US3273041A - Circuit with controlled rectifiers and improved ignition thereof - Google Patents

Circuit with controlled rectifiers and improved ignition thereof Download PDF

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US3273041A
US3273041A US243457A US24345762A US3273041A US 3273041 A US3273041 A US 3273041A US 243457 A US243457 A US 243457A US 24345762 A US24345762 A US 24345762A US 3273041 A US3273041 A US 3273041A
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ignition
voltage
conductor
circuit
controlled
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Strohmeier Walter
Quiros Julio Gonzales Berna De
Ullmann Werner
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Agie Charmilles SA
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Agie Charmilles SA
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    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M7/00—Conversion of AC power input into DC power output; Conversion of DC power input into AC power output
    • H02M7/02—Conversion of AC power input into DC power output without possibility of reversal
    • H02M7/04—Conversion of AC power input into DC power output without possibility of reversal by static converters
    • H02M7/12—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode
    • H02M7/145—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a thyratron or thyristor type requiring extinguishing means
    • H02M7/155—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a thyratron or thyristor type requiring extinguishing means using semiconductor devices only
    • H02M7/1555—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a thyratron or thyristor type requiring extinguishing means using semiconductor devices only with control circuit
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23H—WORKING OF METAL BY THE ACTION OF A HIGH CONCENTRATION OF ELECTRIC CURRENT ON A WORKPIECE USING AN ELECTRODE WHICH TAKES THE PLACE OF A TOOL; SUCH WORKING COMBINED WITH OTHER FORMS OF WORKING OF METAL
    • B23H1/00—Electrical discharge machining, i.e. removing metal with a series of rapidly recurring electrical discharges between an electrode and a workpiece in the presence of a fluid dielectric
    • B23H1/02—Electric circuits specially adapted therefor, e.g. power supply, control, preventing short circuits or other abnormal discharges
    • B23H1/022—Electric circuits specially adapted therefor, e.g. power supply, control, preventing short circuits or other abnormal discharges for shaping the discharge pulse train
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02H—EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS
    • H02H7/00—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions
    • H02H7/10—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for converters; for rectifiers
    • H02H7/12—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for converters; for rectifiers for static converters or rectifiers
    • H02H7/1216—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for converters; for rectifiers for static converters or rectifiers for AC-AC converters
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M1/00—Details of apparatus for conversion
    • H02M1/08—Circuits specially adapted for the generation of control voltages for semiconductor devices incorporated in static converters
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M1/00—Details of apparatus for conversion
    • H02M1/08—Circuits specially adapted for the generation of control voltages for semiconductor devices incorporated in static converters
    • H02M1/081—Circuits specially adapted for the generation of control voltages for semiconductor devices incorporated in static converters wherein the phase of the control voltage is adjustable with reference to the AC source
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M5/00—Conversion of AC power input into AC power output, e.g. for change of voltage, for change of frequency, for change of number of phases
    • H02M5/40—Conversion of AC power input into AC power output, e.g. for change of voltage, for change of frequency, for change of number of phases with intermediate conversion into DC
    • H02M5/42—Conversion of AC power input into AC power output, e.g. for change of voltage, for change of frequency, for change of number of phases with intermediate conversion into DC by static converters
    • H02M5/44—Conversion of AC power input into AC power output, e.g. for change of voltage, for change of frequency, for change of number of phases with intermediate conversion into DC by static converters using discharge tubes or semiconductor devices to convert the intermediate DC into AC
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M5/00—Conversion of AC power input into AC power output, e.g. for change of voltage, for change of frequency, for change of number of phases
    • H02M5/40—Conversion of AC power input into AC power output, e.g. for change of voltage, for change of frequency, for change of number of phases with intermediate conversion into DC
    • H02M5/42—Conversion of AC power input into AC power output, e.g. for change of voltage, for change of frequency, for change of number of phases with intermediate conversion into DC by static converters
    • H02M5/44—Conversion of AC power input into AC power output, e.g. for change of voltage, for change of frequency, for change of number of phases with intermediate conversion into DC by static converters using discharge tubes or semiconductor devices to convert the intermediate DC into AC
    • H02M5/443—Conversion of AC power input into AC power output, e.g. for change of voltage, for change of frequency, for change of number of phases with intermediate conversion into DC by static converters using discharge tubes or semiconductor devices to convert the intermediate DC into AC using devices of a thyratron or thyristor type requiring extinguishing means
    • H02M5/45—Conversion of AC power input into AC power output, e.g. for change of voltage, for change of frequency, for change of number of phases with intermediate conversion into DC by static converters using discharge tubes or semiconductor devices to convert the intermediate DC into AC using devices of a thyratron or thyristor type requiring extinguishing means using semiconductor devices only
    • H02M5/4505—Conversion of AC power input into AC power output, e.g. for change of voltage, for change of frequency, for change of number of phases with intermediate conversion into DC by static converters using discharge tubes or semiconductor devices to convert the intermediate DC into AC using devices of a thyratron or thyristor type requiring extinguishing means using semiconductor devices only having a rectifier with controlled elements
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M7/00—Conversion of AC power input into DC power output; Conversion of DC power input into AC power output
    • H02M7/02—Conversion of AC power input into DC power output without possibility of reversal
    • H02M7/04—Conversion of AC power input into DC power output without possibility of reversal by static converters
    • H02M7/12—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode
    • H02M7/145—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a thyratron or thyristor type requiring extinguishing means
    • H02M7/155—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a thyratron or thyristor type requiring extinguishing means using semiconductor devices only
    • H02M7/162—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a thyratron or thyristor type requiring extinguishing means using semiconductor devices only in a bridge configuration
    • H02M7/1623—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a thyratron or thyristor type requiring extinguishing means using semiconductor devices only in a bridge configuration with control circuit
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M7/00—Conversion of AC power input into DC power output; Conversion of DC power input into AC power output
    • H02M7/42—Conversion of DC power input into AC power output without possibility of reversal
    • H02M7/44—Conversion of DC power input into AC power output without possibility of reversal by static converters
    • H02M7/48—Conversion of DC power input into AC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode
    • H02M7/505—Conversion of DC power input into AC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a thyratron or thyristor type requiring extinguishing means
    • H02M7/515—Conversion of DC power input into AC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a thyratron or thyristor type requiring extinguishing means using semiconductor devices only
    • H02M7/525—Conversion of DC power input into AC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a thyratron or thyristor type requiring extinguishing means using semiconductor devices only with automatic control of output waveform or frequency

Definitions

  • the present invention relates to an electric circuit of the type provided with controlled semi-conductor rectifiers.
  • Rectifiers of this type exhibit a pnpn semi-conductor barrier layer. In the first instance, they block the current in an alternating-current circuit in their backward and in their forward direction. However, they may be influenced in such a manner by application of a control or ignition voltage to their control electrode that they conduct current inthe forward or passing direction. If the rectifiers have once been ignited or brought into their conductive state by a momentary or short-time application of a control voltage, they remain conductive even after removal of the igni-tion voltage, until the main current in the forward direction is once temporarily interrupted. The rectifiers thereby possess a thyratron characteristic, that is to say, the characteristic of gas-filled discharge tubes.
  • Controlled rectifiers of this type find application in a large number of electric circuits, for example with power or full-wave rectifiers, frequency Itransformers or converters, electro-erosion tool machines particularly for spark erosion processes and electrolytic grinding processes and the like.
  • the output voltage should be available immediately after placing the unit in operation. If now, for example, the signal for rendering operative the rectifier appears in the middle of a half-wave and the rectifier each time can only be ignited by an impulse which appears at the beginning of each half-wave of the alternating-current to be rectified, then the output voltage can only first appear at the beginning of the subsequent or following half-wave.
  • the electric circuits of the aforementioned type are associated with other disadvantages. Since the ignition voltage after triggering or switching-in of the electric circuit must immediately be available, and the control impulse occasioning the ignition and lasting for a half-wave must practically be capable at any period of time during such half-wave to deliver the load necessary for igniting a controlled rectifier, the ignition circuit must be capable of carrying out a comparatively large amount 3,273,041 Patented Sept. 13, 1966 ICC of work so that ignition can also be guaranteed with security in an unfavorable situation. An ignition circuit which can fulfill these requirements is comparatively complicated and, moreover, requires a large input load.
  • a further important object of the present invention is to provide an improved electric circuit of the aforementioned type with ignition circuits which are simple in their construction and only have to deliver a relatively small load.
  • the electric circuit according to the present invention is characterized by the fact that the ignition circuits for igniting the controlled rectifiers deliver ignition impulses at least during the provided or prescribed ignition period.
  • the present invention is based upon the recognition that, also with the ignition circuits which deliver an ignition impulse lasting for -a half-wave, a short period of time always transpires until the associated controlled rectifier begins to conduct current in the anode-cathode gap.
  • a series of impulses for igniting the controlled rectifiers can, for example, withdraw the necessary current from a capacitor connected in parallel to the direct-current voltage source, whereby the capacitor can again charge between impulses.
  • the igni-tion impulse thereby primarily takes-up or draws only the load corresponding to the effective current of an individual impulse.
  • the pulse repetition rate or pulse recurrence frequency of the individual impulses can thereby be so selected that such a large number of individual impulses appear during a halfwave ofthe alternating-current voltage of the main circuit that, the resultant time loss due to the spacing in time between two successive impulses, in the majority of cases, corresponds to the arc-through time of the controlled rectifiers.
  • the electric circuit of the present invention is practically adapted for use with all possibilities of application of controlled semi-conductor rectiers.
  • the inventive frequency transformer can also be employed as generator for inductive heating, for generation of ultrasonics, for illuminating purposes, for welding techniques, and for command installations for power supply networks.
  • the elec-tric circuit of the invention has been disclosed hereinafter, however only by way of example, in conjunction with the illustrated frequency transformer, whereby this frequency transformer contains controlled rectifiers in the power section as well as also in the output stage, which in accordance with the teachings of the present invention can be brought into their conducting condition.
  • FIGURE 1 is a block diagram of a frequency transformer or converter
  • FIGURE 2 diagrammatically illustrates the series of ignition impulses necessary for igniting the controlled rectifiers taken with respect to the supplied control voltage
  • FIGURE 3 is a circuit diagram illustrating details of the frequency transformer or converter shown in FIG- URE 1.
  • the frequency transformer or converter illustrated in the block diagram of FIGURE l it will be seen that the input load or energy is applied through a transformer via its primary winding 11.
  • the primary winding can for example be directly connected to a power supply of 220 vol-ts and operating at a frequency of 50 c.p.s.
  • the transformer 10 is provided with three secondary windings 12, '13 and 14.
  • the secondary winding 12 is connected to a full-wave rectifier provided for the power rectification stage A which rectifies the supplied or input alternating-current voltage.
  • the power rectification stage A contains four dry-disk rectifiers or metallic rectifiers 35, 36, 37, 38 (FIG. 3) arranged in a full-wave bridge rectification circuit.
  • Two of these rectifiers 37, 38 are constructed as controlled semi-conductor rectifiers.
  • the direct-current voltage appearing at the conductors 15 and 16 reaches the power output stage B where the direct-current voltage is transformed into an alternating-current voltage of predetermined frequency.
  • the alternating-current voltage then appears at the output terminals 17.
  • the secondary winding 13 of the transformer 10 feeds an ignition circuit C.
  • the ignition circuit C first rectifies the input alternating-current voltage and produces a series of irnpulses for igniting the two controlled rectifiers 37, 38 of the power rectification stage A.
  • the ignition circuit C supplies a continuous series of impulses via -the conductors 19 and 20.
  • the conductor 19 is electrically coupled with the ignition electrodes of the two rectifiers 37, 38 through the agency of resistors 21 and 22.
  • the desired frequency of the -ou-tput voltage appearing at the terminals 17 is determined by a controlling or control alternating-current voltage lsupplied through the terminals 23 of an input transformer 24.
  • This transformer 24 possesses two secondary windings 26 and 27, wherein the secondary winding 26 is operatively connected to the ignition circuit C.
  • the ignition circuit C is therewith so constructednthat, it only then supplies output impulses via the conductors 19 and 20 when an input signal appears a-t the transformer terminals 23. If a signal fails to appear at the terminals 23 and, thus also not at the secondary winding 26, then the ignition circuit C does not deliver any impulses, so that there also does not appear a direct-current voltage at the conductors 15 and 16. A consequence thereof is that also practically no power is removed at the power supply network to which the primary winding 11 of the transformer 10 is connected when the control alternating-current voltage fails to appear at the terminals 23 of the input transformer 24.
  • the secondary winding 27 of the input transformer 24 is operatively connected to an .ignition circuit D which provides the ignition impulses for the two controlled rectifiers 50, 51 of the power output stage B.
  • the ignition impulses for one of Ithe two controlled rectifiers of the power output stage B, such as rectifier 50 appear across ⁇ the connecting terminals 29 and 30, whereas the ignition impulses for the second controlled rectifier 51 appear across the conductors 29 and 31.
  • the frequency transformer or converter of FIGURE 1 additionally contains a safety or security circuit E.
  • This safety circuit E is, on the one hand, electrically coupled with both of the direct-current carrying conductors 15 and 16 at the input side of the power output stage B and, on the other hand, is connected lwith the output terminals 17 at lthe output side thereof.
  • the safety -circuit E for'rns a logical element or circuit which always cuts-off or prevents the genera-tion of ignition impulses in the ignition circuit C for a predetermined time when a voltage appears at the conductors 15, 16, whereas when no voltage appears at the output terminals 17.
  • the logical element permits generation of ignition impulses when a voltage appears at the output terminals 17, as well as then when no voltage appears at the conductors 15, 16 as well as none at the output termin-als 17.
  • the safety circuit E lthere is thus caused to be ensured that the different controlled rectifiers cannot become damaged, for example, by a short circuit appearing at the output terminals 17
  • a controlling or control alternating-current voltage of arbitrary frequency within a large range there is first of all brought about a rectification in the power rectification stage A, and further there is produced an alternating-current voltage possessing the supplied frequency at terminals 23, which then appears at the output terminals 17.
  • FIGURE 2a there is depicted the controlling or control alternating-current voltage as a function of time which is applied to the terminals 23 of the input transformer 24.
  • the voltage supplied at terminals 23 reaches the ignition circuit C there is released an oscillation so that a regular, that is to say, uninterrupted or continuous series of impulses appear at the conductors 19 and 20, as such is approximately illustrated in FIGURE 2b.
  • the pulse repetition rate or pulse recurrence frequency is itself given through the oscillating system and is .largely uncritical.
  • the series of impulses illustrated in FIGURE 2b now reach the two controlled rectifiers 37, 38 of the power rectification stage A via the resistors 21 and 22, whereby it is insignificant that these ignition impulses are maintained during both half-waves, and indeed for the reason that, the ignition impulses cannot then influence the controlled rectifiers when the polarity of thre voltage applied to the main line path corresponds to the high resistance or blocking direction of the rectifiers.
  • FIG. 1 In the ignition circuit D two series of impulses are generated, whereby the first series of impulses as shown in FIGURE 2c, appear only for example during the positive half-wave of the controlling or control alternating-current voltage (FIGURE 2a.), and the second series of impulses illustrated in FIGURE 2d appear -only during the negative half-wave of the controlling or control alternating-current voltage (FIGURE 2a).
  • the voltage of FIG- URE 2c appears for example between the conductors 29 and 30, and the control alternating-current voltage of FIGURE 2d between the conductors 29 and 31.
  • the pulse repetition rate of the series of impulses of FIG- URES 2c and 2d is again independent of the frequency of the control voltage, but must however lie above such.
  • this pulse repetition rate or pulse recurrence frequency is adjustable, as will be explained hereinafter.
  • FIGURE 3 illustrates a circuit diagram of the frequency transformer or converter.
  • the conductors which transmit the power have generally been shown in thickened black lines.
  • the power output stage B with the ignition circuit D is depicted as parallel inverter. However, it is equally possible to use a series inverter. This provides the same results.
  • the illustrated frequency transformer or converter is so constructed that it can be connected to a commercial power supply of, for example, v220 volts and operating at a frequency of 50 c.p.s.
  • a .transformer 10 which, in addition to the primary winding 11, is provided with three secondary windings 12, 13 and 14.
  • the secondary winding 12 is operatively connected to the power rectification stage A comprising the semi-conductor rectifier elements 35, 36, 37 and 38 arranged in a full-wave bridge rectification circuit.
  • the rectifier elements 35 and 36 can be standard barrier layer rectifiers, whereas as previously mentioned the rectifier elements 37 and 38 are controlled rectifier elements with pnpn-senii-conductor barrier layers.
  • the two controlled rectifiers 37 and 38 which are electrically coupled to the conductor 16, which can be viewed as the positive pole or terminal of the direct-current voltage source, are ignited by the ignition circuit C by means of the aforementioned series of impulses, in such a manner that the full-wave bridge rectification circuit A operates as a normal bridge circuit. If the ignition impulses from the control ignition circuit C do not appear, then a direct-current voltage can no longer be produced, so that the power network connected to the primary -winding 11 is no longer loaded by the frequency transformer. Both of the non-controlled rectifier elements 35 and 36 are connected to the conductor which represents the negative pole or terminal of the direct-current outlet side of the rectification stage A.
  • the conductors 15 and 16 conduct the direct-current voltage produced in the power rectification stage A to the power output stage B, in the latter of which this direct-current voltage is transformed into an alternating-current voltage of predetermined frequency.
  • the power output stage B operating as a direct-current to alternating-current inverter contains an output transformer 42 provided with a primary winding 43 and a secondary or output winding 44.
  • the primary winding 43 possesses a center-tap 45 which divides the primary winding 43 into the winding sections or portions 43a and 4311.
  • the illustrated conductor 16 for the positive pole or terminal of the direct-current voltage source is coupled lt-o the center-tap 45 of the transformer winding 43, whereas the illustrated conductor 15 for the negative pole or terminal of the power rectification stage A is connected to a conductor 48 through the intermediary of a choke or impedance ⁇ coil 47, connected to the respestive cathodes of two controlled semiconductor rectifier elements 50 and 51.
  • the ⁇ controlled rectier elements 50 and 51 are in principle similarly constructed as the controlled rectifier elements 37 and 38 of the power rectification stage A.
  • the anodes of the controlled rectifiers 50 and 51 are each connected with a respective end-point or terminal of the primary Winding 43 of the output transformer 42 through the agency of the conductors 52 and 53, respectively, and the diodes 52a and 53a, respectively.
  • the controlled rectifiers 5t) and 51 are each bridged by a series arrangement or connection comprising a resistor 50b and 51h, respectively, and a diode 50c and 51C, respectively.
  • the anodes of the diodes 50c and 51C are, for example, electrically coupled via a conductor 15a directly to the conductor 15. Further, between or across the conduct-ors 52 and 53 there is connected a capacitor 59 which influences commutation, as such will be more specifically described hereinafter.
  • the controlled rectifier 51 is ignited, so that a current can flow in the direction of the arrow 51.
  • the current thereby flows from the positive pole or terminal of the rectification stage A, that is through the conductor 16 over the transformer winding section 43b, the diode 53a, the conductor 53, the controlled rectifier 51, the conductor 48, the .choke coil 47 and the conductor 15 to the negative outlet pole or terminal of the power rectifier stage A.
  • the current thereby ows through the current circuit designated with reference numeral II, where in consequence thereof the change of flux associated with the rise in current induces a voltage in the secondary 44 of the transformer 42.
  • the controlled rectifier 50 is ignited, so that its resistance in the forward direction becomes negligibly small.
  • the stored charge of the capacitor 59 there is applied to the controlled rectifier 51 for a short period of time the stored charge of the capacitor 59, and indeed, such is applied in the blocking or backward direction so that this controlled rectifier element 51 is extinguished. Since the controlled rectifier element 50 is now ignited a current flows in the current circuit I, which comprises the conductor 16, the primary winding section 43a of the output transformer 42, the diode 52a, the conductor 52, the controlled rectifier 50, the conductor 48, the choke coil 47 and lthe conductor 15.
  • the diodes 50c, 51C are provided in order to achieve that the commutation capacitor 59 after commutation can quickly discharge as well as also quickly charge in the opposite direction.
  • the diodes 52a and 53a ensure that the capacitor 59 is able to retain as high a charge as possible and will not partially discharge during a dropping of the voltage at the primary winding 43 of the transformer 42 during a half-wave of the output voltage, for example as a result of a pronounced load appearing at the output.
  • the capacitor 59 and the primary winding 43 of the transformer 42 thereby operate as an oscillating circuit.
  • a respective resistor 55 and 56 there is arranged parallel to both of the primary windingr portions 43a and 43b a respective resistor 55 and 56.
  • the capacitor 59 can discharge through the resistors 55 and 56.
  • the rating or size of the resistors 55 and 56 must thus be such that the charge can still be maintained until, for example, the controlled rectifier 50 is extinguished.
  • the resistors 55 and 56 thereby dampen the oscillating circuit, so that the voltage cannot increase in amplitude. It is further to be mentioned that the capacitor 59 can, of course, also be coupled to the secondary winding 44 of the transformer 42, whereby the same mode of operation is achieved.
  • a full-wave rectifier circuit 60 which contains four individual rectifier members.
  • a smoothing capacitor 64 In order to smooth the direct-current voltage produced in this manner, there is provided a smoothing capacitor 64.
  • the negative pole of the direct-current voltage derived in this manner is formed by the conductor 65, and is coupled with both of the connected cathodes of the power rectiers 37 and 38 via the conductor 20.
  • the control or ignition circuit C contains a so-called double-base transistor 80, the two bases of which are connected with the negative an-d positive poles or terminals of the supply voltage source via the resistors 81 and 82, respectively, that is with the conductors 65 and 72 respectively.
  • double-base transistors, or unijunction transistor-transistors of such type are available on the market. They have the characteristic of suddenly or unsteadily changing the resistance between a base electrode and the emitter as a function of the voltage at such emitter. If, in the previously described embodiment, the potential at the emitter lies below a predetermined critical value, then the resistance between the emitter and the one base electrode is high.
  • the emitter in the abovedescribed instance is connected with the conductor 65 via-a capacitor 83 and is connected to the conductor 72 via a resistor 84.
  • the capacitor 83 and the resistor 84 thereby form an RC-member.
  • the capacitor 83 charges up to the critical voltage in accordance with the timeconstant of the RC-member, whereupon at the resistor 81 a positive impulse appears in consequence of the discharging of the capacitor 83 through the transistor 80.
  • the system formed of the members 80-84 thereby operates as an oscillator or impulse generator, whereby the pulse recurrence frequency is a function of the dimensions of the RC-member.
  • the frequency is considerably higher than that of the power supply network, so that for each half-wave a larger number of impulses arrive at the controlled rectiiiers 37 and 38.
  • the pulse repetition frequency of the ignition impulses of ignition circuit C is larger than the frequency of the input alternating-current voltage to be rectified, and preferably exceeds such by at least a factor of 3.
  • the rectiers 37, 38 are thereby also ignited during each half-wave if, for any reason, such should become extinguished.
  • the impulses appearing at the resistor 81 are transmitted to the ignition electrodes of the controlled rectiers 37 and 38 through the intermediary of the conductor 19 and Via a respective protective resistor 21 and 22, as best seen by an inspection of the circuit diagram of FIGURE 3.
  • the two controlled rectiers 37 and 38 are thereby always then ignited when the resistance between the two base electrodes and the emitter of the transistor 80 suddenly changes and when a voltage appears in the forward direction at the controlled rectifiers. This is -always the case with one of the two controlled rectiers.
  • Arranged in parallel to the capacitor 83 is a further transistor 89 which short-circuits the capacitor 83 when no negative potential or voltage appears at its base electrode.
  • a full-wave rectification circuit 90 Between the base of the transistor 89 and the vconductor 65 there is disposed the direct-current side of a full-wave rectification circuit 90, the alternating-current side of which is coupled to the secondary winding 26 of the input transformer 24. As has been previously mentioned, the control alternating-current voltage is delivered to the primary side of the transformer 24.
  • a capacitor 91 and a protective diode 92 Arranged in parallel to the direct-current side of the bridge rectication circuit 90 is a capacitor 91 and a protective diode 92.
  • the base electrode of the transistor 89 is further con- Inected via a resistor 93 to the conductor 72 which represents the positive pole or terminal of the power rectifier 60. If, now, a voltage does not appear at the secondary winding 26 of the transformer 24, then the base of the transistor 89 is held at a positive potential through the resistor 93, so that the transistor 89 is conductive and the capacitor 83 cannot charge. A consequence hereof is that, the transistor is blocked and no ignition impulses can be delivered to the controlled rect-iers 37 and 38. Thus, a direct-current voltage does not appear between the conductors 15 and 16.
  • the capacitor 91 charges so that there appears a negative potential at the base of the transistor 89 which blocks this transistor. The result of this is that, the capacitor 83 can charge and ignition impulses can again arrive at the controlled rectiers 37 and 38. If the control alternatingcurrent voltage does not appear at the terminals 23, the capacitor 91 discharges through the protective diode 92 so that the transistor 89 again becomes conductive and impulses no longer appear at the transistor 80 or resistor 81.
  • the ignition circuit D serves to produce the control impulses for the controlled rect-ifiers 50 and 51 in the power output stage B designed as a direct-current to alternatingcurrent inverter.
  • the rectification bridge circuit 61 In order to produce the supply directcurrent voltage for the .ignition circuit D, there is electrically coupled to the secondary winding 14 of the transformer 10 a rectification bridge circuit 61.
  • the positive pole or terminal of the thus constructed direct-current voltage source is formed through the conductor 62 and the negative pole by the conductor 63 or 63.
  • a smoothing capacitor 95 In order to smooth the direct-current voltage there is connected across these conductor-s 62 and 63' a smoothing capacitor 95.
  • the impulse generator for the controlled rectifier 50 again contains a double-base transistor which is connected with the conductors 62 and 63 through the resistors 101 and 102.
  • the emitter is likewise connected with these conductors 62 and 63through the intermediary of an adjustable resistor 103 and a capacitor 104.
  • the pulse repetition rate or pulse recurrence frequency adjustable by means of the resistor 103 is transmitted to the control or ignition electrode of the controlled rectier 50 via the conductor 30 and a protective resistor 106.
  • the frequency determining elements 103 and 104 are so dimensioned or adjusted that, the frequency is considerably larger than the frequency of the voltage which lis delivered from the power output stage B, or the frequency of the control voltage.
  • a transistor 107 is arranged in parallel to the capacitor 104 which in the absence of a negative control voltage at its base electrode provides a very small resistance, that is the oscillating system is blocked by short-circuiting of the capacitor 104.
  • the base electrode of the transistor 107 is connected with the conductor 62 via a resistor 108 and with the conductor 63 via a diode 105. Further, the base electrode is coupled to one terminal of the secondary winding 27 of the transformer 24, the primary winding of which is fed with the control voltage whose frequency is to be delivered from the frequency converter.
  • the otherterminal of the secondary winding 27 is connected with the base electrode of the corresponding transistor of the second impulse generator, in a manner shown in FIG- URE 3.
  • This transistor of the second impulse generator is designated by reference numeral 107. It will now become apparent that the two transistors 107 and 107' are alternatingly blocked and opened whereby such alterna- 9 tion always oocurs during the zero crossover of the control alternating-current voltage. Correspondingly, always only one impulse generator can deliver the necessary series of impulses for igniting the associated controlled rectifier.
  • the upper impulse generator of ignition circuit D and shown in FIGURE 3 delivers a series of impulses so that the controlled rectifier 50 isY ignited
  • the lower arranged impulse generator of t-h'is FIGURE 3 delivers a series of impulses to the rectifier 51 for its ignition, in the same manner as such has been described in the previous discussion of FIGURES 2c and 2d.
  • the other impulse generator of ignition circuit D is similar to the one just described, and has corresponding elements identified with like reference numerals but further bear prime markings.
  • the controlling or control voltage does not necessarily have to be sinusoidal or regular.
  • This can then be of particular importance when the frequency converter is employed as a generator for spark erosion processes. Since the frequency converter immediately begins to operate as soon as a signal appears, that is also within the confines of a half-wave of the control voltage, such converter is exceptionally suitable for power command computers in electrical networks. All of the delivered or supplied series ⁇ of impulses appear practically inertialess at the output. As already mentioned, practically no load is removed from the supply power network when an input signal does not appear at the input transformer 24.
  • the safety circuit E serves the purpose of preventing destruction or damage of the rectifiers 50 and 51 if, for example, the output side is short-circuited or when a controlled rectifier is not extinguished in the manner as desired in consequence of a capacitive load.
  • the safety circuit E operates as a logical element or circuit.
  • two diodes 111 or 112 are coupled to the conductors 52 and 53, the junction point of which is connected to the conductor 120.
  • the conductor 110 is connected to the conductor 120 via two resistors 114 and 119.
  • the conductor 120 is connected via a diode 116 with the emitter of the transistor 80 and via a resistor 115 with the conductor 72. Furthe-rmore, there is arranged between the conductor 72 and the junction point of the resistors 114 and 119 a capacitor 117.
  • the first operating condition is that occurring by switching-in, that is at that period of time during which there does not appear a voltage at the conductors or 110, or at the conductor 120.
  • the ignition circuit C operates in a normal manner since no voltage whatsoever effects the base electrode of the transistor 80, which could disadvantageously influence its mode of operation.
  • the voltage will adjust itself in accordance with the dimerisioning of the capacitor 83 and the resistor 84, in a manner as described hereinabove.
  • the second condition of operation the normal operating voltage appears at the conductor 110 as well as at the conductor 120.
  • the voltage at the conductor 120 is thereby maintained at a positive potential, so that likewise no potential can reach the emitter of the transistor 80 which could disadvantageously infiuence such.
  • the safety circuit E is particularly meaningful because of the fact that one of the controlled rectifiers 50 or 51 in consequence of special load requirements cannot be extinguished, so that both controlled rectifiers 5.0 and 51 are ignited at the same time.
  • the dimensioning of the capacitor 117 and the resistors 115, 119 must be so selected that the transistor 80 becomes blocked for such length of time until the two controlled rectifiers 50 and 51 are positively extinguished.
  • the frequency converter will continue to operate, whereby the output voltage in consequence of the fact that the ignition results by a series of impulses, will immediaely adjust itself to the condition which is determined by the alternating-'current voltage appearing at the terminals 23 of the input transformer 24.
  • An electric circuit provided with controlled semi-conductor rectifier means, ignition circuit means for igniting said controlled semi-conductor rectifier means, said ignition circuit means delivering a series of ignition pulses at least during a predetermined ignition period, and wherein said electric circuit is constructed as a direct-current to alternating-current inverter for converting a directcurrent voltage into an alternating current voltage, a transformer provided with a transformer winding having a center-tap, a respective one of said controlled semi-conductor rectifier means coupled to each terminal of said transformer winding, said direct-current voltage being applied to said center-tap and via said respective controlled semi-conductor rectifier means to said terminals of said transformer winding, a capacitor for commutation bridging said terminals of said transformer winding, said ignition circuit means being operatively connected with both of said controlled semi-conductor rectifier means for alternatingly supplying said series of impulses, wherein the lalternation in the transmission of said series of impulses corresponds to the desired frequency of the output alternating-current
  • An electric -circuit provided with controlled semiconductor rectifier means, ignition circuit means for igniting said controlled semi-conductor rectifier means, said ignition circuit means delivering a series of ignition impulses at least during a predetermined ignition period, said electric circuit including a full-Wave rectifier provided with four rectifiers connected in a full-wave bridge rectification circuit, two of said rectifiers including said controlled semi-conductor rectifier means and electrically connected to a common terminal of a directcurrent voltage ⁇ outlet of said full-wave rectifier, said ignition circuit means including a first ignition circuit electrically connected with said two controlled semi-conductor rectifier means for delivering an uninterrupted series of said ignition impulses, the pulse repetition frequency of which lies at least above the frequency of an alternatingcurrent voltage to be rectified byv a factor of 3, said electric circuit further including a direct-current to lalternatingcurrent inverter for converting a direct-current voltage into an alternating-current voltage, a transformer provided with 4a ytransformer winding having a center-tap, said in
  • An electric circuit provided with controlled semiconductor rectifier means, ignition circuit means for igniting sai-d controlled semi-conductor rectifier means, said ignition circuit means delivering a series of ignition impulses at least during a predetermined ignition period, said electric circuit being constructed as a full-wave rectiiier provided with four rectifiers ⁇ connected in a full-wave bridge rectification circuit, two of said rectifiers being said controlled semi-conductor rectifier means and electrically connected to a common terminal of a direct-current voltage outlet of said full-wave rectifier, said ignition circuit means being electrically connected with said two controlled semi-conductor rectifier means for delivering an uninterrupted series of said ignition impulses, the pulse repetition frequency of which lies at least above the frequency of an alternating-current voltage to be rectified by a factor of 3.
  • An electric circuit provided with controlled semiconduct-or rectifier means, ignition circuit means for ignitingsaid controlled semi-conductor rectifier means, saidv ignition circuit means delivering a series of ignition impulses at least during a predetermined ignition period, said electric circuit being constructed as a direct-current to alternating-current .inverter for converting a direct- 12 current voltage into an yalternating-current voltage, a trans'- f-ormer provided with a transformer winding having a center-tap, a respective one of said controlled semi-conductor rectifier means coupled to each termin-al of said transformer winding, a diode connected in series with each terminal of said transformer winding, said directcurrent voltage being applied to said center-tap and via said respective controlled semi-conductor rectifier means to said terminals of said transformer winding, a capacitor for commutation bridging said terminals of said transformer winding, said ignition circuit means being operatively connected with both of said controlled semi-conductor rectifier means for alternatingly supplying said series .of

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Generation Of Surge Voltage And Current (AREA)
  • Rectifiers (AREA)
  • Inverter Devices (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Dc-Dc Converters (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
US243457A 1961-12-13 1962-12-10 Circuit with controlled rectifiers and improved ignition thereof Expired - Lifetime US3273041A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CH1445461A CH402159A (de) 1961-12-13 1961-12-13 Statischer Frequenzumformer
CH1445261A CH395303A (de) 1961-12-13 1961-12-13 Statischer Frequenzumformer
CH1445361A CH397851A (de) 1961-12-13 1961-12-13 Schaltung mit gesteuerten Gleichrichtern

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US3273041A true US3273041A (en) 1966-09-13

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US243457A Expired - Lifetime US3273041A (en) 1961-12-13 1962-12-10 Circuit with controlled rectifiers and improved ignition thereof
US243527A Expired - Lifetime US3259827A (en) 1961-12-13 1962-12-10 Frequency transformer including improved inverter circuit
US243526A Expired - Lifetime US3246227A (en) 1961-12-13 1962-12-10 Frequency transformer including safety circuit

Family Applications After (2)

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US243527A Expired - Lifetime US3259827A (en) 1961-12-13 1962-12-10 Frequency transformer including improved inverter circuit
US243526A Expired - Lifetime US3246227A (en) 1961-12-13 1962-12-10 Frequency transformer including safety circuit

Country Status (6)

Country Link
US (3) US3273041A (enExample)
CH (3) CH397851A (enExample)
DE (5) DE1289575B (enExample)
FR (3) FR1345286A (enExample)
GB (3) GB1006269A (enExample)
SE (1) SE317740B (enExample)

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US3430123A (en) * 1966-11-03 1969-02-25 Gen Motors Corp Rectifier-inverter motor power supply
US3437899A (en) * 1966-08-04 1969-04-08 Tokyo Keiki Kk Power source device for driving step motor of gyro
US3497784A (en) * 1967-07-10 1970-02-24 Ametek Inc Brushless direct current motor circuitry and like circuitry with protection for non-commutating conditions
US3514639A (en) * 1966-10-17 1970-05-26 Emerson Electric Co Variable conduction angle polyphase synchronization circuit
US3557692A (en) * 1968-09-09 1971-01-26 Harris Intertype Corp Plural independently operable motor drive arrangement in printing press
US3566148A (en) * 1968-02-14 1971-02-23 Westinghouse Electric Corp Selective phase angle pulse generating circuit
US3600655A (en) * 1968-05-21 1971-08-17 Beloit Corp System for controlling the speed of a plurality of motors which have output shafts to drive elements that are interrelated
US3656051A (en) * 1970-07-20 1972-04-11 Kohler Co Fast response feedback controlled generator
US3775662A (en) * 1971-12-07 1973-11-27 Bendix Corp Constant frequency power inverter having silicon controlled rectifier multibridge inputs for output wave shaping with variable phase control for overload conditions

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US3260919A (en) * 1962-04-02 1966-07-12 North American Aviation Inc Regulated inverter circuit
US3376493A (en) * 1963-09-16 1968-04-02 Basic Products Corp Inverter circuit having improved control frequency compensating means for producing a regulated a.c. output
US3398352A (en) * 1964-01-20 1968-08-20 Lorain Prod Corp Apparatus and method for starting, operating and stopping an inverter
US3383582A (en) * 1964-05-07 1968-05-14 Bell Telephone Labor Inc Power conversion apparatus employing a magnetic control circuit for actuating gate turn-off switches
US3344326A (en) * 1964-07-13 1967-09-26 Cutler Hammer Inc Adjustable frequency control system
US3366867A (en) * 1964-10-23 1968-01-30 Buoys Inc Static switch for controlling dc to ac inverter
US3351838A (en) * 1964-11-09 1967-11-07 North Electric Co Automatic battery charger using ramp function for error signal reference in scr control of multiphrase load
US3379955A (en) * 1964-11-17 1968-04-23 Lockheed Aircraft Corp Apparatus for protecting the switching elements of static inverters from transient voltages
US3413538A (en) * 1965-04-15 1968-11-26 Gen Electric Control means for starting electric power converters at reduced operating frequencies
US3401326A (en) * 1966-03-11 1968-09-10 North Electric Co Three phase inverter circuit having three stage ring counter and power inverters with ferro-resonant wave shaping circuits
US3437911A (en) * 1966-04-25 1969-04-08 Gen Electric Control circuit for controlling the power to an inductive load from a polyphase source
FR1556270A (enExample) * 1966-12-02 1969-02-07
US3450975A (en) * 1967-05-23 1969-06-17 Lewis G Striggow Impedance network for controlled rectifiers
US3475673A (en) * 1967-05-23 1969-10-28 Lewis G Striggow Control circuit for alternating current and direct current loads and with zero turn-on and zero turn-off
US3527986A (en) * 1967-08-11 1970-09-08 Westinghouse Air Brake Co Fail-safe electronic circuit arrangement
US3670232A (en) * 1970-11-09 1972-06-13 Ltv Ling Altec Inc Protected power supply
GB1381260A (en) * 1970-11-24 1975-01-22 Steghart F L F Electrical power conversion systems
JPS5254730Y2 (enExample) * 1972-07-26 1977-12-12
US3916290A (en) * 1974-09-27 1975-10-28 Hattangady Vasanth Rao Parallel inverters
US3931565A (en) * 1974-10-03 1976-01-06 Hase A M Inverters
US4042871A (en) * 1975-11-14 1977-08-16 Ecc Corporation Conversion system with overcurrent protection and start-up circuitry
DE3025421C2 (de) * 1980-07-04 1985-03-21 Siemens AG, 1000 Berlin und 8000 München Schaltungsanordnung zur Versorgung einer Gasentladungslampe aus einem Wechselstromnetz

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US2925546A (en) * 1959-05-11 1960-02-16 Acf Ind Inc Magnetic reset control for rectifier
US2977523A (en) * 1958-12-31 1961-03-28 Gen Electric Control circuit
US3010062A (en) * 1960-01-27 1961-11-21 Crane Co Converter circuit
AT221673B (de) * 1959-12-09 1962-06-12 Agie A G Fuer Ind Elektronik L Spannungsgenerator für elektrolytische Erosionsprozesse
US3047789A (en) * 1959-11-25 1962-07-31 Gen Electric Inverter circuit
FR1303427A (fr) * 1960-10-14 1962-09-07 Agie Ag Ind Elektronik Transformateur de fréquence pour machines-outils à usiner par étincelage
FR1304263A (fr) * 1960-10-21 1962-09-21 Westinghouse Brake & Signal Circuit de convertisseur
US3075136A (en) * 1961-08-31 1963-01-22 Gen Electric Variable pulse width parallel inverters
US3082369A (en) * 1961-07-27 1963-03-19 Du Pont Inverter apparatus
US3089992A (en) * 1960-05-09 1963-05-14 Du Pont Precision frequency control
US3091729A (en) * 1959-03-06 1963-05-28 Borg Warner Static inverter
US3124740A (en) * 1962-03-16 1964-03-10 Stage
US3197691A (en) * 1962-01-02 1965-07-27 Gen Electric Regulated power supply
US3221183A (en) * 1961-10-03 1965-11-30 Richard L White Solid-state controlled rectifier relay

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US2785370A (en) * 1953-10-26 1957-03-12 Sorensen & Company Inc Dual regulating circuit
US2833977A (en) * 1955-10-10 1958-05-06 Sorensen And Company Protective circuit for inverters
US3146356A (en) * 1960-12-14 1964-08-25 Garrett Corp Repetitive high current semiconductor switch
US3132287A (en) * 1961-03-14 1964-05-05 Ryan Aeronautical Co High frequency circuit breaker utilizing silicon controlled rectifiers
US3196336A (en) * 1961-06-09 1965-07-20 Borg Warner Bidirectional power supply system
US3165649A (en) * 1962-09-04 1965-01-12 Ault Inc Quick turn-off circuit using tunnel diode and inductive kick to effect off condition
US3142392A (en) * 1963-01-18 1964-07-28 Cletus J Vallad Electric mail sorting machine

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Publication number Priority date Publication date Assignee Title
US2977523A (en) * 1958-12-31 1961-03-28 Gen Electric Control circuit
US3091729A (en) * 1959-03-06 1963-05-28 Borg Warner Static inverter
US2925546A (en) * 1959-05-11 1960-02-16 Acf Ind Inc Magnetic reset control for rectifier
US3047789A (en) * 1959-11-25 1962-07-31 Gen Electric Inverter circuit
AT221673B (de) * 1959-12-09 1962-06-12 Agie A G Fuer Ind Elektronik L Spannungsgenerator für elektrolytische Erosionsprozesse
US3010062A (en) * 1960-01-27 1961-11-21 Crane Co Converter circuit
US3089992A (en) * 1960-05-09 1963-05-14 Du Pont Precision frequency control
FR1303427A (fr) * 1960-10-14 1962-09-07 Agie Ag Ind Elektronik Transformateur de fréquence pour machines-outils à usiner par étincelage
FR1304263A (fr) * 1960-10-21 1962-09-21 Westinghouse Brake & Signal Circuit de convertisseur
US3082369A (en) * 1961-07-27 1963-03-19 Du Pont Inverter apparatus
US3075136A (en) * 1961-08-31 1963-01-22 Gen Electric Variable pulse width parallel inverters
US3221183A (en) * 1961-10-03 1965-11-30 Richard L White Solid-state controlled rectifier relay
US3197691A (en) * 1962-01-02 1965-07-27 Gen Electric Regulated power supply
US3124740A (en) * 1962-03-16 1964-03-10 Stage

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3437899A (en) * 1966-08-04 1969-04-08 Tokyo Keiki Kk Power source device for driving step motor of gyro
US3514639A (en) * 1966-10-17 1970-05-26 Emerson Electric Co Variable conduction angle polyphase synchronization circuit
US3430123A (en) * 1966-11-03 1969-02-25 Gen Motors Corp Rectifier-inverter motor power supply
US3497784A (en) * 1967-07-10 1970-02-24 Ametek Inc Brushless direct current motor circuitry and like circuitry with protection for non-commutating conditions
US3566148A (en) * 1968-02-14 1971-02-23 Westinghouse Electric Corp Selective phase angle pulse generating circuit
US3600655A (en) * 1968-05-21 1971-08-17 Beloit Corp System for controlling the speed of a plurality of motors which have output shafts to drive elements that are interrelated
US3557692A (en) * 1968-09-09 1971-01-26 Harris Intertype Corp Plural independently operable motor drive arrangement in printing press
US3656051A (en) * 1970-07-20 1972-04-11 Kohler Co Fast response feedback controlled generator
US3775662A (en) * 1971-12-07 1973-11-27 Bendix Corp Constant frequency power inverter having silicon controlled rectifier multibridge inputs for output wave shaping with variable phase control for overload conditions

Also Published As

Publication number Publication date
CH397851A (de) 1965-08-31
FR1345286A (fr) 1963-12-06
DE1190095C2 (de) 1973-04-05
DE1190095B (de) 1965-04-01
CH402159A (de) 1965-11-15
GB1006269A (en) 1965-09-29
DE1438635A1 (de) 1969-06-04
FR1345287A (fr) 1963-12-06
DE1289575B (de) 1969-02-20
GB1006267A (en) 1965-09-29
CH395303A (de) 1965-07-15
SE317740B (enExample) 1969-11-24
FR1345285A (fr) 1963-12-06
US3246227A (en) 1966-04-12
US3259827A (en) 1966-07-05
GB1006268A (en) 1965-09-29
DE1438633A1 (de) 1969-03-27

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