THERMALLY OXIDIZED ZIRCONIUM NANOCRYSTALLINE THERMAL BARRIER COATING DEPOSITED BY EB-PVD

Authors

  • M. Keshavarz M. Keshavarz Department of Materials Science, Faculty of Mechanical Engineering, Universiti Teknologi Malaysia, 81310 UTM Johor Bahru, Johor, Malaysia
  • M. Hasbullah Idris Department of Materials Science, Faculty of Mechanical Engineering, Universiti Teknologi Malaysia, 81310 UTM Johor Bahru, Johor, Malaysia
  • Z. Othaman Z. Othaman Department of Materials Science, Faculty of Mechanical Engineering, Universiti Teknologi Malaysia, 81310 UTM Johor Bahru, Johor, Malaysia

Keywords:

zirconium oxide, nanocrystalline, EB-PVD, TBC

Abstract

Zirconium oxide nanocrystalline deposited on the bound coat of thermal barrier coating TBC by an electron beam physical vapour deposition EB-PVD was thermally oxidized at oxygen ambient after deposition process within 1073 K resulting in Zirconium oxide top layer with various stoichiometries. Intermetallic alloys based on γ -TiAl due to offer low density over conventional Ni supper alloy was used as substrate. Field emission scanning electron microscopy FESEM observation of the deposited specimens at three different oxygen partial pressure during coating indicate the appropriate adhesion of ZrO2 when thermally grown oxide TGO had been taken place as buffer layer between top coat and bound coat which are contain 8mol% Yttria Stabilized Zirconia (YSZ) and MCrAlY respectively. Energy dispersive spectrometer EDS to determine the composition of present element after deposition was employed. XRD analysis of the ex situ TBC components revealed the phases formed at different oxygen partial pressure. The present of this intermediate TGO layer was confirmed by observation of AL2O3 and yttrium aluminates (YAlO3 and/or Y3Al5O12) phases in the XRD patterns. Al2O3 provides an effective diffusion barrier that protects the underlying metal from deleterious oxidation during thermally oxidizing the zirconium. Using rapid thermal processing RTP analysis data, the effective oxidation temperature on the stoichiometry of zirconium oxide and thickness of grown were investigated therewith, the crystallization of zirconium oxide films was initiated at about 480 K and was almost completed at 525 K. Micro indentation test was accomplished to qualifying the adhesion of Zirconium oxide nanocrystalline and the interfacial of bond coat.

References

Schulz, U. and M. Schmücker, 2000. Microstructure of ZrO2 thermal barrier coatings applied by EB-PVD. Materials Science and Engineering A,. 276 (1-2), 1-8.

M. Hetmańczyk, L.S., B. Mendala, 2007. Advanced materials and protective coatings in aero-engines application. Journal of Achievements in Materials and Manufacturing Engineering,. 24.

Copland, E.H., B. Gleeson, and D.J. Young, 1999. Formation of Z-Ti50Al30O20 in the sub-oxide zones of [gamma]-TiAl-based alloys during oxidation at 1000°C. Acta Materialia, 47 (10), 2937-2949.

Wu, Y., et al., 2006. Isothermal Oxidation Behavior of Ti-50Al Alloy with Y Additions at 800 and 900°C. Oxidation of Metals, 66(5), 321-348.

Afrasiabi, A., M. Saremi, and A. Kobayashi, 2008. A comparative study on hot corrosion resistance of three types of thermal barrier coatings: YSZ, YSZ + Al2O3

and YSZ/Al2O3. Materials Science and Engineering A, 478(1-2), 264-269.

Li, M., et al., 2006. Thermocyclic behavior of sputtered NiCrAlY/EB-PVD 7 wt.%Y2O3-ZrO2 thermal barrier coatings. Surface and Coatings Technology,. 200(12-13), 3770-3774.

Hass, D.D., A.J. Slifka, and H.N.G. Wadley, 2001. Low thermal conductivity vapor deposited zirconia microstructures. Acta Materialia, 49(6), 973-983.

Zhou, W., et al., 2006. Degradation formula and working lifetime prediction for high-temperature coating. Applied Surface Science,. 253(5), 2565-2571.

Toma, D., W. Brandl, and U. Köster, 1999. Studies on the transient stage of oxidation of VPS and HVOF sprayed MCrAlY coatings. Surface and Coatings Technology, 120-121,8-15.

Moskal, G., 2009. Thermal barrier coatings: characteristics of microstructure and properties, generation and directions of development of bond. Journal of Achievements in Materials and Manufacturing Engineering, 37(2): 331.

Zubacheva, O.A., 2004. Plasma-Sprayed and Physically Vapor Deposited Thermal barrier Coatings: Comparative Analysis of Thermoelastic behavior Based on Curvature Studies.

G.W, G., 1998. Progress in coatings for gas turbine airfoils. Surface and Coatings Technology, 108-109(0), 73-79.

Downloads

Published

2018-04-01

How to Cite

M. Keshavarz, M. K., Idris, M. H., & Z. Othaman, Z. O. (2018). THERMALLY OXIDIZED ZIRCONIUM NANOCRYSTALLINE THERMAL BARRIER COATING DEPOSITED BY EB-PVD. Jurnal Mekanikal, 36(2). Retrieved from https://jurnalmekanikal.utm.my/index.php/jurnalmekanikal/article/view/51

Issue

Section

Mechanical