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

超声F扫描检测碳/环氧复合材料层合板冲击损伤—电阻变化
引用本文:谢小林,廖嘉,范红青,王高潮,权红英,李志鹏.超声F扫描检测碳/环氧复合材料层合板冲击损伤—电阻变化[J].航空材料学报,2009,29(3):107-110.
作者姓名:谢小林  廖嘉  范红青  王高潮  权红英  李志鹏
作者单位:1. 武汉理工大学材料科学与工程学院,武汉,430070;南昌航空大学无损检测技术教育部重点实验室,南昌,330063
2. 南昌航空大学无损检测技术教育部重点实验室,南昌,330063
基金项目:教育部无损检测技术重点实验室开放基金 
摘    要:利用超声F扫描方法检测了经不同能量冲击后的碳/环氧复合材料层合板,并测量了复合材料冲击前后电阻.结合冲击能量、电阻变化、超声F扫描图像综合分析了冲击后碳/环氧复合材料的状况.结果表明,超声F扫描能够确定碳/环氧复合材料冲击损伤能量阈值;不同能量的冲击都会使碳/环氧复合材料的电阻发生变化,但只有大于能量阈值的冲击才会在复合材料中产生损伤;超声F扫描提高了基于电阻变化判断复合材料是否损伤的准确性.

关 键 词:碳/环氧复合材料  层合板  超声F扫描  冲击损伤-电阻变化

Detecting Impact Damage-Resistance Change in Carbon Fiber /Epoxy-Matrix Laminate by Ultrasonic F-scan
XIE Xiao-lin,LIAO Jia,FAN Hong-qing,WANG Gao-chao,QUAN Hong-ying,LI Zhi-peng.Detecting Impact Damage-Resistance Change in Carbon Fiber /Epoxy-Matrix Laminate by Ultrasonic F-scan[J].Journal of Aeronautical Materials,2009,29(3):107-110.
Authors:XIE Xiao-lin  LIAO Jia  FAN Hong-qing  WANG Gao-chao  QUAN Hong-ying  LI Zhi-peng
Abstract:Impacted carbon fiber /epoxy-matrix laminates were detected by ultrasonic F-scan,their resistance were measured before and after they had been impacted separately.The status of impacted laminates were analyzed through synthesizing impact energy,resistance change and ultrasonic F-scan graph.The results show that ultrasonic F-scan can ensure impact damage energy threshold value of carbon fiber /epoxy-matrix laminates.The resistance of laminates can be changed after they have been impacted,but there are damage...
Keywords:carbon fiber /epoxy-matrix composites  laminate  ultrasonic F-scan  impact damage-resistance change  
本文献已被 CNKI 维普 万方数据 等数据库收录!
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