WO1993023916A1 - Power generation system with soft-start circuit - Google Patents

Power generation system with soft-start circuit Download PDF

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Publication number
WO1993023916A1
WO1993023916A1 PCT/US1993/004655 US9304655W WO9323916A1 WO 1993023916 A1 WO1993023916 A1 WO 1993023916A1 US 9304655 W US9304655 W US 9304655W WO 9323916 A1 WO9323916 A1 WO 9323916A1
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WIPO (PCT)
Prior art keywords
pulses
inverter
output
soft
input
Prior art date
Application number
PCT/US1993/004655
Other languages
French (fr)
Inventor
John P. Dhyanchand
Chi-Nam Ng
Sunil Patel
Vietson M. Nguyen
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Sundstrand Corporation
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Publication date
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Publication of WO1993023916A1 publication Critical patent/WO1993023916A1/en

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Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02MAPPARATUS 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
    • H02M7/00Conversion of ac power input into dc power output; Conversion of dc power input into ac power output
    • H02M7/42Conversion of dc power input into ac power output without possibility of reversal
    • H02M7/44Conversion of dc power input into ac power output without possibility of reversal by static converters
    • H02M7/48Conversion 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
    • H02M7/483Converters with outputs that each can have more than two voltages levels
    • H02M7/49Combination of the output voltage waveforms of a plurality of converters
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02MAPPARATUS 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
    • H02M1/00Details of apparatus for conversion
    • H02M1/36Means for starting or stopping converters

Definitions

  • the present invention is directed to a power generation system for an aircraft having a stepped- waveform inverter of the type used to generate AC power from DC power and a soft-start circuit to reduce undesirable inrush currents during start-up of the inverter.
  • variable-frequency AC power may be produced by a brushless, synchronous generator driven by a jet engine.
  • the variable-frequency AC power is converted to DC power by an AC/DC converter, such as a rectifier bridge.
  • An inverter is coupled to the AC/DC converter to transform the DC power into constant-frequency AC power, which is then filtered by a filter.
  • the filtered AC output is then provided to an AC load bus which supplies power to various loads.
  • the inverter used in VSCF systems may be of the ⁇ tepped-wavefor type. An inverter of this type is disclosed in U.S. Patent No.
  • Such a stepped-waveform inverter generates an output having a stepped shape that generally approximates a sine wave.
  • the purpose of approximating a sine wave is to reduce the size of the filters, provided at the output of the inverter, that are used to remove unwanted harmonics.
  • Power conversion systems often rely upon saturable reactors such as inductive-type filters or transformers. When the power conversion system is first initiated to begin the power conversion process, the sudden application of power to the saturable reactor may cause it to saturate providing little impedance to current. This current faced with little impedance can become quite large and can possibly damage elements of the power conversion system such as its inverter switches. In order to prevent such damage, it is desired to limit or inhibit this inrush current.
  • the present invention is directed to an arrangement for limiting inrush current. Accordingly, an inverter system is provided having inverter switches for inverting DC to AC.
  • a soft-start pulse supply circuit supplies soft-start pulses to the inverter switches to begin the inverter process. After a time, a controller takes over and supplies normal control pulses to the inverter switches. The soft-start pulses have a higher frequency than the normal control pulses.
  • the soft-start pulses may have a substantially constant duty cycle and amplitude and the frequency of the soft-start pulses also may be substantially constant.
  • An excitation circuit may be provided to supply the soft-start pulses.
  • the excitation circuit has a monostable multivibrator for providing a timing pulse initiated at start-up of the inverter system for controlling the number of soft-start pulses supplied to the inverter switches.
  • the inverter switches may be used to energize the primary windings of two transformers, the second windings of which are interconnected so that voltages induced therein are added.
  • Figure 1 is a block diagram of a VSCF power conversion system in which the present invention can be used;
  • Figure 2 is a block diagram of the inverter of Figure 1;
  • Figure 3 is a circuit diagram of one pair of subinverters and their associated transformers of the inverter of Figure 2;
  • Figure 4 is a circuit diagram of one of the activation circuits of Figure 2;
  • Figure 5 illustrates a first phase relationship of a number of waveforms generated by the inverter and a waveform produced by the summation of those waveforms;
  • Figure 6 illustrates a second phase relationship of a number of waveforms generated by the inverter and a waveform produced by the summation of those waveforms
  • Figure 7 illustrates a third phase relationship of a number of waveforms generated by the inverter and a waveform produced by the summation of those waveforms
  • Figure 8 illustrates a fourth phase relationship of a number of waveforms generated by the inverter and a waveform produced by the summation of those waveforms
  • Figures 9a-9c are vector diagrams illustrating a first mode of operation of the inverter of the invention.
  • Figures lOa-lOc are vector diagrams illustrating a second mode of operation of the inverter of the invention.
  • Figure 11 illustrates various waveforms relating to the operation of the phase angle control circuit of Figure 2;
  • Figure 12 is a circuit diagram of the phase angle control circuit shown schematically in Figure 2;
  • Figure 13 is a circuit diagram of the output sensing circuit shown schematically in Figure 2;
  • Figure 14 is a graph of two voltage signals used in the phase angle control circuit to control the phase relationship of the waveforms generated by the inverter; and Figure 15 is an illustration of a number of waveforms generated during operation of the activation circuit shown in Figure 4.
  • FIG. 1 A block diagram of a preferred embodiment of a VSCF power conversion system 10 incorporating the present invention is shown in Figure 1.
  • the power conversion system 10 includes a prime mover 12 coupled to a generator 14 for generating variable-frequency AC power.
  • An AC/DC converter 16 is coupled to the generator 14 for converting the variable-frequency AC power into DC power.
  • the DC output of the AC/DC converter 16 is supplied to various DC loads via a pair of lines 20a, 20b.
  • a second pair of lines 22a, 22b provides the DC to an inverter 24, which generates three-phase, constant-frequency AC power from this DC.
  • the inverter 24 is coupled to a filter 26 via three output lines 28a, 28b, 28c, each of which supplies a respective phase of the constant-frequency AC output to the filter 26.
  • the output of the filter 26 is provided via lines 29 to a three-phase AC load bus which supplies AC power to various AC loads.
  • a block diagram of the inverter 24 is shown in Figure 2.
  • the inverter 24 includes three subinverter pairs 30, 32, 34, although any number of subinverters may be used.
  • Each of the subinverter pairs 30, 32, 34 is coupled to a respective transformer pair 31, 33, 35.
  • the output lines 28a, 28b, 28c interconnect each of the transformer pairs 31, 33, 35, and the transformer pair 35 is connected to a neutral line 28d.
  • Each of the subinverter pairs 30, 32, 34 is controlled by a respective activation circuit 40a-c.
  • a regulator circuit for regulating the voltage on the transformer output lines 28a, 28b, 28c is shown to comprise an output sensing circuit 50 and a phase angle control circuit 52.
  • the output sensing circuit 50 senses the current on the three transformer output lines 28a, 28b, 28c via three lines 56a, 56b, 56c, and the sensing circuit 50 senses the voltage on the three output lines 28a, 28b, 28c via three lines 58a, 58b, 58c.
  • the output sensing circuit 50 generates a phase control signal, ⁇ c , having a magnitude based on both the voltage and current sensed on the lines 28a-c and provides the ⁇ _ signal to the phase control circuit 52 via a line 60.
  • the phase angle control circuit 52 causes the phase angles between the various waveforms generated by the three subinverter pairs 30, 32, 34 to be varied. As a result of the control of the phase angles, the magnitude of the voltage on the transformer output lines 28a, 28b, 28c is regulated.
  • the regulator circuit could sense the AC output on the lines 29 after the AC output is filtered by the filter 26.
  • the phase angle control circuit 52 varies the magnitude of the phase angles by generating a pair of reset signals, RES2 and RES3, based upon the magnitude of the phase control signal ⁇ c and a pair of reference signals, REF1 and REF2.
  • the REF1 and REF2 signals are transmitted to the phase angle control circuit 52 from the first and second activation circuits 40a, 40b via a pair of lines 66, 68, respectively.
  • the RES2 and RES3 signals are transmitted from the phase angle control circuit 52 to the second and third activation circuits 40b, 40c via a pair of lines 70, 72, respectively.
  • the RES2 signal controls the phase angle between the waveforms generated by the first subinverter pair 30 and the waveforms generated by the second subinverter pair 32
  • the RES3 signal controls the phase angle between the waveforms generated by the second subinverter pair 32 and the waveforms generated by the third subinverter pair 34.
  • the first subinverter pair 30 and the first transformer pair 31 are shown in Figure 3.
  • the first subinverter pair 30 includes two subinverters 30a, 30b, and the first transformer pair 31 includes two three- phase transformers 31a, 31b.
  • the subinverter 30a includes six transistor switches 82a-c, 84a-c, each of which has a diode connected across it.
  • the subinverter 30a is connected to three wye-connected primary windings 80a-c of the transformer 31a which are controlled by the three pairs of switches 82a-c, 84a-c, although these windings alternatively may be delta connected.
  • the upper terminal of the winding 80a is connected to the junction of the switches 82a, 84a; the upper terminal of the winding 80b is connected to the junction of the switches 82b, 84b; and the upper terminal of the winding 80c is connected to the junction of the switches 82c, 84c.
  • the bottom terminals of windings 80a, 80b, 80c are connected together.
  • the primary windings 80a-c of the transformer 31a are inductively coupled to three secondary windings 90a-c, respectively.
  • the switches 82a-c and 84a-c are switched in a conventional manner to generate the waveform 220 in Figure 5 on each of the three wye- connected windings 80a-c, each of the three waveforms differing in phase by 120°. Because the windings 80a-c are wye connected, the waveform 220 has five possible amplitudes at any point in time, +A, +A/2, 0, -A/2, and -A, where A is the maximum amplitude.
  • the subinverter 30b includes six transistor switches 94a-c, 96a-c, each of which has a diode connected across it.
  • the subinverter 30b is connected to three delta-connected primary windings 92a-c of the transformer 31b which are controlled by the three pairs of switches 94a-c, 96a-c, although these windings may be alternatively wye connected.
  • the upper terminal of the winding 92a is connected to the junction of the switches 94a, 96a and to the bottom terminal of winding 92c; the upper terminal of the winding 92b is connected to the junction of the switches 94b, 96b and to the bottom terminal of winding 92a; and the upper terminal of the winding 92c is connected to the junction of the switches 94c, 96c and to the bottom terminal of winding 92b.
  • the three delta-connected primary windings 92a-c are inductively coupled to three secondary windings 98a-c of the transformer 31b, respectively.
  • the switches 94a-c and 96a-c are switched in a manner similar to switches 82a-c and 84a-c to generate the waveform 222 in Figure 5 on each of the three delta-connected windings 92a-c, each of the three waveforms 222 having a phase difference of 120°. Because the windings are delta connected, such a waveform has three possible amplitudes, +A, 0, and -A, where A is the maximum amplitude.
  • switches 82a-c, 84a-c, 94a-c, 96a-c are shown to be transistors, other types of switches may be used, such as thyristors or D' ⁇ rlington- connected transistor pairs.
  • circuit diagrams for the second and third subinverter pairs 32, 34 and the second and third transformer pairs 33, 35 are identical to the one shown in Figure 3 and are not shown separately for purposes of simplicity.
  • the activation of the twelve switches 82a-c, 84a-c, 94a-c, 96a-c in each of the subinverter pairs 30 r 32, 34 is controlled by a respective one of the activation circuits 40a-c. Since the three activation circuits 40a-c are substantially identical, only one is shown. Referring to Figure 4 r the activation circuit 40 includes three four-bit counters 110, 112, 114 connected to an EPRO 116 which in turn is connected to a driver circuit 118. The counters '110, 112, 114 are driven by a clock signal, CLK, generated by a main controller (not shown) .
  • CLK clock signal
  • the carry output of the counter 110 is input to the counter 112 via a line 111, and the carry output of the counter 112 is input to the counter 114 via a line 113.
  • the 10-bit output of the counters 110, 112, 114 is incremented by one. This 10-bit output is used as an address to address the EPROM 116.
  • the EPROM 116 has a six-bit binary code stored in each of its address locations.
  • the six binary bits control the activation of the 12 switches in one of the subinverters.
  • one bit of the six-bit binary code is output on the line 122 to the driver 118, which generates an uncomplemented switching signal on a line 124 and a complemented switching signal on a line 126.
  • the line 124 is connected to the base of one transistor in one vertical branch of one of the subinverters, such as switch 82a, and the line 126 is connected to the base of the other switch in the vertical branch, such as switch 84a.
  • the remaining five bits of the six-bit binary code are output on the lines 130, 132, 134, 136, 138, respectively, to the driver circuit 118, which generates on its outputs a pair of complemented driving signals for each of the five binary signals. These driving signals are supplied to the remaining switches of the subinverter.
  • each of the activation circuits 40 As the CLK signal periodically increments the counters 110, 112, 114, the six bits of the binary code are periodically output from the EPROM 116 via lines 122, 130-138 to the driver 118, and the 12 switches of each corresponding subinverter pair 30a/30b, 32a/32b, and 34a/34b are controlled to generate each corresponding pair of the waveforms 220/222, 224/226, and 228/230 shown in Figure 5 on the primary windings of the corresponding transformers 31a/31b, 33a/33b, and 35a/35b.
  • the EPROM 116 generates a reference signal, REF, on a line 142. As described in more detail below, the REF signal is used as a phase reference signal.
  • a reset signal, RES may be input to the counters 110, 112, 114 via a line 140. When the RES signal is activated, the counters 110, 112, 114 are reset, thus providing a 10-bit address to the EPROM 116 equal to zero.
  • the contents of each EPROM in the three activation circuits 40a-c are identical. If each of the EPROMs is given the same sequence of addresses, the resulting waveforms generated by the subinverters would be identical and thus have zero phase angle.
  • the time of reset of the counters 110, 112, 114 of an activation circuit determines the phase angle between the waveforms generated by that activation circuit and the waveforms generated by the other two activation circuits.
  • the activation circuit 40 of Figure 4 is used for the activation circuit 40a shown in Figure 2
  • the REF line 142 of Figure 4 is connected to the REF1 line 66 of Figure 2
  • the RES line 140 of Figure 4 is not used.
  • the activation circuit 40 of Figure 4 is used for the activation circuit 40b
  • the REF line 142 of Figure 4 is connected to the REF2 line 68 of Figure 2
  • the RES line 140 of Figure 4 is connected to the RES2 line 70 of Figure 2.
  • the RES line 140 of Figure 4 is connected to the RES3 line 72 of Figure 2
  • the REF line 142 of Figure 4 is not used.
  • the activation circuit 40- has a soft-start circuit 150 which, as described in more detail below, is used during a start-up period of the inverter 24 to reduce undesirable inrush currents.
  • Stepped-waveform inverters having six subinverters as shown in Figure 2 are referred to as 36-step inverters.
  • the waveforms generated by one phase of the subinverters 30a, 30b, 32a, 32b, 34a, 34b in the corresponding phase of the primary windings of the transformers 31a, 31b, 33a, 33b, 35a, 35b are shown.
  • the summing transformer output waveform 240 shown in the bottom portion of Figure 5 is generated on each of the three transformer output lines 28a, 28b, 28c, each of the three waveforms 240 being 120° apart.
  • the waveform 240 represents the summation of the waveforms 220, 222, 224, 226, 228, 230.
  • the inverter 24 of the present invention has two modes of operation during steady-state operation.
  • a first mode of operation is used when the current on the output lines 28a-c of the summing transformer is below a predetermined threshold.
  • a second mode of operation is used when the output current is above the predetermined threshold.
  • the phase angle between the waveforms generated by the first subinverter pair 30 and the waveforms generated by the second subinverter pair 32 is held constant, preferably 15°, and the phase angle between the waveforms generated by the second subinverter pair 32 and waveforms generated by the third subinverter pair 34 is varied, depending upon the output voltage sensed on the transformer output lines 28a-c.
  • the waveforms shown in Figures 5 and 6 illustrate the first mode of operation. It should be noted that the first subinverter pair waveforms 220, 222 and the second subinverter pair waveforms 224, 226 of both Figures 5 and 6 have a fixed phase angle of 15°. However, the phase angle between the second subinverter pair waveforms 224, 226 and the third subinverter pair waveforms 228 r 230 is 0° in Figure 5 and 60° in Figure 6. By controlling the phase angle between the second and third subinverter pair wave ⁇ forms, the resultant output voltage may be regulated.
  • the waveform 240 of Figure 5 has a peak positive amplitude of +6A and a peak negative amplitude of -6A
  • the output voltage waveform 240 of Figure 6 has a peak positive amplitude of +5 A and a peak negative amplitude of -5 A.
  • the vector diagrams in those figures illustrate the first mode of operation.
  • the vector V represents the first subinverter pair waveforms 220, 222; the vector V 2 represents the second subinverter pair waveforms 224, 226; and the vector V 3 represents the third subinverter pair waveforms 228, 230.
  • the phase angle between V t and V 2 is constant, at 15°.
  • the phase angle between V 2 and V 3 may vary from a minimum phase angle of 0° as shown in Figure 9a to a maximum phase angle of 120° as shown in Figure 9c. In between the minimum and maximum phase angles, the phase angle may be any variable angle a as shown in Figure 9b.
  • the vector positions shown in Figures 9a and 9c represent the extreme phase angles of the first mode of operation, and during normal operation the phase angles will be as shown in Figure 9b.
  • the phase angle between the waveforms generated by the first and second subinverter pairs is a variable angle between 15° and 120° r while the phase angle between the waveforms generated by the second and third subinverter pairs is held constant, preferably 120°.
  • the voltage on the transformer output lines is gradually reduced to zero.
  • the second mode of operation is used when the current on the output lines 28a-c is above the predetermined threshold.
  • the waveforms shown in Figures 7 and 8 illustrate the second mode of operation.
  • the third subinverter pair waveforms 228, 230 lag the second subinverter pair waveforms 224, 226 by a constant 120°.
  • the phase angle between the first subinverter pair waveforms 220, 222 and the second subinverter pair waveforms 224, 226 is 45° in Figure 7 and 120° in Figure 8.
  • the transformer output voltages, which are represented by the waveforms 240 in Figures 7 and 8, are gradually reduced to zero.
  • the amplitude of the waveform 240 reaches a peak amplitude of +3A between 135° and 150° and -3A between 315° and 330°, and in Figure 8 the waveform 240 has zero amplitude.
  • the vector V represents the first subinverter pair waveforms 220, 222; the vector V 2 represents the second subinverter pair waveforms 224, 226; and the vector V 3 represents the third subinverter pair waveforms 228, 230.
  • the phase angle between V 2 and V 3 is constant, at 120°.
  • the phase angle between V, and V 2 may vary from a minimum phase angle of 15° as shown in Figure 10a to a maximum phase angle of 120° as shown in Figure 10c. In between the minimum and maximum phase angles, the phase angle may be any variable angle b as shown in Figure 10b.
  • Figure 11 illustrates the control of the phase angle between the subinverter 32a waveform 224 and the subinverter 34a waveform 228.
  • the waveform 224 is shown in its phase relationship with respect to the REF2 signal.
  • REF2 changes from zero to positive when waveform 224 transitions to a positive amplitude and from positive to zero when waveform 224 transitions to a negative amplitude.
  • a ramp signal, RAMP is generated based upon the magnitude of the REF2 signal. The rising edge of the REF2 signal corresponds to the beginning of the RAMP signal. When the REF2 signal is positive, the amplitude of the RAMP signal slowly increases.
  • the RAMP signal is used to generate the RES3 signal based on a -phase control signal ⁇ _ generated from the phase control signal ⁇ c of Figure 2.
  • the magnitude of the ⁇ signal varies, depending upon the magnitude of the current and voltage sensed on the transformer output lines 28a, 28b, 28c. "
  • the relative values of the RAMP and ⁇ _ signals are used to generate a comparison signal, COMP, having a positive amplitude when the value of the RAMP signal is greater than the value of the ⁇ signal and a zero amplitude when the value of the RAMP signal is less than the value of the ⁇ signal.
  • COMP comparison signal
  • the point of intersection of the rising portion of the RAMP signal and the ⁇ signal determines the magnitude of the phase delay between the subinverter waveforms. This intersection point is shown as point 260 in Figure 11.
  • the COMP signal changes from zero to a positive amplitude.
  • the rising edge of the COMP signal triggers the RES3 signal to become positive, or activated.
  • the RES3 signal When the RES3 signal is activated, it resets the counters associated with the third subinverter pair 34. As a result, the counters produce a zero 10-bit address, and the EPROM starts to generate the waveform 228.
  • the time- occurrence of the rising edge of the RES3 signal controls the phase difference between the waveform 224 and the waveform 228. This phase difference is shown in Figure 11 as ⁇ .
  • the magnitude of the c3 signal determines the magnitude of the phase delay ⁇ . If the magnitude of ⁇ is larger, the ⁇ signal will intersect the RAMP signal later, thus causing a larger phase delay. If the magnitude of ⁇ is smaller, the ⁇ signal will intersect the RAMP signal earlier, thus causing a smaller phase delay.
  • the manner of varying the phase angle between the first subinverter pair waveforms and the second subinverter pair waveforms is similar to the manner described immediately above, except that the phase angle is between waveforms 220 and 224, REFl is used in place of REF2 , and RES2 is generated instead of RES3.
  • the phase angle control circuit 52 for controlling the phase angles between the three subinverter pairs 30, 32, 34 is shown in Figure 12.
  • the REFl, REF2, and ⁇ . signals are input to the phase angle control circuit 52 via the lines 66, 68, 60, respectively, and the circuit 52 generates the RES2 and RES3 signals on the lines 70, 72, respectively.
  • the circuit 52 includes a ramp generator comprising a comparator 302 . having an inverting input which receives the REFl signal and a noninverting input that receives a predetermined reference voltage.
  • the ramp generator also includes a transistor 304, a capacitor 306, and a constant current source comprising an operational amplifier 308 and a transistor 310.
  • the capacitor 306 is slowly charged by the constant current source .via the transistor 310 when the transistor 304 is nonconducting and is quickly discharged through the transistor 304 when the transistor 304 becomes conductive.
  • the transistor 304 conducts when the value of the REFl signal is less than the predetermined voltage provided at the noninverting input of the comparator 302. As a result, a ramp signal is produced on the line 312.
  • the ramp signal is input to the noninverting input of a comparator 314 via the line 312.
  • the inverting input of the comparator 314 is supplied with a ⁇ signal having a magnitude based upon the ⁇ e signal.
  • the comparator 314 generates on a line 316 a comparison signal having a high output when the value of the ramp signal is greater than ⁇ _ and a low output when the value of the ramp signal is less than the value of ⁇ _.
  • the comparison signal on line 316 is provided to a monostable multivibrator, or one-shot 318 comprising three inverters and a capacitor.
  • the output of the one-shot 318 is the RES2 signal, which determines the phase angle between the waveforms of the first subinverter pair 30 and the waveforms of the second subinverter pair 32.
  • the RES3 signal is generated in a similar manner.
  • a second ramp generator comprises a comparator 332 having an inverting input that receives the REF2 signal and a noninverting input that receives the reference voltage.
  • the second ramp generator also includes a transistor 334, a capacitor 336, and a constant current source comprising an operational amplifier 338 and a transistor 340.
  • the capacitor 336 is slowly charged by the constant current source via the transistor 340 when the transistor 334 is not conducting and is quickly discharged through the transistor 334 when the transistor 334 conducts.
  • the transistor 334 conducts when the value of the REF2 signal is less than the predetermined voltage provided at the noninverting input of the comparator 332. As a result, a ramp signal is produced on the line 342.
  • the ramp signal is input to the noninverting input of a comparator 344 via the line 342.
  • the inverting input of the comparator 344 is supplied with the ⁇ signal.
  • the comparator 344 generates on a line 346 a comparison signal having a high output when the value of the ramp signal is greater than ⁇ and a low output when the value of the ramp signal is less than the value of ⁇ _ .
  • the comparison signal on line 346 is provided to a one-shot 348 comprising three inverters and a capacitor.
  • the output of the one-shot 348 is the RES3 signal which determines the phase angle between the waveforms of the second subinverter pair 32 and the waveforms of the third subinverter pair 34.
  • the magnitude of the ⁇ and ⁇ signals is determined by a third portion of the phase angle control circuit 52 shown in the bottom of Figure 12, based upon the magnitude of the ⁇ c signal.
  • the ⁇ signal is generated by an operational amplifier 350 that acts as a voltage follower. Thus, the output of the amplifier 350 follows the magnitude of the ⁇ c signal.
  • a zener diode 352 is connected to the output of the amplifier 350 and acts to limit the magnitude of the ⁇ c3 signal to a maximum predetermined value. This predetermined value is the voltage that causes a 120° phase angle difference between the second and third subinverter pair waveforms. ⁇
  • the ⁇ _ signal is generated by an operational amplifier 354 that acts as an inverter.
  • the ⁇ c signal is supplied to the noninverting input of the amplifier 354, while a predetermined voltage signal is supplied to its inverting input.
  • the predetermined voltage is produced by an operational amplifier 356 having its noninverting input connected to a reference source 358.
  • the ⁇ c signal is generated by the output sensing circuit 50 based upon the current and voltage sensed on the transformer output lines 28a-c.
  • the output sensing circuit 50 is shown in detail in Figure
  • the output sensing circuit 50 includes a first portion shown at the bottom of Figure 13 that generates a voltage based on the amount of current sensed in the lines 56a, 56b, 56c.
  • the three phases of output current, I ⁇ .A.,' I ⁇ .B ⁇ , I ⁇ .C Conduct, on the lines 56a, 56b,' 56c,' respectively, are rectified by a half-wave rectifier circuit 360.
  • the output of the half-wave rectifier circuit 360 is filtered by a smoothing capacitor 362 and then provided to the inverting input of a operational amplifier 364 used for scaling purposes.
  • the output of the operational amplifier 364 is passed through a zener diode 366 which is coupled to the inverting input of an operational amplifier 368 that acts as an inverter.
  • the operational amplifier 368 generates a negative voltage, -I 0 , that is zero if the amount of current sensed in the lines 56a, 56b, 56c is not above a predetermined threshold.
  • the current threshold corresponds to twice the rated current for the power conversion system 10. If the current sensed is above the threshold, then the magnitude of -I 0 is proportional to the amount of current over the threshold, or overcurrent.
  • the -I grill signal is transmitted to a summing point 370 via a line 372.
  • the upper portion of the output sensing circuit 50 comprises three precision full-wave rectifiers 390, 392, 394 coupled to receive the phase voltages, V 0.A. , V0._B, on the lines 58a, 58b, 58c, respectively.
  • the rectified phase voltages are summed at the inverting input of an operational amplifier 400.
  • the operational amplifier 400 generates a negative voltage at its output, -V 0 , which has a magnitude that is proportional to the average output voltage sensed on the lines 58a, 58b, 58c.
  • the -V 0 signal is transmitted to the summing point 370.
  • the summing point 370 is also connected to a circuit 402 that generates a predetermined reference voltage, V f .
  • the V f voltage represents the desired voltage at which the transformer output lines 28a-c should be kept.
  • V of and -I household signals are summed to produce an error sig •3 nal, i Verr,' which eq ⁇ uals Vref_ - I textile° - V afford°.
  • the value of -I 0 will be zero, and the error signal will equal V _ - V 0 .
  • I 0 will be a nonzero value, and it will effectively reduce the magnitude of the predetermined voltage, V _ . If the overcurrent is large enough, the magnitude of I 0 will become as larg ⁇ e as Vref., and the effective reference voltage, V , - I 0 , will become zero.
  • the actual voltage V 0 will be reduced to zero.
  • the amount of sensed current necessary to reduce the effective reference voltage to zero is three times the rated current for the system 10.
  • the output voltage on the lines 28a-c drops to zero.
  • the summed error voltage at the summing point 370 is input to the inverting input of an operational amplifier 404 which integrates the error.
  • the amplifier 404 is coupled to an operational amplifier 406 that acts as a buffer and which produces the ⁇ . signal, which ultimately determines the phase relationships of the waveforms generated by the three subinverter pairs 30, 32, 34.
  • the magnitude of the phase control signals ⁇ and ⁇ _ is shown in the two modes of operation of the inverter 24 with respect to the magnitude of the ⁇ c signal.
  • the ⁇ signal has a constant voltage that produces a phase angle of 15° between the waveforms of the first subinverter pair 30 and the waveforms of the second subinverter pair 32.
  • the ⁇ signal has a voltage that gradually increases to cause a gradually increasing phase angle between the second and third subinverter pair waveforms, until it hits a peak voltage sufficient to cause a 120° phase angle.
  • the voltage of the ⁇ signal stays at its peak, and the voltage of the ⁇ signal gradually increases until it reaches a maximum voltage sufficient to cause a phase angle of 120° between the waveforms of the first subinverter pair 30 and the waveforms of the second subinverter pair 32.
  • the soft-start circuit 150 shown in Figure 4 is used to drive the subinverter switches 82, 84, 94, 96 at a relatively high frequency during a start-up mode of the inverter 24, prior to the steady-state mode of the inverter 24, to reduce undesirable inrush currents.
  • Figure 15 shows the waveforms on the designated conductors of Figure 4.
  • the soft-start circuit 150 in Figure 4, includes an oscillator 450 that supplies a relatively high frequency, 50% duty cycle signal, Figure 15, to a monostable multivibrator, or one shot 452, via a line 454.
  • the one shot 452 which has a relatively short activation time, generates an output signal on a line 456 having a frequency one-half that of the oscillator output and a duty cycle of approximately 70%.
  • the output signals generated by the oscillator 450 on the line 454 and the one shot 452 on the line 456 are shown in Figure 15.
  • the relatively high frequency signal generated by the one shot 452 is provided to one input of an AND gate 460 via the line 456.
  • the other input of the AND gate 460 is provided with a logic signal on line 474 defining the duration of the start-up mode of operation. That signal is generated by a start signal that is provided to a one shot 470 via a line 472.
  • the rising edge of the start signal defines the beginning of the inverter start-up period, and the end of the start-up period is determined by the falling edge of the signal generated by l the one shot 470 on a first of its two output lines 474.
  • the second output line 476 of the one shot is complemented with respect to its output on the line 474.
  • the start-up signal on the line 472 and both outputs of the one shot 470 are shown in Figure 15.
  • the AND gate performs a logical "and" ' of the two signals provided on the lines 456 and 474 and provides the result on its output line 480.
  • the signal on the line 480 which is shown in Figure 15, is identical to the relatively high frequency signal generated by the one shot 460 during the start-up period, but is zero outside the start-up period.
  • Some additional processing is performed on the signal 480.
  • the purpose of the additional processing is to change the value of the signal 480 from logical "0" to a logical "1" after the completion of the start-up period.
  • This additional processing is performed by an OR gate 484 coupled to an AND gate 486.
  • the OR gate 484 has a first input connected to receive the signal 480 and a second input connected to receive the signal 476.
  • the logical "or” of those two signals is provided by the OR gate 484 to a first input of the AND gate 486 via a line 488.
  • the second input of the AND gate 486 is provided with the start signal via the line 472.
  • the logical "and" of the signals 472, 488 is provided from the AND gate 486 to a buffer 510 via a line 512.
  • the signals on the lines 488 and 512 are shown in Figure 15.
  • the signal 512 which has a relatively high frequency during the start-up period and is logic "1" after the start-up period, is connected through buffer 510 to inputs of driver 118.
  • Driver 118 performs a logical "and” function between the output of buffer 510 and each of the signals on lines 122, 130, 132, 134, 136, 138.
  • Figure 15 shows how driver 118 performs this function using the signal on line 122 as an example.
  • Driver 118 "ands" the soft-start pulses on line 512 with the control pulses on line 122.
  • the signal on output 124 from driver 118 is comprised of the pulses on line 512 while the signal on line 122 is a logical "1.”
  • the soft-start pulses no longer appear on line 124 and line 124 is a logical "0.”
  • the next logical "1" on line 122 occurs after the soft- start pulses having ceased and the output from AND gate 486 remains at a logical "1.” Accordingly, the control pulses on line 122 now appear on output 124 from driver 118.
  • soft-start pulses appear on line 124, they are inverted and appear on line 126 as the complement of the pulses on line 124.
  • the pair of driver 118 outputs associated with line 130 also carry complemented and uncomplemented soft-start pulses as does the pair of driver 118 outputs associated with line 132 and so on.
  • the number of soft-start pulses appearing on any particular pair of driver 118 outputs will depend upon the phase relationship between the signal on the EPROM 116 output line associated with that pair and the soft-start pulses 512 appearing at the output of buffer 510.
  • the frequency of soft-start pulses is higher than the frequency of the control pulses.
  • the frequency of the soft-start pulses 512 may be on the order of 14.4 KHz, whereas the control pulses 122 may have a frequency on the order of 400 Hz. These frequencies are by way of example only and any desired frequencies may be used as long as the frequency of the soft-start pulses is higher than the frequency of the control pulses.

Abstract

The present invention is directed to an arrangement for limiting inrush current in an inverter system (10) having inverter switches (82a-c, 84a-c, 94a-c, 96a-c) for inverting DC to AC, a soft-start pulse supply circuit (150) for supplying soft-start pulses to the inverter switches (82a-c, 84a-c, 94a-c, 96a-c) to begin the inverter process, and a controller (110-118) for supplying normal control pulses to the inverter switches (82a-c, 84a-c, 94a-c, 96a-c) after a predetermined amount of time. The soft-start pulses have a higher frequency than the normal control pulses. The soft-start pulses may have a substantially constant duty cycle and amplitude and the frequency of the soft-start pulses also may be substantially constant.

Description

POWER GENERATION SYSTEM WITH SOFT-START CIRCUIT
TECHNICAL FIELD
The present invention is directed to a power generation system for an aircraft having a stepped- waveform inverter of the type used to generate AC power from DC power and a soft-start circuit to reduce undesirable inrush currents during start-up of the inverter.
BACKGROUND ART
Power generation systems, such as variable- speed, constant-frequency (VSCF) power conversion systems, are commonly used to generate AC and DC power. In one such application, variable-frequency AC power may be produced by a brushless, synchronous generator driven by a jet engine. The variable-frequency AC power is converted to DC power by an AC/DC converter, such as a rectifier bridge. An inverter is coupled to the AC/DC converter to transform the DC power into constant-frequency AC power, which is then filtered by a filter. The filtered AC output is then provided to an AC load bus which supplies power to various loads. The inverter used in VSCF systems may be of the εtepped-wavefor type. An inverter of this type is disclosed in U.S. Patent No. 3,775,662 to Co poly et al. Such a stepped-waveform inverter generates an output having a stepped shape that generally approximates a sine wave. The purpose of approximating a sine wave is to reduce the size of the filters, provided at the output of the inverter, that are used to remove unwanted harmonics. Power conversion systems often rely upon saturable reactors such as inductive-type filters or transformers. When the power conversion system is first initiated to begin the power conversion process, the sudden application of power to the saturable reactor may cause it to saturate providing little impedance to current. This current faced with little impedance can become quite large and can possibly damage elements of the power conversion system such as its inverter switches. In order to prevent such damage, it is desired to limit or inhibit this inrush current.
SUMMARY OF THE INVENTION
The present invention is directed to an arrangement for limiting inrush current. Accordingly, an inverter system is provided having inverter switches for inverting DC to AC. A soft-start pulse supply circuit supplies soft-start pulses to the inverter switches to begin the inverter process. After a time, a controller takes over and supplies normal control pulses to the inverter switches. The soft-start pulses have a higher frequency than the normal control pulses.
The soft-start pulses may have a substantially constant duty cycle and amplitude and the frequency of the soft-start pulses also may be substantially constant.
An excitation circuit may be provided to supply the soft-start pulses. The excitation circuit has a monostable multivibrator for providing a timing pulse initiated at start-up of the inverter system for controlling the number of soft-start pulses supplied to the inverter switches. The inverter switches may be used to energize the primary windings of two transformers, the second windings of which are interconnected so that voltages induced therein are added.
BRIEF DESCRIPTION OF THE DRAWINGS
Other features and other advantages of the present invention will become more apparent from a detailed consideration of the invention when taken in conjunction with the drawings in which: Figure 1 is a block diagram of a VSCF power conversion system in which the present invention can be used;
Figure 2 is a block diagram of the inverter of Figure 1; Figure 3 is a circuit diagram of one pair of subinverters and their associated transformers of the inverter of Figure 2;
Figure 4 is a circuit diagram of one of the activation circuits of Figure 2; Figure 5 illustrates a first phase relationship of a number of waveforms generated by the inverter and a waveform produced by the summation of those waveforms;
Figure 6 illustrates a second phase relationship of a number of waveforms generated by the inverter and a waveform produced by the summation of those waveforms;
Figure 7 illustrates a third phase relationship of a number of waveforms generated by the inverter and a waveform produced by the summation of those waveforms;
Figure 8 illustrates a fourth phase relationship of a number of waveforms generated by the inverter and a waveform produced by the summation of those waveforms;
Figures 9a-9c are vector diagrams illustrating a first mode of operation of the inverter of the invention;
Figures lOa-lOc are vector diagrams illustrating a second mode of operation of the inverter of the invention;
Figure 11 illustrates various waveforms relating to the operation of the phase angle control circuit of Figure 2;
Figure 12 is a circuit diagram of the phase angle control circuit shown schematically in Figure 2;
Figure 13 is a circuit diagram of the output sensing circuit shown schematically in Figure 2;
Figure 14 is a graph of two voltage signals used in the phase angle control circuit to control the phase relationship of the waveforms generated by the inverter; and Figure 15 is an illustration of a number of waveforms generated during operation of the activation circuit shown in Figure 4.
DESCRIPTION OF THE PREFERRED EMBODIMENT
A block diagram of a preferred embodiment of a VSCF power conversion system 10 incorporating the present invention is shown in Figure 1. The power conversion system 10 includes a prime mover 12 coupled to a generator 14 for generating variable-frequency AC power. An AC/DC converter 16 is coupled to the generator 14 for converting the variable-frequency AC power into DC power. The DC output of the AC/DC converter 16 is supplied to various DC loads via a pair of lines 20a, 20b. A second pair of lines 22a, 22b provides the DC to an inverter 24, which generates three-phase, constant-frequency AC power from this DC. The inverter 24 is coupled to a filter 26 via three output lines 28a, 28b, 28c, each of which supplies a respective phase of the constant-frequency AC output to the filter 26. The output of the filter 26 is provided via lines 29 to a three-phase AC load bus which supplies AC power to various AC loads.
A block diagram of the inverter 24 is shown in Figure 2. The inverter 24 includes three subinverter pairs 30, 32, 34, although any number of subinverters may be used. Each of the subinverter pairs 30, 32, 34 is coupled to a respective transformer pair 31, 33, 35. The output lines 28a, 28b, 28c interconnect each of the transformer pairs 31, 33, 35, and the transformer pair 35 is connected to a neutral line 28d. Each of the subinverter pairs 30, 32, 34 is controlled by a respective activation circuit 40a-c. A regulator circuit for regulating the voltage on the transformer output lines 28a, 28b, 28c is shown to comprise an output sensing circuit 50 and a phase angle control circuit 52. The output sensing circuit 50 senses the current on the three transformer output lines 28a, 28b, 28c via three lines 56a, 56b, 56c, and the sensing circuit 50 senses the voltage on the three output lines 28a, 28b, 28c via three lines 58a, 58b, 58c. The output sensing circuit 50 generates a phase control signal, φc , having a magnitude based on both the voltage and current sensed on the lines 28a-c and provides the φ_ signal to the phase control circuit 52 via a line 60. Based on the magnitude of the φc signal, the phase angle control circuit 52,causes the phase angles between the various waveforms generated by the three subinverter pairs 30, 32, 34 to be varied. As a result of the control of the phase angles, the magnitude of the voltage on the transformer output lines 28a, 28b, 28c is regulated.
Alternatively, instead of sensing the AC output on the lines 28a-c, the regulator circuit could sense the AC output on the lines 29 after the AC output is filtered by the filter 26.
The phase angle control circuit 52 varies the magnitude of the phase angles by generating a pair of reset signals, RES2 and RES3, based upon the magnitude of the phase control signal φc and a pair of reference signals, REF1 and REF2. The REF1 and REF2 signals are transmitted to the phase angle control circuit 52 from the first and second activation circuits 40a, 40b via a pair of lines 66, 68, respectively. The RES2 and RES3 signals are transmitted from the phase angle control circuit 52 to the second and third activation circuits 40b, 40c via a pair of lines 70, 72, respectively. As described in more detail below, the RES2 signal controls the phase angle between the waveforms generated by the first subinverter pair 30 and the waveforms generated by the second subinverter pair 32, and the RES3 signal controls the phase angle between the waveforms generated by the second subinverter pair 32 and the waveforms generated by the third subinverter pair 34.
The first subinverter pair 30 and the first transformer pair 31 are shown in Figure 3. The first subinverter pair 30 includes two subinverters 30a, 30b, and the first transformer pair 31 includes two three- phase transformers 31a, 31b.
The subinverter 30a includes six transistor switches 82a-c, 84a-c, each of which has a diode connected across it. The subinverter 30a is connected to three wye-connected primary windings 80a-c of the transformer 31a which are controlled by the three pairs of switches 82a-c, 84a-c, although these windings alternatively may be delta connected. The upper terminal of the winding 80a is connected to the junction of the switches 82a, 84a; the upper terminal of the winding 80b is connected to the junction of the switches 82b, 84b; and the upper terminal of the winding 80c is connected to the junction of the switches 82c, 84c. The bottom terminals of windings 80a, 80b, 80c are connected together. The primary windings 80a-c of the transformer 31a are inductively coupled to three secondary windings 90a-c, respectively.
During operation of the subinverter 30a, exactly one of the two switches in each vertical branch is conducting. In particular, one of the two switches 82a, 84a is conducting and the other is off; one of the switches 82b, 84b is conducting and the other is off; and one of the switches 82c, 84c is conducting and the other is off. The switches 82a-c and 84a-c are switched in a conventional manner to generate the waveform 220 in Figure 5 on each of the three wye- connected windings 80a-c, each of the three waveforms differing in phase by 120°. Because the windings 80a-c are wye connected, the waveform 220 has five possible amplitudes at any point in time, +A, +A/2, 0, -A/2, and -A, where A is the maximum amplitude.
The subinverter 30b includes six transistor switches 94a-c, 96a-c, each of which has a diode connected across it. The subinverter 30b is connected to three delta-connected primary windings 92a-c of the transformer 31b which are controlled by the three pairs of switches 94a-c, 96a-c, although these windings may be alternatively wye connected. The upper terminal of the winding 92a is connected to the junction of the switches 94a, 96a and to the bottom terminal of winding 92c; the upper terminal of the winding 92b is connected to the junction of the switches 94b, 96b and to the bottom terminal of winding 92a; and the upper terminal of the winding 92c is connected to the junction of the switches 94c, 96c and to the bottom terminal of winding 92b. The three delta-connected primary windings 92a-c are inductively coupled to three secondary windings 98a-c of the transformer 31b, respectively.
The switches 94a-c and 96a-c are switched in a manner similar to switches 82a-c and 84a-c to generate the waveform 222 in Figure 5 on each of the three delta-connected windings 92a-c, each of the three waveforms 222 having a phase difference of 120°. Because the windings are delta connected, such a waveform has three possible amplitudes, +A, 0, and -A, where A is the maximum amplitude.
While the switches 82a-c, 84a-c, 94a-c, 96a-c are shown to be transistors, other types of switches may be used, such as thyristors or D'Λrlington- connected transistor pairs.
The circuit diagrams for the second and third subinverter pairs 32, 34 and the second and third transformer pairs 33, 35 are identical to the one shown in Figure 3 and are not shown separately for purposes of simplicity.
The activation of the twelve switches 82a-c, 84a-c, 94a-c, 96a-c in each of the subinverter pairs 30r 32, 34 is controlled by a respective one of the activation circuits 40a-c. Since the three activation circuits 40a-c are substantially identical, only one is shown. Referring to Figure 4r the activation circuit 40 includes three four-bit counters 110, 112, 114 connected to an EPRO 116 which in turn is connected to a driver circuit 118. The counters '110, 112, 114 are driven by a clock signal, CLK, generated by a main controller (not shown) . The carry output of the counter 110 is input to the counter 112 via a line 111, and the carry output of the counter 112 is input to the counter 114 via a line 113. Upon each pulse of the CLK signal, the 10-bit output of the counters 110, 112, 114 is incremented by one. This 10-bit output is used as an address to address the EPROM 116.
The EPROM 116 has a six-bit binary code stored in each of its address locations. The six binary bits control the activation of the 12 switches in one of the subinverters. In particular, one bit of the six-bit binary code is output on the line 122 to the driver 118, which generates an uncomplemented switching signal on a line 124 and a complemented switching signal on a line 126. The line 124 is connected to the base of one transistor in one vertical branch of one of the subinverters, such as switch 82a, and the line 126 is connected to the base of the other switch in the vertical branch, such as switch 84a. The remaining five bits of the six-bit binary code are output on the lines 130, 132, 134, 136, 138, respectively, to the driver circuit 118, which generates on its outputs a pair of complemented driving signals for each of the five binary signals. These driving signals are supplied to the remaining switches of the subinverter.
During operation of each of the activation circuits 40, as the CLK signal periodically increments the counters 110, 112, 114, the six bits of the binary code are periodically output from the EPROM 116 via lines 122, 130-138 to the driver 118, and the 12 switches of each corresponding subinverter pair 30a/30b, 32a/32b, and 34a/34b are controlled to generate each corresponding pair of the waveforms 220/222, 224/226, and 228/230 shown in Figure 5 on the primary windings of the corresponding transformers 31a/31b, 33a/33b, and 35a/35b.
The EPROM 116 generates a reference signal, REF, on a line 142. As described in more detail below, the REF signal is used as a phase reference signal. A reset signal, RES, may be input to the counters 110, 112, 114 via a line 140. When the RES signal is activated, the counters 110, 112, 114 are reset, thus providing a 10-bit address to the EPROM 116 equal to zero. The contents of each EPROM in the three activation circuits 40a-c are identical. If each of the EPROMs is given the same sequence of addresses, the resulting waveforms generated by the subinverters would be identical and thus have zero phase angle. Accordingly, the time of reset of the counters 110, 112, 114 of an activation circuit determines the phase angle between the waveforms generated by that activation circuit and the waveforms generated by the other two activation circuits. When the activation circuit 40 of Figure 4 is used for the activation circuit 40a shown in Figure 2, the REF line 142 of Figure 4 is connected to the REF1 line 66 of Figure 2, and the RES line 140 of Figure 4 is not used. When the activation circuit 40 of Figure 4 is used for the activation circuit 40b, the REF line 142 of Figure 4 is connected to the REF2 line 68 of Figure 2, and the RES line 140 of Figure 4 is connected to the RES2 line 70 of Figure 2. When the activation circuit 40 of Figure 4 is used for the activation circuit 40c, the RES line 140 of Figure 4 is connected to the RES3 line 72 of Figure 2, and the REF line 142 of Figure 4 is not used. •
The activation circuit 40- has a soft-start circuit 150 which, as described in more detail below, is used during a start-up period of the inverter 24 to reduce undesirable inrush currents.
Stepped-waveform inverters having six subinverters as shown in Figure 2 are referred to as 36-step inverters.
Referring to Figure 5, the waveforms generated by one phase of the subinverters 30a, 30b, 32a, 32b, 34a, 34b in the corresponding phase of the primary windings of the transformers 31a, 31b, 33a, 33b, 35a, 35b are shown. The summing transformer output waveform 240 shown in the bottom portion of Figure 5 is generated on each of the three transformer output lines 28a, 28b, 28c, each of the three waveforms 240 being 120° apart. The waveform 240 represents the summation of the waveforms 220, 222, 224, 226, 228, 230.
The inverter 24 of the present invention has two modes of operation during steady-state operation. A first mode of operation is used when the current on the output lines 28a-c of the summing transformer is below a predetermined threshold. A second mode of operation is used when the output current is above the predetermined threshold.
In the first mode of operation, the phase angle between the waveforms generated by the first subinverter pair 30 and the waveforms generated by the second subinverter pair 32 is held constant, preferably 15°, and the phase angle between the waveforms generated by the second subinverter pair 32 and waveforms generated by the third subinverter pair 34 is varied, depending upon the output voltage sensed on the transformer output lines 28a-c. ,
The waveforms shown in Figures 5 and 6 illustrate the first mode of operation. It should be noted that the first subinverter pair waveforms 220, 222 and the second subinverter pair waveforms 224, 226 of both Figures 5 and 6 have a fixed phase angle of 15°. However, the phase angle between the second subinverter pair waveforms 224, 226 and the third subinverter pair waveforms 228r 230 is 0° in Figure 5 and 60° in Figure 6. By controlling the phase angle between the second and third subinverter pair wave¬ forms, the resultant output voltage may be regulated. For example, the waveform 240 of Figure 5 has a peak positive amplitude of +6A and a peak negative amplitude of -6A, whereas the output voltage waveform 240 of Figure 6 has a peak positive amplitude of +5 A and a peak negative amplitude of -5 A.
Referring to Figures 9a-9c, the vector diagrams in those figures illustrate the first mode of operation. The vector V, represents the first subinverter pair waveforms 220, 222; the vector V2 represents the second subinverter pair waveforms 224, 226; and the vector V3 represents the third subinverter pair waveforms 228, 230. In each of Figures 9a-c, the phase angle between Vt and V2 is constant, at 15°. The phase angle between V2 and V3 may vary from a minimum phase angle of 0° as shown in Figure 9a to a maximum phase angle of 120° as shown in Figure 9c. In between the minimum and maximum phase angles, the phase angle may be any variable angle a as shown in Figure 9b. The vector positions shown in Figures 9a and 9c represent the extreme phase angles of the first mode of operation, and during normal operation the phase angles will be as shown in Figure 9b.
In the second mode of operation, the phase angle between the waveforms generated by the first and second subinverter pairs is a variable angle between 15° and 120°r while the phase angle between the waveforms generated by the second and third subinverter pairs is held constant, preferably 120°. As a result, the voltage on the transformer output lines is gradually reduced to zero. The second mode of operation is used when the current on the output lines 28a-c is above the predetermined threshold.
The waveforms shown in Figures 7 and 8 illustrate the second mode of operation. In Figures 7 and 8, the third subinverter pair waveforms 228, 230 lag the second subinverter pair waveforms 224, 226 by a constant 120°. However, the phase angle between the first subinverter pair waveforms 220, 222 and the second subinverter pair waveforms 224, 226 is 45° in Figure 7 and 120° in Figure 8. The transformer output voltages, which are represented by the waveforms 240 in Figures 7 and 8, are gradually reduced to zero. In
Figure 7, the amplitude of the waveform 240 reaches a peak amplitude of +3A between 135° and 150° and -3A between 315° and 330°, and in Figure 8 the waveform 240 has zero amplitude. Now referring to Figures lOa-lOc, the vector diagrams in those figures illustrate the second mode of operation. The vector V, represents the first subinverter pair waveforms 220, 222; the vector V2 represents the second subinverter pair waveforms 224, 226; and the vector V3 represents the third subinverter pair waveforms 228, 230. In Figures lOa-lOc, the phase angle between V2 and V3 is constant, at 120°. The phase angle between V, and V2 may vary from a minimum phase angle of 15° as shown in Figure 10a to a maximum phase angle of 120° as shown in Figure 10c. In between the minimum and maximum phase angles, the phase angle may be any variable angle b as shown in Figure 10b.
One manner of controlling the phase angles is illustrated in Figure 11, which illustrates the control of the phase angle between the subinverter 32a waveform 224 and the subinverter 34a waveform 228. Referring to Figure 11, the waveform 224 is shown in its phase relationship with respect to the REF2 signal. As can be seen, REF2 changes from zero to positive when waveform 224 transitions to a positive amplitude and from positive to zero when waveform 224 transitions to a negative amplitude. A ramp signal, RAMP, is generated based upon the magnitude of the REF2 signal. The rising edge of the REF2 signal corresponds to the beginning of the RAMP signal. When the REF2 signal is positive, the amplitude of the RAMP signal slowly increases. When the magnitude of the REF2 signal changes to zero, the magnitude of the RAMP signal quickly decreases to zero. The RAMP signal is used to generate the RES3 signal based on a -phase control signal φ _ generated from the phase control signal φc of Figure 2. The magnitude of the φ signal varies, depending upon the magnitude of the current and voltage sensed on the transformer output lines 28a, 28b, 28c. " The relative values of the RAMP and φ _ signals are used to generate a comparison signal, COMP, having a positive amplitude when the value of the RAMP signal is greater than the value of the φ signal and a zero amplitude when the value of the RAMP signal is less than the value of the φ signal. The point of intersection of the rising portion of the RAMP signal and the φ signal determines the magnitude of the phase delay between the subinverter waveforms. This intersection point is shown as point 260 in Figure 11.
At the intersection point 260, the COMP signal changes from zero to a positive amplitude. The rising edge of the COMP signal triggers the RES3 signal to become positive, or activated. When the RES3 signal is activated, it resets the counters associated with the third subinverter pair 34. As a result, the counters produce a zero 10-bit address, and the EPROM starts to generate the waveform 228. Thus, the time- occurrence of the rising edge of the RES3 signal controls the phase difference between the waveform 224 and the waveform 228. This phase difference is shown in Figure 11 as Δø.
It should be appreciated that the magnitude of the c3 signal determines the magnitude of the phase delay Δø. If the magnitude of φ is larger, the φ signal will intersect the RAMP signal later, thus causing a larger phase delay. If the magnitude of φ is smaller, the φ signal will intersect the RAMP signal earlier, thus causing a smaller phase delay. The manner of varying the phase angle between the first subinverter pair waveforms and the second subinverter pair waveforms is similar to the manner described immediately above, except that the phase angle is between waveforms 220 and 224, REFl is used in place of REF2 , and RES2 is generated instead of RES3. The phase angle control circuit 52 for controlling the phase angles between the three subinverter pairs 30, 32, 34 is shown in Figure 12. The REFl, REF2, and φ. signals are input to the phase angle control circuit 52 via the lines 66, 68, 60, respectively, and the circuit 52 generates the RES2 and RES3 signals on the lines 70, 72, respectively. The circuit 52 includes a ramp generator comprising a comparator 302.having an inverting input which receives the REFl signal and a noninverting input that receives a predetermined reference voltage. The ramp generator also includes a transistor 304, a capacitor 306, and a constant current source comprising an operational amplifier 308 and a transistor 310. The capacitor 306 is slowly charged by the constant current source .via the transistor 310 when the transistor 304 is nonconducting and is quickly discharged through the transistor 304 when the transistor 304 becomes conductive. The transistor 304 conducts when the value of the REFl signal is less than the predetermined voltage provided at the noninverting input of the comparator 302. As a result, a ramp signal is produced on the line 312. The ramp signal is input to the noninverting input of a comparator 314 via the line 312. The inverting input of the comparator 314 is supplied with a ø signal having a magnitude based upon the øe signal. The comparator 314 generates on a line 316 a comparison signal having a high output when the value of the ramp signal is greater than ø _ and a low output when the value of the ramp signal is less than the value of ø _. The comparison signal on line 316 is provided to a monostable multivibrator, or one-shot 318 comprising three inverters and a capacitor. The output of the one-shot 318 is the RES2 signal, which determines the phase angle between the waveforms of the first subinverter pair 30 and the waveforms of the second subinverter pair 32. The RES3 signal is generated in a similar manner. A second ramp generator comprises a comparator 332 having an inverting input that receives the REF2 signal and a noninverting input that receives the reference voltage. The second ramp generator also includes a transistor 334, a capacitor 336, and a constant current source comprising an operational amplifier 338 and a transistor 340.
The capacitor 336 is slowly charged by the constant current source via the transistor 340 when the transistor 334 is not conducting and is quickly discharged through the transistor 334 when the transistor 334 conducts. The transistor 334 conducts when the value of the REF2 signal is less than the predetermined voltage provided at the noninverting input of the comparator 332. As a result, a ramp signal is produced on the line 342.
The ramp signal is input to the noninverting input of a comparator 344 via the line 342. The inverting input of the comparator 344 is supplied with the ø signal. The comparator 344 generates on a line 346 a comparison signal having a high output when the value of the ramp signal is greater than ø and a low output when the value of the ramp signal is less than the value of ø _ . The comparison signal on line 346 is provided to a one-shot 348 comprising three inverters and a capacitor. The output of the one-shot 348 is the RES3 signal which determines the phase angle between the waveforms of the second subinverter pair 32 and the waveforms of the third subinverter pair 34. The magnitude of the ø and ø signals is determined by a third portion of the phase angle control circuit 52 shown in the bottom of Figure 12, based upon the magnitude of the øc signal. The ø signal is generated by an operational amplifier 350 that acts as a voltage follower. Thus, the output of the amplifier 350 follows the magnitude of the øc signal. A zener diode 352 is connected to the output of the amplifier 350 and acts to limit the magnitude of the øc3 signal to a maximum predetermined value. This predetermined value is the voltage that causes a 120° phase angle difference between the second and third subinverter pair waveforms. ι
The ø _ signal is generated by an operational amplifier 354 that acts as an inverter. The øc signal is supplied to the noninverting input of the amplifier 354, while a predetermined voltage signal is supplied to its inverting input. The predetermined voltage is produced by an operational amplifier 356 having its noninverting input connected to a reference source 358. The øc signal is generated by the output sensing circuit 50 based upon the current and voltage sensed on the transformer output lines 28a-c. The output sensing circuit 50 is shown in detail in Figure
13. The output sensing circuit 50 includes a first portion shown at the bottom of Figure 13 that generates a voltage based on the amount of current sensed in the lines 56a, 56b, 56c. The three phases of output current, Iø.A.,' Iø.Bβ, Iø.C„, on the lines 56a, 56b,' 56c,' respectively, are rectified by a half-wave rectifier circuit 360. The output of the half-wave rectifier circuit 360 is filtered by a smoothing capacitor 362 and then provided to the inverting input of a operational amplifier 364 used for scaling purposes. The output of the operational amplifier 364 is passed through a zener diode 366 which is coupled to the inverting input of an operational amplifier 368 that acts as an inverter. The operational amplifier 368 generates a negative voltage, -I0, that is zero if the amount of current sensed in the lines 56a, 56b, 56c is not above a predetermined threshold. The current threshold corresponds to twice the rated current for the power conversion system 10. If the current sensed is above the threshold, then the magnitude of -I0 is proportional to the amount of current over the threshold, or overcurrent. The -I„ signal is transmitted to a summing point 370 via a line 372. The upper portion of the output sensing circuit 50 comprises three precision full-wave rectifiers 390, 392, 394 coupled to receive the phase voltages, V 0.A. , V0._B, on the lines 58a, 58b, 58c, respectively. The rectified phase voltages are summed at the inverting input of an operational amplifier 400.
The operational amplifier 400 generates a negative voltage at its output, -V0, which has a magnitude that is proportional to the average output voltage sensed on the lines 58a, 58b, 58c. The -V0 signal is transmitted to the summing point 370.
The summing point 370 is also connected to a circuit 402 that generates a predetermined reference voltage, V f . The V f voltage represents the desired voltage at which the transformer output lines 28a-c should be kept. At the summing point 370, the V _, -
Vof and -I„ signals are summed to produce an error sig•3nal,i Verr,' which eq^uals Vref_ - I„° - V„°. In normal operation, when the magnitude of the summing transformer output current is below the predetermined current threshold, the value of -I0 will be zero, and the error signal will equal V _ - V0. However, if the output current exceeds the threshold, then I0 will be a nonzero value, and it will effectively reduce the magnitude of the predetermined voltage, V _ . If the overcurrent is large enough, the magnitude of I0 will become as larg^e as Vref., and the effective reference voltage, V , - I0, will become zero. As a result, the actual voltage V0 will be reduced to zero. The amount of sensed current necessary to reduce the effective reference voltage to zero is three times the rated current for the system 10. Thus, when the current reaches three times the rated current, the output voltage on the lines 28a-c drops to zero.
The summed error voltage at the summing point 370 is input to the inverting input of an operational amplifier 404 which integrates the error. The amplifier 404 is coupled to an operational amplifier 406 that acts as a buffer and which produces the φ. signal, which ultimately determines the phase relationships of the waveforms generated by the three subinverter pairs 30, 32, 34.
Referring to Figure 14 , the magnitude of the phase control signals ø and ø _ is shown in the two modes of operation of the inverter 24 with respect to the magnitude of the øc signal. During the first mode, the ø signal has a constant voltage that produces a phase angle of 15° between the waveforms of the first subinverter pair 30 and the waveforms of the second subinverter pair 32. In this mode the ø signal has a voltage that gradually increases to cause a gradually increasing phase angle between the second and third subinverter pair waveforms, until it hits a peak voltage sufficient to cause a 120° phase angle.
During the second mode of operation, the voltage of the ø signal stays at its peak, and the voltage of theø signal gradually increases until it reaches a maximum voltage sufficient to cause a phase angle of 120° between the waveforms of the first subinverter pair 30 and the waveforms of the second subinverter pair 32.
THE SOFT-START CIRCUIT
The soft-start circuit 150 shown in Figure 4 is used to drive the subinverter switches 82, 84, 94, 96 at a relatively high frequency during a start-up mode of the inverter 24, prior to the steady-state mode of the inverter 24, to reduce undesirable inrush currents. Figure 15 shows the waveforms on the designated conductors of Figure 4.
The soft-start circuit 150, in Figure 4, includes an oscillator 450 that supplies a relatively high frequency, 50% duty cycle signal, Figure 15, to a monostable multivibrator, or one shot 452, via a line 454. The one shot 452, which has a relatively short activation time, generates an output signal on a line 456 having a frequency one-half that of the oscillator output and a duty cycle of approximately 70%. The output signals generated by the oscillator 450 on the line 454 and the one shot 452 on the line 456 are shown in Figure 15.
The relatively high frequency signal generated by the one shot 452 is provided to one input of an AND gate 460 via the line 456. The other input of the AND gate 460 is provided with a logic signal on line 474 defining the duration of the start-up mode of operation. That signal is generated by a start signal that is provided to a one shot 470 via a line 472. The rising edge of the start signal defines the beginning of the inverter start-up period, and the end of the start-up period is determined by the falling edge of the signal generated by lthe one shot 470 on a first of its two output lines 474. The second output line 476 of the one shot is complemented with respect to its output on the line 474. The start-up signal on the line 472 and both outputs of the one shot 470 are shown in Figure 15. The AND gate performs a logical "and"' of the two signals provided on the lines 456 and 474 and provides the result on its output line 480. The signal on the line 480, which is shown in Figure 15, is identical to the relatively high frequency signal generated by the one shot 460 during the start-up period, but is zero outside the start-up period.
Some additional processing is performed on the signal 480. The purpose of the additional processing is to change the value of the signal 480 from logical "0" to a logical "1" after the completion of the start-up period. This additional processing is performed by an OR gate 484 coupled to an AND gate 486. The OR gate 484 has a first input connected to receive the signal 480 and a second input connected to receive the signal 476. The logical "or" of those two signals is provided by the OR gate 484 to a first input of the AND gate 486 via a line 488. The second input of the AND gate 486 is provided with the start signal via the line 472. The logical "and" of the signals 472, 488 is provided from the AND gate 486 to a buffer 510 via a line 512. The signals on the lines 488 and 512 are shown in Figure 15.
The signal 512, which has a relatively high frequency during the start-up period and is logic "1" after the start-up period, is connected through buffer 510 to inputs of driver 118. Driver 118 performs a logical "and" function between the output of buffer 510 and each of the signals on lines 122, 130, 132, 134, 136, 138. Figure 15 shows how driver 118 performs this function using the signal on line 122 as an example. Driver 118 "ands" the soft-start pulses on line 512 with the control pulses on line 122. Accordingly, the signal on output 124 from driver 118 is comprised of the pulses on line 512 while the signal on line 122 is a logical "1." When the signal on line 122 switches to a logical "0," however, the soft-start pulses no longer appear on line 124 and line 124 is a logical "0." The next logical "1" on line 122 occurs after the soft- start pulses having ceased and the output from AND gate 486 remains at a logical "1." Accordingly, the control pulses on line 122 now appear on output 124 from driver 118.
While soft-start pulses appear on line 124, they are inverted and appear on line 126 as the complement of the pulses on line 124. Similarly, the pair of driver 118 outputs associated with line 130 also carry complemented and uncomplemented soft-start pulses as does the pair of driver 118 outputs associated with line 132 and so on. However, the number of soft-start pulses appearing on any particular pair of driver 118 outputs will depend upon the phase relationship between the signal on the EPROM 116 output line associated with that pair and the soft-start pulses 512 appearing at the output of buffer 510. The frequency of soft-start pulses is higher than the frequency of the control pulses. For example, the frequency of the soft-start pulses 512 may be on the order of 14.4 KHz, whereas the control pulses 122 may have a frequency on the order of 400 Hz. These frequencies are by way of example only and any desired frequencies may be used as long as the frequency of the soft-start pulses is higher than the frequency of the control pulses.
Modifications and alternative embodiments of the invention will be apparent to those skilled in the art in view of the foregoing description. Accordingly, this description is to be construed as illustrative only, and is for the purpose of teaching those skilled in the art the best mode of carrying out the invention. The details of the structure may be varied substantially without departing from the spirit of the invention, and the exclusive use of all modifications which come within the scope of the appended claims is reserved.

Claims

WHAT IS CLAIMED IS:
1. An inverter system comprising: inverter switching means having an inverter input for receiving DC and an inverter output, said inverter switching means inverting DC at said inverter input to AC and providing said AC at said inverter output, said inverter switching means including switches having control terminals for controlling conduction of said switches; control means for supplying switch control pulses, said switch control pulses having a first frequency; soft-start means for supplying soft-start pulses, said soft-start pulses having a second frequency, said second frequency being substantially constant, said soft-start pulses having a substantially constant duty cycle and substantially constant amplitude, said second frequency being higher than said first frequency; and pulse control means for supplying only said soft-start pulses and said switch control pulses to said control terminals of said switches, said pulse control means supplying a plurality of said soft-start pulses to said control terminals during a predetermined amount of time at start up and then supplying said switch control pulses to said control terminals thereaf er.
2. The inverter system of claim 1 wherein said soft-start means comprises oscillator means for providing oscillator pulses having said second frequency and timing means responsive to said oscillator means for supplying said soft-start pulses to said pulse control means during said predetermined amount of time.
3. The inverter system of claim 2 wherein said oscillator means comprises an oscillator connected to a first monoεtable multivibrator for supplying said oscillator pulses, and wherein said timing means comprises a second monostable multivibrator and logic gate means, said second monostable multivibrator providing a timing pulse having a length determining said predetermined amount of time, said logic gate means being responsive to said timing pulse and to said oscillator pulses for supplying said soft-start pulses.
4. The inverter system of claim 3 wherein said logic gate means comprises a first AND gate having one input for receiving said oscillator pulses, a second input for receiving said timing pulse, and an output, an OR gate having one input connected to said output of said first AND gate, a second input for receiving an inversion of said timing pulse, and an output, and a second AND gate having one input connected to said output of said OR gate, a second input for receiving a signal indicating start up of said inverter, and output means connected to said pulse control means.
5. The inverter system of claim 4 wherein said inverting switching means comprises a transformer having primary winding means connected to said switches and having secondary winding means for providing said AC.
6. The inverter system of claim 5 wherein said primary winding means comprises first, second and third primary windings and said secondary winding means comprises first, second and third secondary windings, said inverter switching means being arranged to energize said first, second and third primary windings so that three phase AC voltage is induced in said first, second and third secondary windings.
7. The inverter system of claim 4 wherein said inverting switching means comprises first and second transformers having respective primary winding means connected to separate ones of said switches and having respective secondary winding means, said primary winding means of said first transformer inducing a first voltage in said secondary winding means of said first transformer and said primary winding means of said second transformer inducing a second voltage in said secondary winding means of said second transformer, said secondary winding means of said first and second transformers being connected to add said first and second voltages for providing said AC.
8. The inverter system of claim 7 wherein each of said primary winding means comprises first, second and third primary windings and each of said secondary winding means comprises first, second and third secondary windings, said inverter switching means being arranged to energize said first, second and third primary windings of each of said transformers so that three phase AC voltage is induced in said corresponding first, second and third secondary windings.
9. The inverter system of claim 1 wherein said inverting switching means comprises a transformer having primary winding means connected to said switches and having secondary winding means for providing said AC.
10. The inverter system of claim 9 wherein said primary winding means comprises first, second and third primary windings and said secondary winding means comprises first, second and third secondary windings, said inverter switching means being arranged to energize said first, second and third primary windings so that three phase AC voltage is induced in said first, second and third secondary windings.
11. The inverter system of claim 1 wherein said inverting switching means comprises first and second transformers having respective primary winding means connected to separate ones of said switches and having respective secondary winding means, said primary winding means of said first transformer inducing a first voltage in said secondary winding means of said first transformer and said primary winding means of said second transformer inducing a second voltage in said secondary winding means of said second transformer, said secondary winding means of said first and second transformers being connected to add said first and second voltages for providing said AC
12. The inverter system of claim 11 wherein each of said primary winding means comprises first, second and third primary windings and each of said secondary winding means comprises first, second and third secondary windings, said inverter switching means being arranged to energize said first, second and third primary windings of each of said transformers so that three phase AC voltage is induced in said corresponding first, second and third secondary windings.
13. An excitation circuit for use at start up of an inverter, said inverter receiving first pulses for causing said inverter to invert input DC into output AC, said excitation circuit comprising: pulse supply means for supplying second pulses having a frequency greater than said first pulses, said frequency of said second pulses being substantially constant; a monostable multivibrator for providing a relatively long timing pulse at start up; pulse control means coupled to said pulse supply means and to said monostable multivibrator and having an output, said pulse control means supplying said second pulses to said output only during said timing pulse; and pulse selection means for receiving said first and second pulses and for supplying said second pulses to said inverter and then said first pulses thereafter.
14. The excitation circuit of claim 13 wherein said pulse supply means comprises an oscillator and a second monostable coupled to said oscillator for supplying third pulses.
15. The excitation circuit of claim 14 wherein said pulse control means comprises a first AND gate having one input for receiving said third pulses, a second input for receiving. said timing pulse, and an output, an OR gate having one input coupled to said output of said first AND gate, a second input for receiving an inversion of said timing pulse, and an output, and a second AND gate having one input coupled to said output of said OR gate, a second input for receiving a signal indicating start up of said inverter, and output means coupled to said pulse selection means.
16. An inverter system comprising: transformer means having first and second primary winding means and first and second secondary winding means, said first and second secondary winding means being coupled so that voltages induced in said first and second secondary winding means will add; inverter switches coupled to said first and second primary windings means, said inverter switches for controlling supply of DC to said first and second primary winding means so that corresponding first and second voltages are induced in said first and second secondary winding means, said inverter switches having control terminals for controlling conduction of said switches; control means (for supplying switch control pulses, said switch control pulses having a first frequency; soft-start means for supplying soft-start pulses, said soft-start pulses having a second frequency, said second frequency being higher than said first frequency; and pulse control means for supplying said soft- start pulses and said switch control pulses to said control terminals of said switches, said pulse control means supplying a plurality of said soft-start pulses to said control terminals at start up and then connecting said switch control pulses to said control terminals thereafter.
17. The inverter system of claim 16 wherein said soft-start means comprises oscillator means for providing oscillator pulses having said second frequency and timing means responsive to said oscillator means for supplying said soft-start pulses to said pulse control means during said predetermined amount of time.
18. The inverter system of claim 17 wherein said oscillator means comprises an oscillator connected to a first monostable multivibrator for supplying said oscillator pulses, and wherein said timing means comprises a second monostable multivibrator and logic gate means, said second monostable multivibrator providing a timing pulse having a length determining said predetermined amount of time, said logic gate means being responsive to said timing pulse and to said oscillator pulses for supplying said soft-start pulses.
19. The inverter system of claim 18 wherein said logic gate means comprises a first AND gate having one input for receiving said oscillator pulses, a second input for receiving said timing pulse, and an output, an OR gate having one input connected to said output of said first AND gate, a second input for receiving an inversion of said timing pulse, and an output, and a second AND gate having one input connected to said output of said OR gate, a second input for receiving a signal indicating start up of said inverter, and output means connected to said pulse control means.
PCT/US1993/004655 1992-05-13 1993-05-13 Power generation system with soft-start circuit WO1993023916A1 (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007004817A1 (en) * 2007-01-31 2008-08-07 Siemens Ag contraption
US8804383B2 (en) 2012-03-09 2014-08-12 Delta Electronics, Inc. Starter of grid-connected inverter and control method thereof
CN109038795A (en) * 2018-07-20 2018-12-18 上海空间电源研究所 For electrically separated interlock protection and soft-switching device and method

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3264548A (en) * 1961-04-18 1966-08-02 Westinghouse Brake & Signal D. c. to a. c. inverter circuits
US3333179A (en) * 1964-05-12 1967-07-25 Jefferson Electric Co Parallel inverter having higher frequency at start-up
US3350625A (en) * 1963-10-28 1967-10-31 Trw Inc Pulse controlled 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
US3401327A (en) * 1966-03-11 1968-09-10 North Electric Co Inverter circuit having increased frequency starting
US3725770A (en) * 1972-07-25 1973-04-03 Gen Electric Starting circuitry for series/parallel compensated, current-fed inverter
US3757197A (en) * 1972-07-25 1973-09-04 Gen Electric Amping voltage on series compensating capacitor series parallel compensated current source inverter with means for cl
US4161773A (en) * 1978-07-10 1979-07-17 Northern Telecom Limited Push-pull inverter including starter circuit
US4215392A (en) * 1978-12-19 1980-07-29 Ncr Corporation Inverter power supply
US4598351A (en) * 1984-02-27 1986-07-01 Sundstrand Corporation Soft-start control for a push-pull converter-regulator with a flux balancing circuit
US4621313A (en) * 1985-06-28 1986-11-04 Zenith Electronics Corporation Soft-start capacitor discharge circuit
US4625271A (en) * 1984-10-05 1986-11-25 Sundstrand Corporation Soft-start circuit for a power converter
US4992718A (en) * 1989-09-11 1991-02-12 Nihon Patent Electric Co., Ltd. Electric floor cleaner with a soft start function

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3264548A (en) * 1961-04-18 1966-08-02 Westinghouse Brake & Signal D. c. to a. c. inverter circuits
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
US3350625A (en) * 1963-10-28 1967-10-31 Trw Inc Pulse controlled inverter circuit
US3398352A (en) * 1964-01-20 1968-08-20 Lorain Prod Corp Apparatus and method for starting, operating and stopping an inverter
US3333179A (en) * 1964-05-12 1967-07-25 Jefferson Electric Co Parallel inverter having higher frequency at start-up
US3401327A (en) * 1966-03-11 1968-09-10 North Electric Co Inverter circuit having increased frequency starting
US3725770A (en) * 1972-07-25 1973-04-03 Gen Electric Starting circuitry for series/parallel compensated, current-fed inverter
US3757197A (en) * 1972-07-25 1973-09-04 Gen Electric Amping voltage on series compensating capacitor series parallel compensated current source inverter with means for cl
US4161773A (en) * 1978-07-10 1979-07-17 Northern Telecom Limited Push-pull inverter including starter circuit
US4215392A (en) * 1978-12-19 1980-07-29 Ncr Corporation Inverter power supply
US4598351A (en) * 1984-02-27 1986-07-01 Sundstrand Corporation Soft-start control for a push-pull converter-regulator with a flux balancing circuit
US4625271A (en) * 1984-10-05 1986-11-25 Sundstrand Corporation Soft-start circuit for a power converter
US4621313A (en) * 1985-06-28 1986-11-04 Zenith Electronics Corporation Soft-start capacitor discharge circuit
US4992718A (en) * 1989-09-11 1991-02-12 Nihon Patent Electric Co., Ltd. Electric floor cleaner with a soft start function

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007004817A1 (en) * 2007-01-31 2008-08-07 Siemens Ag contraption
US8143954B2 (en) 2007-01-31 2012-03-27 Continental Automotive Gmbh Oscillation device with auxiliary oscillating means
US8804383B2 (en) 2012-03-09 2014-08-12 Delta Electronics, Inc. Starter of grid-connected inverter and control method thereof
CN109038795A (en) * 2018-07-20 2018-12-18 上海空间电源研究所 For electrically separated interlock protection and soft-switching device and method

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