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用于高温应用的碳氧化硅纤维毡静电纺丝的制备与表征

Fabrication and characterization of silicon oxycarbide fibre-mats electrospinning for high temperature applications.

作者信息

Ren Zhongkan, Gervais Christel, Singh Gurpreet

机构信息

Departement of Mechanical and Nuclear Engineering, Kansas State University Manhattan KS 66506 USA

Sorbonne Université, CNRS UMR 7574, Laboratoire de Chimie de la Matière Condensée de Paris 75005 Paris France.

出版信息

RSC Adv. 2020 Oct 19;10(63):38446-38455. doi: 10.1039/d0ra04060f. eCollection 2020 Oct 15.

Abstract

Electrospinning is an emerging technique for synthesizing micron to submicron-sized polymer fibre supports for applications in energy storage, catalysis, filtration, drug delivery and so on. However, fabrication of electrospun ceramic fibre mats for use as a reinforcement phase in ceramic matrix composites or CMCs for aerospace applications remains largely unexplored. This is mainly due to stringent operating requirements that require a combination of properties such as low mass density, high strength, and ultrahigh temperature resistance. Herein we report fabrication of molecular precursor-derived silicon oxycarbide or SiOC fibre mats electrospinning and pyrolysis of cyclic polysiloxanes-based precursors at significantly lower weight loadings of organic co-spin agent. Ceramic fibre mats, which were free of wrapping, were prepared by a one-step spinning (in air) and post heat-treatment for crosslinking and pyrolysis (in argon at 800 °C). The pyrolyzed fibre mats were revealed to be amorphous and a few microns in diameter. Four siloxane-based pre-ceramic polymers were used to study the influence of precursor molecular structure on the compositional and morphological differences of cross-linked and pyrolyzed products. Further thermal characterization suggested the potential of electrospun ceramic mats in high temperature applications.

摘要

静电纺丝是一种新兴技术,用于合成微米至亚微米尺寸的聚合物纤维载体,应用于能量存储、催化、过滤、药物递送等领域。然而,用于航空航天应用的陶瓷基复合材料(CMC)中作为增强相的静电纺丝陶瓷纤维毡的制备在很大程度上仍未得到探索。这主要是由于严格的操作要求,需要低质量密度、高强度和超高温抗性等性能的组合。在此,我们报告了通过静电纺丝和在有机共纺剂重量负载显著降低的情况下对基于环状聚硅氧烷的前驱体进行热解来制备分子前驱体衍生的碳氧化硅(SiOC)纤维毡。通过一步纺丝(在空气中)和后热处理(在800℃的氩气中进行交联和热解)制备了无包裹的陶瓷纤维毡。热解后的纤维毡显示为无定形,直径为几微米。使用四种基于硅氧烷的陶瓷前驱体聚合物来研究前驱体分子结构对交联和热解产物的组成和形态差异的影响。进一步的热表征表明静电纺丝陶瓷毡在高温应用中的潜力。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/183c/9057258/51e96f1aa3b2/d0ra04060f-f1.jpg

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