Apparatus and method for temperature mapping a turbine component in a high temperature combustion environment
Abstract
Method and system for calibrating a thermal radiance map of a turbine component in a combustion environment. At least one spot (18) of material is disposed on a surface of the component. An infrared (IR) imager (14) is arranged so that the spot is within a field of view of the imager to acquire imaging data of the spot. A processor (30) is configured to process the imaging data to generate a sequence of images as a temperature of the combustion environment is increased. A monitor (42, 44) may be coupled to the processor to monitor the sequence of images of to determine an occurrence of a physical change of the spot as the temperature is increased. A calibration module (46) may be configured to assign a first temperature value to the surface of the turbine component when the occurrence of the physical change of the spot is determined.
- Inventors:
- Issue Date:
- Research Org.:
- Siemens Energy, Inc., Orlando, FL (USA)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1133940
- Patent Number(s):
- 8,749,629
- Application Number:
- 13/023,774
- Assignee:
- Siemens Energy, Inc. (Orlando, FL)
- DOE Contract Number:
- FC26-05NT42644
- Resource Type:
- Patent
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 47 OTHER INSTRUMENTATION
Citation Formats
Baleine, Erwan, and Sheldon, Danny M. Apparatus and method for temperature mapping a turbine component in a high temperature combustion environment. United States: N. p., 2014.
Web.
Baleine, Erwan, & Sheldon, Danny M. Apparatus and method for temperature mapping a turbine component in a high temperature combustion environment. United States.
Baleine, Erwan, and Sheldon, Danny M. Tue .
"Apparatus and method for temperature mapping a turbine component in a high temperature combustion environment". United States. https://www.osti.gov/servlets/purl/1133940.
@article{osti_1133940,
title = {Apparatus and method for temperature mapping a turbine component in a high temperature combustion environment},
author = {Baleine, Erwan and Sheldon, Danny M},
abstractNote = {Method and system for calibrating a thermal radiance map of a turbine component in a combustion environment. At least one spot (18) of material is disposed on a surface of the component. An infrared (IR) imager (14) is arranged so that the spot is within a field of view of the imager to acquire imaging data of the spot. A processor (30) is configured to process the imaging data to generate a sequence of images as a temperature of the combustion environment is increased. A monitor (42, 44) may be coupled to the processor to monitor the sequence of images of to determine an occurrence of a physical change of the spot as the temperature is increased. A calibration module (46) may be configured to assign a first temperature value to the surface of the turbine component when the occurrence of the physical change of the spot is determined.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2014},
month = {6}
}
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