NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Special Issue: Environmental Barrier Coatings The global increase in air travel will require commercial vehicles to be more efficient than ever before. Advanced turbine hot section materials are a key technology required to keep fuel consumption and emission to a minimum. Ceramic matrix composites (CMCs) are the most promising material to revolutionize turbine hot section materials because of their excellent high‐temperature properties. Rapid surface recession due to volatilization by water vapor is the Achilles heel of CMCs. Environmental barrier coatings (EBCs), which protect CMCs from water vapor, is an enabling technology for CMCs. The first CMC component entered into service in 2016 in a commercial engine, and more CMC components are scheduled to follow within the next few years. One of the most difficult challenges to CMC components is EBC durability because failure of EBC leads to a rapid reduction in CMC component life. Novel EBC chemistries, creative EBC designs, and robust processes are required to meet EBC durability challenges. Engine-relevant testing, characterization, and lifing methods need to be developed to improve EBC reliability. The aim of this Special Issue is to present recent advances in EBC technology to address current EBC challenges.
Document ID
20205002772
Acquisition Source
Glenn Research Center
Document Type
Accepted Manuscript (Version with final changes)
Authors
Kang N. Lee
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
May 27, 2020
Publication Date
May 27, 2020
Publication Information
Publication: Coatings
Publisher: MDPI
Volume: 10
Issue: 6
Issue Publication Date: January 1, 2020
e-ISSN: 2079-6412
Subject Category
Composite Materials
Funding Number(s)
WBS: 109492.02.03.05.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
EBC, CMC, Oxidation, Volatility, CMAS, Thermomechanical, Modeling
No Preview Available