Turbomachinery system fiberoptic multi-parameter sensing system and method

• US 8,042,412 B2
• Filed: 06/25/2008
• Issued: 10/25/2011
• Est. Priority Date: 06/25/2008
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Wu, Juntao, Ross, Alexander Seth, Pietrzykowski, Matthew Damian, Gawrelski, Richard Joseph, Chan, David So Keung, Li, Yun, Xia, Hua, McCarthy, Kevin Thomas, Zheng, Danian, Turnquist, Norman Arnold
• Primary Examiner(s): Caputo; Lisa
• Assistant Examiner(s): DUNLAP, JONATHAN M
• Application Number:
  US12/215,094
• Publication Number:
  US 20090320609A1
• Time in Patent Office: 1,217 Days
• Field of Search: 738/00, 736/50, 738/623.25, 738/623.24
• US Class Current: 73/862.324
• CPC Class Codes: G01H 9/004 using fibre optic sensors light guides per se G02B6/00, acousto-optical devices specially adapted for gating or modulating in optical wave guides G02F1/125
• CPC Class Codes: G01L 3/109 involving measuring phase difference of two signals or pulse trains
• CPC Class Codes: G01L 3/12 involving photoelectric means
• CPC Class Codes: G01M 11/081 by using a contact-less detection method, i.e. with a camera

Abstract

A fiberoptic multi-parameter sensing system for monitoring turbomachinery system shaft static and dynamic torques, vibration modes and associated operation status includes a multi-furcated fiber bundle based optical splitter configured to transmit light to a surface of at least one turbomachinery system shaft through a plurality of optical fiber bundles disposed at a plurality of locations in proximity to the surface of the at least one shaft, in which the plurality of locations together are arranged in a substantially axial direction between the ends of the at least one shaft. The system further includes an array of high-temperature bifurcated fiber bundle based reflectance probes to receive reflectance signals from the shaft surface and send to an array of photosensitive detectors, configured to detect dynamic light reflected from the at least one turbomachinery system shaft surface in response to the transmitted light during rotation of at least one turbomachinery system shaft and generate dynamic reflected light signals there from. A sensing mechanism is configured to determine a torque or vibration on at least one turbomachinery system shaft in response to the dynamic reflected light signal signatures based on time-domain and frequency-domain signal processes.

Claims

1. A method of sensing turbomachinery system shaft static and dynamic torques, vibration modes and associated operation status, the method comprising:

transmitting light from a single light source to a plurality of shaft surface locations on a turbomachinery system via a plurality of optical fiber bundles, the plurality of shaft surface locations arranged in a substantially axial direction between the ends of at least one shaft, such that a plurality of dynamic reflected light signals are received from the plurality of shaft surface locations by at least one high-temperature fiber bundle-based lensless reflectance sensing probe while at least one shaft is rotating, wherein at least one of the plurality of shaft surface locations has an altered texture defined by a v-groove inscribed into the surface of the shaft by altering the surface depth of desired shaft surface areas relative to other shaft surface areas and at least one other of the plurality of shaft surface locations does not include an altered texture, wherein the depth of the v-groove provides a front working point signal and a rear working point signal such that a corresponding time delay can be detected from any two v-groove locations to determine the shaft twist angle value by differentiating their reflectance pattern signatures during each rotating cycle; and

determining at least one turbomachinery system shaft torque characteristic based on at least one characteristic of the dynamic reflected light signals received from the at least one of the shaft surface locations; and

determining at least one turbomachinery system shaft vibration characteristic based on at least one characteristic of the dynamic reflected light signals received from the at least one other of the surface locations.

2. The method according to claim 1, wherein each optical fiber is multi-furcated such that light is transmitted to each turbomachinery shaft surface location via one leg of a multi-furcated optic fiber splitter and further such that light received from each shaft surface location in response to the transmitted light is received via a bi-furcated optic fiber reflectance probe.

3. The method according to claim 1, wherein transmitting light to a plurality of shaft surface locations on a turbomachinery system comprises transmitting light to an optical encoded turbomachine shaft surface.

4. The method according to claim 3, wherein determining at least one turbomachinery system shaft torque or vibration characteristic based on at least one characteristic of the reflected signals comprises:

determining a shaft twist angle value based on the plurality of reflected signal signatures; and

determining a turbomachinery system shaft torque based on a shaft twist angle value corresponding time delay or phase shift by differentiating any two reflectance signatures.

5. The method according to claim 4, wherein determining a shaft twist value based on the plurality of reflected signals comprises:

measuring when a difference between reflectance pattern signatures of reflected light signals detected via a plurality of reflectance probes at a desired wavelength of interest exceeds a desired threshold via a photodetecting mechanism;

determining differential time delays associated with the reflected signal signature; and

determining a shaft twist angle value based on the reflected signal differential time delays from their reflectance pattern recognition.

6. The method according to claim 4, wherein determining a turbomachinery system shaft torque based on the shaft twist angle value comprises calibrating an industry accepted gold standard torque sensor for use with the respective turbomachinery system shaft such that the twist angle value corresponds to an absolute value of torque retrieved from a look-up table or from a formulas, or from a calibration transfer function.

7. The method according to claim 4, wherein determining a turbomachinery system shaft torque based on the shaft twist angle value comprises calculating a torque value based on the twist angle value.

8. The method according to claim 7, wherein determining a turbomachinery system shaft torque based on the shaft twist angle value further comprises calibrating out any differences between reflectance signals received from different locations along the at least one turbomachinery system shaft such that no measurable differences exist between measured signals associated with the optic fibers while the at least one shaft is stationary and prior to calculating the torque value.

9. The method according to claim 3, wherein determining a turbomachinery system shaft torque or vibration characteristic based on at least one characteristic of the reflected signals comprises:

determining a turbomachinery system shaft fundamental vibration frequency and a desired number of higher order harmonic turbomachinery system shaft vibration frequencies based on the plurality of received reflectance signals; and

determining a turbomachinery system shaft torsional vibration based on the shaft fundamental vibration frequency and shaft higher order harmonic shaft vibration mode frequencies.

10. The method according to claim 1, wherein determining a turbomachinery system shaft torque or vibration characteristic based on at least one characteristic of the reflected signals comprises:

determining a turbomachinery system shaft fundamental vibration frequency and a desired number of higher order harmonic turbomachinery system shaft vibration mode frequencies based on the plurality of received reflectance signals; and

determining a turbomachinery system shaft flexural vibration based on the shaft fundamental vibration frequency and shaft higher order harmonic shaft vibration frequencies.

11. The method according to claim 1, wherein transmitting light to a plurality of shaft surface locations on a turbomachinery system via a plurality of optic fiber bundles, the plurality of shaft surface locations together arranged in a substantially axial direction between the ends of at least one turbomachinery system shaft, such that a plurality of light signals are reflected from the plurality of locations while at least one shaft is rotating, comprises transmitting light via a multifurcated fiber bundle element and, receiving reflected light via a bifurcated fiber bundle element, and further wherein each optic fiber bundle associated with a shaft location is coupled to a respective reflectance probe placed in close proximity to the surface of the at least one turbomachinery shaft.

12. The method according to claim 1, wherein transmitting light to a plurality of shaft surface locations on a turbomachinery system via a plurality of optic fiber bundles, the plurality of shaft surface locations together arranged in a substantially axial direction between the ends of at least one turbomachinery shaft, such that a plurality of light signals are received from the plurality of locations while the at least one shaft is rotating, comprises transmitting light from a light source selected from a single wavelength light source, a LED light source, a broadband light source, and a multi-chromatic light source, operating either in continuous mode or in frequency modulated pulsed mode.

13. A system for sensing turbomachinery system shaft static and dynamic torques, vibration modes and associated operation status, the sensing system comprising:

a single light source configured to transmit light to a surface of at least one turbomachinery system shaft through a plurality of optical fiber bundles disposed at a plurality of locations in proximity to the surface of the at least one shaft, the plurality of locations together arranged in a substantially axial direction between the ends of the at least one shaft;

at least one high-temperature fiber bundle-based lensless reflectance sensing probe configured to detect dynamic light reflected from the at least one turbomachinery system shaft surface in response to the transmitted light during rotation of the at least one turbomachinery system shaft and generate dynamic reflected light signals there from; and

a sensing mechanism configured to determine a torque and a vibration on the at least one turbomachinery system shaft in response to the dynamic reflected light signal signatures or pattern recognition based on time-domain and frequency-domain signal processes,

wherein the turbomachinery shaft comprises an encoding mechanism implemented via an altered texture defined by a v-groove inscribed into the surface of the shaft by altering the surface depth of desired shaft surface areas relative to other shaft surface areas on at least one location of the at least one shaft in proximity to a respective fiber bundle location but not all locations of the at least one shaft in proximity to respective fiber bundle locations, wherein the depth of the v-groove provides a front working point signal and a rear working point signal such that a corresponding time delay can be detected from any two v-groove locations to determine the shaft twist angle value by differentiating their reflectance pattern signatures during each rotating cycle.

14. The system according to claim 13, wherein the at least one turbomachinery system shaft is optical encoded.

15. The system according to claim 14, wherein the vibration is a torsional vibration.

16. The system according to claim 14, wherein the optical encoded shaft comprises an optical encoding mechanism attached onto or embedded into the surface of the shaft either by directly laser micromachining, laser marking or welding.

17. The system according to claim 14, wherein the optical encoded shaft comprises an optical encoding mechanism implemented such that the optical encoding mitigates fault signal detection from rusted or dirty contaminated shaft surface areas.

18. The system according to claim 13, wherein the vibration is a flexural vibration.

19. The system according to claim 13, wherein the light source is selected from a single wavelength light source, a LED light source, a broadband superluminescent light source, and a multi-chromatic light source.

20. The system according to claim 13, wherein each optical fiber transmission line comprises a multi-furcated fiber bundle selected from plastic fibers, silica fibers, and sapphire fibers.

21. The system according to claim 13, wherein the at least one high-temperature fiber bundle-based lensless reflectance sensing probe comprises a silicon-based photo sensor array for visible signal detection.

22. The system according to claim 13, wherein the at least one high-temperature fiber bundle-based lensless reflectance sensing probe comprises a silicon-based charge-couple detector (CCD) or CMOS for visible signal detection.

23. The system according to claim 13, wherein the at least one high-temperature fiber bundle-based lensless reflectance sensing probe comprises a InGaAs or InGaNP based PIN diode or avalanche detector or arrays for near infrared signal detection.

24. The system according to claim 13, further comprising a 1×

2 or 1×

N reflectance probe corresponding to each optical fiber, each reflectance probe configured to transmit light received from the light source along its corresponding optical fiber bundle to the surface of the at least one shaft via a transmission leg of the reflectance probe and further configured to receive light reflected from the surface of the at least one shaft via a measurement leg of the reflectance probe.

25. The system according to claim 13, wherein the sensing mechanism comprises an industry accepted gold standard torque sensor for use with the respective at least one turbomachinery system shaft such that a measured shaft twist angle value corresponds to an absolute value of torque retrieved from a look-up table or from a formulas, or from a calibration transfer function.

26. The system according to claim 13, wherein the sensing mechanism comprises a signal processor configured to determine when the reflectance signatures of received light at a desired wavelength of interest exceeds a desired threshold, determine differential time delays associated with the reflected signal signatures, determine a shaft twist angle value based on the reflected signal differential time delays, and determine a shaft torque based on the shaft twist angle.

27. The system according to claim 26, wherein the signal processor with reflectance signal pattern recognition is further configured to calibrate out any differences between desired reflected signals to mitigate undesired measurable differences between the desired reflected signals.