journal article·2017-07Open access

Thermoablative resistance of ZrB2-SiC-WC ceramics at 2400 °C

Ji Zou, Virtudes Rubio, Jon Binner

Acta Materialia· Volume 133

Abstract

Abstract Although ZrB 2 -SiC ceramics have been extensively researched for applications at ultra-high temperatures (>2000 °C), it is well known that at these temperatures the SiC oxidises actively yielding a gaseous sub-oxide, SiO, rather than the protective, passive oxide product, SiO 2 . This limits the high-temperature range of SiC-bearing ceramics for ultra-high temperature applications. In the present work, the addition of 5 vol% WC has been shown to partially eliminate the active oxidation of SiC in ZrB 2 -SiC ceramics, even when exposed to an oxyacetylene flame at 2400 °C. In contrast to the porous and fragmentary surface observed with ZrB 2 -SiC ceramics tested under the same conditions, a dense oxide surface layer was observed that is believed to have resulted in decreasing pO 2 in the layers beneath. This had the effect of changing the chemistry of the system and hence the composition of the phases produced. Clear evidence of the presence of SiO 2 was observed, thus indicating that the oxidation of the SiC had been partially passive rather than active. A full volatility diagram for WB at 2400 °C was derived, and existing volatility diagrams for ZrB 2 and SiC were extended to the same temperature, in order to develop a theoretical understanding of the ablation mechanism. The significantly improved ablation resistance of ZrB 2 -SiC-WC is consequently mainly attributed to a competitor transition from tungsten boride (WB) to metallic tungsten in the oxygen partial pressure range 10 −8 Pa to 10 −3 Pa, which retards the occurrence of the active oxidation of the SiC phase.
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Research context

OpenAlex topics: Advanced ceramic materials synthesis · Advanced materials and composites · MXene and MAX Phase Materials

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References (26)

Show source-provided references
1. Advanced structural ceramics in aerospace propulsion10.1038/nmat4687 ↗
2. Stability of ultra-high-temperature ZrB2-SiC ceramics under simulated atmospheric re-entry conditions10.1016/j.jeurceramsoc.2007.02.201 ↗
3. X-43A Hypersonic vehicle technology development10.1016/j.actaastro.2006.02.021 ↗
4. Synthesis of ultra-refractory transition metal diboride compounds10.1557/jmr.2016.210 ↗
5. Ultra-high temperature ceramics: materials for extreme environments10.1016/j.scriptamat.2016.10.018 ↗
6. Oxidation transitions for SiC Part I. Active-to-Passive transitions10.1111/jace.12108 ↗
7. High temperature oxidation at 1900oC of ZrB2-xSiC ultrahigh-temperature ceramic composites10.1111/j.1551-2916.2008.02660.x ↗
8. Oxidation-resistant ZrB2–SiC composites at 2200 °C10.1016/j.compscitech.2007.08.017 ↗
9. UHTC–carbon fibre composites: preparation, oxyacetylene torch testing and characterisation10.1016/j.jeurceramsoc.2012.08.018 ↗
10. Effect of SiC content on electrical, thermal and ablative properties of pressureless sintered ZrB2-based ultrahigh temperature ceramic composites10.1016/j.jeurceramsoc.2016.09.024 ↗
11. Oxidation of ultra-high temperature transition metal diboride ceramics10.1179/1743280411Y.0000000012 ↗
12. Effect of rare-earth dopant (Sm) concentration on total hemispherical emissivity and ablation resistance of ZrB2/SiC coatings10.1016/j.jeurceramsoc.2016.04.013 ↗
13. The addition of lanthanum hexaboride to zirconium diboride for improved oxidation resistance10.1016/j.scriptamat.2007.07.036 ↗
14. Heat flux mapping of oxyacetylene flames and their use to characterise Cf-HfB2 composites10.1080/17436753.2015.1104050 ↗
15. Formation of tough interlocking microstructure in ZrB2-SiC-based ultrahigh-temperature ceramics by pressureless sintering10.1557/jmr.2009.0274 ↗
16. Chemical reactions, anisotropic grain growth and sintering mechanisms of self-reinforced ZrB2-SiC doped with WC10.1111/j.1551-2916.2010.04278.x ↗
17. Thermal properties of (Zr,TM)B2 solid solutions with TM = Hf, Nb, W, Ti, and Y10.1111/jace.12893 ↗
18. Thermal and electrical transport in ZrB2-SiC-WC ceramics up to 1800 °C10.1016/j.actamat.2017.02.052 ↗
19. Thermodynamic analysis of ZrB2-SiC oxidation: formation of a SiC-depleted region10.1111/j.1551-2916.2006.01329.x ↗
20. Condensed phase relations in the systems ZrO2-WO2-WO3 and HfO2-WO2-WO310.1111/j.1151-2916.1967.tb15084.x ↗
21. Improved oxidation resistance of zirconium diboride by tungsten carbide additions10.1111/j.1551-2916.2008.02713.x ↗
22. Calcia-magnesia-alumino-silicate (CMAS)-induced degradation and failure of air plasma sprayed yttria-stabilized zirconia thermal barrier coatings10.1016/j.actamat.2015.12.044 ↗
23. Qualitative analysis of hafnium diboride based ultra high temperature ceramics under oxyacetylene torch testing at temperatures above 2100 °C10.1016/j.jeurceramsoc.2013.11.018 ↗
24. Microstructure evolution of a W-doped ZrB2 ceramic upon high-temperature oxidation10.1111/jace.14738 ↗
25. The ZrB2 volatility diagram10.1111/j.1551-2916.2005.00599.x ↗
26. Volatility diagrams for silica, silicon nitride, and silicon carbide and their application to high temperature decomposition and oxidation10.1111/j.1151-2916.1990.tb06677.x ↗