Rotor position detector

• US 5,461,293 A
• Filed: 05/12/1993
• Issued: 10/24/1995
• Est. Priority Date: 05/12/1993
• Status: Expired due to Term

• Current Assignee: Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Markunas, Albert L., Rozman, Gregory I., Weber, Leland E.
• Primary Examiner(s): Shoop, Jr., William M.
• Assistant Examiner(s): Sircus, Brian
• Application Number:
  US08/060,878
• Time in Patent Office: 895 Days
• Field of Search: 318/602, 318/603, 318/605, 318/659-661, 318/778, 318/779, 318/798-803, 318/807-812
• US Class Current: 318/603
• CPC Class Codes: F02N 11/04 the motors being associated with current generators
• CPC Class Codes: H02K 11/042 Rectifiers associated with rotating parts, e.g. rotor cores or rotary shafts
• CPC Class Codes: H02K 29/06 with position sensing devices H02K29/03 takes precedence
• CPC Class Codes: H02P 2101/30 for aircraft
• CPC Class Codes: H02P 6/08 Arrangements for controlling the speed or torque of a single motor H02P6/10, H02P6/28 take precedence
• CPC Class Codes: H02P 6/18 without separate position detecting elements
• CPC Class Codes: H02P 6/20 Arrangements for starting H02P6/08 takes precedence
• CPC Class Codes: H02P 9/02 Details

Abstract

A detector for detecting rotor position of a brushless generator includes a shaft pulse encoder which develops a cycle pulse once per revolution of a motive power shaft and a circuit coupled to armature phase windings of a permanent magnet generator of the brushless generator 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.

Claims

1. 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, comprising:

a shaft pulse encoder disposed on the motive power shaft which develops a cycle pulse once per revolution of the motive power shaft;

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 and responsive to the cycle pulse 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 windings in dependence upon the speed and angular position indications wherein the delivering means comprises;

second developing means for developing a torque command signal and an electrical angle command signal from the speed and angular position indications; and

an inverter responsive to the torque command signal and the electrical angle command signal which develops the AC power.

2. The starting system control of claim 1, wherein the inverter is operated in a current mode of operation.

3. The starting system control of claim 1, further including a second converting means for converting the electrical angle command signal into a sine signal and a cosine signal, first and second multipliers coupled to the second converting means for multiplying the sine and cosine signals with the torque command signal to obtain a pair of current signals and third converting means for converting the pair of current signals into three-phase signals.

4. The starting system control of claim 3, further including three summers each of which sums one of the three-phase signals with a signal representing a magnitude of a phase current of the AC power to obtain an error signal and an inverter control coupled between the summers and the inverter which operates the inverter in accordance with the error signals.

5. The starting system control of claim 1, wherein the main generator portion includes a number of poles and the angular position indication comprises a position signal and wherein the second 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.

6. The starting system control of claim 1, 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 second 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.

7. The starting system control of claim 6, wherein the second developing means further includes third developing means responsive to a speed command signal and the speed indication for developing a speed error signal, fourth developing means responsive to the position reference signal and the angular position indication for developing a position error signal and a further summer for summing the speed error signal and the position error signal.

8. The starting system control of claim 7, wherein the second developing means further includes a limiter coupled to the further summer which develops the torque command signal.

9. The starting system control of claim 1, wherein the measuring means comprises a counter which accumulates clock pulses during time periods between adjacent interval pulses.

10. The starting system control of claim 9, wherein the converting means includes means for inverting a counter output signal developed by the counter to obtain the speed indication.

11. The starting system control of claim 10, wherein the converting means further includes an integrator coupled to the inverting means which develops the angular position indication.

12. The starting system control of claim 11, wherein the integrator is periodically reset once per revolution of the motive power shaft by a reset signal derived from the cycle pulses.