烧蚀
材料科学
热解
渗透(HVAC)
复合材料
碳化硅
硅
化学气相渗透
复合数
化学工程
冶金
工程类
航空航天工程
作者
Jiaping ZHANG,Yuepeng Xin,Run-ning Wang,Qiangang Fu
标识
DOI:10.1016/j.cja.2023.07.018
摘要
C/C-SiC-HfC composites were fabricated by using Precursor Infiltration and Pyrolysis (PIP) combined with Gaseous Silicon Infiltration (GSI) process. Different GSI temperatures (1900 ℃ and 2100 ℃) were selected. The combination of PIP and GSI could significantly reduce the preparation time of the composites. The morphology displaying a rich-Si layer was formed on the surface of the composites prepared at GSI 2100 ℃. Ablation performance of the composites was investigated by oxyacetylene torch. The results showed that after ablation for 120 s, compared to the composites prepared by PIP+1900 ℃ GSI, the linear and mass ablation rates of the composites fabricated by PIP+2100 ℃ GSI were decreased from 8.05 μm/s to 5.06 μm/s and from 1.61 mg/s to 1.03 mg/s, respectively. The coverage of the rich-Si surface layer promoted the generation of more SiO2 during ablation, which not only benefited for decreasing the surface temperature but also contributed to the formation of H-Si-O glass and the HfO2 skeleton, thus better resisting the denudation of the oxyacetylene torch.
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