Rawson Shelley D, Bayram Vildan, McDonald Samuel A, Yang Pei, Courtois Loic, Guo Yi, Xu Jiaqi, Burnett Timothy L, Barg Suelen, Withers Philip J
Henry Royce Institute, Department of Materials, The University of Manchester, Manchester M13 9PL, U.K.
Department of Materials, University of Manchester, Manchester M13 9PL, U.K.
ACS Nano. 2022 Feb 22;16(2):1896-1908. doi: 10.1021/acsnano.1c04538. Epub 2022 Feb 7.
Aerogels are attracting increasing interest due to their functional properties, such as lightweight and high porosity, which make them promising materials for energy storage and advanced composites. Compressive deformation allows the nano- and microstructure of lamellar freeze-cast aerogels to be tailored toward the aforementioned applications, where a 3D nanostructure of closely spaced, aligned sheets is desired. Quantitatively characterizing their microstructural evolution during compression is needed to allow optimization of manufacturing, understand in-service structural changes, and determine how aerogel structure relates to functional properties. Herein we have developed methods to quantitatively analyze lamellar aerogel domains, sheet spacing, and sheet orientation in 3D and to track their evolution as a function of increasing compression through synchrotron phase contrast X-ray microcomputed tomography (μCT). The as-cast domains are predominantly aligned with the freezing direction with random orientation in the orthogonal plane. Generally the sheets rotate toward flat and their spacing narrows progressively with increasing compression with negligible lateral strain (zero Poisson's ratio). This is with the exception of sheets close to parallel with the loading direction (), which maintain their orientation and sheet spacing until ∼60% compression, beyond which they exhibit buckling. These data suggest that a single-domain, fully aligned as-cast aerogel is not necessary to produce a post-compression aligned lamellar structure and indicate how the spacing can be tailored as a function of compressive strain. The analysis methods presented herein are applicable to optimizing freeze-casting process and quantifying lamellar microdomain structures generally.
气凝胶因其功能特性,如轻质和高孔隙率,而受到越来越多的关注,这些特性使其成为储能和先进复合材料的有前途的材料。压缩变形可以使层状冷冻铸造气凝胶的纳米结构和微观结构针对上述应用进行定制,在这些应用中,需要紧密排列、对齐的薄片的三维纳米结构。需要定量表征其在压缩过程中的微观结构演变,以优化制造工艺、了解服役期间的结构变化,并确定气凝胶结构与功能特性之间的关系。在此,我们开发了一些方法,通过同步辐射相衬X射线显微计算机断层扫描(μCT)来定量分析三维层状气凝胶区域、薄片间距和薄片取向,并跟踪它们随压缩增加的演变。铸态区域主要与冷冻方向对齐,在正交平面内具有随机取向。一般来说,薄片会向扁平方向旋转,并且随着压缩增加,它们的间距会逐渐变窄,横向应变可忽略不计(泊松比为零)。与加载方向接近平行的薄片()除外,这些薄片在压缩至约60%之前保持其取向和薄片间距,超过该值后会出现屈曲。这些数据表明,对于产生压缩后排列的层状结构而言,单一区域、完全对齐的铸态气凝胶并非必要,并表明了间距如何根据压缩应变进行调整。本文提出的分析方法通常适用于优化冷冻铸造工艺和量化层状微区结构。