Optical pyrometry for gas turbine aeroengines
- 1 December 2004
- journal article
- Published by Emerald Publishing in Sensor Review
- Vol. 24 (4), 378-386
- https://doi.org/10.1108/02602280410558412
Abstract
Fundamentally, it is advantageous to operate an aeroengine's thermodynamic cycle at as high a turbine entry temperature as practical for the current metallurgical limits of the turbine blades in order to achieve peak cycle efficiency and thus lower specific fuel consumption. However, achieving the highest possible turbine entry temperature requires accurate knowledge of the turbine blade temperatures for control purposes to prolong component life as frequent excursions beyond the design limits of the blades can severely reduce their service life. The optical pyrometry technique represents the best method for providing this crucial temperature data needed for blade condition-based monitoring. This paper presents the general operating principles, system aspects and design considerations for the application of the optical pyrometer instrument for inflight service use on gas turbine aeroengines.Keywords
This publication has 10 references indexed in Scilit:
- A Review of Purge Air Designs for Aeroengine-Based Optical PyrometersJournal of Turbomachinery, 2002
- A strategic review of the large civil aeroengine market and the paradigm shift to a service-The Aeronautical Journal, 2001
- Emissivity measurements for YSZ thermal barrier coating at high temperatures using a 1.6-?m single-wavelength pyrometerOptical Engineering, 1998
- Dynamic turbine blade temperature measurementsJournal of Propulsion and Power, 1994
- Dynamic turbine blade temperature measurementsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Optical Systems For Gas Turbine EnginesPublished by SPIE-Intl Soc Optical Eng ,1986
- Radiation Thermometry—The Measurement ProblemPublished by ASTM International ,1985
- Temperature Measurement for Advanced Gas Turbine ControlsSAE International Journal of Advances and Current Practices in Mobility, 1975
- Experiences in the Design and Application of Turbine Blade PyrometersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Radiation Pyrometer for Gas Turbine BladesSAE International Journal of Advances and Current Practices in Mobility, 1972