journal article·2012-05

Electron beam physical vapour deposition and mechanical properties of c-ZrO2-ZTA-coatings on alloy 617 substrates

E. Roos, S.M. Naga, R.N. Richter, S. Lauf, M. Awaad, A. Lyutovich, M.A. Tameem

Ceramics International· Volume 38· Issue 4
Publisher page

Abstract

Abstract Multilayered zirconia toughened alumina (ZTA) and c-zirconia coatings were prepared using electron beam physical vapour deposition (EB-PVD). Characterizations of the morphology and chemical composition of the deposited coatings were performed using scanning electron microscopy (SEM) and X-ray diffraction analysis (XRD). Scratch resistance, nano-indentation and bending strength were used for the evaluation of the mechanical properties. X-ray diffraction of the top ceramic TBC surface showed that it consists entirely of cubic ZrO 2 phase. The energy-dispersive X-ray spectroscopy analysis (EDS) showed that α-Al 2 O 3 is the only oxide phase present at the interface, while SEM indicated the presence of columnar c-ZrO 2 as the only phase of the top coat. Delamination over a large region was observed in the case of double layer (ZTA) coating. In contrast, the multilayered (ZTA1 + ZTA2 + c-Z) coating showed neither delamination nor cracking. The hardness and scratch measurements showed that the top coat c-ZrO 2 layer is harder than the ZTA layers. The thermal conductivity of the multilayer coatings was estimated using the theoretical density and thermal conductivity values of zirconia toughened alumina (ZTA) and cubic-zirconia (c-ZrO 2 ) together with their experimentally measured data.
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Research context

OpenAlex topics: High-Temperature Coating Behaviors · Metal and Thin Film Mechanics · Semiconductor materials and devices

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (25)

Show source-provided references
1. Materials for advanced power engineering
2. PVD thermal barrier coating applications and process development for aircraft engines10.1007/s11666-997-0008-6 ↗
3. EB-PVD thermal barrier coatings for aeroengines and gas turbines10.1002/1527-2648(200104)3:4<193::AID-ADEM193>3.0.CO;2-U ↗
4. Thermal barrier coatings for gas-turbine engine applications10.1126/science.1068609 ↗
5. The evolution of thermal barrier coatings-status and upcoming solutions for today's key issues10.1016/S0257-8972(99)00342-4 ↗
6. Failure of thermal barrier coating systems under cyclic thermomechanical loading10.1016/S1359-6454(00)00260-3 ↗
7. Effect of interface roughness and coating thickness on interfacial shear mechanical properties of EB-PVD yttria – partially stabilized zirconia thermal barrier coating systems10.1016/j.jeurceramsoc.2007.02.196 ↗
8. Influence of porosity on hardness and Young's modulus of nanoporous EB-PVD-TBCs by nanoindentation10.1016/j.matlet.2005.06.014 ↗
9. Cyclic behaviour of EB-PVD thermal barrier coating systems with modified bond coats10.1016/j.surfcoat.2008.08.056 ↗
10. Effect of bond coat nature and thickness on mechanical characteristic and contact damage of zirconia-based thermal barrier coatings10.1016/j.surfcoat.2006.07.240 ↗
11. Determination of mechanical properties of electron beam – physical vapour deposition – thermal barrier coatings (EB-PVD-TBCs) by means of nanoindentation and impact testing10.1016/S0257-8972(02)00594-7 ↗
12. Relationships between residual stress, microstructure and mechanical properties of electron beam – physical vapour deposition – thermal barrier coatings10.1016/S0257-8972(98)00668-9 ↗
13. Combined zirconia toughened alumina (ZTA) stacks obtained by electron beam physical vapour deposition10.1016/j.ceramint.2010.10.030 ↗
14. Insights into the effectiveness of scratch resistant coatings
15. Neue Erkenntnisse über die Kratzfestigkeit von Klarlacken aus dem Nano-Scratch-Test unter trockenen und nassen Bedingungen
16. Richter · Proc. Macromol. Symp. · 2002 · 187 · 85310.1002/1521-3900(200209)187:1<853::AID-MASY853>3.0.CO;2-Y ↗
17. Nohava · 2009
18. Gottfried Bosch, Enhanced Stiffness Procedure mit dem Messgerät Fischerscope HM2000 und Picodentor HM500, http://www.helmut-fischer.com/globalfiles/DE_ESP%20Applikationsbericht_DE.pdf.
19. Influence of composition and phase distribution on the oxidation behaviour of NiCoCrAlY alloys
20. Oxidation characteristics of a platinised MCrAlY bond coat for TBC systems during cyclic oxidation at 1000°C10.1016/j.surfcoat.2004.11.038 ↗
21. Microstructure of as – coated thermal barrier coating with varying lifetimes10.1016/j.surfcoat.2003.06.021 ↗
22. Thermal conductivity of plasma-sprayed monolithic and multilayer coatings of alumina and yttria-stabilized zirconia10.1111/j.1151-2916.1999.tb01816.x ↗
23. The effect of grain size, porosity and yttria content on the thermal conductivity of nano crystalline zirconia10.1016/S1359-6462(98)00290-5 ↗
24. Thermal properties of zirconia co-doped with trivalent and pentavalent oxides10.1016/S1359-6454(00)00295-0 ↗
25. Mechanical characterization and thermal behaviour of HVOF – sprayed bond coat in thermal barrier coatings (TBCs)10.1016/j.surfcoat.2005.02.170 ↗