Fatigue resistance and damage mechanisms of 2D woven SiC/SiC composites at high temperatures

被引:1
|
作者
Zeng, Bin [1 ,2 ,3 ]
Ma, Qin [1 ,2 ,3 ]
Xue, Yudong [1 ,2 ]
Liao, Chunjing [1 ,2 ]
Qin, Hao [1 ,2 ]
Chen, Xiaowu [1 ,2 ]
Hu, Jianbao [1 ,2 ]
Zhang, Xiangyu [1 ,2 ]
Yang, Jinshan [1 ,2 ,5 ]
Dong, Shaoming [1 ,2 ,4 ,5 ]
机构
[1] Chinese Acad Sci, Shanghai Inst Ceram, State Key Lab High Performance Ceram & Superfine M, Shanghai, Peoples R China
[2] Chinese Acad Sci, Shanghai Inst Ceram, Struct Ceram & Composites Engn Res Ctr, Shanghai, Peoples R China
[3] Univ Chinese Acad Sci, Beijing, Peoples R China
[4] Univ Chinese Acad Sci, Ctr Mat Sci & Optoelect Engn, Beijing, Peoples R China
[5] Chinese Acad Sci, Shanghai Inst Ceram, StateKey Lab High Performance Ceram & Superfine Mi, Shanghai 200050, Peoples R China
基金
中国国家自然科学基金;
关键词
failure mechanisms; fracture microstructure; high-temperature fatigue; mechanical properties; SiC; SiC composites; CERAMIC-MATRIX COMPOSITES; SIC-FIBER; PARALINEAR OXIDATION; DEGREES-C; BEHAVIOR; TENSION; AIR; STABILITY; CREEP; CVD;
D O I
10.1111/ijac.14379
中图分类号
TQ174 [陶瓷工业]; TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Fatigue resistance and damage mechanisms of 2D woven SiC/SiC composites at high temperatures were investigated in this research. Fatigue behavior tests were performed at 1200celcius and 1000 degrees C at 10 Hz and stress ratio of 0.1 for maximum stresses ranging from 80 to 120 MPa, and the fatigue run-out could be defined as 10(6) cycles. Evolution of the cumulative displacement and normalized modulus with cycles was analyzed for each fatigue condition. Fatigue run-out was achieved at 80 MPa and 1000 degrees C. It could be found that the cycle lifetimes of the composites decreased sharply with the increasing maximum stress and temperature conditions significantly affected the fatigue performance under matrix cracking stress. The cumulative displacement showed no noticeable increase before 1000 cycles and the modulus of the failed specimens decreased before fracture. The retained properties of composites that achieved fatigue run-out, as well as the microstructures, were characterized in order to understand the fatigue behavior and failure mechanisms. The composites exhibited similar fracture morphology with matrix crack extension and glass phase oxidation formation under different conditions. In general, the high-temperature fatigue damage and failure of composites could be affected by combination of stress damage and oxidative embrittlement.
引用
收藏
页码:3052 / 3063
页数:12
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