EVER SINCE the invention of the gas turbine engine accurate measurement and indication of the working temperature of the turbine has been a prime requirement, in order to limit the environmental stresses of the very hot components in that area. It is now recognised by most authorities that a radiation pyrometer viewing the rotor blades offers considerable potential advantages as an engine temperature sensor over the use of a thermocouple array in the exhaust gas.
Turbine blade radiation pyrometer system
Aircraft Engineering and Aerospace Technology ; 44 , 12 ; 16-21
1972-12-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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