Apparatus and method for monitoring and quantifying progression of a structural anomaly in a high temperature environment of a combustion turbine engine
US-9354190-B2 · May 31, 2016 · US
US9670793B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9670793-B2 |
| Application number | US-201414255991-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 18, 2014 |
| Priority date | Apr 18, 2014 |
| Publication date | Jun 6, 2017 |
| Grant date | Jun 6, 2017 |
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Official abstract text for this publication.
A thermal imaging system that detects the growth of cracks in a structural element, where the system has particular application for detecting the growth of cracks and similar defects in a turbine blade. The thermal imaging system includes at least one infrared (IR) fiber optic cable where a sensing end of the fiber optic cable is positioned in close proximity to a location where a crack in the structural element may occur. Infrared emissions generated as a result of crack growth are collected by the IR fiber cable and transmitted by the cable to an infrared monitoring device. The amount of heat that is detected provides an indication of whether the crack is growing, and if so, at what rate.
Opening claim text (preview).
What is claimed is: 1. A thermal imaging system for detecting crack growth in a structure, said system comprising: at least one infrared (IR) fiber optic cable including a collection end and a detection end, the fiber optic cable configured to collect and transmit infrared radiation; and a detection and monitoring device coupled to the detection end of the at least one IR fiber optic cable, the at least one infrared fiber optic cable being operable to collect IR emissions generated by heat from the growth of the crack in the structure at the collection end and said detection and monitoring device being operable to receive the IR emissions at the detection end and convert the IR emissions to a signal that identifies the crack growth. 2. The system according to claim 1 wherein the structure is a turbine blade. 3. The system according to claim 1 wherein the at least one IR fiber optic cable includes one or more of the group consisting of a single fiber optical cable, a linear array of fiber optic cables aligned in a straight line, a select array of fiber optic cables, where a group of the fiber optic cables are aimed along a path of crack propagation, a select array of fiber optic cables, where the fiber optic cables are aimed at suspect crack locations, a planar array of individual fiber optic cables, and an infrared camera. 4. The system according to claim 1 wherein the at least one fiber optic cable is a plurality of IR fiber optic cables each including a collection end and a detection end. 5. The system according to claim 4 wherein the collection ends of all of the fiber optic cables are aligned in a row. 6. The system according to claim 4 wherein the detection end of each fiber optic cable is coupled to the detection and monitoring device. 7. The system according to claim 1 wherein the detection and monitoring device monitors operating parameters of a machine in which the structure is located and identifies the operating parameters that cause crack growth to occur. 8. The system according to claim 1 wherein the detection and monitoring device determines the size of the crack and rate that crack growth is occurring. 9. A gas turbine comprising: a shaft rotatably provided along a center line of the turbine; a compressor section responsive to a working fluid and being operable to compress the working fluid to produce a compressed working fluid; a combustion section in fluid communication with the compressor section that receives the compressed working fluid, said combustion section mixing the compressed working fluid with a fuel and combusting the compressed fluid and fuel mixture to produce a hot working fluid; a turbine section in fluid communication with the combustion section, said turbine section expanding the hot working fluid to produce mechanical power through rotation of the shaft; and a thermal imaging system for detecting crack growth on a structure in the compressor section, the combustion section or the turbine section, said system including at least one infrared (IR) fiber optic cable including a collection end and a detection end, and a detection and monitoring device coupled to the detection end of the at least one IR fiber optic cable, the infrared fiber optic cable being operable to collect IR emissions generated by heat from the growth of the crack in the structure at the collection end and said detection and monitoring device being operable to receive the IR emissions at the detection end and convert the IR emissions to a signal that identifies the crack growth. 10. The turbine according to claim 9 wherein the structure is a turbine blade. 11. The turbine according to claim 9 wherein the at least one fiber optic cable is a plurality of IR fiber optic cables each including a collection end and a detection end. 12. The turbine according to claim 11 wherein the collection ends of all of the fiber optic cables are aligned in a row. 13. The turbine according to claim 11 wherein the detection end of each fiber optic cable is coupled to the detection and monitoring device. 14. The turbine according to claim 9 wherein the detection and monitoring device monitors operating parameters of a machine in which the structure is located and identifies the operating parameters that cause crack growth to occur. 15. The turbine according to claim 9 wherein the detection and monitoring device determines the size of the crack and rate that crack growth is occurring.
Testing, e.g. methods, components or tools therefor · CPC title
Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges · CPC title
Arrangements for testing or measuring (for measuring vibrations G01H) · CPC title
to temperature · CPC title
Investigating presence of flaws · CPC title
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