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C/C—SiC复合材料的制备与性能

余惠琴 陈长乐 邹武 闫联生

宇航材料工艺2001,Vol.31Issue(2):28-32,5.
宇航材料工艺2001,Vol.31Issue(2):28-32,5.

C/C—SiC复合材料的制备与性能

Fabrication and Properties of C/C-SiC Matrix Composites

余惠琴 1陈长乐 1邹武 1闫联生1

作者信息

  • 1. 陕西非金属材料工艺研究所
  • 折叠

摘要

Abstract

Fabrication of carbon fiber reinforced carbon-ceramic matrix composites by chemical vapor infiltration (CVI) and liquid impregnation of organic precursors is presented in this paper.Mechanical properties,ablation protection and oxidation resistance of C/C-SiC are characterized.Research results show that C/C-SiC composites with comparable fracture behavior and flexure strength to those of C/C materials,have better ablation protection and oxidation resistance.It is provided a technical approach to manufacture the carbon-ceramic composites which have comparable properties not only to that of C/C materials,but also to that of ceramics.

关键词

C/C一SiC复合材料/制备工艺/抗氧化

分类

航空航天

引用本文复制引用

余惠琴,陈长乐,邹武,闫联生..C/C—SiC复合材料的制备与性能[J].宇航材料工艺,2001,31(2):28-32,5.

宇航材料工艺

OA北大核心CSCD

1007-2330

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