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Thermal barrier coating life prediction modelThe objectives of this research were to determine the predominant modes of degradation of a plasma sprayed thermal barrier coating (TBC) system, and then to develop and verify life prediction models accounting for these degradation modes. The TBC system consists of a low pressure plasma sprayed (LPPS) bond coat layer of Ni-22Cr-10Al-O.3Y, an air plasma sprayed (APS) yttria partially stabilized zirconia (ZrO sub 2-8Y sub 2 O sub 3) top coat on a conventionally cast Rene 80 (Ni base) substrate. Thermal cycle testing of TBCs was employed to evaluate the effect of coating edges, bond coat oxidation, bond coat creep, top coat thickness, and bond coat thickness.
Document ID
19890007961
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Pilsner, B.
(General Electric Co. Cincinnati, OH, United States)
Hillery, R.
(General Electric Co. Cincinnati, OH, United States)
Mcknight, R. L.
(General Electric Co. Cincinnati, OH, United States)
Cook, T.
(General Electric Co. Cincinnati, OH, United States)
Hartle, M.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1987
Publication Information
Publication: NASA, Lewis Research Center, Turbine Engine Hot Section Technology, 1987
Subject Category
Structural Mechanics
Accession Number
89N17332
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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