Control for a brushless generator operable in generating and starting modes

• US 5,495,163 A
• Filed: 05/12/1993
• Issued: 02/27/1996
• Est. Priority Date: 05/12/1993
• Status: Expired due to Term

• Current Assignee: Sundstrand Corporation (Rtx Corporation)
• Original Assignee: Sundstrand Corporation (Rtx Corporation)
• Inventors: Markunas, Albert L., Rozman, Gregory I., Hanson, Michael J.
• Primary Examiner(s): Dougherty, Thomas M.
• Assistant Examiner(s): Ponomarenko, Nicholas
• Application Number:
  US08/061,496
• Time in Patent Office: 1,021 Days
• Field of Search: 322/10, 290/31, 290/46, 310/156, 318/254
• US Class Current: 322/10
• CPC Class Codes: F02N 11/04 the motors being associated with current generators
• CPC Class Codes: H02P 2101/30 for aircraft
• CPC Class Codes: H02P 9/00 Arrangements for controlling electric generators for the purpose of obtaining a desired output
• CPC Class Codes: H02P 9/02 Details of the control

Abstract

A detector for detecting rotor position of a brushless generator having a motive power shaft, a permanent magnet generator (PMG) having a set of armature phase windings and a main generator portion having a set of armature phase windings includes a circuit coupled to the armature phase windings of the PMG for deriving a number of interval pulses per revolution of the motive power shaft. A circuit measures time periods between adjacent interval pulses and the measured time periods are converted into an indication of the angular position of the motive power shaft in accordance with a parameter of power delivered to one of the main generator portion armature phase windings.

Claims

1. A detector for detecting rotor position of a brushless generator having a motive power shaft, a permanent magnet generator (PMG) coupled to the shaft, the PMG having a set of armature phase windings at which a set of PMG phase outputs are produced, and a main generator portion coupled to the shaft, the main generator portion having a set of armature phase windings capable of receiving AC power, comprising:

means coupled to the PMG armature phase windings for deriving a number of internal pulses per revolution of the motive power shaft from the PMG phase outputs;

means coupled to the deriving means for measuring time periods between adjacent interval pulses; and

means coupled to the measuring means for converting the measured time periods into an indication of the angular position of the motive power shaft.

2. A detector for detecting rotor position of a brushless generator having a motive power shaft, a permanent magnet generator (PMG) coupled to the shaft, the PMG having a set of armature phase windings at which a set of PMG phase outputs are produced, and a main generator portion coupled to the shaft, the main generator portion having a set of armature phase windings capable of receiving AC power, comprising:

means coupled to the PMG armature phase windings for deriving a number of internal pulses per revolution of the motive power shaft from the PMG phase outputs;

means coupled to the deriving means for measuring time periods between adjacent interval pulses;

means coupled to the measuring means for converting the measured time periods into an indication of the angular position of the motive power shaft; and

wherein the measuring means comprises a counter which accumulates clock pulses during time periods between adjacent interval pulses.

3. The detector of claim 2, wherein the counter is periodically reset a certain number of times during each revolution of the motive power shaft by the interval pulses.

4. The detector of claim 2, wherein the converting means includes means for inverting a counter output signal developed by the counter to obtain an indication of the speed of the motive power shaft.

5. The detector of claim 4, wherein the converting means further includes an integrator coupled to the inverting means which develops the angular position indication.

6. The deflector of claim 5, wherein the accumulator is reset once per revolution of the motive power shaft by a reset signal derived from a parameter of AC power delivered to one of the main generator portion armature phase windings.

7. A starting system control for operating a brushless generator in a starting mode to convert electrical power into motive power wherein the brushless generator includes a motive power shaft, a permanent magnet generator (PMG) having a set of armature phase windings at which a set of PMG phase outputs are produced and a main generator portion having a set of armature phase windings which receive AC power during operation in the starting mode, comprising:

means coupled to the PMG armature phase windings for deriving a number of interval pulses per revolution of the motive power shaft from the PMG phase outputs;

means coupled to the deriving means for measuring time periods between adjacent interval pulses;

means coupled to the measuring means for converting the measured time periods into indications of the speed and angular position of the motive power shaft; and

means coupled to the converting means for delivering AC power to the set of main generator portion armature phase windings in dependence upon the speed and angular position indications.

8. The starting system control of claim 7, wherein the delivering means comprises first means for developing an electrical angle command signal from the angular position indication, second means for developing a power control signal from the speed indication and an inverter responsive to the electrical angle command signal and the power control signal for delivering the AC power to the set of main generator portion armature phase windings.

9. The starting system control of claim 8, further including second means for converting the electrical angle command signal into a sine signal and a cosine signal and third means for converting the sine and cosine signals into three-phase signals.

10. The starting system control of claim 9, further including three zero crossing detectors each responsive to one of the three-phase signals for producing first, second and third inverter control signals, respectively, and an inverter controller responsive to the power control signal and coupled between the zero crossing detectors and the inverter which operates the inverter in accordance with the first, second and third inverter control signals and the power control signal.

11. The starting system control of claim 10, wherein the converting means is responsive to a parameter of the AC power applied to one of the main generator portion armature phase windings.

12. The starting system control of claim 11, wherein the inverter controller includes means for producing a synchronization signal from the AC power delivered to the main generator portion armature phase windings and wherein the converting means is further responsive to the synchronization signal for converting the measured time periods into the indication of the angular position of the motive power shaft.

13. The starting system control of claim 8, wherein the main generator portion includes a number of poles and the angular position indication comprises a position signal and wherein the first developing means includes a multiplier which multiplies the position signal with a signal proportional to the number of poles to obtain a multiplied signal and a summer for summing the multiplied signal with a phase advance command to obtain the electrical angle command signal.

14. The starting system control of claim 8, wherein the second developing means includes a first summer for summing a power reference with a signal indicative of the power produced by the inverter to produce a power error signal, means for conditioning the power error signal and means for limiting the conditioned power error signal to produce the power control signal.

15. The starting system control of claim 14, wherein the second developing means further includes a multiplier for multiplying the speed indication by a reference signal to produce a ramp signal and a second summer for summing the ramp signal and a boost signal to produce a signal for controlling the limiting means.

16. The starting system control of claim 8, wherein the motive power shaft is accelerated from zero speed to a particular speed over a series of revolutions, the main generator portion includes a number of poles and the angular position indication comprises a position signal and wherein the first developing means includes a position reference signal generator which develops a position reference signal, a switch which provides the position reference signal to an output thereof during an initial portion of the series of revolutions and which provides the position signal to the output after the initial portion of the series of revolutions, a multiplier coupled to the switch which multiplies the signal at the output of the switch with a signal proportional to the number of poles to obtain a multiplied signal and a summer for summing the multiplied signal with a phase advance command to obtain the electrical angle command signal.

17. The starting system control of claim 16, wherein the first developing means further includes means for detecting when a speed reference signal is equal to or greater than a valid speed reference, third means responsive to the position reference signal and the position signal for developing a position error signal, an error comparator for comparing an error reference to the position error signal, and means responsive to an output of the detecting means and to an output of the error comparator for controlling the operation of the switch.

18. The starting system control of claim 17, wherein the controlling means comprises an AND gate.

19. The starting system control of claim 7, wherein the measuring means comprises a counter which accumulates clock pulses during time periods between adjacent interval pulses.

20. The starting system control of claim 19, wherein the converting means includes means for inverting a counter output signal developed by the counter to obtain the speed indication.

21. The starting system control of claim 20, wherein the converting means further includes an accumulator coupled to the inverting means which develops the angular position indication.

22. The starting system control of claim 21, wherein the accumulator is periodically reset once per revolution of the motive power shaft by a reset signal derived from a parameter of the AC power applied to one of the main generator portion armature phase windings.

23. The starting system control of claim 22, further including a conditioner which receives a voltage developed at one of the main generator portion armature phase windings, a zero crossing detector coupled to an output of the conditioner, a frequency divider for dividing the frequency of an output of the zero crossing detector by an amount proportional to the number of poles of the main generator and a one-shot responsive to an output of the frequency divider for producing the reset signal.

24. A method of detecting rotor position of a brushless generator having a motive power shaft, a permanent magnet generator (PMG) having a set of armature phase windings at which a set of PMG phase outputs are produced and a main generator portion having a set of armature phase windings capable of receiving AC power and coupled to an exciter portion, the method comprising the steps of:

deriving a number of interval pulses per revolution of the motive power shaft from the PMG phase outputs;

measuring time periods between adjacent interval pulses;

deriving a reset signal from a parameter of AC power on one of the main generator portion armature phase windings; and

converting the measured time periods into an indication of the angular position of the motive power shaft in accordance with the reset signal.

25. The method of claim 24, in combination with the further step of delivering AC power to the set of main generator portion armature phase windings in dependence upon the angular position indication.

26. The method of claim 24, wherein the step of measuring comprises the step of accumulating clock pulses in a counter during time periods between adjacent interval pulses.

27. The method of claim 26, wherein the step of measuring includes the step of using the interval pulses to periodically reset the counter a certain number of times during each revolution of the motive power shaft.

28. The method of claim 26, wherein the step of converting includes the step of inverting a counter output signal developed by the counter to obtain an indication of the speed of the motive power shaft.

29. The method of claim 28, wherein the step of converting further includes the step of providing an integrator for integrating the inverted counter output signal to develop the angular position indication.

30. The method of claim 29, wherein the step of converting includes the further step of using the reset signal to reset the integrator once per revolution of the motive power shaft.

31. The method of claim 30, in combination with the further step of delivering AC power to the set of main generator portion armature phase windings in dependence upon the angular position indication and the speed indication.