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航空用纤维增强聚合物基复合材料无损检测技术的应用与展望

何方成, 王铮, 史丽军, 刘颖韬, 杨党纲, 王晓

何方成, 王铮, 史丽军, 刘颖韬, 杨党纲, 王晓. 航空用纤维增强聚合物基复合材料无损检测技术的应用与展望[J]. 无损检测, 2018, 40(11): 29-32,41. DOI: 10.11973/wsjc201811008
引用本文: 何方成, 王铮, 史丽军, 刘颖韬, 杨党纲, 王晓. 航空用纤维增强聚合物基复合材料无损检测技术的应用与展望[J]. 无损检测, 2018, 40(11): 29-32,41. DOI: 10.11973/wsjc201811008
HE Fangcheng, WANG Zheng, SHI Lijun, LIU Yingtao, YANG Danggang, WANG Xiao. Application and Development of NDT for Fiber Reinforced Polymer Matrix Composites Used in Aviation[J]. Nondestructive Testing, 2018, 40(11): 29-32,41. DOI: 10.11973/wsjc201811008
Citation: HE Fangcheng, WANG Zheng, SHI Lijun, LIU Yingtao, YANG Danggang, WANG Xiao. Application and Development of NDT for Fiber Reinforced Polymer Matrix Composites Used in Aviation[J]. Nondestructive Testing, 2018, 40(11): 29-32,41. DOI: 10.11973/wsjc201811008

航空用纤维增强聚合物基复合材料无损检测技术的应用与展望

详细信息
    作者简介:

    何方成(1971-),男,研究员,主要从事金属材料和非金属材料的无损检测技术研究工作

    通讯作者:

    何方成, E-mail:fangcheng.he@biam.ac.cn

  • 中图分类号: TG115.28

Application and Development of NDT for Fiber Reinforced Polymer Matrix Composites Used in Aviation

  • 摘要: 近年来,国内航空用纤维增强聚合物基复合材料及制件的无损检测技术获得了较大提高,实现了多种制造工艺、多种复杂结构的可靠检测,同时,除超声、X射线等常规检测方法外,红外热像、激光散斑、空气耦合、超声相控阵等新技术也开始在复合材料检测中应用。今后,航空用复合材料无损检测技术还将结合现代电子信息、计算机等先进技术,向规范化、自动化和多元化方向发展。
    Abstract: The level of NDT technology for the composite used in aviation is recently raised evidently. The parts with sandwich, curvature, R-angle and cavity structure can all be inspected reliably. In addition to the conventional NDT methods of ultrasonic and X ray, the new NDT methods of infrared thermograph, laser speckle, air-coupled ultrasonic and ultrasonic phased array etc are all applicable for the composite. In the future, NDT technology for composites used in aviation must be combined with the advanced technology of electronic information, computer and so on, and developed in the normalized, automated and diversified way.
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    [2] 何方成,王铮,史丽军.不同超声检测技术对复合材料制件拐角部位的适用性[C]//第四届无损检测高等教育发展论坛暨电磁超声无损检测技术交流会.青岛:中国机械工程学会,2012.
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出版历程
  • 收稿日期:  2018-06-28
  • 刊出日期:  2018-11-09

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