Synthesized synchronous sampling and acceleration enveloping for differential bearing damage signature

• US 7,930,111 B2
• Filed: 09/22/2008
• Issued: 04/19/2011
• Est. Priority Date: 09/22/2008
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Luo, Huageng, Ghanime, George Hanna, Qiu, Hai
• Primary Examiner(s): Feliciano; Eliseo Ramos
• Assistant Examiner(s): Suarez; Felix E
• Application Number:
  US12/284,441
• Publication Number:
  US 20100071469A1
• Time in Patent Office: 939 Days
• Field of Search: 702 33- 35, 702/79, 702/113, 702141-142, 702/149, 702176-178, 702182-183, 702/185, 73/18.2, 73/18.4, 735/93, 73658-660, 384/623, 701/93
• US Class Current: 702/34
• CPC Class Codes: F16C 19/527 related to vibration and noise
• CPC Class Codes: F16C 2233/00 Monitoring condition, e.g. temperature, load, vibration
• CPC Class Codes: F16C 2326/43 Aeroplanes; Helicopters in general B64C
• CPC Class Codes: F16C 2360/23 Gas turbine engines in general F02C
• CPC Class Codes: F16C 2360/31 Wind motors in general F03D
• CPC Class Codes: G01M 13/045 Acoustic or vibration analysis

Abstract

A system for detecting differential bearing damages includes a synthesized tachometer that generates a tachometer signal corresponding to the race speed difference of a bearing assembly such that the bearing damage speed difference dependency can be eliminated and the damage features can be enhanced. The system also includes acceleration enveloping in the cycle domain to further enhance the damage signatures.

Claims

1. A method of detecting differential bearing damages, the method comprising:

providing a synthesized tachometer configured to generate a speed signal for a differential bearing assembly such that the speed signal corresponds to the approximate location of a missing tachometer signal based on race speeds of the differential bearing assembly;

providing a sampling mechanism configured to synchronously sample vibration data associated with the differential bearing assembly based on the speed signal to generate synthesized cycle domain data corresponding to at least one damage signature there from;

causing rotation of the differential bearing assembly and generating a plurality of speed signals for inner and outer rotating bearing races in response to the rotation;

synthesizing a missing tachometer signal corresponding to the speed difference of the inner and outer races via the synthesized tachometer based upon the plurality of speed signals;

synchronously sampling bearing vibration data of the differential bearing assembly via the sampling mechanism in response to the synthesized speed difference tachometer signal to generate synthesized cycle domain data corresponding to at least one bearing damage signature of the differential bearing; and

displaying a spectrum of resultant differential bearing damage signatures in the order domain on a graphic display device in response to the synthesized cycle domain data.

2. The method according to claim 1, wherein synthesizing a speed difference tachometer comprises:

assuming the existence of a tachometer pulse at a start time;

locating a tachometer pulse at a first time subsequent to the start time and immediately preceding a missing tachometer pulse;

assuming the existence of a tachometer pulse at a second time corresponding to the missing tachometer pulse;

determining an average bearing assembly shaft speed between the first time and the second time; and

minimizing the absolute value of the difference between a deviation in the first time and a deviation in the second time to determine the approximate location of the at least one synthesized tachometer signal.

3. The method according to claim 1, further comprising applying a fast Fourier transform (FFT) to the synthesized cycle domain data to generate a differential bearing damage signature in the order domain corresponding to increments of orders of differential bearing speed.

4. The method according to claim 3, further comprising applying spectrum averaging to the order domain data to enhance the differential bearing damage signatures.

5. The method according to claim 1, wherein synchronously sampling bearing vibration data in response to the synthesized speed difference tachometer signal to generate synthesized cycle domain data corresponding to at least one bearing damage signature comprises:

preconditioning and digitizing the vibration data at a desired high A/D sampling rate;

bandpass filtering the preconditioned and digitized vibration data to isolate signals in a desired frequency range of interest; and

applying the Hilbert transform to the isolated signals to generate an envelope of the isolated signals.

6. The method according to claim 5, wherein synchronously sampling bearing race vibration data is conducted after generating the envelope of the isolated signals.

7. The method according to claim 1, wherein the inner race and outer races correspond to an aircraft engine differential bearing assembly.

8. The method according to claim 1, wherein the plurality of speed signals are generated via a broadband sensor disposed at a desired location on an aircraft engine case remote from the differential bearing assembly.

9. A method of enhancing a differential bearing damage signature, the method comprising:

providing a synthesized tachometer configured to generate a speed signal for a differential bearing assembly such that the speed signal corresponds to the approximate location of a missing tachometer signal based on race speeds of the differential bearing assembly;

providing a sampling mechanism configured to synchronously sample vibration data associated with the differential bearing assembly based on the speed signal to generate synthesized cycle domain data corresponding to at least one damage signature there from;

causing rotation of the differential bearing assembly and generating a plurality of speed signals for each differential bearing race in response to the rotation;

synthesizing at least one missing tachometer signal for at least one differential bearing race via the synthesized tachometer based upon the plurality of speed signals;

synchronously sampling vibration data of the differential bearing assembly with respect to race speed differences via the sampling mechanism in response to the plurality of speed signals and the at least one synthesized tachometer signal to generate synthesized cycle domain data corresponding to at least one bearing damage signature; and

displaying a spectrum of resultant differential bearing damage signatures in the order domain on a graphic display device in response to the synthesized cycle domain data.

10. The method according to claim 9, further comprising applying a FFT to the synthesized cycle domain data to generate a differential bearing damage signature in the order domain corresponding to increments of orders of differential bearing damage signatures.

11. The method according to claim 10, wherein synthesizing at least one tachometer signal comprises:

locating a tachometer pulse at a first time subsequent to a start time and immediately preceding a missing tachometer pulse;

assuming the existence of a tachometer pulse at a second time corresponding to the missing tachometer pulse;

determining an average bearing assembly shaft speed between the first time and the second time; and

minimizing the absolute value of the difference between a deviation in the first time and a deviation in the second time to determine the approximate location of the at least one synthesized tachometer signal.

12. The method according to claim 10, further comprising applying spectrum averaging to the order domain data to enhance the differential bearing damage signatures.

13. The method according to claim 9, wherein synchronously sampling vibration data associated with the differential bearing with respect to race speed differences in response to the plurality of speed signals and the at least one synthesized tachometer signal to generate synthesized cycle domain data corresponding to at least one bearing damage signature comprises:

preconditioning and digitizing the vibration data at a desired high A/D sampling rate;

bandpass filtering the preconditioned and digitized vibration data to isolate signals in a desired frequency range of interest; and

applying the Hilbert transform to the isolated signals to generate an envelope of the isolated signals.

14. The method according to claim 13, wherein synchronously sampling bearing race vibration data is conducted after generating the envelope of the isolated signals.

15. The method according to claim 9, wherein the differential bearing comprises one portion of an aircraft engine differential bearing assembly.

16. The method according to claim 15, wherein the at least one synthesized tachometer signal is based on both inner race speeds and outer race speeds.

17. The method according to claim 9, wherein the plurality of speed signals are generated via a broadband sensor disposed at a desired location on an aircraft engine case remote from the differential bearing assembly.

18. A system for detecting differential bearing damage, the system comprising:

a synthesized tachometer configured to generate a speed signal for a differential bearing assembly such that the speed signal corresponds to the approximate location of a missing tachometer signal based on both inner and outer race speeds of the bearing assembly;

a sampling mechanism configured to synchronously sample vibration data associated with the differential bearing assembly based on the speed signal to generate synthesized cycle domain data corresponding to at least one differential bearing assembly damage signature; and

a graphic display device configured to display a spectrum of resultant differential bearing damage signatures in the order domain in response to the synthesized cycle domain data.

19. The system for detecting bearing damage according to claim 18, wherein the bearing assembly comprises an aircraft engine differential bearing.

20. The system for detecting bearing damage according to claim 18, further comprising:

a vibration sensor configured to monitor each bearing race and generate vibration signals there from; and

a signal processing means configured to precondition and digitize the vibration signals to generate the vibration data there from.

21. The system for detecting bearing damage according to claim 20, further comprising:

a bandpass filter configured to filter the preconditioned and digitized vibration data to isolate signals in a desired frequency range of interest; and

a signal processing means configured to apply a Hilbert transform to the isolated signals to generate an envelope of the isolated signals corresponding to the vibration data.

22. The system for detecting bearing damage according to claim 18, further comprising signal processing means configured to apply a FFT to the synthesized cycle domain data to generate a differential bearing damage signature in the order domain corresponding to increments of orders of differential bearing damage signatures.

23. The method according to claim 22, further comprising signal processing means for applying spectrum averaging to the order domain data to enhance the differential bearing damage signatures.