Advanced Oxide Material Systems for 1650 °C Thermal/Environmental Barrier Coating Applications
Dongming Zhu, Dennis S. Fox, Narottam P. Bansal, Robert A. Miller
NASA/TM
abstract:Advanced 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.
keywords:Coating; Strain; Crack propagation; Superalloy; Stress; Bond coat; Zirconia; Plasma spraying; Thermal barrier; modulus.
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