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@PHDTHESIS{Heckmann:32189,
author = {Heckmann, S.},
title = {{E}rmittlung des {V}erformungs- und
{S}chädigungsverhaltens von {W}ärmedämmschichtsystemen},
volume = {4077},
issn = {0944-2952},
school = {Techn. Hochsch. Aachen},
type = {Dr. (FH)},
address = {Jülich},
publisher = {Forschungszentrum Jülich GmbH Zentralbibliothek, Verlag},
reportid = {PreJuSER-32189, Juel-4077},
series = {Berichte des Forschungszentrums Jülich},
pages = {163 p.},
year = {2003},
note = {Record converted from VDB: 12.11.2012; Aachen, Techn.
Hochsch., Diss., 2003},
abstract = {The application of gas turbines for the generation of
electricity bas significantly increased over the past
decades. In order to reduce emissions and to conserve fossil
fuels, the thermal efficiency of stationary gas turbines
should be increased. This can be achieved mainly by higher
turbine inlet temperatures and by reduction of the cooling
air flow. The use of thermal barrier coatings (TBCs) has
great potential for increasing the thermal efficiency, while
at the same time limiting metal temperatures of the blades.
The exploitation of the potential of TBCs has, however, been
hampered by the lack of systematic data concerning the
damage development, and of the material properties that
affect it. In the present work, the damage development in a
TBC system has been investigated under simulated service
conditions. The system consisted of an atmospheric plasma
sprayed, yttrium stabilized zirconium oxide; a bond coat
(BC) layer of NiCoCrAlY (balance Ni, $21.1\%Co,$ $17.1\%Cr,$
$12.6\%Al,$ $0.61\%Y,$ $0.4\%Hf)$ that also acts as a
corrosion protection; and a substrate of the polycrystalline
turbine blade alloy IN 792 CC or the single crystalline
CMSX-4. For the isothermal low cycle fatigue (LCF) testing,
additional means for the heating of coated specimens were
developed and for the thermomechanical fatigue (TMF) tests,
completely new test techniques were necessary. The
manufacture of specimens of the isolated coating and
compression testing of these specimen were successfully
carried out. The results obtained show that there are
significant differences in the damage development in TMF
loading and in isothermal (LCF) loading. In TMF loading with
maximum and minimum temperatures of 950 and 450°C, shorter
fatigue lives than those in the LCF tests were measured.
Investigations of the damage in the TBC using acoustic
emission and calculation of the stress in the TBC have
contributed to the understanding of the damage processes. To
obtain data for the analysis of the mechanical behaviour,
the time-dependent deformation behaviours of both TBC and BC
and the elastic modulus of the TBC were determined. Based on
these data, a deformation model was derived, which
interpreted the deformation under compressive stress as a
change in the defect structure of the TBC.},
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/32189},
}