材料科学
陶瓷
复合材料
保温
纳米纤维
压缩性
热导率
热的
假弹性
微观结构
马氏体
物理
工程类
航空航天工程
气象学
图层(电子)
作者
Lvye Dou,Xinxin Zhang,Haoru Shan,Xiaota Cheng,Yang Si,Jianyong Yu,Bin Ding
标识
DOI:10.1002/adfm.202005928
摘要
Abstract Ceramic aerogels are attractive candidates for thermal insulation systems in spaceships, missiles, and aircrafts. However, the general lack of mechanical stability in conventional ceramic aerogels presents a major challenge for their practical applications. To date, the creation of mechanically robust ceramic aerogels has not made significant progress. Herein, a universal strategy is presented to fabricate ceramic nanofibrous aerogels with both superior bendability and compressibility, by assembling flexible silica nanofibers with a high length‐to‐diameter ratio into a highly continuous interwoven cellular structure. The resulting aerogels, with improved structural continuity, exhibit enhanced mechanical properties including large compression and buckling strain recovery (85%), temperature‐invariant superelasticity (from − 196 ° C to 1100 ° C), and robust fatigue tolerance up to 100 000 cycles. In parallel, the low thermal conductivity (0.0223 W m −1 K −1 ), as well as exceptional high‐temperature thermal insulation performance enable them to be ideal candidates for thermal insulation in extreme environments. The successful synthesis of this material may shed light on the development of other mechanically robust ceramic aerogels.
科研通智能强力驱动
Strongly Powered by AbleSci AI