Three important wrought superalloys - Waspaloy, Inconel 718, and Astroloy - are selected for analysis here because of their promising use in the manufacture of gas turbine components. Their exceptional high temperature performance is explained in terms of alloy segregation, thermomechanical techniques, precipitation factors, and final forging characteristics.


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    Title :

    Deformation Processing of Superalloy Gas Turbine Components


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    1969 International Automotive Engineering Congress and Exposition ; 1969



    Publication date :

    1969-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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