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Examination of In-Service Coating Degradation in Gas Turbine Blades Using a Small Punch Testing Method

Published online by Cambridge University Press:  10 February 2011

J. Kameda
Affiliation:
Center for Advanced Technology Development, Iowa State University, Ames, IA 50011
T. E. Bloomer
Affiliation:
Center for Advanced Technology Development, Iowa State University, Ames, IA 50011
C. R. Gold
Affiliation:
Center for Advanced Technology Development, Iowa State University, Ames, IA 50011
Y. Sugita
Affiliation:
Mechanical Engineering Research Laboratory, Hitachi Ltd., Hitachi, 317, Japan
M. Ito
Affiliation:
Electric Power R & D Center, Chubu Electric Power Co., Inc., Nagoya, 458, Japan.
S. Sakurai
Affiliation:
Mechanical Engineering Research Laboratory, Hitachi Ltd., Hitachi, 317, Japan
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Abstract

This paper describes examination of in-service coating degradation in land based gasturbine blades by means of a small punch testing (SP) method and scanning Auger microprobe(SAM). SP tests on coated specimens with unpolished surfaces indicated large variations ofthe mechanical properties because of the surface roughness and curvature in gas turbine blades, SP tests on polished specimens better characterized the mechanical degradation of bladecoatings. The coated specimens greatly softened and the room temperature ductility of thecoatings and substrates tended to decrease with increasing operation time. The ductile-brittletransition temperature of the coatings shifted to higher temperatures during the bladeoperation. From SAM analyses on fracture surfaces of unused and used blades, it has beenshown that oxidation and sulfidation near the coating surface, which control the fractureproperties, result from high temperature environmental attack.

Type
Research Article
Copyright
Copyright © Materials Research Society 1996

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References

1. Viswanathan, R and Allen, J. M.(eds.), Life Assessment and Repair Technology for Combustion Turbine Hot Section Components(ASM International, Materials Park, 1990).Google Scholar
2. Sehitoglu, H. (ed), Thermomechanical Fatigue Behavior of Materials, ASTM STP 1186, (American Society for Testing and Materials, Philadelphia, 1993),Google Scholar
3. Sugita, Y., Ito, M., Isobe, N., Sakurai, S., Gold, C.R, Bloomer, T.E and Kameda, J., Mater. Manuf Proc. 105, 987 (1995).Google Scholar
4. Sugita, Y., Ito, M, Sakurai, S., Gold, C.R, Bloomer, T. E. and Kameda, J., in Materials Aging and Component Life Extension, edited by Bicego, V., Nitta, A. and Viswanathan, R. (EMAS, West Midland, 1995), p. 307.Google Scholar
5. Kameda, J., Bloomer, T. E., Sugita, Y., Ito, M. and Sakurai, S., to be published.Google Scholar
6. Baik, J. M., Kameda, J. and Buck, O, Scripta Metall. 17, 1143 (1983); in The Use of Small-scale Specimen for Testing Irradiated Materials, ASTM STP 888, edited by W. R.Corwin and G. E. Lucas (American Society for Testing and Materials, Philadelphia, 1986), p. 92 X Mao and H Takahashi, J. Nucl. Mater. 150, 42 (1987).Google Scholar
8. Kameda, J. and Mao, X, J. Mater. Sci. 27, 983 (1992).Google Scholar
9. Liu, C T. and White, C. L., Acta Metall. 35, 643 (1987)Google Scholar