Turbomachine monitoring system and method

1. A system, comprising:

a turbomachine comprising a first turbomachine component having a first mechanoluminescent material, wherein the first turbomachine component produces a first light emission upon exposure to a mechanical stimulus sufficient to cause mechanoluminescence by the first mechanoluminescent material; and

a turbomachine monitoring system comprising a controller, wherein the controller comprises data acquisition and processing circuitry configured to monitor the structural health of the first turbomachine component based on an analysis of the first light emission by correlating the first light emission to the mechanoluminescence of the first turbomachine component, and to provide a user-perceivable indication of the structural health of the first turbomachine component, adjust an operating speed of the turbomachine in response to the first light emission, or a combination thereof, based on the analysis.

2. The system of claim 1 , wherein the turbomachine monitoring system comprises a photodetector that detects the first light emission and produces a first electrical signal representative of the first light emission, and wherein the controller is configured to analyze the first electrical signal to measure a parameter relating to the first light emission.

3. The system of claim 2 , wherein the controller is configured to measure the parameter to determine whether the first light emission is indicative of mechanical failure or an incipient mechanical failure of the first turbomachine component.

4. The system of claim 2 , wherein the parameter comprises an intensity of the detected first light emission, a relative intensity of one or more wavelengths within the first light emission, a timing of the first light emission, a wavelength of the first light emission, a frequency of the first light emission, or any combination thereof.

5. The system of claim 2 , wherein the turbomachine monitoring system comprises a fiber optic cable optically coupling the first turbomachine component with the photodetector.

6. The system of claim 1 , wherein the turbomachine monitoring system comprises a camera configured to capture at least a portion of the first light emission.

7. The system of claim 1 , wherein the turbomachine comprises a turbine, a compressor, or a pump, and the first turbomachine component comprises at least a portion of a fuel nozzle, a combustor, an exhaust section, a rotating blade, or any combination thereof.

8. The system of claim 1 , wherein the first turbomachine component comprises a plurality of laminated plies each formed from a ceramic matrix composite (CMC).

9. The system of claim 1 , wherein the turbomachine comprises a second turbomachine component having a second mechanoluminescent material, and the second turbomachine component produces a second light emission upon exposure to a second mechanical stimulus sufficient to cause the emission by the second mechanoluminescent material, and wherein the data acquisition and processing circuitry is configured to monitor the structural health of the second component based on an additional analysis of the second light emission by correlating the second light emission to mechanoluminescence of the second turbomachine component, and wherein the data acquisition and processing circuitry is configured to provide a user-perceivable indication of the structural health of the second turbomachine component, adjust an operating speed of the turbomachine in response to the second light emission, or a combination thereof, based on the additional analysis.

10. The system of claim 9 , wherein the first light emission and the second light emission each comprise one or more characteristic emission parameters, and the turbomachine monitoring system is configured to differentiate between the first and second light emissions to determine whether a mechanical failure or incipient mechanical failure of the first turbomachine component and the second turbomachine component is indicated.

11. The system of claim 1 , wherein the mechanical stimulus comprises at least one of pressure on the first mechanoluminescent material, abrasion on the first mechanoluminescent material, vibratory and steady loads on the first mechanoluminescent material, or foreign object damage on the first mechanoluminescent material.

12. A system, comprising:

a turbomachine monitoring system communicatively coupled to a turbomachine, comprising:

a photodetector that detects a light emission from a turbomachine component having a mechanoluminescent material; and

a controller communicatively coupled to the photodetector and comprising data acquisition and processing circuitry configured to measure a parameter relating to the light emission by correlating the light emission to mechanoluminescence of the turbomachine component, and wherein the data acquisition and processing circuitry is configured to monitor a structural health of the turbomachine based on the parameter and to provide a user-perceivable indication of the structural health of the turbomachine component, adjust an operating speed of the turbomachine in response to the light emission, or a combination thereof.

13. The system of claim 12 , wherein the controller is configured to determine whether the light emission is a result of piezoluminescence, fractoluminescence, or triboluminescence, or a combination thereof, based on the parameter or another measured parameter relating to the light emission.

14. The system of claim 12 , wherein the turbomachine monitoring system comprises a fiber optic waveguide configured to be placed within or proximate a hot gas path of the turbomachine to enable the fiber optic waveguide to transmit at least a portion of the light emission from the turbomachine component to the photodetector.

15. The system of claim 12 , comprising the turbomachine, wherein the turbomachine comprises a gas turbine engine having a hot gas path comprising:

a combustor that combusts a fuel in the presence of compressed air to produce hot combustion gases;

a turbine that receives the hot combustion gases from the combustor and causes an interaction between the hot combustion gases and a turbine blade to produce mechanical energy and exhaust gases; and

an exhaust that outputs the exhaust gases from the gas turbine engine; and

wherein the turbomachine component comprises a combustion liner, an exhaust duct, a turbine shroud, the turbine blade, or a turbine wheel.

16. The system of claim 15 , wherein the turbomachine component comprises a plurality of laminated plies each formed from a ceramic matrix composite (CMC), and at least one of the plurality of laminated plies is formed from a silicon carbide CMC.

17. The system of claim 16 , wherein the silicon carbide CMC is a first mechanoluminescent material that produces a first characteristic mechanoluminescent emission, and at least one other of the plurality of laminated plies comprises a second mechanoluminescent material that produces a second characteristic mechanoluminescent emission, and the controller is configured to determine whether the detected light emission is the first characteristic mechanoluminescent emission, the second characteristic mechanoluminescent emission, or both, to determine the structural health of the turbomachine component.

18. A method, comprising:

monitoring a hot gas path of a gas turbine engine for mechanoluminescent emissions with a turbomachine monitoring system;

detecting a first mechanoluminescent emission using a photodetector of the turbomachine monitoring system; and

determining whether the first mechanoluminescent emission is indicative of a mechanical failure or an incipient mechanical failure of a component of the gas turbine engine using a controller of the turbomachine monitoring system.