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NASA's Advanced Environmental Barrier Coatings Development for SiC/SiC Ceramic Matrix Composites: Understanding Calcium Magnesium Alumino-Silicate (CMAS) Degradations and ResistanceEnvironmental barrier coatings (EBCs) and SiCSiC ceramic matrix composites (CMCs) systems will play a crucial role in next generation turbine engines for hot-section component applications because of their ability to significantly increase engine operating temperatures with improved efficiency, reduce engine weight and cooling requirements. The development of prime-reliant environmental barrier coatings is essential to the viability and reliability of the envisioned CMC engine component applications, ensuring integrated EBC-CMC system durability and designs are achievable for successful applications of the game-changing component technologies and lifing methodologies.This paper will emphasize recent NASA environmental barrier coating developments for SiCSiC turbine airfoil components, utilizing advanced coating compositions, state-of-the-art processing methods, and combined mechanical and environment testing and durability evaluations. The coating-CMC degradations in the engine fatigue-creep and operating environments are particularly complex; one of the important coating development aspects is to better understand engine environmental interactions and coating life debits, and we have particularly addressed the effect of Calcium-Magnesium-Alumino-Silicate (CMAS) from road sand or volcano-ash deposits on the durability of the environmental barrier coating systems, and how the temperature capability, stability and cyclic life of the candidate rare earth oxide and silicate coating systems will be impacted in the presence of the CMAS at high temperatures and under simulated heat flux conditions. Advanced environmental barrier coating systems, including HfO2-Si with rare earth dopant based bond coat systems, will be discussed for the performance improvements to achieve better temperature capability and CMAS resistance for future engine operating conditions.
Document ID
20140017396
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Zhu, Dongming
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
December 16, 2014
Publication Date
June 26, 2014
Subject Category
Composite Materials
Report/Patent Number
GRC-E-DAA-TN15925
Meeting Information
Meeting: Thermal Barrier Coatings IV Conference: An ECI Conference Series
Location: Irsee
Country: Germany
Start Date: June 22, 2014
End Date: June 27, 2014
Sponsors: Engineering Conferences International, Inc.
Funding Number(s)
WBS: WBS 794072.02.03.03.02.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Environmental barrier coatings
Calcium-Magnesium-Alumino-Silicate (CMAS)
ceramic matrix composites
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