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.
New Materials for Fabricated Gas Turbine Hot Section Components
Aircraft Engineering and Aerospace Technology ; 62 , 5 ; 2-7
01.05.1990
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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