Thermal damage and microstructure evolution mechanisms of Cf/SiBCN composites during plasma ablation

被引:31
作者
Ding, Qi [1 ,5 ]
Ni, Dewei [1 ,3 ]
Ni, Na [5 ]
Jiang, Youlin [1 ,3 ,4 ]
Chen, Bowen [1 ,3 ,4 ]
Chen, Xiaowu [1 ,3 ]
Lu, Jun [1 ,3 ,4 ]
Niu, Yaran [6 ]
Zhou, Haijun [1 ,3 ]
Dong, Shaoming [1 ,2 ,3 ]
机构
[1] Chinese Acad Sci, Shanghai Inst Ceram, State Key Lab High Performance Ceram & Superfine, Shanghai 200050, Peoples R China
[2] Univ Chinese Acad Sci, Ctr Mat Sci & Optoelect Engn, Beijing 100049, Peoples R China
[3] Chinese Acad Sci, Struct Ceram & Composites Engn Res Ctr, Shanghai Inst Ceram, Shanghai 200050, Peoples R China
[4] Univ Chinese Acad Sci, Beijing 100049, Peoples R China
[5] Shanghai Jiao Tong Univ, Sch Mech Engn, Key Lab, Educ Minist Power Machinery & Engn, Shanghai 200240, Peoples R China
[6] Chinese Acad Sci, Shanghai Inst Ceram, Key Lab Inorgan Coating Mat CAS, Shanghai 200050, Peoples R China
基金
中国国家自然科学基金;
关键词
C-f/SiBCN composites; Plasma ablation; Thermal damage mechanism; N CERAMICS; MATRIX COMPOSITES; PHASE EVOLUTION; PRECURSOR; CRYSTALLIZATION; BEHAVIOR; STABILITY; INFILTRATION; RESISTANCE; FIBERS;
D O I
10.1016/j.corsci.2020.108621
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Ablation behavior and thermal damage mechanisms of C-f/SiBCN composites were investigated in plasma ablation flame under a heat flux of 4.02 MW/m(2), simulating a hypersonic service environment at similar to 2200 degrees C. Oxide layer formed on the composites surface effectively protects internal C-f/SiBCN composites from further ablation. However, the internal C-f/SiBCN composites endure severe thermal damage and complex reactions, leading to decomposition of SiBCN matrix and formation of alpha/beta-SiC, beta-Si3N4 grains, amorphous C layer and ring-like SiC layer. Based on detailed microstructure and phase composition analysis, thermal damage and microstructure evolution mechanisms of C-f/SiBCN composites during plasma ablation are clarified.
引用
收藏
页数:10
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