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@ARTICLE{Drexler:10212,
author = {Drexler, J.M. and Aygun, A. and Li, D. and Vaßen, R. and
Steinke, T. and Padture, N.P.},
title = {{T}hermal-gradient testing of thermal barrier coatings
under simultaneous attack by molten glassy deposits and its
mitigation},
journal = {Surface and coatings technology},
volume = {204},
issn = {0257-8972},
address = {Amsterdam [u.a.]},
publisher = {Elsevier Science},
reportid = {PreJuSER-10212},
year = {2010},
note = {The authors thank Mr. L Flower (Haynes), Dr. R. Kowalik
(NavAir), Dr. B. Nagaraj (GE Aviation), and Dr. X. Ma
(lnframat Corp.) for their help with this project. The
authors also thank Profs. A. Evans (UCSB) and J. Hutchinson
(Harvard) for fruitful discussions and their help with the
E-H model. The suggestions by Prof. C. Levi (UCSB) on
producing a feasible CMAS source are gratefully
acknowledged. The authors also thank Dr. D. Mack (Julich)
for discussion and support during the thermal-cycling
experiments, and Mrs. N. Adels (Julich) for performing the
burner rig tests. The research at the Ohio State University
was supported by a grant from the U.S. Office of Naval
Research (award no. N00014-08-1-0458) monitored by Dr. D.
Shifler. Additional support was provided by the U.S.
Department of Energy (award no. DE-NT0006552).},
abstract = {Degradation of thermal barrier coatings (TBCs) in
gas-turbine engines by molten
calcium-magnesium-aluminosilicate (CMAS) glassy deposits is
becoming a pressing issue, as engines are required to
operate under increasingly harsh conditions. While new
approaches for mitigating CMAS attack of TBCs are starting
to emerge, there is a need for appropriate tests for
evaluating the efficacy of those approaches. To that end, we
present here a new thermal-cycling test for the evaluation
of TBC performance, where a thermal gradient is applied
across the TBC. with simultaneous injection of CMAS. The
conditions simulated in this new test are closer to actual
conditions in an engine, as compared to the conventional
furnace test without thermal gradient. This new test is
applied to a TBC with a new composition designed for
mitigating CMAS attack, where the mitigation mechanisms are
observed to be similar to those found in the conventional
furnace test. However, based on a previously established
mechanics model it is shown here that thermal-gradient
cyclic testing is essential for evaluating thermomechanical
performance of TBCs under attack by CMAS, and that the use
of just the conventional furnace test can lead to the
underestimation of the TBC performance. (C) 2010 Elsevier
B.V. All rights reserved.},
keywords = {J (WoSType)},
cin = {IEF-1},
ddc = {620},
cid = {I:(DE-Juel1)VDB809},
pnm = {Rationelle Energieumwandlung},
pid = {G:(DE-Juel1)FUEK402},
shelfmark = {Materials Science, Coatings $\&$ Films / Physics, Applied},
typ = {PUB:(DE-HGF)16},
UT = {WOS:000277736100023},
doi = {10.1016/j.surfcoat.2010.02.026},
url = {https://juser.fz-juelich.de/record/10212},
}