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Metallic seal for thermal barrier coating systemsThe invention is particularly concerned with sealing thermal barrier coating systems of the type in use and being contemplated for use in diesel and other internal combustion engines. The invention also would find application in moderately high temperature regions of gas turbine engines and any other application employing a thermal barrier coating at moderate temperatures. Ni-35Cr-6Al-1Y, Ni-35Cr-6Al-1Yb, or other metallic alloy denoted as MCrAlx is applied over a zirconia-based thermal barrier overlayer. The close-out layer is glass-bead preened to densify its surface. This seals and protects the thermal barrier coating system.
Document ID
19910006099
Acquisition Source
Legacy CDMS
Document Type
Other - Patent Application
Authors
Miller, Robert A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
October 23, 1990
Subject Category
Nonmetallic Materials
Report/Patent Number
NAS 1.71:LEW-15020-1
Patent Number: NASA-CASE-LEW-15020-1
Patent Application Number: US-PATENT-APPL-SN-601957
Report Number: NAS 1.71:LEW-15020-1
Accession Number
91N15412
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LEW-15020-1
Patent Application
US-PATENT-APPL-SN-601957
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