锆-硅有机前驱体裂解机理及PIP法制备C/C-ZrC-SiC复合材料的烧蚀行为
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  • 英文篇名:Pyrolysis Mechanism of Zr-Si Precursor and Ablation Behavior of C/C-ZrC-SiC Composites Prepared by PIP Method
  • 作者:刘春轩 ; 曹柳絮 ; 黄启忠
  • 英文作者:LIU Chun-xuan;CAO Liu-xu;HUANG Qi-zhong;Hunan Xiangtou Goldsky Science and Technology Group Co.,Ltd.;Powder Metallurgy Reseach Institute,Central South University;
  • 关键词:Zr-Si ; 裂解机理 ; 前驱体浸渍-裂解法 ; C/C-ZrC-SiC复合材料
  • 英文关键词:Zr-Si;;pyrolysis mechanism;;precursor infiltration and pyrolysis;;C/C-ZrC-SiC composites
  • 中文刊名:XYJY
  • 英文刊名:Rare Metals and Cemented Carbides
  • 机构:湖南湘投金天科技集团有限责任公司;中南大学粉末冶金研究院;
  • 出版日期:2019-04-20
  • 出版单位:稀有金属与硬质合金
  • 年:2019
  • 期:v.47;No.231
  • 语种:中文;
  • 页:XYJY201902005
  • 页数:9
  • CN:02
  • ISSN:43-1109/TF
  • 分类号:26-33+66
摘要
使用有机锆前驱体(POZ)和聚碳硅烷(PCS)作为前驱体,通过前驱体浸渍-裂解工艺(PIP)制备了C/C-ZrC-SiC复合材料。采用热重分析仪、X射线衍射、扫描电子显微镜等手段研究了Zr-Si混合前驱体的裂解过程中的热失重行为、物相转化过程及显微组织,并详细分析了复合材料的微观结构和烧蚀行为。结果表明:将Zr-Si混合前驱体从室温加热至1 200℃时,ZrC首先转化为无机态的ZrO_2,当裂解温度升高至1 600℃时,ZrO_2通过碳热还原反应生成ZrC陶瓷;SiC晶体的转变温度为1 200~2 000℃。对C/C-ZrC-SiC复合材料烧蚀后的显微组织观察表明,所制备的复合材料具有良好的耐烧蚀性能。
        C/C-ZrC-SiC composites were prepared by precursor infiltration and pyrolysis using poly-meric organic zirconium precursor(POZ) and polycarbosilane(PCS) as precursor.Thermogravimetric behavior,phase conversion and microstructure of Zr-Si mixed precursors during pyrolysis were studied by thermal gravimetric analyzer,X-ray diffraction and scanning electron microscope,and the microstructure and ablation behavior of the composites were analyzed in detail.The results indicate that when Zr-Si mixed precursors is heated from room temperature to 1 200 ℃,ZrC precursor transforms to inorganic ZrO_2.When the pyrolysis temperature rises to 1 600 ℃,ZrO_2 can be reduced to ZrC ceramics by carbothermal reduction reaction.The transition temperature of the SiC crystal is 1 200~2 000 ℃.The microstructure of the C/C-ZrC-SiC composites after ablation shows that the prepared composites exhibit good ablation resistance.
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