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Advanced thermal barrier coating systemsCurrent state-of-the-art thermal barrier coating (TBC) systems consist of partially stabilized zirconia coatings plasma sprayed over a MCrAlY bond coat. Although these systems have excellent thermal shock properties, they have shown themselves to be deficient for a number of diesel and aircraft applications. Two ternary ceramic plasma coatings are discussed with respect to their possible use in TBC systems. Zirconia-ceria-yttria (ZCY) coatings were developed with low thermal conductivities, good thermal shock resistance and improved resistance to vanadium containing environments, when compared to the baseline yttria stabilized zirconia (YSZ) coatings. In addition, dense zirconia-titania-yttria (ZTY) coatings were developed with particle erosion resistance exceeding conventional stabilized zirconia coatings. Both coatings were evaluated in conjunction with a NiCr-Al-Co-Y2O3 bond coat. Also, multilayer or hybrid coatings consisting of the bond coat with subsequent coatings of zirconia-ceria-yttria and zirconia-titania-yttria were evaluated. These coatings combine the enhanced performance characteristics of ZCY with the improved erosion resistance of ZTY coatings. Improvement in the erosion resistance of the TBC system should result in a more consistent delta T gradient during service. Economically, this may also translate into increased component life simply because the coating lasts longer.
Document ID
19890004287
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dorfman, M. R.
(Metco, Inc. Westbury, NY, United States)
Reardon, J. D.
(Metco, Inc. Westbury, NY, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Publication Information
Publication: NASA, Lewis Research Center, Thermal Barrier Coatings. Abstracts and Figures
Subject Category
Nonmetallic Materials
Accession Number
89N13658
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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