journal article·2013-04

Influence of partial substitution of Sc2O3 with Gd2O3 on the phase stability and thermal conductivity of Sc2O3-doped ZrO2

Leilei Sun, Hongbo Guo, Hui Peng, Shengkai Gong, Huibin Xu

Ceramics International· Volume 39· Issue 3
Publisher page

Abstract

Abstract Multi-rare earth elements doping is one of effective methods to improve the phase stability and thermal barrier property of zirconia for thermal barrier coatings (TBCs) application. In this paper, the phase stability and thermo-physical properties of 7.5 mol% Sc 2 O 3 and Gd 2 O 3 co-doped ZrO 2 (ScGdSZ) were investigated. ScGdSZ after 150 h heat-treatment at 1400 °C exhibited no monoclinic phase, showing high phase stability. The substitution of Sc 2 O 3 with Gd 2 O 3 increased the fraction of c-phase, however, t′-phase was still the dominant phase when the substitution amount was less than 2 mol%. The thermal conductivities of ScGdSZ gradually decreased with the increasing Gd 2 O 3 proportion. 3.7 Sc 2 O 3 and 3.7 Gd 2 O 3 co-doped ZrO 2 (in mol%) showed the lowest thermal conductivity, which was 20% lower than 7.5 Sc 2 O 3 -doped ZrO 2 and 40% lower than 4.5 Y 2 O 3 -doped ZrO 2 .
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Research context

OpenAlex topics: High-Temperature Coating Behaviors · Nuclear Materials and Properties · Advanced ceramic materials synthesis

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References (19)

Show source-provided references
1. Current status of thermal barrier coatings—an overview10.1016/0257-8972(87)90003-X ↗
2. Thermal barrier coatings for gas-turbine engine applications10.1126/science.1068609 ↗
3. Ceramic materials for thermal barrier coatings10.1016/S0955-2219(03)00129-8 ↗
4. Thermal barrier coatings for aircraft engines: history and directions10.1007/BF02646310 ↗
5. Structure and thermal properties of heat treated plasma sprayed ceria–yttria co-stabilized zirconia coatings10.1016/j.ceramint.2009.10.020 ↗
6. Thermal expansion and thermal conductivity of SmxZr1−xO2−x/2 (0.1≤x≤0.5) ceramics10.1016/j.ceramint.2008.02.016 ↗
7. Preparation and thermophysical properties of NdxZr1−xO2−x/2 (x=0.1, 0.2, 0.3, 0.4, 0.5) ceramics10.1016/j.jallcom.2007.11.147 ↗
8. Thermal conductivity and phase stability of plasma sprayed ZrO2–Y2O3–La2O3 coatings10.1016/j.surfcoat.2004.04.078 ↗
9. Phase stability, sintering, and thermal conductivity of plasma-sprayed ZrO2–Gd2O3 compositions for potential thermal barrier coating applications10.1016/j.actamat.2005.11.033 ↗
10. Effect of gadolinia on phase structure and thermal conductivity of ZrO2–4.5mol%Y2O3 ceramics10.1016/j.matlet.2008.03.052 ↗
11. Improved tetragonal phase stability at 1400°C with scandia, yttria-stabilized zirconia10.1016/S0257-8972(96)03006-X ↗
12. Phase stability of scandia–yttria-stabilized zirconia TBCs10.1016/S0257-8972(98)00617-3 ↗
13. The system zirconia–scandia10.1111/j.1151-2916.1977.tb15521.x ↗
14. Phase stability in plasma sprayed partially stabilized zirconia–yttria
15. Liang · 1993
16. Low-thermal-conductivity rare-earth zirconates for potential thermal-barrier-coating applications10.1111/j.1151-2916.2002.tb00574.x ↗
17. Theory of the thermal conductivity of solids
18. Defect clustering and nano-phase structure characterization of multi-component rare-earth oxide doped zirconia–yttria thermal barrier coatings10.1002/9780470294802.ch75 ↗
19. Low thermal conductivity without oxygen vacancies in equimolar YO1.5+TaO2.5- and YbO1.5+TaO2.5-stabilized tetragonal zirconia ceramics10.1016/j.actamat.2010.04.040 ↗