New Materials for Fabricated Gas Turbine Hot Section Components PUBLIC ACCESS

[+] Author Affiliations
M. F. Rothman, C. R. Patriarca

Haynes International, Inc, Kokomo, IN

Paper No. 87-GT-59, pp. V005T11A003; 8 pages
  • ASME 1987 International Gas Turbine Conference and Exhibition
  • Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Process Industries; General
  • Anaheim, California, USA, May 31–June 4, 1987
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7927-6
  • Copyright © 1987 by ASME


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 flameholders, 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.

Copyright © 1987 by ASME
Topics: Gas turbines
This article is only available in the PDF format.



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