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Thermal Barrier Coating Life Prediction Model Development

A thermal barrier coated (TBC) turbine component design system, including an accurate TBC life prediction model, is needed to realize the full potential of available TBC engine performance and/or durability benefits. The objective of this work, which was sponsored in part by NASA under the Hot Secti...

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Published in:Journal of engineering for gas turbines and power 1992-04, Vol.114 (2), p.258-263
Main Authors: Meier, S. M, Nissley, D. M, Sheffler, K. D, Cruse, T. A
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Language:English
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container_end_page 263
container_issue 2
container_start_page 258
container_title Journal of engineering for gas turbines and power
container_volume 114
creator Meier, S. M
Nissley, D. M
Sheffler, K. D
Cruse, T. A
description A thermal barrier coated (TBC) turbine component design system, including an accurate TBC life prediction model, is needed to realize the full potential of available TBC engine performance and/or durability benefits. The objective of this work, which was sponsored in part by NASA under the Hot Section Technology (HOST) Program (Contract NAS3-23944), was to generate a life prediction model for electron beam-physical vapor deposited (EB-PVD) zirconia TBC. Specific results include EB-PVD zirconia mechanical and physical properties, coating adherence strength measurements, interfacial oxide growth characteristics, quantitative cyclic thermal spallation life data, and a spallation life model.
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ispartof Journal of engineering for gas turbines and power, 1992-04, Vol.114 (2), p.258-263
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subjects Applied sciences
Energy
Energy. Thermal use of fuels
Engines and turbines
Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc
Exact sciences and technology
title Thermal Barrier Coating Life Prediction Model Development
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