Part One reviews the application of turbine blade and vane cooling in current Rolls-Royce civil aero engines, together with some side effects on engine design and development.Part Two presents a history of turbine blade and vane material improvement and of aircooling development as applied in these engines. Related problems affecting turbine blade and vane deterioration in engines are described, and an outline is given of a method of creep life determination in cooled blades.


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    Title :

    Cooling Modern Aero Engine Turbine Blades and Vanes


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    1966 Automotive Engineering Congress and Exposition ; 1966



    Publication date :

    1966-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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