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碳-高硅氧纤维增强C-SiC防热隔热一体化材料

A thermal protective and heat-insulated integration material:carbon fibers and high-silica fibers reinforced C-SiC matrix composites

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【作者】 周星明汤素芳邓景屹刘文川杜海峰

【Author】 ZHOU Xingming TANG Sufang DENG Jingyi LIU Wenchuan DU Haifeng (Institute of Metal Research,Chinese Academy of Sciences,Shen Yang 110016)

【机构】 中国科学院金属研究所中国科学院金属研究所 沈阳 110016沈阳 110016

【摘要】 制备了一种新型的防热隔热一体化材料-碳-高硅氧纤维增强 C-SiC 复合材料,沿厚度方向从抗烧蚀层渐次过渡到隔热层,其组成依次是致密 C/C-SiC,致密 C/C,多孔 C/C,通过界面处过渡到变密度多孔 HSF/C.这种材料既具有抗烧蚀性能又具有隔热性能.C/C-SiC 复合材料的烧蚀表面平滑,线烧蚀率只有0.028mm/s.烧蚀性能的提高得益于 SiC 颗粒原位氧化生成 SiO2黏附在碳材料表面,对氧气有一定的阻挡遮蔽作用.密度为0.80 g/cm3的 HSF/C 材料,热导率为0.59 W/mK.在碳纤维与高硅氧织物的界面处,针刺纤维与热解碳的结合良好,密度为1.69g/cm3的 C-HSF/C 复合材料界面处的剪切强度达到16.7MPa.

【Abstract】 A novel composite,carbon fibers and high-silica fibers reinforced carbon matrix and silicon carbide matrix(C-HSF/C-SiC),was prepared.The material consisted of four layers,which were densified C/C-SiC,densified C/C,porous C/C and porous HSF/C.The two formers act as the heat-protective layers while the two latter the heat-insulated layers.The composite possesses a smooth ablation surface after an ablation test performed on an engine torch and the erosion rate is only 0.028mm/s.The better anti-ablation properties should attribute to SiO2 formed by SiC oxidation holding up the flame further attack.The thermal conductivity of HSF/C with the density of 0.80g/cm3 is 0.59W/mK,which has a good thermal insulation action.The needling fiber bundles and pyrocarbon have integrated tightly carbon fiber fabric and HSF fabric.The interfacial shear strength between the two fabics is 16.7MPa.

【基金】 国家自然科学基金 No.90205017资助项目~~
  • 【文献出处】 材料研究学报 ,Chinese Journal of Materials Research , 编辑部邮箱 ,2006年02期
  • 【分类号】TB332
  • 【被引频次】12
  • 【下载频次】573
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