Phosphor thermometry in gas turbines: Consideration factors

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Volumn 224, Issue 7, 2010, Pages 745-755

  Khalid, A H ^a   Kontis, K ^a   Behtash, H Z ^a  

^a UNIVERSITY OF MANCHESTER   (United Kingdom)

Author keywords

consideration factors; design; engine; phosphor; rotating; thermometry; turbines

Indexed keywords

ACCURATE MEASUREMENT; BLACK BODY RADIATION; BONDING TECHNIQUES; CONSIDERATION FACTORS; DESIGN LIMITS; DESIGN PHILOSOPHY; ENGINEERS DESIGN; GAS TURBINE EFFICIENCY; HIGH TEMPERATURE; MEASUREMENT SYSTEM; OPTICAL ACCESS; OPTIMUM TEMPERATURE; PHOSPHOR THERMOMETRY; PROBE DESIGN; TEMPERATURE LIMITS; THERMAL EFFICIENCY; THERMAL MAPS; TURBINE ENGINE; TURBINE INLET TEMPERATURE;

ANTENNA RADIATION; ENGINES; GAS TURBINES; LIGHT EMISSION; MEASUREMENTS; PHILOSOPHICAL ASPECTS; PHOSPHORS; ROTATION; TEMPERATURE; TEMPERATURE MEASUREMENT; TEMPERATURE SENSORS; THERMOCOUPLES; THERMOMETERS; TURBOMACHINERY;

DESIGN;

EID: 77954037830     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/09544100JAERO560     Document Type: Article

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