US2488734A - Dynamo transformer - Google Patents

Dynamo transformer Download PDF

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US2488734A
US2488734A US652523A US65252346A US2488734A US 2488734 A US2488734 A US 2488734A US 652523 A US652523 A US 652523A US 65252346 A US65252346 A US 65252346A US 2488734 A US2488734 A US 2488734A
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rotor
poles
torque
coils
proportional
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Robert K Mueller
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Research Corp
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    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D3/00Control of position or direction
    • G05D3/12Control of position or direction using feedback
    • G05D3/121Control of position or direction using feedback using synchromachines (selsyns)
    • G05D3/122Control of position or direction using feedback using synchromachines (selsyns) without modulation
    • 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
    • Y10T74/00Machine element or mechanism
    • Y10T74/12Gyroscopes
    • Y10T74/1261Gyroscopes with pick off

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  • the present invention relates to electromagnetic apparatus and more particularly to torque motors and related devices, herein referred to under the general designation of variable dynamo transformers.
  • the torque motor may be considered.
  • any motor can be classed as a torque motor but the term is usually applied to a motor which is not continuously rotatable and in particular cases is capable of movement through only a relatively small angle.
  • Such motors are useful in servomechanisms and in other applications where a definite torque is required which is dependent on an electrical input.
  • One of the objects of the present invention is to provide a torque motor in which the generated torque is substantially independent of displacement over the working range and in which a precise value of torque in accordance with the electrical input may be obtained.
  • Another form of the invention comprises what may be termed a stiffness motor in which a torque substantially proportional to displacement may be obtained.
  • A'device of this type is of great importance as an electrical means to take the place of a mechanical spring. It has the advantage that the spring constan may be made practically uniform over the working range and further that the constant may be easily adjusted by electrical means.
  • Another embodiment of the invention is an electrical transformer or pickofi in which an output voltage may be obtained which is proportional to the mechanical displacement of the rotor.
  • This device is likewise an apparatus of high precision and finds utility in servomechanisms and systems of similar character.
  • Fig. 1 is an elevation of one form of apparatus according to the present invention.
  • Figs. 2, 3 and 4 are diagrams of the magnetomotive force patterns for differ ent coil connections; Figs. 5, 6, 7 and 8 are diagrams of winding connections;
  • Fig. 9 is a perspective view illustrating fringing effects;
  • Fig. 10 is a diagram of a combined torque and stifiness motor;
  • Fig. 11 is a diagram of a modified construction;
  • Fig. 12 is an elevation of a device in which the motion is rectilinear;
  • Figs. 13 to 15 are diagrams of magnetomotive force patterns;
  • Fig. 16 shows a modification of Fig. 12;
  • FIG. 17 is an elevation showing a moving element pivoted on a remote axis;
  • Fig. 18 is a diagram of a simple and precise servomechanism embodying devices of the type described herein; and
  • Fig. 19 is a diagram of a variable-ratio device.
  • the device shown in Fig. 1 comprises a stator Ill preferably constructed of laminations of magnetic material.
  • the shape is essentially circular with four re-entrant poles [2.
  • a rotor I4 is pivoted or journaled in suitable bearings about an axis at the center of the stator frame.
  • Each pole I2 is provided with either one or two windings indicated as double windings l6 and I8 in Fig. 1.
  • a single winding for each pole is sumcient and in other cases the double windings are required.
  • the rotor is of magnetic material, such as soft iron, and is not permanently magnetized, nor does it carry any windings. It has circular end portions 20, each spanning the distance between centers of two adjacent poles. The pole faces are formed to provide an accurately uniform air gap with relation to the ends of the rotor.
  • the sides 22 of the rotor are not of critical shape and are conveniently formed as circular arcs tangent to the radii drawn to the extreme edges of the circular end portions 20.
  • the normal or neutral position of the rotor is with its edges at the centers of the pole faces as indicated in Fig. 1.
  • FIG. 3 The connections shown in Fig. 3 are similar to those in Fig. 2 except that the coils for poles a and c are reversed.
  • the magnetomotive force patterns of Figs. 2 and 3 are therefore similar in that forces on two of the adjacent poles are directed inwardly. while those of the other two poles are directed outwardly.
  • the connections in Fig. 4 are such that the magnetomotive forces are consecutively directed inwardly and outwardly for the several poles.
  • a combination of the connections of Figs. 2 and 3 may be used. These connections are shown in Fig. 5 wherein one of the windings I6 is connected as in Fig. 2 and the other winding II is connected as in Fig. 3.
  • the two windings are connected to separate inputs indicated as input i and input 2, each of which may include a resistor 24 for a purpose to be presently described.
  • One winding carries a current 11; the other winding carries a current in.
  • the currents may be either direct current or alternating current of the same frequency.
  • the torque tending to move the rotor from neutral position is proportional to an.
  • the torque is substantially constant over the range of motion for which fringing effects arenegligible, as will be explained later. In general only a few degrees of motion are required, say ten or twenty degrees, at the most, and within that range a remarkably uniform torque'is obtained. It will be understood that if the torque is unresisted the rotor will move until it is centered with respect to one opposite pair of poles. In most applications, however, the torque is resisted by other torques and only a small range of motion is permitted.
  • the torque should be proportional to voltagw, rather than currents, and to this end resistors 24, II are connected in series with the inputs, the resistors being of sufliciently high resistance that the currents, and hence the magnetomotive forces, are substantially proportional to the input voltages, notwithstanding changes in mutual inductance, as will be explained later. Then if the input voltages are er and ea, the torque is proportional to e132- If there is a time phase diflerence between the inputs this product must be multiplied by the cosine of the phase angle. In any event a torque is obtained which is proportional to the two quantities er and 8:. If one of the inputs is a constant reference voltage, the torque will be proportional to the other input voltage.
  • the mutual inductance between the windings l6 and il changes with displacement from neutral position.
  • the net mutual flux is zero, but with a change in position, flux due to the magnetomotive forces of one winding will link the coils of the other winding.
  • the mutual flux linkages, and hence the mutual inductance are proportional to the angle of displacement.
  • the energy output upon motion from neutral to any angular position is the mutual inductance times the product of the currents in the two sets of windings.
  • the torque is proportional to the derivative of energy with respect to displacement, and since the mutual inductance is proportional to displacement the torque is constant for all displacements.
  • the magnetomotive force pattern of Fig. 4 in which the magnetomotive forces are alternately toward and away from the rotor produces a different operation.
  • the motor is one in which the torque is proportional to displacement of the rotor from neutral. It is the equivalent of a spring and is useful for many purposes. Only one winding i0 is required and its four coils are connected in series according to the convention of Fig. 4. For this connection the total self-inductance does not remain constant for different positions of the rotor.
  • V Eor purposes of explanation the rotor can be considered as divided along its axis as indicated by the dot-and-dash line in Fig. 4. No flux crosses that line and each half of the rotor may be considered separately. The flux passing through one half of the rotor crosses two air gaps in series. Upon any movement from neutral position one of the gaps is increased in area while the other is reduced. The total reluctance of the flux path is not maintained constant.
  • the reluctance of one gap is a 60 (where a and b are constants and 0 is the angle of displacement from neutral) and the reluctance of the other gap is a-b0
  • the total reluctance of the flux path is the sum of these expressions which is equal to is proportional to th magnetomotive force squared, which, in turn, is proportional to the current squared in the winding.
  • the strength of the spring is easily varied by the series resistor 28 or any suitable means for varying the current. The device thus offers an opportunity for accurate spring adjustment.
  • these patterns may be obtained by various winding connections, some of which may b preferred to the connections of Fig. 5 because of their simplicity or their better adaptation to associated equipment.
  • a simple modification of Fig. 5 is shown in Fig. 6 wherein the windings l6 and i8 have their coils connected in series-parallel fashion (but with necessary reversal of some coil connections in order to duplicate the magnetomotive force patterns of Figs. 2 and 3); the same results are obtained as in Fig. 5 and the same theoretical considerations are applicable.
  • Fig. 7 only a single set of four coils is used, the coils being connected in the form of a square with inputs l and 2 connected to diagonally opposite corners. It will be seen that the coils may be connected in such a manner that the winding convention of the coils for input I is the same as for Fig. 2 and the winding convention for input 2 is the same as for Fig. 3. Current ii if impressed alone would produce the magnetomotive force pattern of Fig. 2. and current is alone would produce the pattern of Fig. 3. In combination the same results are obtained as in the double winding construction of Fig. 5. ment of Fig. 7 cannot be used, however, if input circuits have to be isolated.
  • Fig. 8 represents a further simplification in the that only two coils are used for each input. In-.
  • Fig. 9 I is a perspective view of a portion of the rotor opposite one of the pole faces, the rotor being shown as displaced counterclockwise from neutral. At this position a certain portion of the width of the rotor is directly opposed to the pole face according to the dimension indicated at h. The length of the airgap is indicated by g.
  • the range of movement of the rotor should be limited so that h is always somewhat larger than 9 and preferably not less than twice as large. This is the requirement for high precision since variable fringing effects may disturb the linear relationships heretofore described if the rotor is allowed to turn farther toward the edge of the pole face.
  • Fig. 10 B p- Connections for a combined torque and stiffness motor are shown in Fig. 10.
  • a source of potential 2E1 is connected to two diagonal corners of the bridge and another source 2E2 is connected to the other two corners.
  • These potentials may be supplied by transformers, the secondaries of which are indicated at 28 and 30.
  • Another source of potential indicated as of magnitude IE is connected at its ends to the mid-points of the transformer secondaries 28 and 30.
  • the point of zero potential for the system may be taken as the mid-point of the source designated 2E.
  • the currents due to these separate voltages produce a magnetomotive force pattern which is equivalent to the superposition of the three pattoms of Figs. 2, 3 and 4.
  • neutral position is not necessarily that shown in- Fig. 10 but depends upon the solution of the above expression for zero torque. It is to be noted that the three voltages E, E1 and E2 need not all be of the same frequency. The voltage E which is the only one appearing in the stiffness term may tween E1 and E2 the constant torque component is proportional to the cosine of the phase angle.
  • Apparatus of similar form may be used as a pick-oif or variable transformer to give a variable voltage or current in accordance with the position of the rotor.
  • the connections of any of Figs. 5, 6, 7 and 8 may be used except that one of the inputs, say input 2, becomes an output.
  • an output voltage appears at the terminals of the output, and the magnitude of the voltage is varied by displacing the rotor.
  • the output voltage is zero.
  • the phase of the output voltage differs degrees for motions in opposite directions from neutral.
  • a pick-off having an output voltage proportional to the square of the rotor displacement is useful in some measuring applications and is 7 provided by connecting each winding (l4 and II) in the same coil sequence as shown for the single winding of Fig. 4.
  • the selfinductance of each winding is variable and is in fact represented by an expression of the form a'-b'l'.
  • the back electromotive force involves a term proportional to that is, proportional to the square of the displacement.
  • FIG. 11 A modified construction of the apparatus is shown in Fig. 11 wherein the coils are wound on the portions of the stator between the pole faces.
  • the stator is conveniently built up of identical lamlnatlons of the shape indicated at 25, the laminations of alternate layers being inverted and having their long end portions It inserted through the coils 3
  • This construction permits the use of wide angle pole-faces as indicated at 52. although the device may be constructed with narrow pole faces if desired.
  • the wide poles allow a greater range of movement of the rotor, but with some slight loss of linear characteristics at the ends of the range.
  • Magnetomotive force patterns identical to those shown in Figs. 2 to 4 may be obtained with this construction by appropriate coil connections which need not be described in detail.
  • This embodiment of the invention may be used in any of the ways described for the construction of Fig. 1.
  • the principles of the present invention may also be applied to motors and pick-oil's in which the motion of the moving part is in translation or about an axis remote from the center of the stator.
  • the stator 33 is provided with four re-entrant poles I4 lettered a, b, c and d. Poles 0 and b are at one side of the frame and are respectively opposed to poles c and d at the other side.
  • a rectangular movable membr 35 is used in place of the rotor.
  • Each pole is provided with suitable coils ll and 40.
  • the apparatus may -be used either as a force motor or as a pick-oil.
  • force motor is used in contradistinction to a torque motor because the member 36 is constrained to move sidewise instead of rotating.
  • the magnetomotive force patterns for difierent coil connections are indicated by Figs. 13, 14 and 15, in which the same notation for indicating the magnetomotive forces is used as in Figs. 2, 3 and 4, but for convenience the coils are omitted.
  • the double arrows on the member 35 indicate that the member is mounted for sidewise movement.
  • Fig. 13 corresponds exactly to Fig. 2 in principle
  • the coils are connected to give a magnetomotive force pattern which is a combination of the patterns of Figs. 13 and 14.
  • a constant force will be exerted on the member 36 independently oi its position (so far as fringing effects are negligible) and the force is proportional to the product of the currents in the two sets of coils.
  • the same connections are used and with a current of constant amplitude in one set of coils, the voltage induced in the other set of coils will be proportional to the sidewise displacement of the element 36 from neutral.
  • Fig. 15 represents a stifi'ness motor, in which the force on the element It is proportional to the displacement from neutral position.
  • FIG. 18 Various simplified coil connections for the translational device may be used in exactly the same manner as for the rotary form. Moreover, instead of using coils wound on the pole-pieces, as in Fig. 18, the coils may be wound on the legs between the coils, as indicated at 42 and 44. It will be apparent to those skilled in the art that the windings may be connected to give any desired magnetomotive force pattern represented by Figs. 13 to 15.
  • the member 36 In actual construction, to avoid the use of a mounting for sliding movement of the member 36, it is preferably mounted on an arm 46 for rotation about a remote axis 48, as shown in Fig. 17.
  • the element 35 and pole faces are formed on arcs about the axis 48. The motion of the movable element is in effect a translation with respect to the poles.
  • Fig. 18 An extremely precise servomechanism for following small angular displacements and embodying several of the variable dynamo-transformers heretofore described is shown in Fig. 18.
  • the preferred units are a transmitting pick-off II, a following pick-off 52 and a servomotor 54.
  • the motor 54 may be of the type shown in Fig. 8.
  • the following pick-01f 52 and the motor 54 are mounted on the same shaft.
  • the winding connections of the units 50 and 52 are the same as illustrated in Fig. 5.
  • the coils i 6 of one set of the unit 50 are connected in series and in the same sense with the corresponding coils of the unit 52 whereby these coils carry the current i; supplied from any suitable reference source.
  • the output coils l8 are connected in series opposition and to a transformer 55 forming the input of a sense detecting rectifier and amplifier It.
  • the voltage applied to the amplifier is proportional to the "error," that is, to the difference between the angular positions of the rotors of the units II and 52.
  • the amplifier output feeds direct current to the motor 54 for which the connections are as in Fig. 8.
  • the coils on two opposite poles carry a current i: and the coils on the other two opposite poles carry a current is.
  • the construction of the sense detecting rectifier is well known in the art and is not described in detail here.
  • the motor may be made to follow the transmitting pick-01f with a displacement ratio different from unity. This is accomplished by relatively varying the magnetomotive forces of the two windings l6. By using a turns ratio different from unity in either or both sets of coils of the units 50 and 52, the magnetomotive force ratio may be made different from unity. Thus if the winding I6 of the pick-off 52 has twice as many turns as the corresponding winding of the pick-01f 50, the output will have only one-half the angular motion of the input.
  • FIG. 19 Another connection for obtaining a desired displacement ratio is shown in Fig. 19.
  • the windings 16 of the pick-offs 50 and 52 are connected to the ends of a current divider, consisting of a large inductive impedance 60.
  • One side of the source of reference voltage is connected to a line 62 joining the ends of the windings, and the other side of the source is connected to the impedance 60 through a variable tap 64.
  • the current will divide between the two windings in a ratio dependent on the position of the tap.
  • the ratio of rotor displacements of the two pick-offs is inversely proportional to the ratio of currents.
  • the impedance is preferably a large inductance, in order that the currents in the two windings will remain in substantially the same phase.
  • a dynamo transformer comprising a stator having four symmetrically disposed poles, a movable element of magnetic material mounted within the stator and having a neutral position with respect to the poles, the movable element being capable of limited movement from said neutral position, two sets of stator windings, one set of windings being associated with all four poles and connected to produce a magnetomotive force pattern in which the forces are directed inwardly in two adjacent poles and outwardly in the other two poles, and the other 'set of windings being associated with all four poles and connected to produce a similar pattern but displaced from that of the first set.
  • a dynamo transformer comprising a stator having four symmetrically disposed poles, a movable element of magnetic material mounted within the stator and having a neutral position symmetrical with respect to the poles, the movable element being capable of limited movement from said neutral position, two sets of stator windings, one set of windings being associated with all four poles and connected to produce a magnetomotive force'pattern in which the forces are directed inwardly in two adjacent poles and outwardly in the other two poles, said set of windings having a substantially constant self inductance, and the other set of windings being associated with all four poles and connected to produce a similar pattern but displaced from that of the first set, said other set of windings being also of substantially constant self-inductance, the mutual inductance of the windings being substantially proportional to the displacement of the movable element from neutral position.

Description

Nov, 22, 1949' R. K. MUELLER DYNAMO TRANSFORMER 4 Sheets-Sheet 1 Filed March 7, 194a Nov. 22, 1949 R. K. MUELLER DYNAIO TRANSFORMER 4 Sheets-Sheet 2 Filed March 7, 1946 lNPUT 1 INPUT 2' INPUT 2 INPUT 1 Nov. 22, 1949 R. K. MUELLER DYNAMO TRANSFORMER 4 Sheets-Sheet 5 Filed March 7. 1946 Nov. 22, 1949 R. K. MUELLER 2,488,734
DYNAMO TRANSFORMER Filed March 7, 1946 4 Sheets-Sheet 4 TRANSMITTING FOLLOWING PIC/('OFF P/CK-OFF REFERENCEAC.
5EN$E- 55., DE TE CT/NG AMPL lF/ER L 0 Fly 19 1 REFERENCE A.C
Patented Nov. 22, 1949 DYNAMO TRANSFORMER Robert K. MnelleryNewton, Mass., assignor, by mesne assignments, to Research Corporation, New York, N. Y., a corporation of New York Application March 7, 194.6, Serial No. 652,523
2 Claims.
The present invention relates to electromagnetic apparatus and more particularly to torque motors and related devices, herein referred to under the general designation of variable dynamo transformers.
As a specific example of apparatus in this general category the torque motor may be considered. In general any motor can be classed as a torque motor but the term is usually applied to a motor which is not continuously rotatable and in particular cases is capable of movement through only a relatively small angle. Such motors are useful in servomechanisms and in other applications where a definite torque is required which is dependent on an electrical input. One of the objects of the present invention is to provide a torque motor in which the generated torque is substantially independent of displacement over the working range and in which a precise value of torque in accordance with the electrical input may be obtained.
Another form of the invention comprises what may be termed a stiffness motor in which a torque substantially proportional to displacement may be obtained. A'device of this type is of great importance as an electrical means to take the place of a mechanical spring. It has the advantage that the spring constan may be made practically uniform over the working range and further that the constant may be easily adjusted by electrical means.
Another embodiment of the invention is an electrical transformer or pickofi in which an output voltage may be obtained which is proportional to the mechanical displacement of the rotor. This device is likewise an apparatus of high precision and finds utility in servomechanisms and systems of similar character.
I have devised a simple form of apparatus useful for these and other purposes. The general construction of the apparatus is substantially alike for the various embodiments and only the winding connections need to be varied for different uses.
In the accompanying drawings Fig. 1 is an elevation of one form of apparatus according to the present invention. Figs. 2, 3 and 4 are diagrams of the magnetomotive force patterns for differ ent coil connections; Figs. 5, 6, 7 and 8 are diagrams of winding connections; Fig. 9 is a perspective view illustrating fringing effects; Fig. 10is a diagram of a combined torque and stifiness motor; Fig. 11 is a diagram of a modified construction; Fig. 12 is an elevation of a device in which the motion is rectilinear; Figs. 13 to 15 are diagrams of magnetomotive force patterns; Fig. 16 shows a modification of Fig. 12; Fig. 17 is an elevation showing a moving element pivoted on a remote axis; Fig. 18 is a diagram of a simple and precise servomechanism embodying devices of the type described herein; and Fig. 19 is a diagram of a variable-ratio device.
The device shown in Fig. 1 comprises a stator Ill preferably constructed of laminations of magnetic material. The shape is essentially circular with four re-entrant poles [2. A rotor I4 is pivoted or journaled in suitable bearings about an axis at the center of the stator frame. Each pole I2 is provided with either one or two windings indicated as double windings l6 and I8 in Fig. 1. For some purposes which will be hereinafter described a single winding for each pole is sumcient and in other cases the double windings are required.
The rotor is of magnetic material, such as soft iron, and is not permanently magnetized, nor does it carry any windings. It has circular end portions 20, each spanning the distance between centers of two adjacent poles. The pole faces are formed to provide an accurately uniform air gap with relation to the ends of the rotor. The sides 22 of the rotor are not of critical shape and are conveniently formed as circular arcs tangent to the radii drawn to the extreme edges of the circular end portions 20. The normal or neutral position of the rotor is with its edges at the centers of the pole faces as indicated in Fig. 1.
Various uses of the apparatus as torque motors, stiffness motors and transformers depend on the connections of the windings. The different possible connections will be explained in connection with the diagrams of Figs. 2, 3 and 4. In each diagram the four poles are designated consecutively by the letters a, b, c and d. In each case a single winding I6 is shown, consisting of all four of its coils connected in series. For simplicity the coils are shown as arranged outside the frame but it will be understood that they are wound on the pole pieces as shown in Fig. 1. A convention designating the directions of the magnetomotive forces is necessary. In these diagrams the ends of each coil are designated l and 2. The convention is that when current flows in the coil between points I and 2 the magnetomotive force due to the coil is inward toward the rotor, and when the current is from 2 to l the magnetomotive force is outward away from the rotor. Thus in Fig. 2 the magnetomotive forces are inward for poles b and c and outward for poles a and d.
3 The connections shown in Fig. 3 are similar to those in Fig. 2 except that the coils for poles a and c are reversed. The magnetomotive force patterns of Figs. 2 and 3 are therefore similar in that forces on two of the adjacent poles are directed inwardly. while those of the other two poles are directed outwardly. The connections in Fig. 4 are such that the magnetomotive forces are consecutively directed inwardly and outwardly for the several poles.
For a torque motor a combination of the connections of Figs. 2 and 3 may be used. These connections are shown in Fig. 5 wherein one of the windings I6 is connected as in Fig. 2 and the other winding II is connected as in Fig. 3. The two windings are connected to separate inputs indicated as input i and input 2, each of which may include a resistor 24 for a purpose to be presently described. One winding carries a current 11; the other winding carries a current in. The currents may be either direct current or alternating current of the same frequency.
The torque tending to move the rotor from neutral position is proportional to an. The torque is substantially constant over the range of motion for which fringing effects arenegligible, as will be explained later. In general only a few degrees of motion are required, say ten or twenty degrees, at the most, and within that range a remarkably uniform torque'is obtained. It will be understood that if the torque is unresisted the rotor will move until it is centered with respect to one opposite pair of poles. In most applications, however, the torque is resisted by other torques and only a small range of motion is permitted.
In most instances it is desirable that the torque should be proportional to voltagw, rather than currents, and to this end resistors 24, II are connected in series with the inputs, the resistors being of sufliciently high resistance that the currents, and hence the magnetomotive forces, are substantially proportional to the input voltages, notwithstanding changes in mutual inductance, as will be explained later. Then if the input voltages are er and ea, the torque is proportional to e132- If there is a time phase diflerence between the inputs this product must be multiplied by the cosine of the phase angle. In any event a torque is obtained which is proportional to the two quantities er and 8:. If one of the inputs is a constant reference voltage, the torque will be proportional to the other input voltage.
For practical applications simpler winding connections may be used than are shown in Fig. 5. Before describing such connections the principles on which the device operates will be explained. The operation depends on two fundamental principles; flrst that the self-inductance for each input is constant for all angular positions within the working range; and second that the mutual inductance increases linearly with the displacement from neutral.
That the self-inductance for each input remains constant may be seen by considering Fig. 2. with the rotor in neutral position the inductance has a certain value which depends primarily on the length of the air gaps between the rotor and the pole pieces. In the succeeding description the entire magnetic reluctance is considered to be concentrated in the air gaps. The reluctance of the paths through the rotor and frame will be neglected since it has been found in practical experience to be negligible. If the rotor is turned slightly from neutral, say in a clockwise direction, the reluctance decreases at poles a and c and increases at poles b and d. More flux will pass into the rotor through poles a and c and less through poles b and d but it can be readily seen that the total flux through the four gaps remains constant. Since the coils are all in series the inductance of the entire winding II is a constant regardless of the angular position of the rotor. This is true if fringing eifects are neglected which is proper within the limited range of motion for which the motor is particularly useful. From similar considerations the total self-inductance of each winding II and II in Fig. 5 is likewise constant regardless of the angular position of the rotor.
It can also be readily seen that the mutual inductance between the windings l6 and il changes with displacement from neutral position. For in neutral position the net mutual flux is zero, but with a change in position, flux due to the magnetomotive forces of one winding will link the coils of the other winding. The mutual flux linkages, and hence the mutual inductance, are proportional to the angle of displacement. The energy output upon motion from neutral to any angular position is the mutual inductance times the product of the currents in the two sets of windings. The torque is proportional to the derivative of energy with respect to displacement, and since the mutual inductance is proportional to displacement the torque is constant for all displacements.
The magnetomotive force pattern of Fig. 4 in which the magnetomotive forces are alternately toward and away from the rotor produces a different operation. The motor is one in which the torque is proportional to displacement of the rotor from neutral. It is the equivalent of a spring and is useful for many purposes. Only one winding i0 is required and its four coils are connected in series according to the convention of Fig. 4. For this connection the total self-inductance does not remain constant for different positions of the rotor. V Eor purposes of explanation the rotor can be considered as divided along its axis as indicated by the dot-and-dash line in Fig. 4. No flux crosses that line and each half of the rotor may be considered separately. The flux passing through one half of the rotor crosses two air gaps in series. Upon any movement from neutral position one of the gaps is increased in area while the other is reduced. The total reluctance of the flux path is not maintained constant.
The reluctance of one gap is a 60 (where a and b are constants and 0 is the angle of displacement from neutral) and the reluctance of the other gap is a-b0 The total reluctance of the flux path is the sum of these expressions which is equal to is proportional to th magnetomotive force squared, which, in turn, is proportional to the current squared in the winding. The strength of the spring is easily varied by the series resistor 28 or any suitable means for varying the current. The device thus offers an opportunity for accurate spring adjustment.
Referring to the torque motor exemplified by the magnetomo-tive force patterns of Figs. 2 and 3, these patterns may be obtained by various winding connections, some of which may b preferred to the connections of Fig. 5 because of their simplicity or their better adaptation to associated equipment. A simple modification of Fig. 5 is shown in Fig. 6 wherein the windings l6 and i8 have their coils connected in series-parallel fashion (but with necessary reversal of some coil connections in order to duplicate the magnetomotive force patterns of Figs. 2 and 3); the same results are obtained as in Fig. 5 and the same theoretical considerations are applicable.
In Fig. 7 only a single set of four coils is used, the coils being connected in the form of a square with inputs l and 2 connected to diagonally opposite corners. It will be seen that the coils may be connected in such a manner that the winding convention of the coils for input I is the same as for Fig. 2 and the winding convention for input 2 is the same as for Fig. 3. Current ii if impressed alone would produce the magnetomotive force pattern of Fig. 2. and current is alone would produce the pattern of Fig. 3. In combination the same results are obtained as in the double winding construction of Fig. 5. ment of Fig. 7 cannot be used, however, if input circuits have to be isolated.
Fig. 8 represents a further simplification in the that only two coils are used for each input. In-.
put I is connected to the coils on poles a and-c in series and input 2 is connected to the coils on poles b and d in series. It will be observed that if the two currents are equal in magnitude, the same magnetomotive force pattern is obtained as in Fig. 2. When the currents are unequal, the pattern is a composite of Figs. 2 and 3; hence the connection is proper for a torque motor. The torque is constant for all angular positions but is proportional to (i1+i2)(i1-i2). The fact that the torque is dependent on sum and difference terms makes the arrangement convenient for application in some electronic circuits and particularly for the servomechanism to be described later.
Mention has been made of fringing effects.
These are explained by reference to Fig. 9 which I is a perspective view of a portion of the rotor opposite one of the pole faces, the rotor being shown as displaced counterclockwise from neutral. At this position a certain portion of the width of the rotor is directly opposed to the pole face according to the dimension indicated at h. The length of the airgap is indicated by g. In general it has been found that the range of movement of the rotor should be limited so that h is always somewhat larger than 9 and preferably not less than twice as large. This is the requirement for high precision since variable fringing effects may disturb the linear relationships heretofore described if the rotor is allowed to turn farther toward the edge of the pole face.
In cases where extreme precision is not essential an increased motion of the rotor may be permitted. It will be noted from Fig. 9 that the rotor and pole faces are of considerable thickness so that the thickness is always large in The arrange-' comparison to the other dimensions of theair B p- Connections for a combined torque and stiffness motor are shown in Fig. 10. Here a single coil per pole may be used. A source of potential 2E1 is connected to two diagonal corners of the bridge and another source 2E2 is connected to the other two corners. These potentials may be supplied by transformers, the secondaries of which are indicated at 28 and 30. Another source of potential indicated as of magnitude IE is connected at its ends to the mid-points of the transformer secondaries 28 and 30. The point of zero potential for the system may be taken as the mid-point of the source designated 2E. The currents due to these separate voltages produce a magnetomotive force pattern which is equivalent to the superposition of the three pattoms of Figs. 2, 3 and 4.
Assuming that the currents in the coils are proportional to the potential differences across them an expression for torque in terms of the voltages can be obtained. The derivation of this expression would serve no useful purpose here but the final expression is that the torque is equal to k1E1E2+k26E where in and k2 are constants determined by the characteristics of the motor. It will be noted that the total torque is made up of a constant term proportional to the product of the voltages E1 and E2 and a stiffness torque proportional to El and also proportional to the displacement angle from a neutral position. The
neutral position is not necessarily that shown in- Fig. 10 but depends upon the solution of the above expression for zero torque. It is to be noted that the three voltages E, E1 and E2 need not all be of the same frequency. The voltage E which is the only one appearing in the stiffness term may tween E1 and E2 the constant torque component is proportional to the cosine of the phase angle.
The devices heretofore described are useful as motors. Apparatus of similar form may be used as a pick-oif or variable transformer to give a variable voltage or current in accordance with the position of the rotor. For a pick-off in which the output voltage is proportional to rotor' displacement, the connections of any of Figs. 5, 6, 7 and 8 may be used except that one of the inputs, say input 2, becomes an output. For a constant excitation voltage applied to input I an output voltage appears at the terminals of the output, and the magnitude of the voltage is varied by displacing the rotor. When the rotor. is in neutral position the output voltage is zero. As the rotor is moved the output voltage increases. The phase of the output voltage differs degrees for motions in opposite directions from neutral. The
operation of the device as a pick-off depends upon principles heretofore explained, namely, the constancy of self-inductance and the fact that the F mutual inductance is a linear function of disticularly applicable to servomechanisms and similar equipment.
A pick-off having an output voltage proportional to the square of the rotor displacement is useful in some measuring applications and is 7 provided by connecting each winding (l4 and II) in the same coil sequence as shown for the single winding of Fig. 4. As heretofore noted in connection with the description of Fig. 4, the selfinductance of each winding is variable and is in fact represented by an expression of the form a'-b'l'. Upon passage of a current through the input winding, the back electromotive force involves a term proportional to that is, proportional to the square of the displacement. The
mutual inductance is constant, regardless of rotor position, hence, a voltage proportional to the square of the displacement appears at the output terminals.
A modified construction of the apparatus is shown in Fig. 11 wherein the coils are wound on the portions of the stator between the pole faces. The stator is conveniently built up of identical lamlnatlons of the shape indicated at 25, the laminations of alternate layers being inverted and having their long end portions It inserted through the coils 3|. This construction permits the use of wide angle pole-faces as indicated at 52. although the device may be constructed with narrow pole faces if desired. The wide poles allow a greater range of movement of the rotor, but with some slight loss of linear characteristics at the ends of the range. Magnetomotive force patterns identical to those shown in Figs. 2 to 4 may be obtained with this construction by appropriate coil connections which need not be described in detail. This embodiment of the invention may be used in any of the ways described for the construction of Fig. 1.
The principles of the present invention may also be applied to motors and pick-oil's in which the motion of the moving part is in translation or about an axis remote from the center of the stator. In this type of device, one form of which is shown in Fig. 12, the stator 33 is provided with four re-entrant poles I4 lettered a, b, c and d. Poles 0 and b are at one side of the frame and are respectively opposed to poles c and d at the other side. A rectangular movable membr 35 is used in place of the rotor. Each pole is provided with suitable coils ll and 40. The apparatus may -be used either as a force motor or as a pick-oil.
The term force motor is used in contradistinction to a torque motor because the member 36 is constrained to move sidewise instead of rotating.
The magnetomotive force patterns for difierent coil connections are indicated by Figs. 13, 14 and 15, in which the same notation for indicating the magnetomotive forces is used as in Figs. 2, 3 and 4, but for convenience the coils are omitted. The double arrows on the member 35 indicate that the member is mounted for sidewise movement.
Fig. 13 corresponds exactly to Fig. 2 in principle,
Fig. 14 to Fig. 3, and Fig. 15 to Fig. 4. Thus for a force motor the coils are connected to give a magnetomotive force pattern which is a combination of the patterns of Figs. 13 and 14. A constant force will be exerted on the member 36 independently oi its position (so far as fringing effects are negligible) and the force is proportional to the product of the currents in the two sets of coils. For a pick-oil, the same connections are used and with a current of constant amplitude in one set of coils, the voltage induced in the other set of coils will be proportional to the sidewise displacement of the element 36 from neutral. Fig. 15 represents a stifi'ness motor, in which the force on the element It is proportional to the displacement from neutral position.
The theoretical considerations for the translational device are identical with those for the rotary device, namely, that for Figs. 13 and 14, the self-inductance of each winding is constant and the mutual inductance is proportional to displacement, and that for Fig. 15 the reluctance involves a term dependent on the square of the displacement. In actual construction and arrangement the translational form differs from the rotary form. Thus in the rotary form the rotor always presents the same aspect to diametrically opposite poles, a, c and b, (1, while in the translational form the member 15 presents the same aspect to directly opposite poles which are likewise indicated as a, c and b, d. Various simplified coil connections for the translational device may be used in exactly the same manner as for the rotary form. Moreover, instead of using coils wound on the pole-pieces, as in Fig. 18, the coils may be wound on the legs between the coils, as indicated at 42 and 44. It will be apparent to those skilled in the art that the windings may be connected to give any desired magnetomotive force pattern represented by Figs. 13 to 15.
In actual construction, to avoid the use of a mounting for sliding movement of the member 36, it is preferably mounted on an arm 46 for rotation about a remote axis 48, as shown in Fig. 17. The element 35 and pole faces are formed on arcs about the axis 48. The motion of the movable element is in effect a translation with respect to the poles.
An extremely precise servomechanism for following small angular displacements and embodying several of the variable dynamo-transformers heretofore described is shown in Fig. 18. The preferred units are a transmitting pick-off II, a following pick-off 52 and a servomotor 54. The motor 54 may be of the type shown in Fig. 8. The following pick-01f 52 and the motor 54 are mounted on the same shaft. The winding connections of the units 50 and 52 are the same as illustrated in Fig. 5. The coils i 6 of one set of the unit 50 are connected in series and in the same sense with the corresponding coils of the unit 52 whereby these coils carry the current i; supplied from any suitable reference source. The output coils l8 are connected in series opposition and to a transformer 55 forming the input of a sense detecting rectifier and amplifier It. The voltage applied to the amplifier is proportional to the "error," that is, to the difference between the angular positions of the rotors of the units II and 52. The amplifier output feeds direct current to the motor 54 for which the connections are as in Fig. 8. Thus the coils on two opposite poles carry a current i: and the coils on the other two opposite poles carry a current is. The construction of the sense detecting rectifier is well known in the art and is not described in detail here. It is sufficient to note'that with zero input to the amplifier the currents is and ii are the same, but with an input other than zero to the amplifier one of the currents increases and the other decreases. As heretofore shown the motor torque is proportional to (is-H4) (i:i4).
When the rotors of the pick-ofis III and 52 are ence. The currents i3 and it will then assume such values as to bring the motor 54 into correspondence with the pick-off 50. Thus the motor follows the motions of the transmitting pick-off 50 with high precision. It will be understood that the accuracy of the system depends upon the precision with which the induced voltages in the pick-offs 50 and 52 can be brought into balance. The transformers herein described have been found especially suitable for this type of system.
If desired the motor may be made to follow the transmitting pick-01f with a displacement ratio different from unity. This is accomplished by relatively varying the magnetomotive forces of the two windings l6. By using a turns ratio different from unity in either or both sets of coils of the units 50 and 52, the magnetomotive force ratio may be made different from unity. Thus if the winding I6 of the pick-off 52 has twice as many turns as the corresponding winding of the pick-01f 50, the output will have only one-half the angular motion of the input.
Another connection for obtaining a desired displacement ratio is shown in Fig. 19. Here the windings 16 of the pick-offs 50 and 52 are connected to the ends of a current divider, consisting of a large inductive impedance 60. One side of the source of reference voltage is connected to a line 62 joining the ends of the windings, and the other side of the source is connected to the impedance 60 through a variable tap 64. The current will divide between the two windings in a ratio dependent on the position of the tap. The ratio of rotor displacements of the two pick-offs is inversely proportional to the ratio of currents. The impedance is preferably a large inductance, in order that the currents in the two windings will remain in substantially the same phase.
Although the invention has been illustrated and described as embodied in several particular modifications it will be understood that the invention is not limited to these constructions but may be embodied in other forms.
Having thus described the invention, I claim:
1. A dynamo transformer comprising a stator having four symmetrically disposed poles, a movable element of magnetic material mounted within the stator and having a neutral position with respect to the poles, the movable element being capable of limited movement from said neutral position, two sets of stator windings, one set of windings being associated with all four poles and connected to produce a magnetomotive force pattern in which the forces are directed inwardly in two adjacent poles and outwardly in the other two poles, and the other 'set of windings being associated with all four poles and connected to produce a similar pattern but displaced from that of the first set.
2. A dynamo transformer comprising a stator having four symmetrically disposed poles, a movable element of magnetic material mounted within the stator and having a neutral position symmetrical with respect to the poles, the movable element being capable of limited movement from said neutral position, two sets of stator windings, one set of windings being associated with all four poles and connected to produce a magnetomotive force'pattern in which the forces are directed inwardly in two adjacent poles and outwardly in the other two poles, said set of windings having a substantially constant self inductance, and the other set of windings being associated with all four poles and connected to produce a similar pattern but displaced from that of the first set, said other set of windings being also of substantially constant self-inductance, the mutual inductance of the windings being substantially proportional to the displacement of the movable element from neutral position.
ROBERT K. MUELLER.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS
US652523A 1946-03-07 1946-03-07 Dynamo transformer Expired - Lifetime US2488734A (en)

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US2629859A (en) * 1948-12-18 1953-02-24 Norden Lab Corp Electrical rate generator
US2644916A (en) * 1951-02-06 1953-07-07 Gen Electric Electronic motor and commutating means therefor
US2752792A (en) * 1951-03-22 1956-07-03 Research Corp Gyroscopic apparatus
US2752793A (en) * 1951-03-22 1956-07-03 Research Corp Gyroscopic apparatus
US2752790A (en) * 1951-08-02 1956-07-03 Research Corp Gyroscopic apparatus
US2758288A (en) * 1952-01-29 1956-08-07 Servomechanisms Inc Electromechanical transducer
US2802956A (en) * 1951-04-25 1957-08-13 Research Corp Pendulum apparatus
US2825830A (en) * 1953-05-08 1958-03-04 Bosch Arma Corp Electromechanical device
US2842749A (en) * 1953-09-04 1958-07-08 Honeywell Regulator Co Dynamo electric device
US2864066A (en) * 1954-09-29 1958-12-09 Honeywell Regulator Co Transducer
US2882484A (en) * 1956-10-19 1959-04-14 American Radiator & Standard Null shifting device for variable dynamo transformers
US2894395A (en) * 1956-03-26 1959-07-14 Honeywell Regulator Co Apparatus for producing a negative elastic restraint
US2930010A (en) * 1956-09-13 1960-03-22 American Radiator & Standard Dynamo transformer
US2935875A (en) * 1954-11-15 1960-05-10 Licentia Gmbh Device for electrically tele-transmitting the measured value of pressure indicators
US2956436A (en) * 1953-05-28 1960-10-18 Jr Harry E Ellerman Rate gyroscope
US2975384A (en) * 1954-09-24 1961-03-14 Sprague Electric Co Toroidal inductor combinations
US2976734A (en) * 1957-12-18 1961-03-28 Genisco Inc Accelerometer
US2986714A (en) * 1958-10-21 1961-05-30 Clevite Corp Position measuring device
US3001127A (en) * 1961-09-19 Electromagnetic pick-off devices
US3005969A (en) * 1957-07-06 1961-10-24 Constr Meccaniche Riva S P A Position transducer adapted to transduce the displacement of a mechanical member into an alternate voltage
US3024409A (en) * 1957-02-02 1962-03-06 Ferranti Ltd Electromagnetic pick-off devices
US3027749A (en) * 1957-02-25 1962-04-03 Miniature Prec Bearings Inc Bearing torque test instrument
US3032730A (en) * 1958-08-11 1962-05-01 Northrop Corp Null shifting device for microsyn
US3040279A (en) * 1958-03-17 1962-06-19 American Radiator & Standard Sensitivity adjustment
US3112375A (en) * 1960-01-20 1963-11-26 Mechanies For Electronic Inc Loudspeaker construction
US3177385A (en) * 1963-01-10 1965-04-06 Mechanics For Electronics Electric motor for limited rotation
US3192495A (en) * 1961-11-29 1965-06-29 Gen Precision Inc Electromagnetic transducers
US3201981A (en) * 1957-02-25 1965-08-24 Miniature Prec Bearings Inc Bearing torque test instrument
US3222937A (en) * 1959-01-23 1965-12-14 Special Devices Lab Inc Gyroscope
US3375421A (en) * 1964-04-21 1968-03-26 Lear Siegler Inc Combined torquer and pickoff means
US3425283A (en) * 1965-09-09 1969-02-04 Us Time Corp The Rate gyroscope
US3568119A (en) * 1969-08-26 1971-03-02 Aeroflex Lab Inc Dynamic transformer
US3641467A (en) * 1969-05-13 1972-02-08 Allis Chalmers Mfg Co Rotary inductor
US3671904A (en) * 1971-01-22 1972-06-20 Us Navy Pick-off
US3704407A (en) * 1969-11-21 1972-11-28 Sperry Sun Well Surveying Co Gyro servo control system & structure
US4347491A (en) * 1981-02-02 1982-08-31 Pickering & Company, Inc. Rotary variable differential transformer with substantially linear output
US4347489A (en) * 1980-11-12 1982-08-31 Bambozzi B Variable three-phase inductor
US4763967A (en) * 1986-11-18 1988-08-16 General Scanning, Inc. Tunable resonant device
US4816920A (en) * 1986-11-18 1989-03-28 General Scanning, Inc. Planar surface scanning system
US4845424A (en) * 1987-11-16 1989-07-04 Gamble John G Rotary displacement motor
US4874215A (en) * 1987-04-23 1989-10-17 General Scanning, Inc. Tunable resonant mechanical system
US4959568A (en) * 1986-08-05 1990-09-25 General Scanning, Inc. Dynamically tunable resonant device with electric control
US4991301A (en) * 1987-02-27 1991-02-12 Radiodetection Limited Inductive displacement sensors
US5402096A (en) * 1992-03-27 1995-03-28 Penny & Giles Position Sensors Limited Transducers
US5424595A (en) * 1993-05-04 1995-06-13 General Electric Company Integrated magnetic bearing/switched reluctance machine
US20030057781A1 (en) * 2001-09-25 2003-03-27 Yoichi Shukuri Brushless DC motor, pump, and electronic apparatus
US9265262B1 (en) 2011-04-06 2016-02-23 John L. Albanese Hand held deer de-hide tool

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Cited By (48)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3001127A (en) * 1961-09-19 Electromagnetic pick-off devices
US2629859A (en) * 1948-12-18 1953-02-24 Norden Lab Corp Electrical rate generator
US2644916A (en) * 1951-02-06 1953-07-07 Gen Electric Electronic motor and commutating means therefor
US2752792A (en) * 1951-03-22 1956-07-03 Research Corp Gyroscopic apparatus
US2752793A (en) * 1951-03-22 1956-07-03 Research Corp Gyroscopic apparatus
US2802956A (en) * 1951-04-25 1957-08-13 Research Corp Pendulum apparatus
US2752790A (en) * 1951-08-02 1956-07-03 Research Corp Gyroscopic apparatus
US2758288A (en) * 1952-01-29 1956-08-07 Servomechanisms Inc Electromechanical transducer
US2825830A (en) * 1953-05-08 1958-03-04 Bosch Arma Corp Electromechanical device
US2956436A (en) * 1953-05-28 1960-10-18 Jr Harry E Ellerman Rate gyroscope
US2842749A (en) * 1953-09-04 1958-07-08 Honeywell Regulator Co Dynamo electric device
US2975384A (en) * 1954-09-24 1961-03-14 Sprague Electric Co Toroidal inductor combinations
US2864066A (en) * 1954-09-29 1958-12-09 Honeywell Regulator Co Transducer
US2935875A (en) * 1954-11-15 1960-05-10 Licentia Gmbh Device for electrically tele-transmitting the measured value of pressure indicators
US2894395A (en) * 1956-03-26 1959-07-14 Honeywell Regulator Co Apparatus for producing a negative elastic restraint
US2930010A (en) * 1956-09-13 1960-03-22 American Radiator & Standard Dynamo transformer
US2882484A (en) * 1956-10-19 1959-04-14 American Radiator & Standard Null shifting device for variable dynamo transformers
US3024409A (en) * 1957-02-02 1962-03-06 Ferranti Ltd Electromagnetic pick-off devices
US3027749A (en) * 1957-02-25 1962-04-03 Miniature Prec Bearings Inc Bearing torque test instrument
US3201981A (en) * 1957-02-25 1965-08-24 Miniature Prec Bearings Inc Bearing torque test instrument
US3005969A (en) * 1957-07-06 1961-10-24 Constr Meccaniche Riva S P A Position transducer adapted to transduce the displacement of a mechanical member into an alternate voltage
US2976734A (en) * 1957-12-18 1961-03-28 Genisco Inc Accelerometer
US3040279A (en) * 1958-03-17 1962-06-19 American Radiator & Standard Sensitivity adjustment
US3032730A (en) * 1958-08-11 1962-05-01 Northrop Corp Null shifting device for microsyn
US2986714A (en) * 1958-10-21 1961-05-30 Clevite Corp Position measuring device
US3222937A (en) * 1959-01-23 1965-12-14 Special Devices Lab Inc Gyroscope
US3112375A (en) * 1960-01-20 1963-11-26 Mechanies For Electronic Inc Loudspeaker construction
US3192495A (en) * 1961-11-29 1965-06-29 Gen Precision Inc Electromagnetic transducers
US3177385A (en) * 1963-01-10 1965-04-06 Mechanics For Electronics Electric motor for limited rotation
US3375421A (en) * 1964-04-21 1968-03-26 Lear Siegler Inc Combined torquer and pickoff means
US3425283A (en) * 1965-09-09 1969-02-04 Us Time Corp The Rate gyroscope
US3641467A (en) * 1969-05-13 1972-02-08 Allis Chalmers Mfg Co Rotary inductor
US3568119A (en) * 1969-08-26 1971-03-02 Aeroflex Lab Inc Dynamic transformer
US3704407A (en) * 1969-11-21 1972-11-28 Sperry Sun Well Surveying Co Gyro servo control system & structure
US3671904A (en) * 1971-01-22 1972-06-20 Us Navy Pick-off
US4347489A (en) * 1980-11-12 1982-08-31 Bambozzi B Variable three-phase inductor
US4347491A (en) * 1981-02-02 1982-08-31 Pickering & Company, Inc. Rotary variable differential transformer with substantially linear output
US4959568A (en) * 1986-08-05 1990-09-25 General Scanning, Inc. Dynamically tunable resonant device with electric control
US4763967A (en) * 1986-11-18 1988-08-16 General Scanning, Inc. Tunable resonant device
US4816920A (en) * 1986-11-18 1989-03-28 General Scanning, Inc. Planar surface scanning system
US4991301A (en) * 1987-02-27 1991-02-12 Radiodetection Limited Inductive displacement sensors
US4874215A (en) * 1987-04-23 1989-10-17 General Scanning, Inc. Tunable resonant mechanical system
US4845424A (en) * 1987-11-16 1989-07-04 Gamble John G Rotary displacement motor
US5402096A (en) * 1992-03-27 1995-03-28 Penny & Giles Position Sensors Limited Transducers
US5424595A (en) * 1993-05-04 1995-06-13 General Electric Company Integrated magnetic bearing/switched reluctance machine
US20030057781A1 (en) * 2001-09-25 2003-03-27 Yoichi Shukuri Brushless DC motor, pump, and electronic apparatus
US6856054B2 (en) * 2001-09-25 2005-02-15 Matsushita Electric Industrial Co., Ltd Brushless DC motor, pump, and electronic apparatus
US9265262B1 (en) 2011-04-06 2016-02-23 John L. Albanese Hand held deer de-hide tool

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