Spectral analysis of induction motor current to detect rotor faults with reduced false alarms

• US 5,049,815 A
• Filed: 08/27/1990
• Issued: 09/17/1991
• Est. Priority Date: 04/20/1990
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Kliman, Gerald B.
• Primary Examiner(s): Karlsen, Ernest F.
• Application Number:
  US07/572,578
• Time in Patent Office: 386 Days
• Field of Search: 324/158 MG, 324/545, 324/546, 324/77 B, 340/648, 361/5, 361/20, 361/31, 322/99, 364/485
• US Class Current: 324/545
• CPC Class Codes: G01R 31/343 in operation
• CPC Class Codes: G01R 31/346 Testing of armature or field windings

Abstract

Pursuant to detecting rotor faults in an induction motor by analysis of a frequency spectrum of the current drawn by the motor under test, wherein success of the fault analysis requires an accurate determination of the fundamental frequency of the motor current and the motor slip frequency, method and apparatus are disclosed for determining the fundamental and slip frequency values solely from analysis of the motor current spectra.

Claims

1. A method of detecting rotor faults in an induction motor, wherein the motor includes a rotor having a multiplicity of conductive bars and a stator drawing motor current from a power supply, the method comprising the steps of:

A. deriving a current signal indicative of said motor current;

B. sampling said current signal at a predetermined sampling rate to obtain a time succession of current values over a predetermined sampling period;

C. transferring said current values to a frequency spectrum;

D. determining the fundamental frequency of said motor current from said frequency spectrum;

E. scanning said frequency spectrum in a lower sideband of said fundamental frequency for current peaks exceeding a threshold amplitude;

F. ascribing the frequency of each said current peak as a candidate indicating the slip frequency of the motor;

G. checking predetermined harmonic sidebands of said frequency spectrum at frequencies predicted from each said slip frequency candidate for matching current peaks until all but one of said slip frequency candidates are disqualified; and

H. conducting a rotor fault analysis of said frequency spectrum using the determined fundamental frequency and the qualified remaining one of said slip frequency candidates as the motor slip frequency.

2. The method defined in claim 1, wherein the checked frequencies in said harmonic sidebands predicted from said slip frequency candidates include at least two of the frequencies F_o (5-4s), f_o (5-6s), f_o (7-6s), f_o (7-8s), f_o (11-10s), f_o (11-12s), f_o (13-12s) and f_o (13-14s), where f_o is said fundamental frequency, and s is the frequency of each said slip frequency candidate divided by said fundamental frequency.

3. The method defined in claim 2, where said slip frequency candidates are disqualified when matching current peaks are not found at said predicted frequencies.

4. The method defined in claim 3, which further includes the steps of checking an upper sideband of said fundamental frequency for matching current peaks at frequencies symmetrically related with the lower sideband frequencies of said slip frequency candidates and disqualifying said slip frequency candidates when matching current peaks in said upper sideband are not found.

5. The method defined in claim 3, wherein, in the event no current peaks are found in said fundamental frequency lower sideband, the rotor is declared free of fault without conducting method steps F, G and H.

6. The method defined in claim 3, wherein said scanning step E is conducted over a range of frequencies based on an estimate of the motor slip frequency.

7. The method defined in claim 6, wherein said slip frequency estimate is obtained from the motor'"'"'s nameplate data and the characteristics of the motor'"'"'s loading.

8. The method defined in claim 6, which further includes the steps of checking an upper sideband of said fundamental frequency for matching current peaks at frequencies symmetrically related with the lower sideband frequencies of said slip frequency candidates and disqualifying said slip frequency candidates when matching current peaks in said upper sideband are not found.

9. The method defined in claim 8, wherein, in the event no current peaks are found in said fundamental frequency lower sideband, the rotor is declared free of fault without conducting method steps F, G and H.

10. Apparatus for detecting rotor faults in an induction motor having a rotor including a plurality of conductive bars and a stator drawing motor current from a power source, said apparatus including:

A. a current sensor for deriving a current signal indicative of said motor current;

B. sampling means for storing a time series of current values over a predetermined sampling period;

C. transform means for generating a frequency spectrum of said current values;

D. first means for determining the fundamental frequency of said motor current from said frequency spectrum of said current values;

E. second means for determining the slip frequency of the motor from said frequency spectrum of said current values; and

F. third means for analyzing said frequency spectrum of said current values at certain fundamental and harmonic sideband frequencies determined from said fundamental and slip frequencies to identify the presence and severity of any rotor faults.

11. The apparatus defined in claim 10, wherein said second means scans a lower sideband of said fundamental frequency for current peaks exceeding a threshold amplitude;

ascribes each said current peak as a candidate indicating the motor slip frequency, checks predetermined harmonic lower sidebands at certain frequencies predicted from each said slip frequency candidate for matching signal peaks until all but one of said slip frequency candidates are disqualified, and declares the one remaining slip frequency candidate the true indicator of motor slip frequency.

12. The apparatus defined in claim 11, wherein said second means checks for matching current peaks at least two of the predicted frequencies f_o (5-4s), f_o (5-6s), f_o (7-6s), f_o (7-8s), f_o (11-10s), f_o (11-12s), f_o (13-12s) and f_o (13-14s), where f_o is the fundamental frequency and s is the frequency of each slip frequency candidate divided by the fundamental frequency.

13. The apparatus defined in claim 12, wherein said second means disqualifies said slip frequency candidates when matching current peaks are not found at said predicted frequencies.

14. The apparatus defined in claim 13, which further includes fourth means responsive to said second means for indicating no rotor faults when no current peaks are found in said lower sideband of said fundamental frequency.

15. A method for detecting rotor faults in an induction motor having a rotor including a plurality of conductive bars and a stator drawing motor current from a power supply, said method comprising the steps of:

A. deriving a current signal indicative of motor current;

B. sampling said current signal at a predetermined sampling rate to obtain a time succession of current values over a predetermined sampling period;

C. transforming said current values to a frequency spectrum;

D. determining the fundamental frequency of said motor current from said frequency spectrum of current values;

E. analyzing said frequency spectrum of current values to identify the true slip frequency of the motor; and

F. conducting a rotor fault analysis of said frequency spectrum of current values using the fundamental frequency value determined in step D and the true slip frequency value identified in step E.

16. The method defined in claim 15, wherein said analyzing step E includes the steps of scanning a sideband of said fundamental frequency for signals indicative of motor slip frequency, and checking each of said signals at predicted frequencies in at least one predetermined harmonic sideband to identify which one of said signals is a true indicator of motor slip frequency.

17. The method defined in claim 16, which further includes the step of declaring the rotor free of fault upon the failure of step E to find slip frequency indicative signals in said fundamental frequency sideband.