Effects of High Temperature Deformation and Thermal Exposure on Microstructure and Mechanical Properties of Co-Based Superalloy

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Abstract:

The gas turbine components operated in hot combustion gas undergo material degradation due to the thermal cycles. The failure mechanism of the hot gas components would be accompanied by material degradation in the properties of high temperature strength and creep rupture time. Many stationary parts in gas turbine are made of Co-based superalloy because of their high temperature performance. In this work, we survey the time and temperature dependent degradation of Co-based superalloy. We prepared the specimens of Co-based superalloy ECY768 that are exposed at 871 and 982 oC in 1000 ~ 5000 hours. We carried out the mechanical test and microstructural observation.

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121-123

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July 2011

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© 2011 Trans Tech Publications Ltd. All Rights Reserved

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[1] J.S. Lee, H.C. Kim, J.H. Lee, S.M. Seo and C.Y. Jo : Solidification Microstructure and Carbide Formation Behaviors in the Co-base Superalloy ECY768, Korean Journal of Materials Research 13, 381-388 (2003).

DOI: 10.3740/mrsk.2003.13.6.381

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[2] Heat-Resistant Materials, ASM Specialty Handbook, ASM Inter. (1977).

Google Scholar

[3] M. Durand-Charre : The Microstructure of Superalloys, CRC Press (1997).

Google Scholar

[4] C.T. Sims, N.S. Stoloff and W.C. Hagel : Superalloys , John Wiley & Sons (1987).

Google Scholar

[5] G. E. Dieter : Mechanical Metallurgy, McGraw-Hill (1986).

Google Scholar