THE DEVELOPMENT OF THE
CMSX®-11B AND CMSX®-11C ALLOYS
FOR INDUSTRIAL GAS TURBINE APPLICATION
G. L. Erickson
Cannon-Muskegon Corporation
[SPS Technologies]
Muskegon, MI U.S.A.
ABSTRACT
Two different, non-Re containing
single crystal (SX) superalloys are defined primarily for industrial
turbine application. The alloys, CMSX®-11B and CMSX-®-11C, contain
respective chromium levels of about 12.5% and 14.5%. Both materials
develop unique and extremely good blends of hot corrosion and oxidation
resistance. They exhibit extremely good castability, employ relatively
simple solution heat treatments and provide creep strength which is as
good or better in comparison to other first generation SX materials such
as CMSX-2/3, PWA 1480 and René N4. Moreover, at certain engine-pertinent
temperature/stress conditions, and particularly in long-term tests, the
alloys appear to exhibit density corrected strengths which are similar
or better than CMSX-4® and other second generation SX casting
superalloys
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