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作 者:叶丽[1] 陈于蓝[1] 韩伟健[1] 冀志宏[1] 赵彤[1]
出 处:《宇航材料工艺》2009年第6期19-22,共4页Aerospace Materials & Technology
摘 要:以间苯二酚(R)和甲醛(F)为碳源,以3-胺丙基三乙氧基硅烷(APTES)为硅源,一步溶胶-凝胶法简单快捷地合成了SiO2-RF复合气凝胶,高温碳化后得到SiO2-C复合气凝胶,并用扫描电镜、比表面分析仪对所得样品的结构进行了研究,并讨论了不同投料比对气凝胶结构的影响。结果表明碳化前,投料比APTES/R=1时,所得气凝胶具有最大的比表面积(SBET=606.1m2/g),碳化后,由于体积收缩和酚醛热解产生新孔隙双重因素的影响,投料比APTES/R=1/2时样品的比表面积达到最大(SBET=704.2m2/g)。SiO2 -RF composite aerogels were prepared by one-step sol-gel method by using resorcinol (R), formaldehyde (F) and 3-aminopropyhriethoxytsilane (APTES) as starting materials. After carbonization, SiO2 - C composite aerogels were obtained. The structure of the aerogels was characterized by scanning electron microscopy and nitrogen adsorption/desorption analysis. The structure of SiO2 - RF snd SiO2 - C composite aerogels are strongly dependent on the APTES/R molar ratio. When APTES/R = 1, SiO2 - RF composite aerogel has the highest specific surface area SRET (606.1 m2/g). However, the highest specific surface area SBET (704. 2 m2/g) is obtained when APTES/ R = 1/2 after carbonization for two reason:volume shrinkage and new pore come into being.
分 类 号:TQ264.12[化学工程—有机化工] TN6[电子电信—电路与系统]
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