Method and apparatus for detecting alternator rectifier diode short fault

• US 9,431,941 B1
• Filed: 02/12/2015
• Issued: 08/30/2016
• Est. Priority Date: 02/12/2015
• Status: Active Grant

• Current Assignee: GE Global Sourcing LLC (Westinghouse Air Brake Technologies Corporation)
• Original Assignee: General Electric Company
• Inventors: Verma, Rajeev, Worden, Bret Dwayne
• Primary Examiner(s): Cuevas, Pedro J
• Application Number:
  US14/620,218
• Publication Number:
  US 20160241176A1
• Time in Patent Office: 565 Days
• Field of Search: 322/58, 322/59, 322/99, 361/58, 363/17
• US Class Current: 1/1
• CPC Class Codes: H02P 9/102 for limiting effects of transients
• CPC Class Codes: H02P 9/48 Arrangements for obtaining a constant output value at varying speed of the generator, e.g. on vehicle H02P9/04 - H02P9/46 take precedence
• CPC Class Codes: Y02E 10/72 Wind turbines with rotation axis in wind direction

Abstract

Methods for detecting a short fault of an alternator rectifier electronic component include sampling a field winding voltage or current signal of an alternator, during operation of the alternator, and determining a fault ripple period at which the alternator field winding signal exceeds a fault threshold. A short fault of an electronic component of a rectifier coupled to the alternator is detected in the event that the fault ripple period closely matches an alternator armature period. Alternatively or additionally, the sampled field winding signal is band pass filtered, and a short fault is detected in the event that an amplitude of the band pass filtered field winding signal exceeds a fault threshold. The methods can be implemented, for example, by an apparatus that includes a hysteresis frequency counter, a frequency comparator, and a countdown timer.

Claims

1. A method comprising:

sampling a field winding signal of an alternator, during operation of the alternator;

determining a fault ripple period at which the field winding signal exceeds a fault threshold; and

detecting a short fault of an electronic component of a rectifier coupled to an output of the alternator in the event that the fault ripple period closely matches an armature period of the alternator.

2. The method of claim 1 wherein the short fault is detected only if the fault ripple period closely matches the armature period throughout a countdown.

3. The method of claim 2 wherein the countdown is at least twenty times the armature period.

4. The method of claim 2 wherein the countdown is no more than fifty times the armature period.

5. The method of claim 2 wherein the countdown is at least twenty times the armature period and no more than fifty times the armature period.

6. The method of claim 1 wherein the short fault is detected if a difference between the fault ripple period and the armature period is no more than 1 Hz.

7. The method of claim 1 wherein the fault threshold is at least 500% of a normal ripple amplitude.

8. The method of claim 1 wherein the fault threshold is at least 10,000% of a normal ripple amplitude.

9. The method of claim 1 wherein the fault ripple period is determined by obtaining a spectral density of the field winding signal.

10. A method comprising:

sampling a field winding signal of an alternator, during operation of the alternator;

band pass filtering the field winding signal that is sampled; and

detecting a short fault of an electronic component of a rectifier coupled to an output of the alternator in the event that an amplitude of the band pass filtered field winding signal exceeds a fault threshold.

11. The method of claim 10 wherein the band pass filtering is accomplished by tuning a band pass filter with reference to a sampled alternator armature frequency.

12. The method of claim 10 wherein the band pass filtering is accomplished by using a filter set to a design range of values for an alternator armature frequency.

13. The method of claim 10 wherein the band pass filtering is accomplished by selecting one of a plurality of band pass filters based on an operating condition of a prime mover that drives the alternator.

14. The method of claim 10 wherein the band pass filtering is accomplished by selecting one of a plurality of band pass filters based on a rotational speed of the alternator.

15. The method of claim 10 wherein the fault threshold is set based on an operating condition of a prime mover that drives the alternator.

16. An apparatus comprising:

a hysteresis frequency counter that is operatively connected to sample a field winding signal of an alternator and to output a value indicative of a fault ripple frequency, based on a ripple of the field winding signal exceeding a fault threshold;

a countdown timer; and

a frequency comparator that is operatively connected to compare the fault ripple frequency to an alternator armature frequency, and to actuate the countdown timer in the event that the fault ripple frequency closely matches the armature frequency;

wherein the countdown timer is operatively connected to be actuated by the frequency comparator, and is configured to signal a short fault of an electronic component of a rectifier coupled to an output of the alternator in the event that the fault ripple frequency closely matches the armature frequency for a countdown time.

17. The apparatus of claim 16 wherein the countdown timer is configured to signal the short fault if a difference between the fault ripple frequency and the armature frequency is no more than 1 Hz for the countdown time.

18. The apparatus of claim 16 wherein the fault threshold is at least 500% of a normal ripple amplitude.

19. The apparatus of claim 16 wherein the fault threshold is at least 10,000% of a normal ripple amplitude.

20. The apparatus of claim 16 wherein the countdown time is at least twenty times an armature period of the alternator.

21. The apparatus of claim 16 wherein the countdown time is no more than fifty times an armature period of the alternator.

22. The apparatus of claim 16 wherein the countdown time is at least twenty times an armature period of the alternator and no more than fifty times the armature period.