材料科学
三元运算
气凝胶
复合材料
复合数
陶瓷
热导率
保温
图层(电子)
计算机科学
程序设计语言
作者
Jianyu Wang,Hongyan Li,Hongli Liu,Zhijie Feng,Zijian Cui,Xiaolan Liao,Baolian Zhang,Qi Li
标识
DOI:10.1016/j.jeurceramsoc.2023.04.049
摘要
Highly porous, heat resisting ceramic aerogels are considered as promising materials for high-temperature insulation. However, the general structural characteristics of ceramic aerogel, such as poor mechanical strength and transparency to infrared radiation, pose a major obstacle to their practical application. In this paper, we report a general strategy to prepare hollow mullite fiber (HMF) structures by coaxial electrostatic spinning and grow TiO2 nanorods (TiO2/NAs) in situ on HMF. The ternary composite ceramic aerogel material was prepared by filling the pores of HMF-TiO2/NAs with SiCN aerogel. The TiO2/NAs increased the fiber/aerogel interfacial bonding of the composite (0.392 MPa, 30% strain) and improved the IR transmittance (∼0%, 1200 ℃) without sacrificing their low density and thermal conductivity. In addition, low thermal conductivity (0.041 W/(m·K), 1200 °C) and excellent high-temperature insulation properties allow the composite aerogel to meet the urgent need for lightweight, high-strength, high-temperature insulation systems for spacecraft.
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