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Thermal barrier coating systemA high temperature oxidation resistant, thermal barrier coating system is disclosed for a nickel cobalt, or iron base alloy substrate. An inner metal bond coating contacts the substrate, and a thermal barrier coating covers the bond coating. NiCrAlR, FeCrAlR, and CoCrAlR alloys are satisfactory as bond coating compositions where R=Y or Yb. These alloys contain, by weight, 24.9-36.7% chromium, 5.4-18.5% aluminum, and 0.05 to 1.55% yttrium or 0.05 to 0.53% ytterbium. The coatings containing ytterbium are preferred over those containing yttrium. An outer thermal barrier coating of partial stabilized zirconium oxide (zirconia) which is between 6% and 8%, by weight, of yttrium oxide (yttria) covers the bond coating. Partial stabilization provides a material with superior durability. Partially stabilized zirconia consists of mixtures of cubic, tetragonal, and monoclinic phases.
Document ID
19850012956
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Stecura, S.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
November 27, 1984
Subject Category
Composite Materials
Report/Patent Number
NAS 1.71:LEW-13324-2
Patent Number: US-PATENT-4,485,151
Patent Application Number: US-PATENT-APPL-SN-523297
Report Number: NAS 1.71:LEW-13324-2
Patent Application Number: US-PATENT-APPL-SN-375784
Patent Number: NASA-CASE-LEW-13324-2
Accession Number
85N21266
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,485,151|NASA-CASE-LEW-13324-2
Patent Application
US-PATENT-APPL-SN-523297|US-PATENT-APPL-SN-375784
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