journal article·2022-11

Microstructural evolution mechanism of plain-woven SiC/SiC during thermal ablation

Jinkang Du, Guoqiang Yu, Huajun Zhang, Yunfa Jia, Ruixiang Chen, Chenyang Liu, Xiguang Gao, Fang Wang, Yingdong Song

Corrosion Science· Volume 208
Publisher page

Abstract

The ablation characteristics of plain-woven SiC/SiC composites were investigated using an oxy-acetylene flame to reveal the failure process. The results showed that the linear ablation rate decreased linearly with time to 0.035 mm/s at 60 s of ablation. The ablation process of single SiC fibers resulted in the formation of a characteristic SiO 2 broken porous tubular structure on the external surface. Due to the characteristics of the warp and weft weave structure of the material, resulting in the formation of "micro-pits" on the surface of the SiC fibers.
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Research context

OpenAlex topics: Advanced ceramic materials synthesis · Advanced materials and composites · Aluminum Alloys Composites Properties

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

References (40)

Show source-provided references
1. T. Ohji, M. Singh, Engineered Ceramics: Current Status and Future Prospects, 2016. 〈https://doi.org/10.1002/9781119100430〉.10.1002/9781119100430 ↗
2. Development of advanced environmental barrier coatings for SiC/SiC ceramic matrix composites: path toward 2700 F temperature capability and beyond
3. Advanced ceramic matrix composite materials for current and future propulsion technology applications10.1016/j.actaastro.2004.05.052 ↗
4. Development of CMC vane for gas turbine engine
5. Advanced structural ceramics in aerospace propulsion10.1038/nmat4687 ↗
6. Ceramic matrix composites taking flight at GE Aviation
7. Evaluation of ceramic matrix composite technology for aircraft turbine engine applications10.2514/6.2013-539 ↗
8. Design, preparation and properties of carbon fiber reinforced ultra-high temperature ceramic composites for aerospace applications: a review10.1016/j.jmst.2016.08.004 ↗
9. Fabrication and characterization of 2. 5D and 3D SiC f / SiC composites10.1016/j.fusengdes.2013.04.002 ↗
10. A review of numerical models for 3D woven composite reinforcements10.1016/j.compstruct.2018.10.085 ↗
11. Ablative polymers in aerospace technology10.1080/10601326908053818 ↗
12. Ablation behaviors of ultra-high temperature ceramic composites10.1016/j.msea.2007.02.040 ↗
13. Gas turbine heat transfer: ten remaining hot gas path challenges10.1115/1.2464142 ↗
14. Effect of oxidation on elastic modulus of C/C-SiC composites10.1016/j.msea.2007.09.078 ↗
15. Oxidation-resistant ZrB2-SiC composites at 2200 °C10.1016/j.compscitech.2007.08.017 ↗
16. Comparison of morphology and microstructure of ablation centre of C/SiC composites by oxy-acetylene torch at 2900 and 3550 °C10.1016/j.corsci.2008.07.019 ↗
17. Effects of ablation at different regions in three-dimensional orthogonal C/SiC composites ablated by oxyacetylene torch at 1800 °C10.1016/j.jmatprotec.2008.08.002 ↗
18. Microstructure and ablation properties of zirconium carbide doped carbon/carbon composites10.1016/j.carbon.2009.09.035 ↗
19. The effect of zirconium carbide on ablation of carbon/carbon composites under an oxyacetylene flame10.1016/j.corsci.2010.09.028 ↗
20. A multilayer SiC/ZrB2/SiC ablation resistance coating for carbon/carbon composites10.1002/adem.201800774 ↗
21. Synergetic effects of Kevlar fibers and polyimide powder fillers on performances of Poly(diaryloxyphosphazene) based elastomeric heat shielding materials10.1016/j.compscitech.2022.109439 ↗
22. Ablation performance of C/HfC-SiC composites with in-situ HfSi2/HfC/SiC multi-phase coatings under 3000 °C oxyacetylene torch10.1016/j.corsci.2022.110218 ↗
23. Analytical modeling of the steady state ablation of a 3D C/C composite10.1016/j.ijheatmasstransfer.2008.01.008 ↗
24. A Brownian motion technique to simulate gasification and its application to C/C composite ablation10.1016/j.commatsci.2008.07.015 ↗
25. Ablation of carbon-based materials: multiscale roughness modelling
26. Ablation behavior and mechanism of SiC/Zr-Si-C multilayer coating for PIP-C/SiC composites under oxyacetylene torch flame10.1016/j.compositesb.2013.10.033 ↗
27. Formation of oxide scales on zirconium diboride-silicon carbide composites during oxidation: Relation of subscale recession to liquid oxide flow10.1111/j.1551-2916.2008.02639.x ↗
28. Evolution of surface droplets and flow patterns on C/SiC during thermal ablation10.1016/j.jeurceramsoc.2019.05.037 ↗
29. Revealing thermal ablation mechanisms of C/SiC with in situ optical observation and numerical simulation10.1016/j.jeurceramsoc.2020.04.010 ↗
30. Morphology and microstructure of SiC/SiC composites ablated by oxyacetylene torch at 1800 °C10.1016/j.jeurceramsoc.2021.06.026 ↗
31. Ultra-high temperature ablation behaviour of 2.5D SiC/SiC under an oxy-acetylene torch10.1016/j.corsci.2022.110263 ↗
32. National Standard Committee of China, GJB323A-96: Measurement Standard of Ablation Properties of Materials, Natl. Stand. Comm. China, Beijing, 1996.
33. Effects of TaC amount on the properties of 2D C/SiC-TaC composites prepared via precursor infiltration and pyrolysis10.1016/j.matdes.2013.03.073 ↗
34. Microstructure and ablation mechanism of C/C-SiC composites10.1016/j.jeurceramsoc.2013.08.026 ↗
35. Ablation behavior and mechanism analysis of C/SiC composites10.1016/j.jmrt.2015.10.004 ↗
36. SiC recession caused by SiO2 scale volatility under combustion conditions: I. Experimental results and empirical model10.1111/j.1151-2916.1999.tb02004.x ↗
37. Adopting traditional image algorithms and deep learning to build the finite model of a 2.5D composite based on X-Ray computed tomography10.1016/j.compstruct.2021.114440 ↗
38. Y.I. Dimitrienko, Thermomechanics of Composite Structures under High Temperatures, 2016. 〈http://link.springer.com/10.1007/978-94-017-7494-9〉.10.1007/978-94-017-7494-9 ↗
39. SiC recession caused by SiO2 scale volatility under combustion conditions: II, thermodynamics and gaseous-diffusion model10.1111/j.1151-2916.1999.tb02004.x ↗
40. A combined thermodynamic/kinetic modeling approach to predict SiC recession due to SiO2 scale volatility under combustion environments10.1007/s11669-014-0336-4 ↗