材料科学
碳化硅
复合材料
涂层
陶瓷基复合材料
硅
热解
化学气相渗透
热冲击
多孔性
陶瓷
化学工程
冶金
工程类
作者
Bernd Mainzer,Martin Frieß,Kristina Roder,Daisy Nestler,D. Wett,Lydia Wöckel,Thomas Ebert,Guntram Wagner,Stefan Spange,Dietmar Koch
出处
期刊:Materials Science Forum
日期:2015-07-01
卷期号:825-826: 224-231
被引量:4
标识
DOI:10.4028/www.scientific.net/msf.825-826.224
摘要
SiC/SiC ceramics consist of silicon carbide fibres embedded in a silicon carbide matrix. As an alternative to classic CVI and PIP routes, Liquid Silicon Infiltration (LSI) was chosen as a technique with short process times to obtain composites with low porosity. Silicon carbide composites show good thermal shock resistance, a low coefficient of thermal expansion and excellent physical and chemical stability at elevated temperatures and are therefore regarded as promising candidates for various applications in jet engines and in power engineering. To build up the matrix, different phenolic resin based carbon precursors were infiltrated in fibre preforms and thermally cured, pyrolysed and siliconized. The aim is to obtain a high carbon yield during pyrolysis and to control the pore morphology in a way that the following liquid silicon infiltration leads to a complete reaction of the carbon matrix with silicon to SiC. The siliconization behaviour and conversion into SiC in dependence of pore morphology and chosen precursor is analysed.At the same time a functional fibre coating has to be developed which protects the fibres from liquid silicon and simultaneously provides a weak fibre matrix bonding. A LPCVD-SiN x fibre coating has been chosen and is investigated in fibre composites especially in terms of protection and reactivity in different atmospheres during pyrolysis and siliconization.
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