime US3334642A (en)

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US47993565 US3334642A (en) 1965-08-16 1965-08-16 Electro-pneumatic transducer
FR45697A FR1467313A (en) 1965-08-16 1966-01-12 Electro-pneumatic transducer
DE19661523496 DE1523496A1 (en) 1965-08-16 1966-01-21 Electropneumatic converter
GB2235866A GB1117794A (en) 1965-08-16 1966-05-19 Electro-pneumatic transducer

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US3500722A (en) * 1968-12-16 1970-03-17 Rudolph L Franz Electro-magnetic transducer
DE3116640A1 (en) * 1981-04-27 1982-11-11 Samson Ag, 6000 Frankfurt Pneumatic position controller having a limit switch
EP0120594A2 (en) * 1983-02-24 1984-10-03 The Babcock & Wilcox Company Electro-pneumatic transducer assemblies
US5439021A (en) * 1992-09-09 1995-08-08 Fisher Controls International, Inc. Electro-pneumatic converter
WO2016210397A1 (en) * 2015-06-25 2016-12-29 Tescom Corporation Non-inert gas certified electronic controller
US20170368393A1 (en) * 2016-06-27 2017-12-28 Jacob T. R. Renollett Explosion resistant electro-pneumatic controller

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Publication number Priority date Publication date Assignee Title
US3911238A (en) * 1973-12-06 1975-10-07 Automatic Switch Co Condition responsive control device with capacity for independent adjustment of control points and transducer therefor
DE3437487A1 (en) * 1984-10-12 1986-04-17 H. Kuhnke Gmbh Kg, 2427 Malente BISTABLE SOLENOID VALVE
DE3500731A1 (en) * 1985-01-11 1986-07-17 Honeywell Gmbh, 6050 Offenbach Electro-pneumatic signal converter or pneumatic actuator
GB9519578D0 (en) * 1995-09-26 1995-11-29 Grau Ltd Pneumatic relay valve

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US2844158A (en) * 1955-08-29 1958-07-22 Ex Cell O Corp Electro-hydraulic servo actuators
US2954794A (en) * 1955-11-01 1960-10-04 William A Paine Electro-hydraulic servo and inverter system
US3058038A (en) * 1959-11-20 1962-10-09 Weston Hydraulics Ltd Torque motor with null balance
US3155104A (en) * 1962-03-23 1964-11-03 Johnson Service Co Electric-pressure transducers
US3165262A (en) * 1963-07-15 1965-01-12 Fischer & Porter Co Pneumatic computer
US3194998A (en) * 1961-12-13 1965-07-13 Gen Electric Magnetic temperature-compensating structure

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US2844158A (en) * 1955-08-29 1958-07-22 Ex Cell O Corp Electro-hydraulic servo actuators
US2954794A (en) * 1955-11-01 1960-10-04 William A Paine Electro-hydraulic servo and inverter system
US3058038A (en) * 1959-11-20 1962-10-09 Weston Hydraulics Ltd Torque motor with null balance
US3194998A (en) * 1961-12-13 1965-07-13 Gen Electric Magnetic temperature-compensating structure
US3155104A (en) * 1962-03-23 1964-11-03 Johnson Service Co Electric-pressure transducers
US3165262A (en) * 1963-07-15 1965-01-12 Fischer & Porter Co Pneumatic computer

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3500722A (en) * 1968-12-16 1970-03-17 Rudolph L Franz Electro-magnetic transducer
DE3116640A1 (en) * 1981-04-27 1982-11-11 Samson Ag, 6000 Frankfurt Pneumatic position controller having a limit switch
EP0120594A2 (en) * 1983-02-24 1984-10-03 The Babcock & Wilcox Company Electro-pneumatic transducer assemblies
EP0120594B1 (en) * 1983-02-24 1988-06-22 The Babcock & Wilcox Company Electro-pneumatic transducer assemblies
US5439021A (en) * 1992-09-09 1995-08-08 Fisher Controls International, Inc. Electro-pneumatic converter
US5533544A (en) * 1992-09-09 1996-07-09 Fisher Controls International, Inc. Supply biased pneumatic pressure relay
WO2016210397A1 (en) * 2015-06-25 2016-12-29 Tescom Corporation Non-inert gas certified electronic controller
US10197181B2 (en) 2015-06-25 2019-02-05 Tescom Corporation Non-inert gas certified electronic controller
US20170368393A1 (en) * 2016-06-27 2017-12-28 Jacob T. R. Renollett Explosion resistant electro-pneumatic controller
US10385879B2 (en) * 2016-06-27 2019-08-20 Tescom Corporation Explosion resistant electro-pneumatic controller

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FR1467313A (en) 1967-01-27
GB1117794A (en) 1968-06-26

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