首页 | 本学科首页   官方微博 | 高级检索  
     检索      

高性能玻璃纤维增强树脂基复合材料拉-压疲劳行为
引用本文:马丹,方允伟,王佳庆,王玉梅,徐琪.高性能玻璃纤维增强树脂基复合材料拉-压疲劳行为[J].宇航材料工艺,2018,48(4):63-66.
作者姓名:马丹  方允伟  王佳庆  王玉梅  徐琪
作者单位:中材科技股份有限公司南京玻璃纤维研究设计院
基金项目:江苏省创新能力建设计划(BM2015001)
摘    要:对LTX1240玻璃纤维/环氧复合材料开展拉-压疲劳试验,绘制S-N曲线进行疲劳寿命预测,利用扫描电镜观察疲劳试样断口形貌,分析其在拉-压循环载荷作用下的失效模式。结果表明:LTX1240玻璃纤维增强环氧树脂基复合材料的条件疲劳极限为278 MPa;失效过程为树脂基体最先破坏,接着界面分层乃至纤维拉伸、剪切破坏,它们相互作用形成了弥散损伤区并据此扩展发生材料断裂。

关 键 词:玻璃纤维  复合材料  拉-压疲劳  S-N曲线  失效分析
收稿时间:2017/9/12 0:00:00
修稿时间:2018/5/14 0:00:00

Tension-Compression Fatigue Behavior of High Performance Glass Fiber Reinforced Resin Matrix Composites
MA Dan,FANG Yunwei,WANG Jiaqing,WANG Yumei and XU Qi.Tension-Compression Fatigue Behavior of High Performance Glass Fiber Reinforced Resin Matrix Composites[J].Aerospace Materials & Technology,2018,48(4):63-66.
Authors:MA Dan  FANG Yunwei  WANG Jiaqing  WANG Yumei and XU Qi
Institution:Sinoma Science & Technology Co., Ltd., Nanjing Fiber Glass Research & Design Institute, Nanjing 210012,Sinoma Science & Technology Co., Ltd., Nanjing Fiber Glass Research & Design Institute, Nanjing 210012,Sinoma Science & Technology Co., Ltd., Nanjing Fiber Glass Research & Design Institute, Nanjing 210012,Sinoma Science & Technology Co., Ltd., Nanjing Fiber Glass Research & Design Institute, Nanjing 210012 and Sinoma Science & Technology Co., Ltd., Nanjing Fiber Glass Research & Design Institute, Nanjing 210012
Abstract:Tension-compression fatigue test of LTX 1240 fiber/epoxy composite was studied in this paper. The fatigue life was predicted by plotting S-N curve, fracture surface were observed in SEM, and the failure mode was analyzed. The results show that the conditional fatigue limit of the composite laminates is 278MPa. The failure process is the first resin matrix failure, and then generate interface stratification and even the tensile and shear failure of the fiber, then the interactings form the dispersion damage zone lead to the material fracture occurred.
Keywords:Fiber glass  Composites  Tension-compression  S-N curve  Failure analysis
本文献已被 CNKI 等数据库收录!
点击此处可从《宇航材料工艺》浏览原始摘要信息
点击此处可从《宇航材料工艺》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号