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碳纤维增强超高温陶瓷基复合材料的性能与微结构
引用本文:孙银洁,李秀涛,宋扬,石晓斌,许春来.碳纤维增强超高温陶瓷基复合材料的性能与微结构[J].宇航材料工艺,2011,41(6).
作者姓名:孙银洁  李秀涛  宋扬  石晓斌  许春来
作者单位:航天材料及工艺研究所,先进功能复合材料技术重点实验室,北京100076
摘    要:利用前驱体浸渍、裂解方法制备了两种超高温陶瓷基复合材料,并对材料的力学性能进行了评价.采用SEM、EDS表征手段分析了材料复合过程中的微观结构特征,获得了工艺过程中碳纤维、基体、界面特征及其变化规律.结果表明,材料致密化周期减少,热处理时间缩短,对纤维的损伤减轻,能充分提高碳纤维的强度利用率,从而提高材料的力学性能.

关 键 词:超高温陶瓷复合材料  碳纤维  前驱体  微观结构  性能

Properties and Microstructures of Carbon Fiber Reinforced Ultra-High Temperature Ceramic Matrix Composites
Sun Yinjie,Li Xiutao,Song Yang,Shi Xiaobin,Xu Chunlai.Properties and Microstructures of Carbon Fiber Reinforced Ultra-High Temperature Ceramic Matrix Composites[J].Aerospace Materials & Technology,2011,41(6).
Authors:Sun Yinjie  Li Xiutao  Song Yang  Shi Xiaobin  Xu Chunlai
Affiliation:Sun Yinjie Li Xiutao Song Yang Shi Xiaobin Xu Chunlai (National Key Laboratory of Advanced Functional Composite Materials Aerospace,Aerospace Research Instutute of Materials & Processing Technology,Beijing 100076)
Abstract:Carbon fiber reinforced ultra high temperature ceramic composites were prepared by precursor infiltration pyrolysis.The characteristics of carbon fiber,matrix and fiber-matrix interface of the composites were obtained by microstructures analysis.The correlations of processing-microstructure-mechanical properties were illustrated by the analysis of the precursor properties,the preparation,mechanical properties and microstructure.Results show that less dipping cycles and pyrolysis time can reduce the damage o...
Keywords:Ultra-high temperature ceramic composite  Carbon fiber  Precursor  Microstructure  Properties  
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