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The effect of reheat treatments on recovering the creep behavior of a corrosion-resistant nickel-based superalloy
The present work is an attempt to possibly obtain the most suitable reheat treatment, which could provide the optimal microstructural characteristics for creep-exposed superalloys. After creep at 850°C/350MPa for 96h and 140h a cast nickel-based superalloy was reheat-treated with different programs,...
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Published in: | Materials science & engineering. A, Structural materials : properties, microstructure and processing Structural materials : properties, microstructure and processing, 2013-01, Vol.560, p.25-33 |
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Main Authors: | , , , , , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | The present work is an attempt to possibly obtain the most suitable reheat treatment, which could provide the optimal microstructural characteristics for creep-exposed superalloys. After creep at 850°C/350MPa for 96h and 140h a cast nickel-based superalloy was reheat-treated with different programs, and then the specimens were subjected to creep again at the same condition. Creep tests indicate that during reheat treatment applying aging at lower temperature, 850°C, for proper time (4h) before aging at 1050°C rather than a repeated standard heat treatment is beneficial to restore creep life. Creep-induced changes in the microstructure, such as excessive grain-boundary secondary M23C6 and/or M6C carbides formation, and primary MC carbides decomposition, are noticeably more advanced in the reheat-treated alloys. A quantitative study on the dissolution of σ phases and the formation of cavitations is presented. After the interrupted creep, the γ′ particles at dendrite cores remained cubic-shaped. However, the rafting of cuboidal γ′ precipitates was observed in the same creep condition by the reheat treatment programs. Design of a reheat treatment for recovering the creep properties should emphasize the promotion of ductility rather than strength of the alloy. An equation based on the continuum damage-mechanics theory, was suggested to evaluate the remaining creep life. |
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ISSN: | 0921-5093 1873-4936 |
DOI: | 10.1016/j.msea.2012.07.068 |