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Effects of temperature and hold time on creep-fatigue crack-growth behavior of HAYNES ® 230 ® alloy

The creep-fatigue crack-growth behavior of a HAYNES 230 superalloy was investigated at the temperatures of 649, 816 and 927 °C in laboratory air. The crack-growth experiments were conducted under the stress-intensity-factor-range or load-range control. Hold times in the range of 3 s to 5 h were impo...

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Published in:Materials science & engineering. A, Structural materials : properties, microstructure and processing Structural materials : properties, microstructure and processing, 2006-08, Vol.429 (1), p.1-10
Main Authors: Lu, Y.L., Chen, L.J., Liaw, P.K., Wang, G.Y., Brooks, C.R., Thompson, S.A., Blust, J.W., Browning, P.F., Bhattacharya, A.K., Aurrecoechea, J.M., Klarstrom, D.L.
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Language:English
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Summary:The creep-fatigue crack-growth behavior of a HAYNES 230 superalloy was investigated at the temperatures of 649, 816 and 927 °C in laboratory air. The crack-growth experiments were conducted under the stress-intensity-factor-range or load-range control. Hold times in the range of 3 s to 5 h were imposed at the maximum load to study the influence of hold time on the crack-growth behavior. The fatigue and creep crack-propagation experiments were also performed as zero and infinite hold-time experiments, respectively. The crack-growth rate increased continuously with increasing the test temperature and/or hold time. The fracture surfaces and cross-sections through the fracture surfaces were examined. As the hold time increased, the fracture appearance changed from the transgranular to intergranular mode. At higher temperatures, this transgranular–intergranular transition occurred at a shorter hold time.
ISSN:0921-5093
1873-4936
DOI:10.1016/j.msea.2005.07.039