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Effect of thermal cycling on ZrO2-Y2O3 thermal barrier coatingsThe paper studies the comparative life of plasma-sprayed ZrO2-Y2O3 thermal barrier coatings on NiCrAlY bond coats on Rene 41 in short (4 min) and long (57 min) thermal cycles at 1040 C in a 0.3-Mach flame. Attention is given to determining the effect of short- and long-duration cycles on ZrO2-Y2O3 coatings, the cause of any cycle frequency effects, and methods to improve tolerance to thermal stress. Short cycles greatly reduced the life of the ceramic coating in terms of time at temperatures as compared to longer cycles, the failed coating indicating compressive failure. The experiments and stress calculations show that repeatedly subjecting a ceramic coating to high rates of initial heating has a more destructive influence on the coating than sustained operation at temperature. The effect of such thermal compressive stresses might be minimized through coating deposition and thickness control and by turbine cycle measurement to keep starting heating rates below critical values.
Document ID
19800051729
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcdonald, G.
(NASA Lewis Research Center Cleveland, OH, United States)
Hendricks, R. C.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 10, 2013
Publication Date
April 1, 1980
Subject Category
Nonmetallic Materials
Meeting Information
Meeting: International Conference on Metallurgical Coatings
Location: San Diego, CA
Start Date: April 21, 1980
End Date: April 25, 1980
Sponsors: American Vacuum Society
Accession Number
80A35899
Distribution Limits
Public
Copyright
Other

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