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Creep Behavior of Hafnia and Ytterbium Silicate Environmental Barrier Coating Systems on SiC/SiC Ceramic Matrix CompositesEnvironmental barrier coatings will play a crucial role in future advanced gas turbine engines because of their ability to significantly extend the temperature capability and stability of SiC/SiC ceramic matrix composite (CMC) engine components, thus improving the engine performance. In order to develop high performance, robust coating systems for engine components, appropriate test approaches simulating operating temperature gradient and stress environments for evaluating the critical coating properties must be established. In this paper, thermal gradient mechanical testing approaches for evaluating creep and fatigue behavior of environmental barrier coated SiC/SiC CMC systems will be described. The creep and fatigue behavior of Hafnia and ytterbium silicate environmental barrier coatings on SiC/SiC CMC systems will be reported in simulated environmental exposure conditions. The coating failure mechanisms will also be discussed under the heat flux and stress conditions.
Document ID
20110008749
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Zhu, Dongming
(NASA Glenn Research Center Cleveland, OH, United States)
Fox, Dennis S.
(NASA Glenn Research Center Cleveland, OH, United States)
Ghosn, Louis J.
(NASA Glenn Research Center Cleveland, OH, United States)
Harder, Bryan
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
January 23, 2011
Subject Category
Composite Materials
Report/Patent Number
E-17715
Meeting Information
Meeting: International Conference on Advanced Ceramics and Composites
Location: Cleveland, OH
Country: United States
Start Date: January 23, 2011
End Date: January 28, 2011
Funding Number(s)
WBS: WBS 984753.02.07.03.16.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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