用3D-C/SiC和重结晶SiC陶瓷材料在光辐射热震试验机上进行了两种温度落差(AT=600 ℃,800 ℃)和不同应力的热震试验.3D-C/SiC用弹性模量和电阻表征的热震损伤曲线有相似的规律,即都大致由三阶段构成,首先是损伤急剧增加阶段,紧接着是损伤缓慢增加阶段,最后为损伤短暂的急剧增加阶段.个别电阻表征的热震损伤曲线仅在初始阶段损伤有下降现象.3D-C/SiC复合材料的抗热震性能明显优于重结晶SiC陶瓷材料;三种界面层的3D-C/SiC中,以热解碳沉积时间为20h获得的界面层复合材料热震寿命最长.
参考文献
[1] | Ko F;Koczak M;Layden G.Structural Toughening of Glass Matrix Composites by 3-D Fiber Architecture[J].Ceramic Engineering and Science Proceedings,1998:822-831. |
[2] | S. Zhu;M. Mizuno .Monotonic tension, fatigue and creep behavior of SiC-fiber-reinforced SiC-matrix composites: a review[J].Composites science and technology,1999(special section):833-85. |
[3] | 杜双明;乔生儒;吕宝桐.光辐射热机械疲劳试验机[A].,2000 |
[4] | Hwang;R N Singh .Thermal shock behaviour of ceramics and ceramic composites[J].International Materials Reviews,1994,39:6. |
[5] | 李灏.损伤力学基础[M].济南:山东科学技术出版社,1992 |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%