SYSTEM AND METHOD FOR ROTOR BLADE HEALTH MONITORING

• US 20100161245A1
• Filed: 12/22/2008
• Published: 06/24/2010
• Est. Priority Date: 12/22/2008
• Status: Active Grant

• Current Assignee: GE Infrastructure Technology, LLC (GE Vernova, Inc.)
• Original Assignee: General Electric Company
• Inventors: Jammu, Vinay Bhaskar, Behera, Ajay Kumar, Naithani, Nidhi, Badami, Vivek Venugopal, Pandey, Achalesh Kumar, Bhattacharya, Aninda, Rajagopalan, Venkatesh, Prabhu, Rahul Srinivas, Rai, Sudhanshu
• Granted Patent: US 7,941,281 B2
• Time in Patent Office: Days
• US Class Current: 702/35
• CPC Class Codes: F01D 21/003 Arrangements for testing or measuring for measuring vibrations G01H
• CPC Class Codes: F05D 2230/80 Repairing, retrofitting or upgrading methods
• CPC Class Codes: G05B 23/0221 Preprocessing measurements, e.g. data collection rate adjustment; Standardization of measurements; Time series or signal analysis, e.g. frequency analysis or wavelets; Trustworthiness of measurements; Indexes therefor; Measurements using easily measured parameters to estimate parameters difficult to measure; Virtual sensor creation; De-noising; Sensor fusion; Unconventional preprocessing inherently present in specific fault detection methods like PCA-based methods
• CPC Class Codes: G05B 23/0235 based on a comparison with predetermined threshold or range, e.g. "classical methods", carried out during normal operation; threshold adaptation or choice; when or how to compare with the threshold
• CPC Class Codes: G05B 23/0245 based on a qualitative model, e.g. rule based; if-then decisions

Abstract

A system for rotor blade health monitoring include time of arrival (TOA) sensors and a controller comprising a processor configured for obtaining TOA signals indicative of times of arrival of rotating rotor blades from the respective TOA sensors and for determining initial features from the TOA signals; and a feature level fuser configured for fusing the initial features received from the processor for use in evaluating health of the rotating rotor blades.

Claims

1. A system comprising:

time of arrival (TOA) sensors; and

a controller comprising

a processor configured for obtaining TOA signals indicative of times of arrival of rotating rotor blades from the respective TOA sensors and for determining initial features from the TOA signals; and

a feature level fuser configured for fusing the initial features received from the processor for use in evaluating health of the rotating rotor blades.

2. The system of claim 1 wherein the controller further comprises a sensor level fuser for obtaining combined features by fusing TOA signals obtained from the TOA sensors.

3. The system of claim 2 wherein the feature level fuser is further configured for fusing the combined features in addition to the initial features for use in evaluating the health of the rotating rotor blades.

4. The system of claim 1 wherein the sensors comprise leading edge sensors, trailing edge sensors or combinations thereof.

5. The system of claim 1 wherein the initial features comprise static deflection, dynamic deflection, clearance, blades twist profile, frequency detuning during transient operation, or any combination thereof.

6. The system of claim 1 wherein the processor is further configured to determine a delta TOA using the TOA and a predetermined TOA, determine a corrected delta TOA by normalizing the delta TOA for variations in the operational parameters of the rotating rotor blades, and determine the initial features using the corrected delta TOA.

7. A system comprising:

time of arrival (TOA) sensors; and

a controller comprising

a sensor level fuser configured for obtaining TOA signals indicative of times of arrival of the rotating rotor blades and fusing the TOAs signals for obtaining combined features; and

a processor configured for fusing times of arrival signals obtained from the time of arrival sensors and the combined features from the sensor level fuser for use in evaluating health of the rotating rotor blades.

8. A system comprising:

time of arrival (TOA) sensors; and

a controller comprising

a processor for obtaining TOA signals indicative of times of arrival of rotating rotor blades from the respective TOA sensors and for determining, from the TOA signals, initial features for use in evaluating the health of the rotating rotor blades;

a sensor level fuser for obtaining combined features by fusing data obtained from the TOA sensors,

a feature level fuser for fusing the times of arrival signals from the time of arrival sensors and the combined features,

a physics modeler for receiving the initial features from the processor and estimating data regarding rotor blade crack length and rotor blade crack propagation time,

a reliability modeler for estimating data regarding probability of the rotor blade crack, and

a decision level fuser for fusing data received from the feature level fuser, the physics modeler, and the reliability modeler, for determining the health of the rotating rotor blades from the fused data.

9. The system of claim 8 wherein the controller further comprises:

an onsite monitor for determining operational parameters data of the rotating rotor blades and providing the operational parameters data to the feature level fuser and the physics modeler.

10. The system of claim 9 wherein the physics modeler is further configured to receives operational parameters from the onsite monitor for estimating data regarding rotor blade crack length and rotor blade crack propagation time

11. The system of claim 9 wherein the rotor blades are housed in a compressor of a gas turbine, and wherein the onsite monitor is configured to determine at least one of a load on gas turbine, inlet guide vane angle, fuel stroke ratio, speed of the rotor blades, abnormal vibration in the rotor blades, performance of the compressor stage efficiency, temperature deviation, and pressure deviation.

12. A method comprising:

determining a time of arrival (TOA) and operational parameters of rotating rotor blades;

determining a delta TOA using the TOA and a predetermined TOA;

determining a corrected delta TOA by normalizing the delta TOA for variations in the operational parameters of the rotating rotor blades;

obtaining initial features from the corrected delta TOA; and

obtaining crack length and crack propagation time of the rotating rotor blades by fusing the initial features and the operational parameters.

13. The method of claim 12 wherein the predetermined TOA is determined using multiple TOAs of the rotating blades operating in baseline conditions.

14. The method of claim 12 further comprising:

determining TOAs for the rotating rotor blade and fusing the TOAs to determine a fused TOA;

determining combined features of the rotating rotor blades using the TOAs and the fused TOA;

wherein the combined features are fused with the initial features for determination of health of the rotating rotor blades.