Patent GB-1243389-A (GB)
Title: Inverter circuits, particularly for motor control
Inventor: TURNBULL FRED GERDES
IPC: H02M7/515
Filed: 1968-10-07
Abstract: 1,243,389. D.C. to A.C. static converters; electric motor control systems. GENERAL ELECTRIC CO. 7 Oct., 1968 [31 Oct., 1967], No. 47484/68. Headings H2F and H2J. To ensure adequate commutation energy independent of output voltage, commutating pulses to turn-off SCR.s 15, 17 (Fig. 1) of a main inverter 11 connected to a variable D.C. source 13, 14; are supplied via an H.F. coupling transformer 24p, 24s by a self commutating auxiliary inverter 12 connected to a separate fixed voltage D.C. source 30, 31. The pulses from inverter 12 are half sinewaves as shown Fig. 2b and have a repetition rate the same as the square wave output (Fig. 2a) of the main inverter but are shorter in wave length. The SCR's 15, 17 may be turned on and off rapidly in any one cycle (as shown dotted in Fig. 2a) for voltage control also the output voltage in succeeding half cycles can be made different, to give a net direct current to the load 18, by controlling SCR's 15, 17 independently. The input voltage and gating frequency of inverter 11 may be varied to vary the speed of an A.C. motor load: Commutation, of main inverter.-Thyristors 15 and 17 are fired alternately to pass current in opposite directions through load 18 via inductor 16a, 16b and capacitors 21, 20 respectively. To turn off SCR 15 for example, commutating SCR 32 is triggered and a current pulse is produced by secondary 24S and passes via L16a in opposition to the load current causing it to drop to zero and current begins to flow through feedback diode 22 reverse biasing SCR 15 and turning it off. The circuit for the commutating pulse is completed via C25 and C27 and the D.C. source 13, 14. Likewise SCR 17 can be turned off by triggering SCR 34. Auxiliary inverter.-When SCR 32 is gated a current pulse (which is a half sine wave because of the series resonance circuit it flows into) flows through SCR 32, L33a, primary 24p and divides equally to C35, C36. C36 is charged via winding 24p from the current source 30, 31 while a charge on C35 accumulated during a previous half-cycle, is discharged through primary 24p. At the end of this half-cycle current through SCR 32 drops below the holding value and the voltage at junction point 37 rises above the D.C. supply volts so that SCR 32 is reverse biased and turns off. Likewise when SCR 34 is conducting a negative going half sine wave current pulse is passed through the primary 24p via L33b, C35 and SCR 34. C35 is charged from the D.C. source while C36 discharges through 24p and SCR 34 which turns off when the current falls below its holding value. Instead of a single inductor 33 there may be two separate inductors in series and feedback diodes may be connected in anti-parallel across the SCR's 32, 34 (Fig. 4, not shown). In an alternative embodiment Fig. 3. (not shown) the main inverter is modified in that one end of the secondary 24S is connected to a junction between a pair of diodes across the D.C. source 13, 14, instead of between C25 and C26, while its other end is connected between the SCR's 15, 17 the commutating choke 16 being deleted. The voltage at one end of 24S is clamped to the supply terminal voltage by a capacitor across the supply; In Fig. 5 (not shown) three single phase inverters as Fig. 1 are combined to provide a 3 phase supply to an A.C. motor e.g. in a battery electric vehicle. The main D.C. source is variable from 0 to 330 volts; while the auxiliary D.C. source is derived from fuel cells and is stabilized.