Materials have been developed in recent years which are particularly well-suited for use in fabricated gas turbine hot section components. Among these are HAYNES® alloy No. 230 and HASTELLOY® alloy S. These alloys combine very good performance characteristics with capability for fabrication into such complex components as combustion chambers, afterburner flame-holders, seal rings, and thermocouple/probe assemblies. The properties and fabrication characteristics of these two materials are reviewed and compared with other well-known gas turbine alloys.


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    Title :

    New Materials for Fabricated Gas Turbine Hot Section Components


    Contributors:


    Publication date :

    1990-05-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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