NASA NTRS · 19890007961
Thermal barrier coating life prediction model
Abstract
The 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.
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Pilsner, B., Hillery, R., Mcknight, R. L., Cook, T., Hartle, M.. 1987-10-01. Thermal barrier coating life prediction model. https://ntrs.nasa.gov/citations/19890007961
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