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先进树脂基复合材料纤维褶皱缺陷阵列超声全聚焦成像

周正干 朱甜甜 马腾飞 李洋

周正干, 朱甜甜, 马腾飞, 等. 先进树脂基复合材料纤维褶皱缺陷阵列超声全聚焦成像[J]. 复合材料学报, 2022, 39(9): 4384-4392. doi: 10.13801/j.cnki.fhclxb.20220707.001
引用本文: 周正干, 朱甜甜, 马腾飞, 等. 先进树脂基复合材料纤维褶皱缺陷阵列超声全聚焦成像[J]. 复合材料学报, 2022, 39(9): 4384-4392. doi: 10.13801/j.cnki.fhclxb.20220707.001
ZHOU Zhenggan, ZHU Tiantian, MA Tengfei, et al. Array ultrasonic total-focus imaging for advanced resin matrix composite fiber wrinkle defect arrays[J]. Acta Materiae Compositae Sinica, 2022, 39(9): 4384-4392. doi: 10.13801/j.cnki.fhclxb.20220707.001
Citation: ZHOU Zhenggan, ZHU Tiantian, MA Tengfei, et al. Array ultrasonic total-focus imaging for advanced resin matrix composite fiber wrinkle defect arrays[J]. Acta Materiae Compositae Sinica, 2022, 39(9): 4384-4392. doi: 10.13801/j.cnki.fhclxb.20220707.001

先进树脂基复合材料纤维褶皱缺陷阵列超声全聚焦成像

doi: 10.13801/j.cnki.fhclxb.20220707.001
基金项目: 国家商用飞机制造工程技术研究中心创新基金(COMAC-SFGS-2021-666)
详细信息
    通讯作者:

    周正干,博士,教授,博士生导师,研究方向为超声无损检测 E-mail: zzhenggan@buaa.edu.cn

  • 中图分类号: V467;TB553

Array ultrasonic total-focus imaging for advanced resin matrix composite fiber wrinkle defect arrays

Funds: National Commercial Aircraft Manufacturing Engineering Technology Research Center Innovation Fund Project (COMAC-SFGS-2021-666)
  • 摘要: 先进树脂基复合材料因其密度低、强度高等特点,广泛应用于航空航天领域。纤维褶皱是先进树脂基复合材料制造过程中产生的一种缺陷,常规超声检测效率低,而阵列超声全聚焦成像检测技术则依赖准确的声传播延时。针对先进树脂基复合材料中的各向异性和多层折射界面而导致声波延时计算困难的问题,提出了一种使用Viterbi搜索算法的声线示踪方法,用于计算阵列超声全聚焦成像检测的时间延迟。对5.92 mm厚的多向碳纤维复合材料层压板进行阵列超声全聚焦成像检测实验,结果表明,使用声线示踪法计算延时,可以使采集的全矩阵信号被准确地相干叠加,有效检测出多向碳纤维复合材料层压板中的纤维褶皱缺陷。

     

  • 图  1  碳纤维增强树脂基复合材料(CFRP)多向板Viterbi声线示踪方法流程图

    Figure  1.  Flow chart of Viterbi ray tracing method for carbon fiber reinforced plastics (CFRP) multidirectional plate

    图  2  4层网格化模型声线示踪示意图

    Figure  2.  Schematic diagram of 4-layer gridded model for ray tracing method

    图  3  CFRP试样褶皱缺陷分布示意图

    Figure  3.  Schematic diagram of the distribution of wrinkle defects in CFRP specimen

    图  4  CFRP试样褶皱缺陷的金相图

    Figure  4.  Metallographic view of CFRP specimen with wrinkle defects

    图  5  在0°、±45°和90°单向铺层中qP波群速度随传播角度的变换

    Figure  5.  Variation of qP-wave group velocity with propagation angle for 0°, ±45° and 90° unidirectional CFRP plies

    图  6  第1个阵元发射不同阵元接收声线路径示意图

    Figure  6.  Schematic diagram of ray path for the 1st array transmit and the different array receive

    图  7  三种不同方法计算的qP波传播时间差曲线

    Figure  7.  qP wave propagation time difference curves calculated by three different methods

    BRM—Back-wall reflection method; tij—Time from the ith element transmitting sound wave to the jth element receiving sound wave

    图  8  褶皱1均质化全聚焦方法(TFM)和声线示踪TFM成像

    Figure  8.  Images of wrinkle 1 isotropic total focusing method (TFM) and ray tracing TFM

    图  9  褶皱2均质化TFM和声线示踪TFM成像

    Figure  9.  Images of wrinkle 2 isotropic TFM and ray tracing TFM

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出版历程
  • 收稿日期:  2022-06-13
  • 修回日期:  2022-06-23
  • 录用日期:  2022-07-03
  • 网络出版日期:  2022-07-08
  • 刊出日期:  2022-08-22

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