基于主动深度学习的飞机结构腐蚀损伤检测

Yalew Mekonnen Fenta, G. Kamath
{"title":"基于主动深度学习的飞机结构腐蚀损伤检测","authors":"Yalew Mekonnen Fenta, G. Kamath","doi":"10.12783/shm2021/36295","DOIUrl":null,"url":null,"abstract":"Lamb wave-based damage detection has been demonstrated to be an efficacious method for structural health monitoring (SHM) in general, and corrosion in particular, and is thus deployed in this study. Since a large amount of data is needed for the deep learning networks, this study relies heavily on simulations as the data source and the waveforms are thus generated using simulations. The propagation of the Lamb waves is determined by finite element analysis which is carried out using ABAQUS. The signal features are extracted using continuous wavelet transform for amplitude change observation for presence and extent of the damage. One of the key aspects this paper focuses on is the application of the SHM methodology proposed here for realistic dimensions of corrosion pits. Thus, damage sizes are considered which fall in the range of pitting corrosion morphologies. Simulations are carried out with idealized corrosion pits of varying depths. Methods based on Artificial Neural Networks (ANN) and Convolutional Neural Networks (CNN) are used for the inverse problem solution to find the damage parameters and are compared with the numerical results. The results show much promise and could be a viable means of detecting corrosion in aircraft structures.","PeriodicalId":180083,"journal":{"name":"Proceedings of the 13th International Workshop on Structural Health Monitoring","volume":"39 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2022-03-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"ACTIVE DEEP LEARNING-BASED CORROSION DAMAGE DETECTION IN AIRCRAFT STRUCTURES\",\"authors\":\"Yalew Mekonnen Fenta, G. Kamath\",\"doi\":\"10.12783/shm2021/36295\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Lamb wave-based damage detection has been demonstrated to be an efficacious method for structural health monitoring (SHM) in general, and corrosion in particular, and is thus deployed in this study. Since a large amount of data is needed for the deep learning networks, this study relies heavily on simulations as the data source and the waveforms are thus generated using simulations. The propagation of the Lamb waves is determined by finite element analysis which is carried out using ABAQUS. The signal features are extracted using continuous wavelet transform for amplitude change observation for presence and extent of the damage. One of the key aspects this paper focuses on is the application of the SHM methodology proposed here for realistic dimensions of corrosion pits. Thus, damage sizes are considered which fall in the range of pitting corrosion morphologies. Simulations are carried out with idealized corrosion pits of varying depths. Methods based on Artificial Neural Networks (ANN) and Convolutional Neural Networks (CNN) are used for the inverse problem solution to find the damage parameters and are compared with the numerical results. The results show much promise and could be a viable means of detecting corrosion in aircraft structures.\",\"PeriodicalId\":180083,\"journal\":{\"name\":\"Proceedings of the 13th International Workshop on Structural Health Monitoring\",\"volume\":\"39 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2022-03-15\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of the 13th International Workshop on Structural Health Monitoring\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.12783/shm2021/36295\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of the 13th International Workshop on Structural Health Monitoring","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.12783/shm2021/36295","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

摘要

基于Lamb波的损伤检测已被证明是一种有效的结构健康监测(SHM)方法,特别是腐蚀,因此在本研究中得到了应用。由于深度学习网络需要大量的数据,因此本研究严重依赖于模拟作为数据源,因此波形是使用模拟生成的。利用ABAQUS进行有限元分析,确定了兰姆波的传播规律。利用连续小波变换提取信号特征,观察损伤的存在程度和幅度变化。本文重点关注的一个关键方面是本文提出的腐蚀坑实际尺寸的SHM方法的应用。因此,损伤尺寸被认为落在点蚀形态范围内。用不同深度的理想腐蚀坑进行了模拟。采用基于人工神经网络(ANN)和卷积神经网络(CNN)的反问题求解方法求出损伤参数,并与数值结果进行比较。结果显示了很大的希望,并可能是一种可行的方法来检测腐蚀的飞机结构。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
ACTIVE DEEP LEARNING-BASED CORROSION DAMAGE DETECTION IN AIRCRAFT STRUCTURES
Lamb wave-based damage detection has been demonstrated to be an efficacious method for structural health monitoring (SHM) in general, and corrosion in particular, and is thus deployed in this study. Since a large amount of data is needed for the deep learning networks, this study relies heavily on simulations as the data source and the waveforms are thus generated using simulations. The propagation of the Lamb waves is determined by finite element analysis which is carried out using ABAQUS. The signal features are extracted using continuous wavelet transform for amplitude change observation for presence and extent of the damage. One of the key aspects this paper focuses on is the application of the SHM methodology proposed here for realistic dimensions of corrosion pits. Thus, damage sizes are considered which fall in the range of pitting corrosion morphologies. Simulations are carried out with idealized corrosion pits of varying depths. Methods based on Artificial Neural Networks (ANN) and Convolutional Neural Networks (CNN) are used for the inverse problem solution to find the damage parameters and are compared with the numerical results. The results show much promise and could be a viable means of detecting corrosion in aircraft structures.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信