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Advanced Oxide Material Systems for 1650 C Thermal/Environmental Barrier Coating ApplicationsAdvanced thermal and environmental barrier coatings (TEBCs) 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 advanced 1650 C TEBC system is required to have a better high-temperature stability, lower thermal conductivity, and more resistance to sintering and thermal stress than current coating systems under engine high-heat-flux and severe thermal cycling conditions. In this report, the thermal conductivity and water vapor stability of selected candidate hafnia-, pyrochlore- and magnetoplumbite-based TEBC materials are evaluated. The effects of dopants on the materials properties are also discussed. The test results have been used to downselect the TEBC materials and help demonstrate the feasibility of advanced 1650 C coatings with long-term thermal cycling durability.
Document ID
20050041916
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Zhu, Dong-Ming
(Army Research Lab. 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
December 1, 2004
Subject Category
Composite Materials
Report/Patent Number
NASA/TM-2004-213219
E-14726
ARL-TR-3298
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
Sponsors: American Ceramic Society
Funding Number(s)
PROJECT: DA Proj. 1L1-61102-AF-20
WBS: WBS 22-714-20-09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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