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Durability of zirconia thermal-barrier ceramic coatings on air-cooled turbine blades in cyclic jet engine operationThermal barrier ceramic coatings of stabilized zirconia over a bond coat of Ni Cr Al Y were tested for durability on air cooled turbine rotor blades in a research turbojet engine. Zirconia stabilized with either yttria, magnesia, or calcia was investigated. On the basis of durability and processing cost, the yttria stabilized zirconia was considered the best of the three coatings investigated.
Document ID
19760025104
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Liebert, C. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Jacobs, R. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Stecura, S.
(NASA Lewis Research Center Cleveland, OH, United States)
Morse, C. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1976
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-X-3410
E-8700
Report Number: NASA-TM-X-3410
Report Number: E-8700
Accession Number
76N32192
Funding Number(s)
PROJECT: RTOP 505-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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