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Thermal barrier coating life prediction model developmentIn order to fully exploit thermal barrier coatings (TBCs) on turbine components and achieve the maximum performance benefit, the knowledge and understanding of TBC failure mechanisms must be increased and the means to predict coating life developed. The proposed program will determine the predominant modes of TBC system degradation and then develop and verify life prediction models accounting for those degradation modes. The successful completion of the program will have dual benefits: the ability to take advantage of the performance benefits offered by TBCs, and a sounder basis for making future improvements in coating behavior.
Document ID
19870001765
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hillery, R. V.
(General Electric Co. Fairfield, CT, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1984
Publication Information
Publication: NASA. Lewis Research Center Turbine Engine Hot Section Technology, 1984
Subject Category
Quality Assurance And Reliability
Accession Number
87N11198
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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