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Improved metallic and thermal barrier coatingsLow thermal conductivity two layer ceramic coatings are efficient thermal barriers between cooled matallic components and high temperature combustion gases. Potential components are combustors, blades, and vanes in aircraft engines of power-generating turbines. Presence of two layer coatings greatly reduces temperature and coolant requirements.
Document ID
19800000353
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Stecura, S.
Date Acquired
August 10, 2013
Publication Date
January 1, 1981
Publication Information
Publication: NASA Tech Briefs
Volume: 5
Issue: 3
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
LEW-13324
Accession Number
80B10353
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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