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Thursday, June 9, 2005 - 10:30 AM
HTM053.7

Next Generation Thermal Barrier Coating (TBC) Designs with Increased Reflectivity and Lower Thermal Conductivity for High Temperature Turbine Applications

J. Singh, D. E. Wolfe, Penn State University, University Park, PA; J. I. Eldridge, D. M. Zhu, NASA Glenn Research, Cleveland, OH

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Summary: This paper discusses the current and future trends with next generation thermal barrier coating (TBC) designs in developing TBC with lower thermal conductivity, increased reflectivity, and increased performance through nano-layered structures, microstructural modifications and rare-earth dopants for non-intrusive evaluation of coating life.