材料科学
保温
热的
复合材料
碳纤维
图层(电子)
气象学
物理
复合数
作者
Xinyi Chang,Fan Wu,Xiaota Cheng,Hao Zhang,Lijuan He,Wenjing Li,Xia Yin,Jianyong Yu,Yitao Liu,Bin Ding
标识
DOI:10.1002/adma.202308519
摘要
Abstract With ultralight weight, low thermal conductivity, and extraordinary high‐temperature resistance, carbon aerogels hold tremendous potential against severe thermal threats encountered by hypersonic vehicles during the in‐orbit operation and re‐entry process. However, current 3D aerogels are plagued by irreconcilable contradictions between adiabatic and mechanical performance due to monotonicity of the building blocks or uncontrollable assembly behavior. Herein, a spatially confined assembly strategy of multiscale low‐dimensional nanocarbons is reported to decouple the stress and heat transfer. The nanofiber framework, a basis for transferring the loading strain, is covered by a continuous thin‐film‐like layer formed by the aggregation of nanoparticles, which in combination serve as the fundamental structural units for generating an elastic behavior while yielding compartments in aerogels to suppress the gaseous fluid thermal diffusion within distinct partitions. The resulting all‐carbon aerogels with a hierarchical cellular structure and quasi‐closed cell walls achieve the best thermomechanical and insulation trade‐off, exhibiting flyweight density (24 mg cm −3 ), temperature‐constant compressibility (−196–1600 °C), and a low thermal conductivity of 0.04 829 W m −1 K −1 at 300 °C. This strategy provides a remarkable thermal protection material in hostile environments for future aerospace exploration.
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