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碳纤维增强SiBCN陶瓷基复合材料的制备及性能

王秀军 张宗波 曾凡 李永明 徐彩虹

宇航材料工艺2013,Vol.43Issue(2):47-50,4.
宇航材料工艺2013,Vol.43Issue(2):47-50,4.

碳纤维增强SiBCN陶瓷基复合材料的制备及性能

Fabrication and Properties of Carbon Fiber Reinforced SiBCN Matrix Composites

王秀军 1张宗波 2曾凡 1李永明 2徐彩虹1

作者信息

  • 1. 中国科学院化学研究所,北京100190
  • 2. 中国科学院研究生院,北京100049
  • 折叠

摘要

Abstract

Carbon fiber reinforced SiBCN-matrix composites were fabricated by polymer infiltration and pyrolysis route (PIP) with a lab-produced SiBCN precursor (P-SiBCN) as a matrix source.Their mechanical properties were investigated.The composite obtained from 8 PIP-cycles showed its flexure strengths of 334 MPa at room temperature,and in-situ flexure strength of 367 MPa at 800℃ in inert gas atmosphere.The composite retained its 60% strengths upon bending even at 800℃ in air.

关键词

聚硼硅氮烷/前驱体浸渍裂解技术/陶瓷基复合材料

Key words

Polyborosilazane/ Polymer infiltration and pyrolysis/ Ceramic matrix composites

引用本文复制引用

王秀军,张宗波,曾凡,李永明,徐彩虹..碳纤维增强SiBCN陶瓷基复合材料的制备及性能[J].宇航材料工艺,2013,43(2):47-50,4.

宇航材料工艺

OA北大核心CSCDCSTPCD

1007-2330

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