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Thermo-Span® Alloy

(U.S. Patent No. 5,283,032)

Nominal Analysis
0.05 C, 0.50 Mn, 0.30 Si, 0.015 P, 0.015 S, 5.50 Cr, 25.00 Ni, 29.00 Co, 0.80 Ti, 4.80 Cb, 0.50 Al, 0.50 Cu, 0.01 B, Bal. Fe

Precipitation hardenable superalloy exhibiting a low coefficient of thermal expansion over a broad temperature range, high tensile and rupture strengths, and good thermal fatigue resistance. Significant improvement in environmental resistance over CTX alloys due to chromium addition. Excellent combination of tensile properties and stress rupture strength in the recrystallized condition with the use of common solution and age hardening treatments. Should be considered for use in all applications for which the current low expansion superalloys are suited, including compressor and exhaust casings, seals, and other gas turbine engine components.

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