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Creep-fatigue behavior of a new generation Ni-base superalloy for aeroengine usage

✍ Scribed by J.M. Silva; R.A. Cláudio; C. Moura Branco; J. Martins Ferreira

Book ID
108255664
Publisher
Elsevier
Year
2010
Tongue
English
Weight
595 KB
Volume
2
Category
Article
ISSN
1877-7058

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Nickel-based superalloy single crystal specimens have been tested under anisothermal creep conditions using two different routes, both including an overheating stage. In the first route, the material is tested under creep conditions at 1050 • C, then submitted to an overheating regime at 1200 • C, a