High temperature C/C-SiC composite by liquid silicon infiltration: a literature review

被引:74
|
作者
Patel, Manish [1 ]
Saurabh, Kumar [1 ]
Prasad, V. V. Bhanu [1 ]
Subrahmanyam, J. [1 ]
机构
[1] Def Met Res Lab, Hyderabad 500058, Andhra Pradesh, India
关键词
CMC; C/C-SiC composite; processing; properties; application; CHEMICAL-VAPOR INFILTRATION; ADVANCED FRICTION SYSTEMS; OXIDATION RESISTANCE; MELT INFILTRATION; CARBIDE; MECHANISM;
D O I
10.1007/s12034-011-0247-5
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The ceramic matrix carbon fibre (CMC) reinforced composite has received great attention for use in aerospace engineering. In aerospace, the atmosphere is highly oxidative and experiences very high temperature. In addition to this, the materials require high thermal stability and high abrasion resistance in that atmosphere. The C/C-SiC composite meets with these requirements. In this paper, the C/C-SiC composite by liquid silicon infiltration is reviewed thoroughly.
引用
收藏
页码:63 / 73
页数:11
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