• 中国科技论文统计源期刊
  • 中文核心期刊
  • 中国科技核心期刊
  • 中国机械工程学会无损检测分会会刊
高级检索

碳纤维复合材料板冲击损伤计算及超声检测

邬冠华, 王丹, 贺小玉, 杨小林

邬冠华, 王丹, 贺小玉, 杨小林. 碳纤维复合材料板冲击损伤计算及超声检测[J]. 无损检测, 2011, 33(11): 42-45.
引用本文: 邬冠华, 王丹, 贺小玉, 杨小林. 碳纤维复合材料板冲击损伤计算及超声检测[J]. 无损检测, 2011, 33(11): 42-45.
WU Guan-Hua, WANG Dan, HE Xiao-Yu, YANG Xiao-Lin. The Calculation and Detection of Impact Damage in Carbon Fiber Reinforced Composites[J]. Nondestructive Testing, 2011, 33(11): 42-45.
Citation: WU Guan-Hua, WANG Dan, HE Xiao-Yu, YANG Xiao-Lin. The Calculation and Detection of Impact Damage in Carbon Fiber Reinforced Composites[J]. Nondestructive Testing, 2011, 33(11): 42-45.

碳纤维复合材料板冲击损伤计算及超声检测

基金项目: 

无损检测技术教育部重点实验室开放基金资助项目(ZB201029008)

详细信息
    作者简介:

    邬冠华(1963-),男,教授,南昌航空航天大学国防研究院常务副院长,从事无损检测技术教育和科研工作。

  • 中图分类号: TG115.28

The Calculation and Detection of Impact Damage in Carbon Fiber Reinforced Composites

  • 摘要: 文章采用显式有限元法、三维Tsai-Wu失效准则和刚度折算准则来模拟T300/QY8911矩形层压板低速冲击下逐渐损伤的过程,预测了复合材料冲击损伤的程度。根据HB 72242—1995《复合材料构件通用技术条件》、GJB 28952—1997《碳纤维复合材料层合板和层合件通用规范》要求制作冲击试样,进行低能量冲击试验。采用超声C扫描检测不同能量冲击作用造成的损伤,将有限元计算结果和超声C扫描检测结果进行对比。结果表明,在损伤面积尺寸确定方面,有限元分析的结果和超声C扫描检测结果吻合较好,三维Tsai-Wu失效准则和刚度折算准则适合模拟分析碳纤维复合材料板冲击损伤,超声C扫描检测可以较好地检测出冲击能量高于4.5 J的分层损伤。
    Abstract: In the paper, explicit finite element method, three-dimensional Tsai-Wu failure criterion and material stiffness criteria for conversion were used to simulate the impact damage process of the rectangular laminates T300/QY8911, and to predict the extend of impact damage. According to the standards of ‘the general technical specifications of HB 72242—1995 composite structures’ and ‘the general specification of GJB 28952—1997 carbon fiber composite laminates’, the impact specimens were designed, and low-energy impact experiments were carried out. The ultrasonic C scan was used to detect the damages of different impact energy, and compared with the results of finite element method. It showed that the results of finite element simulation were consistent with those of the ultrasonic C scan test on the size of damage areas. Three-dimensional Tsai-Wu failure criterion for damage and material stiffness criteria for conversion were also proved by the experiment results, When the energy reached more than 4.5 J, the delamination of impact damage could be detected by the ultrasonic C scan testing.
  • [1] 崔海坡,温卫东,崔海涛.复合材料层合板冲击损伤及剩余强度研究进展[J].材料科学与工程学报,2005,23(3):466-472.
    [2] Greszczuk L B. Damage in composite materials due to low velocity impact[J]. Impact Dynamics,1982:55-94.
    [3] 杨小林,江涛,冯立春.飞机复合材料结构冲击损伤的红外检测[J].无损检测,2009,31(2):121-123.
    [4] 郑立胜.基于红外成像检测的飞机复合材料冲击试验研究[J].玻璃钢/复合材料,2009(1):19-21.
    [5] 何涛,杨竞.ANSYS10/LS-DYNA非线性有限元分析实例指导教程[M].北京:机械工业出版社,2007.
    [6] Finn Scott R, Springer George S. Delaminations in composite plates under transverse static or impact loads[J]. A model Composite structure,1993,23(3):177-190.
    [7] 陈小金,高宇建.含穿透损伤复合材料桨叶结构静强度分析[J].失效分析与预防,2011,6(1):23-27.
计量
  • 文章访问数:  1
  • HTML全文浏览量:  0
  • PDF下载量:  3
  • 被引次数: 0
出版历程
  • 收稿日期:  2011-05-29
  • 刊出日期:  2011-11-09

目录

    /

    返回文章
    返回