采用扫描电镜原位观察方法研究了束丝SiC纤维增强铝复合丝在低频疲劳和静拉伸过程中的损伤过程,实验发现,经过较短时间的疲劳加载或在较低的载荷下就出现纤维裂纹,裂纹向基体方向扩展,没有明显的界面脱粘现象.损伤过程可分为三个阶段,包括以纤维裂纹萌生为主的损伤起始阶段、以纤维多次断裂和基体裂纹扩展为主的损伤累计阶段以及裂纹迅速扩展和主裂纹连接的失稳破坏阶段.根据剪滞模型计算的表观界面强度表明该复合丝为强结合界面.
参考文献
[1] | Kazumi H. Fatigue crack growth characteristics of metal matrix composites[A]. In: Jono M, Inoue T, eds. Proc. of ICM-6[C]. London: Oxford Pergamon Press, 1991. 93- 100. |
[2] | Bowen P, Ibotson A R, Beevers C J. Fatigue crack growth in continuous fiber reinforced titanium alloy metal matrix compos ites[A]. In: Jono M, Inoue T, eds. Proc. of ICM 6 [C]. London: Oxford Pergamon Press, 1991. 107-112. |
[3] | Yang N H, Bowen P. Fatigue crack growth resistance of contin uous fiber reinforced composite Al6061/SiC [J]. Chinese Journal of Materials Research, 1998, 12(s): 66. |
[4] | Yang D M, Yin X F, Pan J. Continuous yarn fiber reinforced a luminum composites prepared by the ultrasonic liquid infiltration method [J]. J Mater Sci Letters, 1993, 30(1):252. |
[5] | Zhu Z M, Shi N L, Wang Z G, et al. Effect of surface treat ment of SiC fiber on the interface strength between SiC and Al matrix [J]. Acta Metallurgiea Sinica, 1996, 32(9): 1008. |
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%