基于卷积神经网络的CFRP/Ti复合结构钻削分层损伤程度识别研究
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1.沈阳航空航天大学机电工程学院,沈阳 110136;2.沈阳飞机工业(集团)有限公司,沈阳 110086]

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TH164

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辽宁省“兴辽英才计划”项目(XLYC2003025)


Research on the Identification of Drilling Layered Damage Degree of CFRP/Ti Composite Structures Based on Convolutional Neural Networks
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1.School of Mechatronics Engineering,Shenyang Aerospace University,Shenyang 110136;2.Shenyang Aircraft Corporation,Shenyang 110136

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    摘要:

    针对碳纤维增强树脂基复合材料(CFRP)试样与钛合金试样叠层装配钻孔时出现的CFRP分层缺陷质量问题,提出了一种基于卷积神经网络的CFRP分层损伤识别方法。通过工艺参数优化,选取对CFRP分层损伤程度影响小的工艺参数开展钻削实验。采集钻孔过程中的轴向力信号,将轴向力信号通过连续小波变换得到小波尺度图作为输入集,分层因子作为标签集,构建卷积神经网络模型。结果表明,轴向力信号与CFRP分层损伤程度具有正相关性,通过卷积神经网络模型监测制孔力信号来识别CFRP分层损伤程度是可行的。搭建VGGNet-16、LeNet和AlexNet三种网络结构模型,通过对比发现VGGNet-16模型识别效果较好,识别准确率可以达到91.84%。

    Abstract:

    To address the quality issue of CFRP delamination defects during the drilling process of laminated assemblies involving carbon fiber reinforced polymer (CFRP) specimens and titanium alloy specimens, a CFRP delamination damage identification method based on convolutional neural networks was proposed. Drilling tests were conducted using process parameters selected through an optimization experiment designed to minimize the impact on delamination. Axial force signals during the drilling process were collected, and continuous wavelet transform was applied to obtain wavelet scale maps as input sets, with delamination factors serving as label sets to construct a convolutional neural network model. The results indicate a positive correlation between axial force signals and CFRP delamination damage levels, demonstrating the feasibility of monitoring drilling force signals via the convolutional neural network model to identify CFRP delamination damage. Three network architectures VGGNet-16, LeNet, and AlexNet are implemented, and comparative analysis reveals that the VGGNet-16 model achieve the best recognition performance, with an accuracy rate reaching 91.84%.

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聂鹏,王巍森,于家鹤,潘五九.基于卷积神经网络的CFRP/Ti复合结构钻削分层损伤程度识别研究[J].宇航材料工艺,2025,55(6):83-91.

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  • 收稿日期:2023-10-08
  • 最后修改日期:2024-03-07
  • 录用日期:2024-03-08
  • 在线发布日期: 2025-12-29
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