System and method for monitoring component health using resonance

• US 10,018,596 B2
• Filed: 03/04/2016
• Issued: 07/10/2018
• Est. Priority Date: 03/04/2016
• Status: Active Grant

• Current Assignee: GE Infrastructure Technology, LLC (General Electric Company)
• Original Assignee: General Electric Company
• Inventors: Tralshawala, Nilesh, D'Souza, Prashanth, Yoganatha Babu, Ravi
• Primary Examiner(s): SAINT SURIN, JACQUES M
• Application Number:
  US15/061,505
• Publication Number:
  US 20170254783A1
• Time in Patent Office: 858 Days
• Field of Search: 73587
• CPC Class Codes: G01N 2291/014 Resonance or resonant frequency
• CPC Class Codes: G01N 2291/0258 Structural degradation, e.g. fatigue of composites, ageing of oils
• CPC Class Codes: G01N 2291/044 Internal reflections (echoes), e.g. on walls or defects
• CPC Class Codes: G01N 2291/2693 Rotor or turbine parts
• CPC Class Codes: G01N 29/12 by measuring frequency or resonance of acoustic waves measuring frequency or resonant frequency of mechanical vibrations or acoustic waves in general G01H1/06, G01H3/04, G01H13/00; acoustic resonators G10K11/04; vibration or shock testing of structures G01M7/00
• CPC Class Codes: G01N 29/14 using acoustic emission techniques echo of particles G01N29/046; measuring mechanical vibrations or acoustic waves in solids in general G01H1/00
• CPC Class Codes: G01N 29/4445 Classification of defects
• CPC Class Codes: G01N 29/46 by spectral analysis, e.g. Fourier analysis or wavelet analysis spectral signal processing per se G06F17/14

Abstract

This disclosure provides systems and methods for using a health monitoring system with acoustic emissions (AE) signals and the resonance frequency of the damage state of a component in a machine to monitor component health. AE signals collected from sensors on an operating machine are analyzed to identify signal features or events that correspond to component resonance frequencies. The AE signal features proximate to the component resonance frequencies and how those features and the component resonance frequency changes over time enable the identification and monitoring of damage states, such as cracks in the stator vanes of a compressor, gas turbine, steam turbine, or generator.

Claims

1. A system comprising:

a plurality of sensing devices configured to generate acoustic emission (AE) signals that are representative of acoustic emission waves propagating through at least one component of a machine, wherein the at least one component has a damage state and the damage state has a resonance frequency; and

a processing subsystem that is in operational communication with the plurality of sensing devices to receive AE signals, wherein the processing subsystem includes a resonance detection system that identifies the resonance frequency of the damage state during operation of the machine using the AE signals;

wherein the processing subsystem monitors the damage state of the at least one component using the resonance detection system; and

wherein the resonance frequency of the damage state of the at least one component changes over time and the processing subsystem monitors the magnitude of the AE signals proximate the resonance frequency and the change in the resonance frequency over time to determine risk to health of the at least one component.

2. The system of claim 1, wherein the processing subsystem is configured to monitor health of a plurality of components by location during real-time operation of the machine, the plurality of components including the at least one component.

3. The system of claim 1, wherein the at least one component is a stator vane.

4. The system of claim 1, wherein the machine is selected from a compressor, a gas turbine, a steam turbine, and a generator.

5. The system of claim 1, wherein the resonance frequency of the damage state is detected during a change in an operational state of the machine that causes an excitation in the component at the resonance frequency of the damage state and creates a detectable event in the AE signals.

6. The system of claim 5, wherein the resonance detection system operates during a start-up operation and a shutdown operation of the machine.

7. The system of claim 1, wherein the AE signals proximate the resonance frequency of the damage state are associated with rubbing of crack faces and the resonance detection system distinguishes rubbing of crack faces from crack propagation.

8. The system of claim 7, wherein the resonance detection system uses a rise time value and an amplitude value of the AE signals proximate the resonance frequency to distinguish rubbing of crack faces from crack propagation.

9. The system of claim 1, wherein the resonance detection system comprises a plurality of crack detection algorithms based on AE signal features, machine operating data, and models of crack behavior.

10. A method of monitoring the health of a component of a machine, the method comprising:

generating acoustic emission (AE) signals that are representative of acoustic emission waves propagating through at least one component of the machine, wherein the at least one component has a damage state and the damage state has a resonance frequency;

identifying the resonance frequency of the damage state during operation of the machine using received AE signals; and

monitoring the damage state of the at least one component using the received AE signals proximate the resonance frequency of the damage state, wherein the resonance frequency of the damage state of the at least one component changes over time and the monitoring of the damage state comprises monitoring the magnitude of the AE signals proximate the resonance frequency and the change in the resonance frequency over time to determine risk to health of the at least one component.

11. The method of claim 10, wherein monitoring the damage state further comprises monitoring the health of a plurality of components by location during real-time operation of the machine, the plurality of components including the at least one component.

12. The method of claim 10, wherein the at least one component is a stator vane.

13. The method of claim 10, wherein the machine is selected from a compressor, a gas turbine, a steam turbine, and a generator.

14. The method of claim 10, wherein the resonance frequency of the damage state is identified during a change in an operational state of the machine that causes an excitation in the component at the resonance frequency of the damage state and creates a detectable event in the received AE signals.

15. The method of claim 14, wherein monitoring the damage state operates during a start-up operation and a shutdown operation of the machine.

16. The method of claim 10, wherein the received AE signals proximate the resonance frequency of the damage state are associated with rubbing of crack faces and the monitoring of the damage state distinguishes rubbing of crack faces from crack propagation.

17. The method of claim 16, wherein the monitoring of the damage state uses a rise time value and an amplitude value of the received AE signals proximate the resonance frequency to distinguish rubbing of crack faces from crack propagation.

18. The method of claim 10, wherein identifying the resonance frequency comprises a plurality of crack detection algorithms based on AE signal features, machine operating data, and models of crack behavior.

19. A system for monitoring component health of a machine, comprising:

an acoustic emission (AE) data receiver for receiving AE signals that are representative of acoustic emission waves propagating through at least one component of the machine, wherein the at least one component has a damage state and the damage state has a resonance frequency;

a resonance detection system for identifying the resonance frequency of the damage state during operation of the machine using the AE signals; and

a health response system for monitoring the damage state of the at least one component using the AE signals proximate the resonance frequency of the damage state, wherein the health response system uses the magnitude of the AE signals proximate the resonance frequency and the change in the resonance frequency over time to calculate a crack growth rate and the crack growth rate is used to generate the response to the detected risk to health of the at least one component.

20. The system of claim 19, further comprising an AE feature extraction system and an operations data receiver used by the resonance detection system for identifying the resonance frequency of the damage state.

21. The system of claim 19, wherein the health response system uses the magnitude of the AE signals proximate the resonance frequency and the change in the resonance frequency over time to calculate a crack growth rate and the crack growth rate is used to generate the response to the detected risk to health of the at least one component.