ICMCTF 2012! - CD-Lab Application Oriented Coating Development
ICMCTF 2012! - CD-Lab Application Oriented Coating Development
ICMCTF 2012! - CD-Lab Application Oriented Coating Development
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10:20am A2-1-8 New Perspectives on the Phase Stability Challenge in<br />
Zirconia-based TBCs, J. Krogstad (jkoschmeder@engineering.ucsb.edu),<br />
S. Krämer, University of California, Santa Barbara, US, R. Leckie, Los<br />
Alamos National <strong>Lab</strong>oratory, US, M. Lepple, Karlsruhe Institute of<br />
Technology, Germany, Y. Gao, D. Lipkin, GE Global Research, US, C.G.<br />
Levi, University of California, Santa Barbara, US<br />
Zirconia-based ceramics have long been used to provide thermal protection<br />
to the structural components of modern gas turbine engines. Economic and<br />
environmental considerations have motivated higher engine operating<br />
temperatures, potentially leading to more rapid degradation of thermal<br />
barrier coating (TBC) systems dependent on a metastable phase, namely t’-<br />
8YSZ (ZrO2+7-8wt%YO1.5) TBCs. The t’-phase was originally thought to<br />
decay slowly into the equilibrium Y-lean tetragonal phase and Y-rich cubic<br />
phase, the former of which may undergo further transformation to the<br />
monoclinic phase. However, it has recently been shown that the t’-phase<br />
destabilizes at a small fraction of the time necessary to form the deleterious<br />
monoclinic phase. The rapid decay of t’-YSZ into a modulated<br />
microstructure of coherent domains offers additional insight on the<br />
importance of microstructural control in the phase evolution of YSZ TBCs.<br />
Traditional phase stability characterization techniques have been<br />
reevaluated in order to provide a more complete description of this process.<br />
In particular, x-ray diffraction (XRD) techniques, both at room temperature<br />
and elevated temperatures, have been used to quantify the changing phase<br />
fractions and composition of each phase, with additional implications for<br />
the equilibrium phase diagram. XRD is more powerful when used in<br />
conjunction with microstructural observations. As such, three different<br />
starting morphologies will be compared on the basis of phase stability.<br />
Stemming from this comparison, potential pathways for further delaying the<br />
onset of the monoclinic transformation will be explored. While the<br />
effectiveness of these measures is expected to be modest, lessons can be<br />
learned from the t’-8YSZ system. In particular, maintaining a high degree<br />
of tetragonality over the entire range of relevant temperatures may be key to<br />
supporting or improving the in service toughness and durability. A novel<br />
TBC system will be introduced in which a relatively large single phase<br />
tetragonal field with exceptional tetragonality has been stabilized and has<br />
demonstrated comparable or improved toughness, making it a promising<br />
alternative for next generation TBCs.<br />
This work was partially supported with funding from the US DoE via<br />
Cooperative Agreement DE-FC26-05NT42643 and the NSF via FRG-<br />
GOALI Contract NSF/DMR0605700. Any opinions, findings, conclusions or<br />
other recommendations expressed are those of the authors and do not<br />
necessarily reflect the views of the US Department of Energy or the<br />
National Science Foundation.<br />
10:40am A2-1-9 Influence of the mechanical behaviour of the under<br />
layer in coating spallation, V. Maurel (vincent.maurel@mat.ensmp.fr), A.<br />
Koster, Mines-ParisTech, UMR CNRS 7633, France, L. Rémy, Mines-<br />
ParisTech,UMR CNRS 7633, France INVITED<br />
<strong>Coating</strong>s designed for high temperature protection, Aluminium rich<br />
intermetallic coating as well as thermal barrier coatings (TBC), are prone to<br />
damage when exposed to stages of high temperature and cooling. Coupling<br />
thermal and mechanical loading tests provide an accurate simulation of inservice<br />
loadings and the generation of subsequent realistic damage. Thus,<br />
the aim of this study is to clarify the way the mechanical behaviour of the<br />
under-layer interacts with surface damage. This point will be examined for<br />
room temperature mechanical tests performed up to oxide or TBC<br />
spallation. The specimens were initially subjected to high temperature<br />
thermal loading for both isothermal and thermal cycling.<br />
When single crystals coated with TBC are subjected to mechanical<br />
compression, the strain localisation arising in the single crystal has been<br />
already been shown to drive the ceramic coating to spallation. In the same<br />
manner, when the oxide is growing on a free surface, the oxide spallation<br />
due to mechanical compression is dependent of the local behaviour of the<br />
coating. Indeed, for a typical CVD-NiAl coating, strain localisation is<br />
related to the coating microstructure. Moreover, the oxide morphology will<br />
also contribute to localisation of strain and hence oxide spallation. The<br />
chosen experimental methodology will be explained since it offers a<br />
complement to thermo-gravimetric analysis. It particularly includes the<br />
intensive use of full-field analysis by surface strain field measurement. This<br />
technique enables a quantitative characterisation of surface damage and can<br />
be used to define intrinsic rupture material parameter. Complementary finite<br />
element analysis of both test configuration and principal microstructural<br />
features are performed. It allows a close view of the mechanical state<br />
leading to rupture to be obtained. Finally, assessment of thermo-mechanical<br />
coupling will be discussed for complex loading paths.<br />
Tuesday Morning, April 24, <strong>2012</strong> 24<br />
11:20am A2-1-11 Inhibiting High Temperature Densification Through<br />
Multi-Phase TBCs, J.S. Van Sluytman<br />
(jason.vans@engineering.ucsb.edu), C.G. Levi, University of California,<br />
Santa Barbara, US, V.K. Tolpygo, Honeywell Aerospace, Pheonix, AZ, US<br />
Thermal barrier coatings (TBCs) are essential for the effective operation of<br />
turbine blades in high temperature gas environments. The drive for next<br />
generation TBCs, however, poses new demands that the current TBC, 7.6<br />
mol% YO1.5 stabilized zirconia (7YSZ) is unlikely to satisfy. At issue is the<br />
phase stability of the coating and its resistance to sintering, both of which<br />
are explored in the YO1.5 - TaO2.5 - ZrO2 (Y-Ta-Zr) system. This research<br />
addresses the issue of high temperature densification and its mitigation<br />
using multi-phase compositions within this ternary system. In addition to<br />
the baseline 7YSZ, four compositions were selected for investigation<br />
representing four different phase constitutions: 16Y-16Ta-Zr (stable<br />
tetragonal, t); 20Y-20Ta-Zr (two-phase tetragonal zirconia solid solution, t,<br />
and monoclinic yttrium tantalate, m-YTaO4); 22Y-13Ta-Zr (two-phase non<br />
transformable tetragonal, t, and fluorite, c); and finally 18Y-28Ta-Zr<br />
(three-phase mixture of t, m-YTaO4, and orthorhombic Zr3TaO8 phases).<br />
Densification studies were performed at 1250 °C with dwell times of 1, 4, 9,<br />
and 300 h. Pore size distributions have been quantified at each sintering<br />
time using BET analysis. Remarkably, the 18Y-28Ta-Zr composition<br />
increased only to 55% of its theoretical density from a green body density<br />
of 49% after 300 h. Pore size analysis indicates that the pores are relatively<br />
stable from 1 to 300 h at 1250°C. This compares with 22Y-13Ta-Zr and<br />
7.6YSZ, which reached 70% and 85% of their theoretical densities,<br />
respectively, after the same exposure. The 22Y-13Ta-Zr, along with 18Y-<br />
28Ta-Zr, which are also phase stable and offer lower thermal conductivity<br />
than 7YSZ, suggests alternate regions within the Y-Ta-Zr system offering<br />
promise for future development.<br />
Hard <strong>Coating</strong>s and Vapor Deposition Technology<br />
Room: Royal Palm 4-6 - Session B1-3<br />
PVD <strong>Coating</strong>s and Technologies<br />
Moderator: P. Eklund, Linköping University, Sweden, J.H.<br />
Huang, National Tsing Hua University, Taiwan, J. Vetter,<br />
Sulzer Metaplas GmbH, Germany<br />
8:00am B1-3-1 Preparation and characterization of anti-wear and<br />
anti-bacteria TaN-Cu, TaN-Ag, TaN(Ag,Cu) nanocomposite thin films,<br />
J.H. Hsieh (jhhsieh@mail.mcut.edu.tw), Ming Chi University of<br />
Technology, Taiwan INVITED<br />
The processes and functions of MeN-(soft metal) nanocomposite films were<br />
first reviewed. Following that, the processing, structure, and multifunctional<br />
properties of TaN-Cu, TaN-Ag, and TaN-(Cu,Ag)<br />
nanocomposite films were discussed and compared. The TaN-(soft metal)<br />
films were prepared by a hybrid process that combines co-sputtering<br />
deposition and rapid thermal annealing. After the surface morphologies as<br />
well as the microstructures were analyzed and compared, the samples were<br />
examined for their tribological properties. It is found that the tribological<br />
properties could be improved when the soft metals were smeared out and<br />
functioned as solid lubricants. All TaN-(soft metal) nanocomposite thin<br />
films showed similar behaviors. However, it is found further that Cuincorporated<br />
films could behave better under low load or low contact<br />
temperature while Ag-incorporated films could do better under high load or<br />
high temperature. For TaN-(Cu,Ag), the films might behave more like Agincorporated<br />
films. The samples were also tested for their anti-bacterial<br />
behaviors against Gram-negative (E. coli) and Gram-positive ( S. Aureus )<br />
bacteria. It is found that the antibacteria efficiency against either E.coli or S.<br />
aureus can be much improved for TaN-(Cu,Ag), comparing with TaN-Ag or<br />
TaN-Cu films. The annealing temperature for TaN-(Cu,Ag) can be as low<br />
as 200 o C. Being annealed at this temperature, the film still shows good<br />
antibacterial behaviors against either bacterium. The synergistic effect due<br />
to the co-existence of Ag and Cu would be discussed.<br />
8:40am B1-3-3 Effects of sputtering gas for the preparation of CNx<br />
films by RF reactive sputtering, T.S. Shiroya (s0721171KH@itchiba.ac.jp),<br />
Graduate School, Chiba Institute of Technology, Japan, Y.<br />
Sakamoto, Chiba Institute of Technology, Japan<br />
CNx is nitrogen contained Diamond-Like Carbon (DLC) and it has<br />
excellent mechanical properties such as high hardness and low friction<br />
coefficient especially in nitrogen gas atmosphere. These properties may be<br />
controlled by controlling of nitrogen content. In addition, CNx is capable of<br />
preparation by using thin film deposition techniques both Physical Vapor<br />
Deposition (PVD) and Chemical Vapor Deposition (CVD) and expected to<br />
apply for mechanical parts. On the other hand, reactive sputtering is one of<br />
method prepared oxide and nitride easily by chemical reaction with the