Prediction of effective elastic modulus of plain weave multiphase and multilayer silicon carbide ceramic matrix composite

2008 ◽  
Vol 24 (4) ◽  
pp. 435-442 ◽  
Author(s):  
Y. J. Xu ◽  
W. H. Zhang ◽  
H. B. Wang
2020 ◽  
Vol 47 (6) ◽  
pp. 0600002
Author(s):  
翟兆阳 Zhai Zhaoyang ◽  
梅雪松 Mei Xuesong ◽  
王文君 Wang Wenjun ◽  
崔健磊 Cui Jianlei

2019 ◽  
Vol 103 (5-8) ◽  
pp. 3175-3186 ◽  
Author(s):  
Yadong Gong ◽  
Shuoshuo Qu ◽  
Yuying Yang ◽  
Chunyou Liang ◽  
Pengfei Li ◽  
...  

Author(s):  
Venkat Vedula ◽  
Jun Shi ◽  
David Jarmon ◽  
Scott Ochs ◽  
Lola Oni ◽  
...  

Ceramic matrix composite (CMC) turbine vanes, due to their high temperature capability, allow significantly higher firing temperatures with minimal cooling. Turbine vanes were designed for a gas turbine engine with special attention to attachment methods that minimize thermal stresses due to large differences in coefficients of thermal expansion between the CMC airfoil and metal platforms. Detailed aerodynamic, thermal and structural analyses were performed to ensure component reliability. The paper describes the component design, analysis, fabrication, and rig testing of a silicon carbide fiber reinforced silicon carbide matrix (SiC/SiC) turbine vane.


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