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.


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    Titel :

    Turbine blade radiation pyrometer system


    Beteiligte:
    CURWEN, K.R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1972-12-01


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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