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@PHDTHESIS{Blandin:58846,
author = {Blandin, Gwendolin and Steinbrech, Rolf Willi},
title = {{T}hermomechanisches {V}erhalten von plasmagespritzten
{S}chichtsystemen zur {W}ärmedämmung},
volume = {3954},
issn = {0944-2952},
school = {Techn. Hochsch. Aachen},
type = {Dr. (FH)},
address = {Jülich},
publisher = {Forschungszentrum Jülich GmbH Zentralbibliothek, Verlag},
reportid = {PreJuSER-58846, Juel-3954},
series = {Berichte des Forschungszentrums Jülich},
pages = {IV, 121 p.},
year = {2002},
note = {Record converted from VDB: 12.11.2012; Aachen, Techn.
Hochsch., Diss., 2002},
abstract = {Thermal barrier coatings are increasingly utilized to
protect gas turbine components from high temperature
exposure. Thus the use of TBCs allows an improvement of the
system efficiency, since the coated components can support
higher inlet temperatures. For stationary gas turbine
applications, the combination of an oxidation resistant
MCrAlY bond coat and a 7-8 WL $\%$ Y$_{2}$O$_{3}$-ZrO$_{2}$
plasma sprayed top coat is currently the favored TBC-system.
To predict the life duration of the TBC-system, the
determination of the high temperature behavior of the
protective coatings in composite geometry is indispensable.
Also the residual stresses, which result from spraying
process and thermal expansion misfit between the bonded
layers, are of crucial importance. In the present study,
experiments were selected to evaluate the thermoelastic
properties of a plasma sprayed TBC in composite geometry.
The curvature behavior of three-layer specimen strips was
observed between room temperature and 1000°C, when
submitted exclusively to temperature. Also isothermal
4-point bending tests were performed at room temperature,
600°C and 950°C. During curvature and bending experiments,
shape and structure changes were monitored in-situ using a
high resolution telescope in combination with a digital data
acquisition system. In parallel, a linear-elastic model was
developed to calculate analytically the stress distribution
in multi-layered systems. The high temperature experiments
on the TBC-specimen strips demonstrate that the bonded
materials behave elastically up to 600°C. Depending on the
specimens geometry, i.e. on the stress distribution,
non-elastic effects can occur above 600°C (crack formation
in the ceramic coating or stress relaxation and phase
changes in the bond coat). When all layers show an elastic
behavior, the stress distribution can be calculated at room
and at high temperatures. Using the proposed linear-elastic
model, the temperature dependent elastic modulus of the
ceramic TBC in composite geometry can also be derived. The
obtained values are about 20 \% behind the modulus offree
standing layers.},
cin = {IWV-2},
cid = {I:(DE-Juel1)VDB2},
pnm = {Werkstoffsysteme für Kraftwerke},
pid = {G:(DE-Juel1)FUEK248},
typ = {PUB:(DE-HGF)11 / PUB:(DE-HGF)3},
url = {https://juser.fz-juelich.de/record/58846},
}