Effect of Interfacial Roughness of Bond Coat on the Residual Adhesion Strength of a Plasma Sprayed TBC System after Thermal Cycle Fatigue(Thermal Barrier Coating Systems for Gas Turbines)

Author:

YAMAZAKI Yasuhiro1,FUKANUMA Hirotaka,OHNO Naoyuki

Affiliation:

1. Department of Mechanical and Control Engineering, Niigata Institute of Technology

Publisher

Japan Society of Mechanical Engineers

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference14 articles.

1. 1) ZHU D. Thermophysical and thermomechanical properties of thermal barrier coating systems. (2000)

2. 2) RENUSCH D. New approaches to the understanding of failure and life time prediction of thermal barrier coating systems. Conference Proceedings in Life Time Modeling of High Temperature Corrosion Process, 2001. (2001) p.324-339.

3. 3) RENUSCH D. Progress in life time modeling of APS-TBC Part I : residual, thermal and growth stresses including the role of thermal fatigue. Materials at High Temperatures. (2004) vol.21, no.2, p.65-76.

4. 4) Subcommittee on Superalloys and Coatings JSMS. Reports of Phase III Activities-Adhesion Strength of Thermal Barrier Coatings Subjected to High Temperature Exposure and Thermal Cycles-. The Society of Materials Science, Japan. (2009) vol.Section 4.3,

5. 5) YAMAZAKI Y. Influence of the spray process parameters and the thermal exposure on the mechanical properties of the free-standing air-plasma sprayed thermal barrier coating. Journal of Japan Thermal Spraying Society. (2007) vol.44, no.3, p.88-95.

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