Superalloy heat treatment for promoting crack growth resistance

Alloys or metallic compositions – Nickel base – Chromium containing

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148410, 148675, C22C 1905

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active

053286596

ABSTRACT:
Nickel base superalloy articles, especially gas turbine disks, are provided with substantially enhanced resistance to crack growth through a specific heat treatment. The heat treatment employs a true solution treatment step followed by a subsolvus solution treatment step, followed by at least one aging step. The effect of this series of heat treatment steps is to provide a microstructure having an optimum arrangement of gamma prime particles, with respect to both size and location. Reductions in crack growth rates of several hundred percent relative to prior art heat treatments are achieved.

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The Effects of Microstructure on Elevated Temperature Crack Growth in Nickel-Base Superalloys, by H. F. Merrick et al., Metallurgical Transactions, Feb. 1978.
Metallurgical Factors Affecting the Crack Growth Resistance of a Superalloy by J. M. Larson et al., Metallurgical Transactions, Jan. 1977.

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