4.7 Article

Ablation behavior of C/C-ZrC and C/SiC-ZrC composites fabricated by a joint process of slurry impregnation and chemical vapor infiltration

期刊

CERAMICS INTERNATIONAL
卷 44, 期 5, 页码 4777-4782

出版社

ELSEVIER SCI LTD
DOI: 10.1016/j.ceramint.2017.12.062

关键词

Ceramic matrix composites; Ultra-high temperature ceramics; Slurry infiltration; Ablation behavior; Microstructure

资金

  1. National Key Research and Development Program of China [2017YFB0703200]
  2. National Natural Science Foundation of China [51772308, 51702341]
  3. Chinese Academy of Sciences Innovative Funding [CXJJ-17-M169]
  4. CAS Pioneer Hundred Talents Program

向作者/读者索取更多资源

C/C-ZrC and C/SiC-ZrC composites were fabricated by a joint process of slurry impregnation and chemical vapor infiltration, in which ZrC matrix was obtained by slurry impregnation process, while C or SiC matrix was introduced by chemical vapor infiltration process. The as fabricated C/C-ZrC and C/SiC-ZrC composites have densities of 1.67 g cm(-3) and 1.91 g cm(-3) respectively. Tensile strength is 89.4 +/- 8.4 MPa and 182.2 +/- 14.0 MPa respectively for the as prepared C/C-ZrC and C/SiC-ZrC. Ablation behavior of the C/C-ZrC and C/SiC-ZrC composites under air plasma was studied and compared in detail. Due to different oxidation resistance and heat transfer capacity of the matrix, these two ZrC based composites showed various ablation behavior. The linear erosion rate is 48 mu m s(-1) and 39 mu m s(-1) respectively for C/C-ZrC and C/SiC-ZrC composites.

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