DocumentCode :
1689370
Title :
Phosphor thermometry for high temperature gas turbine applications
Author :
Feist, J.P. ; Heyes, A.L. ; Choy, K.L. ; Su, B.
Author_Institution :
Dept. of Mech. Eng., Imperial Coll. of Sci., Technol. & Med., London, UK
fYear :
1999
fDate :
6/21/1905 12:00:00 AM
Firstpage :
42522
Lastpage :
42528
Abstract :
In the paper developments and some preliminary experiments concerning the application of thermographic phosphors for surface temperature and heat flux measurements in gas turbine combustion chambers are presented. When illuminated with UV light (typically from a pulsed laser) these material exhibits phosphorescence, which is temperature dependent by virtue of variations in the relative intensity of distinct emission lines or of variations in the time constant of the exponential emission decay which occurs once excitation has ceased. Both modes of sensitivity have been investigated with a range of phosphors including are YAG:Tb, YAG:Dy and Y2O3:Eu. Of these YAG:Dy has been shown to be best suited to measurements in combustion chambers. It is sensitive to temperatures in the range 300 to 1500 K, emits light in the blue green region of the spectrum where blackbody radiation is relatively weak and exhibits both modes of sensitivity. In addition a number of techniques for laying down phosphor coatings on metal substrates are reviewed and an experimental investigation of two techniques is presented Firstly, the use of chemical binders similar to those used in thermal paints and, secondly, a new cost effective coating technique referred to as Electrostatic assisted Combustion Chemical Vapour Deposition (EACVD) which has been developed in the Materials Department at Imperial College. The latter allows thin layers of phosphors to be laid down without the need for a chemical binder and with close control of coating composition and thickness. To demonstrate the technique a 2 μm thick layer of Y2O3:Eu has been laid down on a nimonic substrate and a performance comparison made with a similar coating laid down using the alternative chemical binder technique. The EACVD coating has been shown to be more robust than those laid down with chemical binders whilst the coating shows similar temperature sensitivity
Keywords :
CVD coatings; aerospace engines; chemical vapour deposition; combustion; dysprosium; europium; gas turbines; high-temperature techniques; phosphors; temperature measurement; terbium; yttrium compounds; 2 mum; 300 to 1500 K; Imperial College; UV light; Y2O3:Eu; YAG:Dy; YAG:Tb; YAl5O12:Dy; YAl5O12:Tb; blackbody radiation; blue green region; chemical binder; chemical binders; coating composition; coating thickness; electrostatic assisted combustion CVD; emission lines; gas turbine combustion chamber; heat flux measurement; high temperature gas turbine; metal substrates; nimonic substrate; phosphor coatings; surface temperature; temperature sensitivity; thermal paints; thermographic phosphor; Chemicals; Coatings; Combustion; Gas lasers; Laser modes; Optical pulses; Phosphors; Surface emitting lasers; Temperature sensors; Turbines;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation in Aerospace Simulation Facilities, 1999. ICIASF 99. 18th International Congress on
Conference_Location :
Toulouse
Print_ISBN :
0-7803-5715-9
Type :
conf
DOI :
10.1109/ICIASF.1999.827145
Filename :
827145
Link To Document :
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