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Advanced Oxide Material Systems For 1650 C Thermal/Environmental Barrier Coating ApplicationsAdvanced thermal/environmental barrier coatings (T/EBCs) are being developed for low emission SiC/SiC ceramic matrix composite (CMC) combustor and vane applications to extend the CMC liner and vane temperature capability to 1650 C (3000 F) in oxidizing and water-vapor containing combustion environments. The 1650 C T/EBC system is required to have better thermal stability, lower thermal conductivity, and improved sintering and thermal stress resistance than current coating systems. In this paper, the thermal conductivity, water vapor stability and cyclic durability of selected candidate zirconia-/hafnia-, pyrochlore- and magnetoplumbite-based T/EBC materials are evaluated. The test results have been used to downselect the T/EBC coating materials, and help demonstrate advanced 1650OC coatings feasibility with long-term cyclic durability.
Document ID
20050199717
Acquisition Source
Headquarters
Document Type
Preprint (Draft being sent to journal)
Authors
Zhu, Dongming
(NASA Glenn Research Center Cleveland, OH, United States)
Fox, Dennis S.
(NASA Glenn Research Center Cleveland, OH, United States)
Bansal, Narottam P.
(NASA Glenn Research Center Cleveland, OH, United States)
Miller, Robert A.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Composite Materials
Meeting Information
Meeting: Fifth International Conference on High Temperature Ceramic Matrix Composites
Location: Seattle, WA
Country: United States
Start Date: September 12, 2004
End Date: September 16, 2004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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