Abstract
The changes in hardness and room temperature impact toughness of Hastelloy ∗ Alloy X∗Hastelloy is a registered trademark of Cabot Corporation. after aging at 1000, 1200, 1400 and 1600°F (538, 649, 760 and 871°) for times up to 10,000 h were investigated. The alloy exhibits age-hardening at 1200 and 1400°F (649 and 760°).’A slight hardness increase was observed at 1600°F (871°) followed by overaging after 4000 h. No age-hardening was observed at 1000°F (538°) up to 10,000 h. Aging at all temperatures resulted in a substantial drop in room temperature impact toughness. The microstructure after aging was characterized by optical metallography and X-ray diffraction, while fracture mode was characterized by scanning electron microscopy. The results suggest that the toughness degradation is primarily associated with carbide precipitation. M6C’ type carbides are believed to be the major phase precipitated during aging at all temperatures, although σ and µphases were also detected after 10,000 h at 1400 and 1600°F (760 and 871°), respectively.
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References
W. L. Clarke and G. W. Titus: Report No. AGN-8289, vol. 1, Nuclear Division, Aerojet-General Corporation, San Ramon, California, June 1968.
S. J. Matthews: Report No. 8979, Stellite Division, Cabot Corporation, Kokomo, Indiana, February 1976.
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Lai, G.Y. An investigation of the thermal stability of a commercial Ni-Cr-Fe-Mo alloy (hastelloy alloy X). Metall Trans A 9, 827–833 (1978). https://doi.org/10.1007/BF02649792
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DOI: https://doi.org/10.1007/BF02649792