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Advanced Environmental Barrier Coatings Developed for SiC/SiC Composite VanesCeramic components exhibit superior high-temperature strength and durability over conventional component materials in use today, signifying the potential to revolutionize gas turbine engine component technology. Silicon-carbide fiber-reinforced silicon carbide ceramic matrix composites (SiC/SiC CMCs) are prime candidates for the ceramic hotsection components of next-generation gas turbine engines. A key barrier to the realization of SiC/SiC CMC hot-section components is the environmental degradation of SiC/SiC CMCs in combustion environments. This is in the form of surface recession due to the volatilization of silica scale by water vapor. An external environmental barrier coating (EBC) is a logical approach to achieve protection and long-term durability.
Document ID
20050214693
Acquisition Source
Glenn Research Center
Document Type
Other
Authors
Lee, Kang N.
(NASA Glenn Research Center Cleveland, OH, United States)
Fox, Dennis S.
(NASA Glenn Research Center Cleveland, OH, United States)
Eldridge, Jeffrey I.
(NASA Glenn Research Center Cleveland, OH, United States)
Zhu, Dongming
(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
March 1, 2003
Publication Information
Publication: Research and Technology 2002
Subject Category
Composite Materials
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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