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SiC维纤增强钛基复合材料的疲劳裂纹扩展速率
引用本文:王海丽,杨延清,冯广海,罗 贤,张荣军,刘 斌.SiC维纤增强钛基复合材料的疲劳裂纹扩展速率[J].稀有金属材料与工程,2012,41(4):635-639.
作者姓名:王海丽  杨延清  冯广海  罗 贤  张荣军  刘 斌
作者单位:西北工业大学凝固技术国家重点实验室,陕西西安,710072
基金项目:国家自然科学基金(51071122);凝固技术国家重点实验室自主课题(KP200906);高等学校学科创新引智计划 (B08040)
摘    要:用箔-纤维-箔法制备SiC纤维增强Ti-6Al-4V复合材料,研究复合材料在加载频率f=10Hz、应力比R=0.1、最大应力σmax=300MPa条件下的疲劳裂纹扩展速率(da/dN),并采用扫描电子显微镜对疲劳破坏断口进行观察和分析。结果显示,在该加载条件下,复合材料第Ⅱ阶段疲劳裂纹扩展速率符合高斯函数。断口观察表明,复合材料的基体在裂纹稳态扩展区出现明显的疲劳条带,复合材料的疲劳损伤可以分为纤维断裂、基体开裂和纤维/基体界面脱粘等多种形式。

关 键 词:钛基复合材料  SiC纤维  疲劳裂纹  扩展速率
收稿时间:4/8/2011 12:00:00 AM

Fatigue Crack Growth Rate in SiC Fiber Reinforced Titanium Matrix Composites
Wang Haili,Yang Yanqing,Feng Guangh,Luo Xian,Zhang Rongjun and Liu Bin.Fatigue Crack Growth Rate in SiC Fiber Reinforced Titanium Matrix Composites[J].Rare Metal Materials and Engineering,2012,41(4):635-639.
Authors:Wang Haili  Yang Yanqing  Feng Guangh  Luo Xian  Zhang Rongjun and Liu Bin
Affiliation:(State Key Laboratory of Solidification Processing,Northwestern Polytechnical University,Xi’an 710072,China)
Abstract:SiC fiber reinforced Ti-6Al-4V composites(TMCs) was prepared by the foil-fiber-foil method.The fatigue crack growth rate of the TMCs was investigated under the condition of f=10 Hz,R=0.1 and σmax =300 MPa,and the fracture surface of TMCs was observed by scanning electron microscopy(SEM).Results show that the crack growth rate at the stage Ⅱ of crack propagation is well consistent with Gaussian function.SEM observation indicates that distinct fatigue striations exist in the stable propagation area of the fatigue crack of the Ti-6Al-4V matrix.The failure modes of TMCs include fiber breakage,matrix cracking,fiber/matrix interfacial debonding,et al under the loading condition.
Keywords:titanium matrix composite  SiC fiber  fatigue crack  propagation rate
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