SiC_f/Al复合丝变形损伤过程的原位观察  

IN SITU OBSERVATION ON FRACTURE PROCESS OF SiC_f/Al METAL MATRIX COMPOSITES

作　　者：杨盛良[1] 杨德明[1] 权高峰[2] 何家文[2] 

机构地区：[1]国防科技大学材料工程与应用化学系,长沙410073 [2]西安交通大学金属材料强度国家重点实验室,西安710049

出　　处：《复合材料学报》2002年第6期47-51,共5页Acta Materiae Compositae Sinica

基　　金：国家自然科学基金重点资助项目(59731020)

摘　　要：　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。The fracture process in the fatigue and tensile test of SiC fiber reinforced aluminum composites was observed in situ with a scanning electron microscope. It is found there exist three stages of damage. At the first stage the cracks caused by fiber fracturing initiate at the stress-concentrated sites, which increase as the load cycles increase. The second stage is characterized by multi-cracks in each fiber and the extension of cracks. The last stage indicates the coalescence of cracks and the formation of a main cracked plane. No fiber-matrix interface debonding was observed during the fracture process. The apparent interfacial bonding strength evaluated according to the shear lag model indicates a strong interfacial bonding for SiCf/Al metal matrix composites.

关 键 词：复合丝 变形损伤 SIC/AL复合材料 原位观察 界面强度 碳化硅 纤维增强铝基复合材料 

分 类 号：TB333[一般工业技术—材料科学与工程]