US2444813A - Servo control system - Google Patents

Servo control system Download PDF

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US2444813A
US2444813A US626406A US62640645A US2444813A US 2444813 A US2444813 A US 2444813A US 626406 A US626406 A US 626406A US 62640645 A US62640645 A US 62640645A US 2444813 A US2444813 A US 2444813A
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motor
servo
fuse
rotor
driven member
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US626406A
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Frederick W Cunningham
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ARMA CORP
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ARMA 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
    • G05D3/14Control of position or direction using feedback using an analogue comparing device
    • G05D3/1436Control of position or direction using feedback using an analogue comparing device with fine or coarse devices

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  • This invention relates to servo control systems, and has particular reference to an accurate servo mechanism for precisely reproducing a series of intermittent and irregular adjustments at a remote point.
  • servo mechanisms of various forms have increased materially and much improvement has been directed particularly toward making them more accurate by minimizing overrunning, hunting, and the like.
  • Most servo systems are used for transmitting continuous movements or movements of substantial duration, so that the 'overrunning and hunting problems are not as serious as in the cases where the transmitted movements are short and rapid, for in that event a hunting oscillation may be a large percentage of the transmitted movement, whereby a substantial error is introduced.
  • An example of a requirement for precise remote adjustments without transmission error is the fuse adjustments on a continuous series of gun shells in ordnance and the like.
  • each shell of a series is placed in a not which has a pair of concentric pawls rotatable about the center line of the shell for finding and attaching themselves to corresponding slots in the nose of the shell.
  • the pawls are adapted to make, firstly, a rapid motion past each other seeking the slots in the shell and, secondly, when they have found the slots, a further motion to precisely set or determine the fuse-setting and keep it current, that is, in strict synchronism with the continuously changing fuse-setting order until the instant of removal of the shell from the pot for firing.
  • Such a fuse-setting mechanism has only one mechanical input which is required not only to find and engage the fuse but to also set it.
  • the present invention may be readily adapted for the precise setting of fuses equipped with fuse-setting lugs instead of fuse-setting slots, and the term slots as used herein is intended to apply equally well to an equivalent detent for engagement by the setting means.
  • an accurate servo control system in which the order of transmitted movements is reproduced at low speed, whereby the synchronism is retained under all conditions and actual transmission is effected at high speed so that the transmitted movements are precisely reproduced without transmission lag, thus enabling the system to be employed with safety and confidence for the setting of fuses on a continuous series of gun shells, and for other uses requiring reliability and precision.
  • the invention utilizes self-synchronou electrical transmission in which the usual pair of synchronous units is doubled and are of the so-called control transformer type comprising a distributed three-phase stator winding operating with a shuttle type armature having a single coil thereon like a self-synchronous receiver in construction.
  • the action is of the null type, a servomotor being provided to bring the rotor to its null or zero voltage position in respect to the stator field and to continuously keep it there, the servo-motor being operated by the amplified error voltages from the rotor coil.
  • This servo-motor in response to the control transformer error voltages is transmitted to' the fusesetter input through a mechanical differential, in order that a second motor may cooperate with it, the purpose of this second motor being to initially find and engage the setting slots of the shell to be set while the servo-motor creates and keeps a mechanical fuse-setting value at all times in synchronism with the electrical fuse-setting order received by the self-synchronous system.
  • Both motors operate while engagement of the fuse is being effected, but during fuse-setting the servomotor alone is operating. Control of the interaction of the two motors is accomplished by an electro-mechanlcal arrangement of relays and cam-switches as will be hereinafter described.
  • the placing of a shell in the fuse pot of the fusesetter trips a trigger which initiates a cycle of operations comprising (1) engaging the fuse, (2) rough-setting the fuse, and finally, (3) justifying the fuse-setting and resetting the apparatus for a repetition of the cycle.
  • Means are also provided to smooth the action of the apparatus and to prevent incorrect synchronizing under any operating conditions.
  • Figure 1 is a schematic view of the servo control system of this invention
  • Fig. 2 is a schematic electrical diagram of the synchronizin means included in the invention.
  • Fig. 3 is a graph of the electrical action of the same.
  • numeral l0 designates the fuse-setter operated by the mechanism of the present invention, and including the housing ll having the shell-receiving pot [2 into which the nose of the shell I3 is adapted to be inserted for setting the fuse thereof.
  • the fuse-setting pawls l4 and It are spring-pressed against the smooth curve of the shell nose as indicated, and are vertically aligned with the fuse-setting slots l3 and II, respectively.
  • the pawls i4 and I5 about the axes of the shell will cause them to engage the corresponding shell slots I8 and I1.
  • these pawls l4 and ii are inter-connected by gearing, including a mechanical differential gear [3, in such a way that the pawls travel oppositely to each other upon rotation of the single input shaft l9.
  • gearing including a mechanical differential gear [3, in such a way that the pawls travel oppositely to each other upon rotation of the single input shaft l9.
  • the pawls i4 and iii are free to rotate in the same direction, while the input shaft i9 remains at rest.
  • the angle of separation between the two pawls i4 and 15 represents fusesetting angle when the device is synchronized in accordance with the invention and the orientation of the pawls as a pair has no significance, being made necessary by reason of the random orientation of the fuse slots "5 and ii on the shell l3 when inserted in the fuse-setter I0.
  • the shell I3 when the shell I3 is inserted in the pot i2, its nose engages and depresses rod 45 which closes switch 46 to set into rotation the pawls l4 and IS in a manner to be described.
  • the pawls l4 and l5 When the shell I3 isso inserted in pot l2, with random orientation of the slots l6 and II, the pawls l4 and l5 will be given relative rotation of at least two turns and will thus locate and engage their respective shell slots l6 and i1.
  • slots l6 and l! have been found, their included angle may then be adthrough a relative angle of at least two turns plus one additional turn to take care of any rapid change of fuse-setting which may occur during the enga ing period.
  • Exactly three turns of the fuse-setter pawls i4 and i5 is desired to avoid a loss of precise synchronism when engagement is complete, as well as to assure engagement of the fuse slots I3 and t1, the clutch-brake-motor combination 25-32 being adapted to give precisely three turns of the fuse-setter pawls l4 and IS with a very small margin of error.
  • fusesetting angle change is also being applied to the end gear34 of the differential 24 by the fusesetting follow-up motor 35 and the control transformers 36 and 31 fed by the high-speed and low speed synchronized supply lines 39 and 38, re-
  • the mechanism for operating the fuse-setting instrument In includes the assembly of mechanism shown in Fig. 1, and comprises a fuse-slot engagement drive 1mit designated 2i, a rough fuse-setting unit designated 22, and an arcuate fuse-setting or justifying unit designated 23. These three units are connected mechanically through the-diiferential 24 and by the various electrical connections shown.
  • the fuse-slot engagement unit 2i is driven by the continuously running electric motor 25 supplied from the service wires 26 and having a clutch-brake combination which operates when electrically energized to release the output disc 2'") from the fixed braking surface 28 carried on the frame 23 of the unit. Simultaneously clutch disc 210 is pressed against the rapidly rotating clutch surface of the motor flywheel 30.
  • the fuse-setting angle change value so applied to differential gear 34 passes through differential 24 and merges with the slot-engaging motion from end gear 33' to appear on spider shaft 40 and gear 4
  • the fuse-setting value is kept up to date for the fuse although temporarily set aside by the fuse-engaging motion from motor 25.
  • the pawls l4 and I5 have completed the relative three turns required, they have engaged and set the fuse slots i8 and I! to approximate fuse value.
  • Switch t8 then appropriates control from relay 41 by by-passing contacts 53 and and, by breaking the coil circuit, also allows relay contact 5
  • the cam 49 will transfer control from control transformers 36, 31 back to control transformers t3 and M by action of shift relay 56 by breaking of contact 5
  • follow-up motor 35 is continuously following fuse-setting order as electrically demanded by the control transformers, transformers t3 and 44 operating when setting the fuse and the transformers 36 and 31 operating when the fuse-engaging operation is occurring.
  • the high speed control transformer 36 or 44 of one pair or the other are in control for the major part of the operation, the low speed transformers 31 or 43 being in control only when synchronism is lost, as for instance, when the ma chine is starting into operation.
  • the relay 51 shown in detail in Fig. 2, is provided to swing control from low speed to high speed and back as often as necessary, being operated by the error voltage output of the low speed control transformers themselves. For instance, when a low speed control transformer 31 or 43 is controlling the motor 35 and it is following closely, the relay 51, responsive to the low error voltage from the same, quickly switches control to the corresponding high speed unit for greater accuracy of following.
  • the relay 51 shifts control of motor 35 back to the corresponding one speed control transformer, which cannot lose synchronism at any time. From the relay 51 the error voltages are fed, as shown, to the amplifier 58 the power output of which feeds the motor 35 as previously explained.
  • the circuit also includes damping and compensating generators indicated at 59, 60 and BI for smooth action, as will be described.
  • the relay 51 which operates as described to maintain synchronism under all conditions, includes the low speed or rough control transformer 31, whose stator is supplied by lead Wires 69 from low speed selfsynchronous bus wires 38, whereby the signal actuated rotating field of transformer 31 is established Similarly, high speed or fine control transformer 36 is supplied by the stator lead wires 10 from high-speed self-synchronous bus wires 39.
  • bus wires 38 carry the low-speed or rough following self-synchronous transmission of the signal or order to be reproduced mechanically by motor 35
  • numeral 39 designates the self-synchronous buswires for the high-speed or accurate transmission which appropriates control when the low-speed system has achieved rough synchronism.
  • the low speed system is only in control when the mechanical parts slip out of synchronism with the signal order, for instance while the instrument is ole-energized.
  • the followup motor will be under control of the high-speed control transformer 36 because the relay 51 is de-energized and the relay spring is holding its relay contacts 12 and 13 closed.
  • the switching mechanism includes vacuum tube 16 biased negatively by the well-known means of connecting its cathode 11 to groimd by means of a resistance 18 in the plate circuit, so that any voltage to operate relay ill applied to grid ll, must be positive and of greater voltage than the biasing voltage.
  • the voltage from control transformer 31 is, of course, a single phase alternating voltage but the positive peaks of the waves will all'ect amplification if they lie above the critical or predetermined voltage value, the pulsations being smoothed out sufiiciently by the condenser Ill.
  • This arrangement provides an accurate and reliable shifting device from control transformer 36 to control transformer 31 whenever loss of synchronism exceeds a predetermined value, indicating angular deviation between the nal on busses 38 and 39 and the mechanical output from motor 35.
  • horizontal line 82 represents zero voltage output from rotor coils 311' and 361' of resnective control transformers 31 and 36 and the point of the center marked 0 the condition of synchronism which is the condition when the field of the rotor coil 381' is being maintained at right angles to the resultant field 0f the threephase type stator winding 36s carrying the rotating signal and there is no voltage induced in the rotor coil 38r.
  • This coil 361' is driven through gearing 92 by the servo-motor 35 at a rate eight times as fast as the signal itself varies, and its voltage wave is therefore labeled 8 speed" in Hg. 3.
  • the voltage value induced in it for each degree of lag may be plotted as the dotted line curve ll.
  • the opposite sign voltages may be plotted as the dotted line curve 8
  • the voltages which would be generated in the rotor coil 311- of low speed control transformer 31 when it is losing synchronism may be plotted as the dash line curve 85, 8B.
  • the points l1 and II on the curve portions ll and 83, respectively, indicate the permissible error voltages beyond which the relay 51 operates, to switch control from high to low speed control as described. The voltage in control, beyond these points would normally be found on the curve 85, It
  • this curve l5, I6 is not employed because at 180 out of synchronism, as at point 89, there is a second accidental synchronizing point.
  • a voltage error curve 80, BI is therefore substituted, which does not align at 180 with the extended high speed curve 84 and therefore the second synchronizin point is eliminated.
  • may be shown to be the curve 85, 86
  • comprises a lever fixed on the shaft of rotor 31r and shiftable relatively to the gearing 92 to throw the rotor coil 111' of the control transformer 31 out of angular alignment with the rotor coil 36r of control transformer 38, thus shifting curve 85, 86 bodily to the left and the constant root-meansquare voltage from transformer 68 realigns curve 85, 86 at zero with the high speed curve 83, 84.
  • the actual operating error voltage-output curve of a pair of transformers 38, I1 is that shown by the full line, composed of that part of the high speed curve 83, 84 across zero between 81 and 88, and the balance of the amended low-speed curve 9
  • the synchronous bus wires 38 and 39 transmit to the control transformers 31 and 36 a set of three spacephased alternating currents, the root-meansquare values of which are peculiar to the angle value of the signal required to be reproduced, as is well understood in self-synchronous transmission.
  • These currents flowing in stator winding 31s produce a directional field in which the rotor coil 311' has some orientation. If the synchronism is accurate within the limit predetermined by the biasing voltage on the resistor 18, as previously explained, no effect will be caused by induction on the coil 311- because its output circuit is interrupted at the points 14 and 15 of relay 51.
  • the high speed synchronous bus wires 39 are feeding space-phased currents to stator coils 36s of control transformer 36, designating an angle eight times as great as the angle produced in control transformer 31, so that induction from stator coil 36s produces voltage in rotor coil 361' eight times as great as the voltage produced in rotor coil 311'.
  • This voltage passes through contacts 12 and 13 to the power anplifier 58, thus causing servo-motor 35 to run in the right direction to adjust the rotor coil 36r through gearing 92 precisely into non-inductive or null position in the field produced by stator winding 36s, thereby reducing the voltage on coil 3Br to zero.
  • the output shaft l9 may have been turned manually to about 160 out of alignment with the signal, or temporary failure in the amplifier 58 may have caused misalignment of the motor 35, so that the action occurs on the extended portion of the curve 84 which is embraced between the points 83 and 84.
  • the control transformer 36 is therefore in control but, due to the fact that voltages in this area are opposite to those in the area between points 81 and 88 on the curve, the motor 35 is driven away from synchronism at this point towards the correct point of alignment at under control of transformer 35 until its rotor coil voltage becomes greater than that indicated at points 93 and at when the motion towards synchronizing is continued under control of transformer 31.
  • point 81 is reached. control will be again given to transformer 36 and the action will be normal and accurate.
  • a second like generator 60 is also driven by the servo-motor 35 but through a flexible drive 95 by shaft 91 and gearing 98, 99.
  • the speed of the servo-motor 35 is uniform, the voltages from the two generators 59 and 60 exactly nullify each other, but when there is acceleration, the output of the flexibly driven generator 69 falls out of phase with the rigidly driven generator 59 and a voltage opposed to the driving voltage results which damps the oscillation.
  • the flexibility of the flexible drive 96 is such that any acceleration belonging to the signal to be reproduced is unable to flex it to any appreciable extent, then any extensive flexing will be due to acceleration of the servo-motor 35 when it is attempting to achieve synchronism and it is under such conditions that the damping voltage takes effect.
  • Any tendency of the flexible drive 96 itself to oscillate is controlled by use of a viscous damping device 6
  • an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a driven member, means for driving said driven member, a transformer having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servomotor electrically connected to said rotor winding for energization in accordance with the voltage induced therein, operative connections between said servo-motor and said rotor winding for drivingthe same to non-inductive relation with said stator winding, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
  • servo-motor electrically connected to said rotor winding for energization in accordance with the voltage induced therein, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the angle of drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
  • an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary driven member, means for driving said driven signals transmember, a normally disengaged electromagnetic clutch means interposed between said driving means and said driven member, a switch controlling said clutch, timing mechanism actuating said clutch switch to effect a predetermined ansic of rotation of said driven member, a transformer having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servo-motor electrically connected to said rotor winding for energization in accordance with the voltage induced therein, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the angle of drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
  • a rotary driven member having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servo-motor electrically connected to said rotor winding for energization in accordance with the voltage induced therein.
  • a transformer having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servo-motor electrically connected to said rotor winding for energization in accordance with the voltage induced therein. perative connections between said servo-motor and said rotor winding for driving the same to non-inductive relation with said stator winding, a. differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the angle of drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
  • an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary driven member, means for driving said driven member, a high-speed transformer and a low-speed transformer each having a stator winding energized by said transmitting means and a rotor winding inductivel coupled to each stator winding, a servo-motor alternatively electrically connected to said rotor winding of one of said transformers for energization in accordance with the voltage induced therein, a relay interposed between said servo-motor and the rotor windings of said transformers, means responsive to asynchronism between said servo-motor and said transmitting means for energizing said relay to selectively connect the corresponding rotor winding to said servo-motor, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the drive of said driven member by
  • an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary driven member, means for driving said driven member, a high-speed transformer and a lowspeed transformer each having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said'stator winding, a servo-motor alternatively electrically connected to said rotor winding of one of said transformers for energization in accordance with the voltage induced therein, a relay interposed between said servo-motor and the rotor windings of said transformers, means responsive to asynchronism between said servo-motor and said transmitting means for energizing said relay to selectively energize said transformers, gearing between the rotor windings of said transformers, means for varying the angular relationship between the rotor winding of one of said transformers and the other rotor, winding and said gearing
  • an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary member, means for driving said driven member, a high-speed and a low-speed transformer each having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servo-motor alternatively electrically connected to said rotor winding of one of said transformers for energization in accordance with the voltage induced therein, a relay for selectively connecting one of said rotor windings to said servo-motor, gearing between the rotor windings of said transformers, means for varying the angular relationship between the one rotor winding and the other and said gearing for preventing pseudo-synchronism between said servo-motor and said transmitting means, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for
  • a rotary member means for driving said driven member, a high-speed transformer and a low-speed transformer each having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servomotor alternatively electrically connected to said rotor winding of one of said transformers for energization in accordance with the voltage induced therein, a relay interposed between said servo-motor and the rotor windings of said transformers, means responsive to asynchronism between said servo-motor and said transmitting means for energizing said relay to selectively energize said transformers, operative connections between said servo-motor and said rotor winding for driving the same to non-inductive relation with said stator winding, a differential interposed between said driven member and the means for driving the same, and operative
  • a servo-motor alternatively electrically connected to said rotor winding for energization in accordance with the voltage induced therein, a relay interposed between said servo-motor and the rotor windings of said transformers, means responsive to asynchronism between said servomotor and said transmitting means for energizing said relay to selectively energize said transformers, gearing between the rotor windings of said transformers, means for varying the angular relationships between the rotor winding of one of said transformers and the other rotor winding and said gearing to prevent pseudo synchronism between said servo-motor and said transmitting means, operative connections between said servo-motor and said rotor winding for driving the same to non-inductive relation with said stator winding, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the drive of said driven member by said driving means in accordance with signals transmitted by said transmitting
  • a rotary driven member having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servo-motor electrically connected to said rotor winding for energization in accordance with the voltage induced therein, a differential interposed between said driven member and the means for driving the same, operative connections between said servo-motor and said difierential for modifying the angle of drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means, a second transformer having a stator winding energized by said transmitting means and a rotor having a winding inductively coupled to said stator winding for rotation in response to the field of said stator winding, and operative connections between said second rotor and said driven member
  • an electro-mechanical servo-control system for setting fuses on shells equipped with fuse slots or their equivalent in accordance with the movement of a remote self-synchronous fuseangle transmitting means, the combination of a shell nose receiving pot, relatively rotary pawls thereonfor engaging the shell fuse slots, a motor for driving said fuse pawls around the nose of the shell for engagement with the corresponding fuse slots thereon, a switch in the circuit of the motor for energizing the same, means responsive to the insertion of a shell nose in said pot for actuating said switch, timing means driven by said motor for controlling the angle of rotation of said pawls, a high-speed transformer and a low-speed transformer each having a stator winding energized by said fuse angle'transmitting means and a rotor winding inductively coupled to the corresponding stator winding, 9.
  • servo-motor alternatively energized by the voltage induced in one of said stator windings, gearing connecting the rotor windings of said transformers, a two-way switch interposed between the rotor winding and said servo-motor, a relay responsive to asynchronism between one of said transformers and said transmitting means for actuating said switch to shift the connection of said servo-motor from one to the other rotor windings, operative connections between said servo-motor and said gearing for driving the active rotor winding to a non-inductive relation with its corresponding stator winding, a differential interposed between said motor and servomotor and having an output, operative connections between said differential output and said fuse'pawls for setting the fuse slots on said shell in accordance with transmitted fuse angle after said pawls are engaged by said motor with said fuse slots, a third transformer having a stator winding energized by said fuse angle transmitting means and a, rotor having a winding, and operative connections

Description

F. w. cuwwmgm SERVO CONTROL SYS'IW Filed Nov. 2, 1945 2 Sheets-Sheet J.
INVE N TOR Frederick W. Cunningham.
M A H 6 m N N U c w E SERVO CONTROL SYSTEM 2 Sheets-Sheet 2 Filed Nov. 2, 1945 INVENTOR Frederick M Cunnhgham snnvo CONTROL SYSTEM Frederick W. Cunningham, Stamford, CODIL, as-
signor to Arma Corporation, Brooklyn, N. 1., a corporation of New York 17 Claims.
This invention relates to servo control systems, and has particular reference to an accurate servo mechanism for precisely reproducing a series of intermittent and irregular adjustments at a remote point.
The uses of servo mechanisms of various forms have increased materially and much improvement has been directed particularly toward making them more accurate by minimizing overrunning, hunting, and the like. Most servo systems are used for transmitting continuous movements or movements of substantial duration, so that the 'overrunning and hunting problems are not as serious as in the cases where the transmitted movements are short and rapid, for in that event a hunting oscillation may be a large percentage of the transmitted movement, whereby a substantial error is introduced. An example of a requirement for precise remote adjustments without transmission error is the fuse adjustments on a continuous series of gun shells in ordnance and the like.
In modern fuse-setting practice the nose of each shell of a series is placed in a not which has a pair of concentric pawls rotatable about the center line of the shell for finding and attaching themselves to corresponding slots in the nose of the shell. The pawls are adapted to make, firstly, a rapid motion past each other seeking the slots in the shell and, secondly, when they have found the slots, a further motion to precisely set or determine the fuse-setting and keep it current, that is, in strict synchronism with the continuously changing fuse-setting order until the instant of removal of the shell from the pot for firing. Such a fuse-setting mechanism has only one mechanical input which is required not only to find and engage the fuse but to also set it. with the aid of the present invention." The present invention may be readily adapted for the precise setting of fuses equipped with fuse-setting lugs instead of fuse-setting slots, and the term slots as used herein is intended to apply equally well to an equivalent detent for engagement by the setting means.
In accordance with the present invention, an accurate servo control system is provided in which the order of transmitted movements is reproduced at low speed, whereby the synchronism is retained under all conditions and actual transmission is effected at high speed so that the transmitted movements are precisely reproduced without transmission lag, thus enabling the system to be employed with safety and confidence for the setting of fuses on a continuous series of gun shells, and for other uses requiring reliability and precision.
The invention utilizes self-synchronou electrical transmission in which the usual pair of synchronous units is doubled and are of the so-called control transformer type comprising a distributed three-phase stator winding operating with a shuttle type armature having a single coil thereon like a self-synchronous receiver in construction. The action, however, is of the null type, a servomotor being provided to bring the rotor to its null or zero voltage position in respect to the stator field and to continuously keep it there, the servo-motor being operated by the amplified error voltages from the rotor coil. The motion of this servo-motor in response to the control transformer error voltages is transmitted to' the fusesetter input through a mechanical differential, in order that a second motor may cooperate with it, the purpose of this second motor being to initially find and engage the setting slots of the shell to be set while the servo-motor creates and keeps a mechanical fuse-setting value at all times in synchronism with the electrical fuse-setting order received by the self-synchronous system. Both motors operate while engagement of the fuse is being effected, but during fuse-setting the servomotor alone is operating. Control of the interaction of the two motors is accomplished by an electro-mechanlcal arrangement of relays and cam-switches as will be hereinafter described. The placing of a shell in the fuse pot of the fusesetter trips a trigger which initiates a cycle of operations comprising (1) engaging the fuse, (2) rough-setting the fuse, and finally, (3) justifying the fuse-setting and resetting the apparatus for a repetition of the cycle. Means are also provided to smooth the action of the apparatus and to prevent incorrect synchronizing under any operating conditions.
For a more complete understanding of the invention, reference may be had to the accompanying drawings, in which:
Figure 1 is a schematic view of the servo control system of this invention;
Fig. 2 is a schematic electrical diagram of the synchronizin means included in the invention; and
Fig. 3 is a graph of the electrical action of the same.
Referring to Fig. 1 of the drawings, numeral l0 designates the fuse-setter operated by the mechanism of the present invention, and including the housing ll having the shell-receiving pot [2 into which the nose of the shell I3 is adapted to be inserted for setting the fuse thereof. With the shell l3 in that position the fuse-setting pawls l4 and It are spring-pressed against the smooth curve of the shell nose as indicated, and are vertically aligned with the fuse-setting slots l3 and II, respectively. Positioned in the shell nose, as shown. With this arrangement, rotation of the pawls i4 and I5 about the axes of the shell will cause them to engage the corresponding shell slots I8 and I1.
As shown in Fig. 1, these pawls l4 and ii are inter-connected by gearing, including a mechanical differential gear [3, in such a way that the pawls travel oppositely to each other upon rotation of the single input shaft l9. For one di-,
rection of rotation of input shaft IS the pawls l4 and I5 separate. and for the opposite direction of input rotation they approach each other. Be-
a cause of the differential gearing l3, the pawls i4 and iii are free to rotate in the same direction, while the input shaft i9 remains at rest. By this arrangement the angle of separation between the two pawls i4 and 15 represents fusesetting angle when the device is synchronized in accordance with the invention and the orientation of the pawls as a pair has no significance, being made necessary by reason of the random orientation of the fuse slots "5 and ii on the shell l3 when inserted in the fuse-setter I0.
According to the present invention, when the shell I3 is inserted in the pot i2, its nose engages and depresses rod 45 which closes switch 46 to set into rotation the pawls l4 and IS in a manner to be described. When the shell I3 isso inserted in pot l2, with random orientation of the slots l6 and II, the pawls l4 and l5 will be given relative rotation of at least two turns and will thus locate and engage their respective shell slots l6 and i1. When slots l6 and l! have been found, their included angle may then be adthrough a relative angle of at least two turns plus one additional turn to take care of any rapid change of fuse-setting which may occur during the enga ing period. Exactly three turns of the fuse-setter pawls i4 and i5 is desired to avoid a loss of precise synchronism when engagement is complete, as well as to assure engagement of the fuse slots I3 and t1, the clutch-brake-motor combination 25-32 being adapted to give precisely three turns of the fuse-setter pawls l4 and IS with a very small margin of error.
While this engagement of the fuse slots i8 and H by pawls i4 and I5 is taking place, fusesetting angle change is also being applied to the end gear34 of the differential 24 by the fusesetting follow-up motor 35 and the control transformers 36 and 31 fed by the high-speed and low speed synchronized supply lines 39 and 38, re-
' spectively. Follow-up motor 35 is energized by justed to correspond to fuse-setting order, both I these actions being effected precisely, in a very short time, as will be described.
The mechanism for operating the fuse-setting instrument In includes the assembly of mechanism shown in Fig. 1, and comprises a fuse-slot engagement drive 1mit designated 2i, a rough fuse-setting unit designated 22, and an arcuate fuse-setting or justifying unit designated 23. These three units are connected mechanically through the-diiferential 24 and by the various electrical connections shown.
The fuse-slot engagement unit 2i is driven by the continuously running electric motor 25 supplied from the service wires 26 and having a clutch-brake combination which operates when electrically energized to release the output disc 2'") from the fixed braking surface 28 carried on the frame 23 of the unit. Simultaneously clutch disc 210 is pressed against the rapidly rotating clutch surface of the motor flywheel 30. The
' transfer is made magnetically by the double coil solenoid 21, the coil 3| being the brake coil, and the coil 32 being the clutch coil, of the energizing solenoid. By this arrangement, when the engagement gearing 33 is not operating, it is held very rigidly by the brake 28 and, when the gearing is required to run, the clutch operates very quickly, since the plate 210 drops directly against the rapidly running motor flywheel 30.
By this drive from motor 25, clutch 21c, 30, gearing 33, shaft 40 connected to the spider of differential 24, gearing ll, 42, and shaft I 9, the fuse-setter pawls i4 and I5 are suddenly accelerated into rapid rotation past each other conventional electronic amplifier 58 connected to power line 25 and amplifying the modulated inputs from 36, 31, 43 and 44, as will be described.
The fuse-setting angle change value so applied to differential gear 34 passes through differential 24 and merges with the slot-engaging motion from end gear 33' to appear on spider shaft 40 and gear 4|, and fuse-setter mechanism I ll through gearing 42 and shaft l3, so that the motion appears as a change in angular spacing of pawls I4 and I5. Thus, the fuse-setting value is kept up to date for the fuse although temporarily set aside by the fuse-engaging motion from motor 25. However, before the pawls l4 and I5 have completed the relative three turns required, they have engaged and set the fuse slots i8 and I! to approximate fuse value.
This fuse value is not quite accurate because of the difflculty of getting exactly three turns at the fuse from motor 25 without a dead stop of such rapidly moving parts as to give prohibitive stresses in the mechanism. For this reason, a slight re-synchronizing operation is necessary to compensate for the inaccuracy in the pawlengaging rotation, whenever the engaging operation has occurred, for it is obvious that if exactly three turns of the pawls could be given by the motor 25, synchronism would remain undisturbed and would be the case if the number of turns is any integer. However, since it is impractical to obtain exact integral turns from motor 25, it fol-' ond direct mechanical control for the fuse-setter shaft i9 is provided and includes a second pair of control transformers 43 and 44 supplied electrically by the same fuse-setting order from synchronous supply busses 38 and 33. This mechanical connection comprises an extension 40' of the differential spider shaft 40 to the rotor of control transformer 43, so that the same angle value applied as input to shaft I9 is likewise applied to that transformer rotor. Accordingly. when the aforementioned slot-engagement movement of pawls i4 and I5 is completed, and a slight misalignment of shaft l3 results. the rotor of angle accurately thereafter until the shell I3 is removed and another one inserted at l2 for setting in the same way.
The energization of clutch coil 32 to effect the pawl-engaging operation of fuse-setter I is initiated by the aforementioned activation by the nose of the shell l3 of the rod 45 to close the switch t6, which applies current from source 26 to the delayed response type relay 41. Both the relay t1 and switch 46 are in series with a multiple switch 68 operated by a cam 49 and follower 50. Before a shell is inserted in the unit it the contact arm 5| of the relay i1 is held up against the contact 52 by spring 53. Hence the brake coll 3| is energized and the disc 21b is held immovably against the stationary brake disc 23, the differential gear 23 consequently acting as a simple straight gearing. Also, at this time the cam 39 is at rest, but the angle between the pawls M and i5 is changing according to fusesetting order on the bus wires 38 and 39.
Energization of relay 41 as the result of insertion of shell i3 in pot I2, causes its armature to. break contact between the elements 5| and 52, thus releasing brake 21b--28 and to make contact between element 5| and the two lower contacts 5t and 55. The closure of contact 55 causes energization of clutch coil 32 to move clutch-plate No immediately into driving contact with spining motor flywheel 30, so that motor 25 can make a quick swing of pawls M and I5 to engage them in slots l6 and ill on shell l3. This motion also turns cam M, which throws lever to operate switch 38. Switch t8 then appropriates control from relay 41 by by-passing contacts 53 and and, by breaking the coil circuit, also allows relay contact 5| to go slowly back against stop contact 52, This action resets the brake 2821b immediately upon one turn of cam 49, which is equivalent to the three turns of pawls If and I5.
At this time also, the cam 49 will transfer control from control transformers 36, 31 back to control transformers t3 and M by action of shift relay 56 by breaking of contact 5|, 54 at relay ill. In other words, introduction of a shell |3 at If initiates a three-turn cycle of the pawls M, |5 under control of a different pair of control transformers in order that synchronism may be retained for a quick application of fuse-setting to the fuse when the engaging cycle is completed and control restored to the regular control transformers t3 and M which have the advantage of direct connection to the load. By this means of engaging the fuse slots I6 and I1, synchronism is retained at all times by the other set of control transformers 36, 31 within a small margin of error so that the required final justification of the fuse-setting value is not great enough to consume any appreciable time.
As stated, follow-up motor 35 is continuously following fuse-setting order as electrically demanded by the control transformers, transformers t3 and 44 operating when setting the fuse and the transformers 36 and 31 operating when the fuse-engaging operation is occurring. In either case, the high speed control transformer 36 or 44 of one pair or the other are in control for the major part of the operation, the low speed transformers 31 or 43 being in control only when synchronism is lost, as for instance, when the ma chine is starting into operation.
The relay 51, shown in detail in Fig. 2, is provided to swing control from low speed to high speed and back as often as necessary, being operated by the error voltage output of the low speed control transformers themselves. For instance, when a low speed control transformer 31 or 43 is controlling the motor 35 and it is following closely, the relay 51, responsive to the low error voltage from the same, quickly switches control to the corresponding high speed unit for greater accuracy of following.
Conversely, should the error voltage from the low speed unit rise, thus indicating loss of synchronism, then before the misalignment can become serious, the relay 51 shifts control of motor 35 back to the corresponding one speed control transformer, which cannot lose synchronism at any time. From the relay 51 the error voltages are fed, as shown, to the amplifier 58 the power output of which feeds the motor 35 as previously explained. The circuit also includes damping and compensating generators indicated at 59, 60 and BI for smooth action, as will be described.
Referring particularly to Fig. 2, the relay 51 which operates as described to maintain synchronism under all conditions, includes the low speed or rough control transformer 31, whose stator is supplied by lead Wires 69 from low speed selfsynchronous bus wires 38, whereby the signal actuated rotating field of transformer 31 is established Similarly, high speed or fine control transformer 36 is supplied by the stator lead wires 10 from high-speed self-synchronous bus wires 39. It will be understood that bus wires 38 carry the low-speed or rough following self-synchronous transmission of the signal or order to be reproduced mechanically by motor 35, and that numeral 39 designates the self-synchronous buswires for the high-speed or accurate transmission which appropriates control when the low-speed system has achieved rough synchronism. At 61 is shown the usual alternating current bus wires for supplying power to any other self-synchronous units, not shown, on the lines 38 and 39, here also supplying a transformer 68 for a purpose to be described.
As is usual in self-synchronous servo-systems, the low speed system is only in control when the mechanical parts slip out of synchronism with the signal order, for instance while the instrument is ole-energized. In such a case, as soon as the apparatus is again energized the followup motor will be under control of the high-speed control transformer 36 because the relay 51 is de-energized and the relay spring is holding its relay contacts 12 and 13 closed. But if synchronization has been lost while the apparatus was de-energized, the error voltage from the displaced rotor of low-speed control transformer 31 will be greater than the predetermined permissible value, the vacuum tube amplifier 1| will be triggered, the relay 51 will open the contacts 12 and 13 and close the contacts 14 and 15 and the low-speed control transformer 31 will assume control. This control transformer will seek rough alignment and, when it has found it, the error voltage from its rotor will drop and the relay 51 will switch back to the high speed or precision control by transformer 36 for normal following of the signal.
The switching mechanism includes vacuum tube 16 biased negatively by the well-known means of connecting its cathode 11 to groimd by means of a resistance 18 in the plate circuit, so that any voltage to operate relay ill applied to grid ll, must be positive and of greater voltage than the biasing voltage. The voltage from control transformer 31 is, of course, a single phase alternating voltage but the positive peaks of the waves will all'ect amplification if they lie above the critical or predetermined voltage value, the pulsations being smoothed out sufiiciently by the condenser Ill. This arrangement provides an accurate and reliable shifting device from control transformer 36 to control transformer 31 whenever loss of synchronism exceeds a predetermined value, indicating angular deviation between the nal on busses 38 and 39 and the mechanical output from motor 35.
Such a system is practical and reliable except under the remote circumstance that synchronization should fall 180' out of step. Thus, if the normal synchronizing point is 0, there is another possible synchronizing point at 180, and should the instrument be de-energlzed and during deenergization the mechanical output is turned so that the rotor of the slow speed control transformer 31 is rotated nearly 180 from its correct synchronizing position, the device will synchronize at this point rather than find its way back to true synchronism at 0, which impairs the effectiveness of the instrument as a servo-systern. This condition of control transformer 31 is illustrated in Fig. 3, which also illustrates the electrical action of both transformers 35 and 31.
In. Fig. 3 horizontal line 82 represents zero voltage output from rotor coils 311' and 361' of resnective control transformers 31 and 36 and the point of the center marked 0 the condition of synchronism which is the condition when the field of the rotor coil 381' is being maintained at right angles to the resultant field 0f the threephase type stator winding 36s carrying the rotating signal and there is no voltage induced in the rotor coil 38r. This coil 361' is driven through gearing 92 by the servo-motor 35 at a rate eight times as fast as the signal itself varies, and its voltage wave is therefore labeled 8 speed" in Hg. 3. When the rotor 36r of the control transformer l6 lags behind its rotating signal field, the voltage value induced in it for each degree of lag may be plotted as the dotted line curve ll. Similarly, for each degree that the rotor 361- leads the signal field, the opposite sign voltages may be plotted as the dotted line curve 8|. Likewise the voltages which would be generated in the rotor coil 311- of low speed control transformer 31 when it is losing synchronism may be plotted as the dash line curve 85, 8B. The points l1 and II on the curve portions ll and 83, respectively, indicate the permissible error voltages beyond which the relay 51 operates, to switch control from high to low speed control as described. The voltage in control, beyond these points would normally be found on the curve 85, It
In the system of the present invention, however, this curve l5, I6 is not employed because at 180 out of synchronism, as at point 89, there is a second accidental synchronizing point. A voltage error curve 80, BI is therefore substituted, which does not align at 180 with the extended high speed curve 84 and therefore the second synchronizin point is eliminated. This curve ll, 8| may be shown to be the curve 85, 86
8 with its zero point shifted to the left and downwards along itself by means of the mechanical offset device at 8| and the action of the transformer 68. The offset device 8| comprises a lever fixed on the shaft of rotor 31r and shiftable relatively to the gearing 92 to throw the rotor coil 111' of the control transformer 31 out of angular alignment with the rotor coil 36r of control transformer 38, thus shifting curve 85, 86 bodily to the left and the constant root-meansquare voltage from transformer 68 realigns curve 85, 86 at zero with the high speed curve 83, 84. In the diagram of Fig. 3 and considering the action of the relay 51, the actual operating error voltage-output curve of a pair of transformers 38, I1 is that shown by the full line, composed of that part of the high speed curve 83, 84 across zero between 81 and 88, and the balance of the amended low-speed curve 9|], 9|.
The operation of the mechanism just described and illustrated in Fig. 2, for preventin asynchronism or pseudo synchronism, the synchronous bus wires 38 and 39 transmit to the control transformers 31 and 36 a set of three spacephased alternating currents, the root-meansquare values of which are peculiar to the angle value of the signal required to be reproduced, as is well understood in self-synchronous transmission. These currents flowing in stator winding 31s produce a directional field in which the rotor coil 311' has some orientation. If the synchronism is accurate within the limit predetermined by the biasing voltage on the resistor 18, as previously explained, no effect will be caused by induction on the coil 311- because its output circuit is interrupted at the points 14 and 15 of relay 51.
At the same time, the high speed synchronous bus wires 39 are feeding space-phased currents to stator coils 36s of control transformer 36, designating an angle eight times as great as the angle produced in control transformer 31, so that induction from stator coil 36s produces voltage in rotor coil 361' eight times as great as the voltage produced in rotor coil 311'. This voltage passes through contacts 12 and 13 to the power anplifier 58, thus causing servo-motor 35 to run in the right direction to adjust the rotor coil 36r through gearing 92 precisely into non-inductive or null position in the field produced by stator winding 36s, thereby reducing the voltage on coil 3Br to zero.
Thereafter, if the field of stator coil 35s rotates, it will be understood that the rotor coil 361' will be compelled by motor 35 to follow that field, thus keeping its output shaft accurately aligned with the signal through the action of control transformer 18 only. Under these ideal conditions, synchronism is maintained and the operation occurs along that portion of curve 90, 9| of Fig. 3 embraced between the two shift points 81 and 88.
However, should there be a large initial misalignment between the motor 35 and the signal,
- so as to induce in rotor coil 31:- a voltage greater than that indicated by points 81 and B8 on Fig. 3, then the period of accurate following described above is preceded by a period when control transformer I1 governs the motor 35, because such excess voltage will have dominated the blocking bias on tube 16, causing relay 51 to switch rotor coil Sir out of control and rotor coil 311 into control of amplifier 58 and the servo-motor 35. In this case, before the relay 51 operates, the action will occur at some point on the curve between the points 81 and I8 and will then shift to curve Ill or It, as described above.
Finally, in an extreme case, the output shaft l9 may have been turned manually to about 160 out of alignment with the signal, or temporary failure in the amplifier 58 may have caused misalignment of the motor 35, so that the action occurs on the extended portion of the curve 84 which is embraced between the points 83 and 84. The control transformer 36 is therefore in control but, due to the fact that voltages in this area are opposite to those in the area between points 81 and 88 on the curve, the motor 35 is driven away from synchronism at this point towards the correct point of alignment at under control of transformer 35 until its rotor coil voltage becomes greater than that indicated at points 93 and at when the motion towards synchronizing is continued under control of transformer 31. Eventually, however, when point 81 is reached. control will be again given to transformer 36 and the action will be normal and accurate.
In the servo control system described, in which the error between the demand quantity and the response actuates the servo-motor 35, regeneration in the circuit causes oscillation in the response, as is well understood. In order to make such a system dead-beat, the mechanism shown in Fig. 1 is used, including a generator 59 which may be driven by the servo-motor 35 through gearing 95 and the resulting speed-proportional voltage output of generator 59 fed in to the amplifler 58 of the servo-motor circuit to oppose the driving current. This method destroys the phase relations on which the undesired oscillation is based, but introduces a dynamic error in the servo control system since it follows a value which lags the order signal value to be reproduced. In order to prevent such lag, a second like generator 60 is also driven by the servo-motor 35 but through a flexible drive 95 by shaft 91 and gearing 98, 99. When the speed of the servo-motor 35 is uniform, the voltages from the two generators 59 and 60 exactly nullify each other, but when there is acceleration, the output of the flexibly driven generator 69 falls out of phase with the rigidly driven generator 59 and a voltage opposed to the driving voltage results which damps the oscillation.
1f the flexibility of the flexible drive 96 is such that any acceleration belonging to the signal to be reproduced is unable to flex it to any appreciable extent, then any extensive flexing will be due to acceleration of the servo-motor 35 when it is attempting to achieve synchronism and it is under such conditions that the damping voltage takes effect. Any tendency of the flexible drive 96 itself to oscillate is controlled by use of a viscous damping device 6|, preferably of the eddy-current type flxed on the flexibly driven generator shaft.
The detailed operation of the servo control system of this invention has been described as the description of its construction progressed. The system accordingly accurately transmits small and rapid angular adjustments without hunting or other unintended oscillations to remote points in series to enable fuse-setting of a series of projectiles and the like. Although the invention has been illustrated and described in connection with fuse-setting operations, the invention is not limited thereby but is adaptable to other uses without material change and to variations in construction within the scope of the appended claims.
' I claim:
1. In an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a driven memher, means for driving said driven member, a transformer having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a. servomotor electrically connected to said rotorwinding for energization in accordance with the voltage induced therein, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
2. In an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a driven member, means for driving said driven member, a transformer having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servomotor electrically connected to said rotor winding for energization in accordance with the voltage induced therein, operative connections between said servo-motor and said rotor winding for drivingthe same to non-inductive relation with said stator winding, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
3. In an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary driven member, means for driving said driven member. timing mechanism adjusted in accordance with the movements of said driven member for regulating the angle of rotation thereof by said driving means, a transformer having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, 9. servo-motor electrically connected to said rotor winding for energization in accordance with the voltage induced therein, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the angle of drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
4. In an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary driven member, means for driving said driven member, a normally disengaged clutch means interposed between said driving means and said driven member, timing mechanism actuating said clutch to effect a predetermined angle of rotation of said driven member, a transformer having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servo-motor electrically connected to said rotor winding for energization in accordance with the voltage induced therein, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the angle of drive of said driven member by said driving means in accordance with mitted by said transmitting means.
5. In an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary driven member, means for driving said driven signals transmember, a normally disengaged electromagnetic clutch means interposed between said driving means and said driven member, a switch controlling said clutch, timing mechanism actuating said clutch switch to effect a predetermined ansic of rotation of said driven member, a transformer having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servo-motor electrically connected to said rotor winding for energization in accordance with the voltage induced therein, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the angle of drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
6. In an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary driven member, means for driving said driven member, timing mechanism actuated in accordance with the movements of said driven member for regulating the angle of rotation thereof by said driving means. a transformer having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servo-motor electrically connected to said rotor winding for energization in accordance with the voltage induced therein. perative connections between said servo-motor and said rotor winding for driving the same to non-inductive relation with said stator winding, a. differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the angle of drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
'7. In an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary driven member, means for driving said driven member. a normally disengaged clutch means interposed between said driving means and said driven member, timing mechanism actuating said clutch to effect a predetermined angle of rotation of said driven member, a transformer having a stator winding energized b said transmitting means and a rotor windin inductively coupled to said stator winding, a servo-motor electrically connected to said rotor winding for energization in accordance with the voltage induced therein, operative connections between said servo-motor and said rotor winding for driving the'same to non-inductive relation with said stator winding, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said difierential for modifying the angle of drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
8. In an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary driven member, means for driving saiddriven member, a normally disengaged electromagnetic clutch means interposed between said driving means and said driven member, a switch controlling said clutch, timing mechanism actuating said clutch switch to effect a predetermined angle of rotation of said driven member, a transformer having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servo-motor electrically connected to said rotor winding for energization in accordance with the voltage induced therein, operative connections between said servo-motor and said rotor winding for driving the same to non-inductive relation with said stator winding, a differential interposed between said driven member and the means for driving the same. and operative connections between said servo-motor and said differential for modifying the angle of drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
9. In an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary driven member, means for driving said driven member, a high-speed transformer and a low-speed transformer each having a stator winding energized by said transmitting means and a rotor winding inductivel coupled to each stator winding, a servo-motor alternatively electrically connected to said rotor winding of one of said transformers for energization in accordance with the voltage induced therein, a relay interposed between said servo-motor and the rotor windings of said transformers, means responsive to asynchronism between said servo-motor and said transmitting means for energizing said relay to selectively connect the corresponding rotor winding to said servo-motor, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
10. In an electro-mechanical servo-control system, adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary driven member, means for driving said driven member, a high-speed transformer and a lowspeed transformer each having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said'stator winding, a servo-motor alternatively electrically connected to said rotor winding of one of said transformers for energization in accordance with the voltage induced therein, a relay interposed between said servo-motor and the rotor windings of said transformers, means responsive to asynchronism between said servo-motor and said transmitting means for energizing said relay to selectively energize said transformers, gearing between the rotor windings of said transformers, means for varying the angular relationship between the rotor winding of one of said transformers and the other rotor, winding and said gearing to prevent pseudo asynchronism between said servo-motor and said transmitting means, a diflerential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
11. In an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary member, means for driving said driven member, a high-speed and a low-speed transformer each having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servo-motor alternatively electrically connected to said rotor winding of one of said transformers for energization in accordance with the voltage induced therein, a relay for selectively connecting one of said rotor windings to said servo-motor, gearing between the rotor windings of said transformers, means for varying the angular relationship between the one rotor winding and the other and said gearing for preventing pseudo-synchronism between said servo-motor and said transmitting means, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
12. In an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary member. means for driving said driven member, a high-speed transformer and a low-speed transformer each having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servomotor alternatively electrically connected to said rotor winding of one of said transformers for energization in accordance with the voltage induced therein, a relay interposed between said servo-motor and the rotor windings of said transformers, means responsive to asynchronism between said servo-motor and said transmitting means for energizing said relay to selectively energize said transformers, operative connections between said servo-motor and said rotor winding for driving the same to non-inductive relation with said stator winding, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said difl'erential for modifying the drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
13. In an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary driven member, means for driving said driven member, a high-speed transformer and a lowspeed transformer each having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding. a servo-motor alternatively electrically connected to said rotor winding for energization in accordance with the voltage induced therein, a relay interposed between said servo-motor and the rotor windings of said transformers, means responsive to asynchronism between said servomotor and said transmitting means for energizing said relay to selectively energize said transformers, gearing between the rotor windings of said transformers, means for varying the angular relationships between the rotor winding of one of said transformers and the other rotor winding and said gearing to prevent pseudo synchronism between said servo-motor and said transmitting means, operative connections between said servo-motor and said rotor winding for driving the same to non-inductive relation with said stator winding, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
14. In an electro-mechanical servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rota y driven member, means for driving said driven member, a high-speed transformer and a lowspeed transformer each having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servo-motor alternately electrically connected to said rotor winding of one of said transformers for energization in accordance with the voltage induced therein, a relay for selectively connecting one of said rotor windings to said servo-motor, gearing between the rotor windings of said transformers, means for varying the angular relationship between one rotor winding and the other and said gearing for preventing pseudosynchronism between said servo-motor and said transmitting means, operative connections between said servo-motor and said rotor winding for driving the same to non-inductive relation with said stator winding, a differential interposed between said driven member and the means for driving the same, and operative connections between said servo-motor and said differential for modifying the drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means.
15. In an electro-mechanic-al servo-control system adapted to be actuated in accordance with the movements of remote self-synchronous transmitting means, the combination of a rotary driven member, means for driving said driven member, a, transformer having a stator winding energized by said transmitting means and a rotor winding inductively coupled to said stator winding, a servo-motor electrically connected to said rotor winding for energization in accordance with the voltage induced therein, a differential interposed between said driven member and the means for driving the same, operative connections between said servo-motor and said difierential for modifying the angle of drive of said driven member by said driving means in accordance with signals transmitted by said transmitting means, a second transformer having a stator winding energized by said transmitting means and a rotor having a winding inductively coupled to said stator winding for rotation in response to the field of said stator winding, and operative connections between said second rotor and said driven member for further modifying the angle thereof.
16. In an electro-mechanical servo-control system for setting fuses on shells equipped with fuse slots or their equivalent in accordance with the movement of a remote self-synchronous fuse- 15 angle transmitting means, the combination of a shell nose receiving pot, relatively rotary pawls thereon for engaging the shell fuse slots, a motor for driving said fuse pawls around the nose of the shell for eng ement with the corresponding fuse slots thereon, a switch in'the circuit of the motor for energizing the same, means responsive to the insertion of a shell nose in said pot for actuating said switch, timing means driven by said motor for controlling the angle of rotation of said pawls, a high-speed transformer and a low-speed transformer each having a stator winding energized by said fuse angle transmitting means and a rotor winding inductively coupled to the corresponding stator winding, a servo-motor alternatively energized by the voltage induced in one of said stator windings, gearing connecting the rotor windings of said transformers, a two-way switch interposed between the rotor winding and said servo-motor, a relay responsive to asynchronism between one of said transformers and said transmitting means for actuating said switch to shift the connection of said servo-motor from one to the other rotor windings, operative connections between said serve-motor and said gearing for driving the active rotor winding to noninductive relation with its corresponding stator winding, a differential interposed between said motor and servo-motor and having an output, and operative connections between said differential output and said fuse pawls for setting the fuse slots on said shell in accordance with transmitted fuse angle after said pawls are engaged by said motor with said fuse slots.
17. In an electro-mechanical servo-control system for setting fuses on shells equipped with fuse slots or their equivalent in accordance with the movement of a remote self-synchronous fuseangle transmitting means, the combination of a shell nose receiving pot, relatively rotary pawls thereonfor engaging the shell fuse slots, a motor for driving said fuse pawls around the nose of the shell for engagement with the corresponding fuse slots thereon, a switch in the circuit of the motor for energizing the same, means responsive to the insertion of a shell nose in said pot for actuating said switch, timing means driven by said motor for controlling the angle of rotation of said pawls, a high-speed transformer and a low-speed transformer each having a stator winding energized by said fuse angle'transmitting means and a rotor winding inductively coupled to the corresponding stator winding, 9.
servo-motor alternatively energized by the voltage induced in one of said stator windings, gearing connecting the rotor windings of said transformers, a two-way switch interposed between the rotor winding and said servo-motor, a relay responsive to asynchronism between one of said transformers and said transmitting means for actuating said switch to shift the connection of said servo-motor from one to the other rotor windings, operative connections between said servo-motor and said gearing for driving the active rotor winding to a non-inductive relation with its corresponding stator winding, a differential interposed between said motor and servomotor and having an output, operative connections between said differential output and said fuse'pawls for setting the fuse slots on said shell in accordance with transmitted fuse angle after said pawls are engaged by said motor with said fuse slots, a third transformer having a stator winding energized by said fuse angle transmitting means and a, rotor having a winding, and operative connections between said third transformer rotor and said differential output for justifying the fuse-setting of said fuse slots.
FREDERICK W. CUNNINGHAM.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,299,509 Rey Apr. 8, 1919 1,500,860 Yo July 8, 1924 1,985,982 Edwards Jan. 1, 1935? 2,115,086 Riggs Apr. 26, 1938 2,351,743 Chappell et a1. June 6, 1944
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2582222A (en) * 1945-06-07 1952-01-15 Gen Electric Control system of the correspondence kind for movable members
US2792759A (en) * 1951-12-13 1957-05-21 Ernest F Campbell Projectile fuze setting apparatus
US2864043A (en) * 1955-11-10 1958-12-09 Hershey John Houck Motor control for a radar ranging unit
US3052162A (en) * 1960-08-26 1962-09-04 Rovin Herman Timer device
US3494251A (en) * 1968-10-22 1970-02-10 Us Navy Fuze setter apparatus

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1299509A (en) * 1914-11-30 1919-04-08 Jean Alexandre Rey Mechanism for controlling movement
US1500860A (en) * 1922-05-17 1924-07-08 Gen Electric Electric control system
US1985982A (en) * 1934-03-21 1935-01-01 Gen Electric Control system
US2115086A (en) * 1933-09-23 1938-04-26 Sperry Gyroscope Co Inc Nonhunting or dead beat remote control
US2351743A (en) * 1943-05-05 1944-06-20 Bendix Aviat Corp Automatic fuse setting apparatus

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1299509A (en) * 1914-11-30 1919-04-08 Jean Alexandre Rey Mechanism for controlling movement
US1500860A (en) * 1922-05-17 1924-07-08 Gen Electric Electric control system
US2115086A (en) * 1933-09-23 1938-04-26 Sperry Gyroscope Co Inc Nonhunting or dead beat remote control
US1985982A (en) * 1934-03-21 1935-01-01 Gen Electric Control system
US2351743A (en) * 1943-05-05 1944-06-20 Bendix Aviat Corp Automatic fuse setting apparatus

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2582222A (en) * 1945-06-07 1952-01-15 Gen Electric Control system of the correspondence kind for movable members
US2792759A (en) * 1951-12-13 1957-05-21 Ernest F Campbell Projectile fuze setting apparatus
US2864043A (en) * 1955-11-10 1958-12-09 Hershey John Houck Motor control for a radar ranging unit
US3052162A (en) * 1960-08-26 1962-09-04 Rovin Herman Timer device
US3494251A (en) * 1968-10-22 1970-02-10 Us Navy Fuze setter apparatus

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