Machine learning algorithms for delaminations detection on composites panels by wave propagation signals analysis: Review, experiences and results

IF 11.5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Progress in Aerospace Sciences Pub Date : 2024-03-14 DOI:10.1016/j.paerosci.2024.100994
E. Monaco , M. Rautela , S. Gopalakrishnan , F. Ricci
{"title":"Machine learning algorithms for delaminations detection on composites panels by wave propagation signals analysis: Review, experiences and results","authors":"E. Monaco ,&nbsp;M. Rautela ,&nbsp;S. Gopalakrishnan ,&nbsp;F. Ricci","doi":"10.1016/j.paerosci.2024.100994","DOIUrl":null,"url":null,"abstract":"<div><p>Performances are a key concern in aerospace vehicles, requiring safer structures with as little consumption as possible. Composite materials replaced aluminum alloys even in primary aerospace structures to achieve higher performances with lighter components. However, random events such as low-velocity impacts may induce damages that are typically more dangerous and mostly not visible than metals. The damage tolerance (DT) approach is adopted for the fatigue design of aircraft, but fracture mechanisms and propagation of failure prediction in composite structures are much more challenging. Consequently, the DT approach is still costly for these types of structures. It can be achieved only through expensive experimental testing and a drastic reduction of allowable stress levels and maintenance intervals by applying scattering factors due to the uncertainties involved in their original estimations. Structural health monitoring (SHM) systems deal mainly with sensorised structures providing signals related to their “load and health status” to reduce maintenance and weights. At the same time, the use of Deep Neural Networks (DNNs) based on strategic engineering criteria, for instance, may represent an effective and efficient analysis tool to promote faster data analysis and classification. In the field of aircraft maintenance, this approach may lead, for example, to a faster awareness of an aircraft/fleet situation or predict failures. Deep learning-based networks provide automatic feature extraction at different levels of abstraction. With the universal function approximation property of neural networks, it learns the inverse mapping from input space (signals) to target space (damage classes). Starting from the well-established Structural Health Monitoring (SHM) technologies, a network of distributed sensors embedded throughout the structure could be used for real-time structural monitoring and data acquisition. Structural data will constitute an enormous amount of information that can be adequately filtered with the help of specific DNNs designed and trained for the structural context and aimed to classify and identify significant parameters. The authors have collaborated for some years to collect wave propagation signals through experimental tests and validated numerical models of healthy and damaged composite structures, and developed machine learning algorithms (mainly dense and convolutional neural networks) aimed at signal classification and analysis for damage detection and localization. This paper presents a brief review of relevant works about SHM employing Machine Learning methodologies and summarizes the most promising approaches developed during the last years jointly by the two research groups and presents a critical analysis of obtained results and subsequent future activities.</p></div>","PeriodicalId":54553,"journal":{"name":"Progress in Aerospace Sciences","volume":"146 ","pages":"Article 100994"},"PeriodicalIF":11.5000,"publicationDate":"2024-03-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S0376042124000204/pdfft?md5=fb3c7515ab53e24a29f5985bd22f0ae3&pid=1-s2.0-S0376042124000204-main.pdf","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Progress in Aerospace Sciences","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0376042124000204","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

Abstract

Performances are a key concern in aerospace vehicles, requiring safer structures with as little consumption as possible. Composite materials replaced aluminum alloys even in primary aerospace structures to achieve higher performances with lighter components. However, random events such as low-velocity impacts may induce damages that are typically more dangerous and mostly not visible than metals. The damage tolerance (DT) approach is adopted for the fatigue design of aircraft, but fracture mechanisms and propagation of failure prediction in composite structures are much more challenging. Consequently, the DT approach is still costly for these types of structures. It can be achieved only through expensive experimental testing and a drastic reduction of allowable stress levels and maintenance intervals by applying scattering factors due to the uncertainties involved in their original estimations. Structural health monitoring (SHM) systems deal mainly with sensorised structures providing signals related to their “load and health status” to reduce maintenance and weights. At the same time, the use of Deep Neural Networks (DNNs) based on strategic engineering criteria, for instance, may represent an effective and efficient analysis tool to promote faster data analysis and classification. In the field of aircraft maintenance, this approach may lead, for example, to a faster awareness of an aircraft/fleet situation or predict failures. Deep learning-based networks provide automatic feature extraction at different levels of abstraction. With the universal function approximation property of neural networks, it learns the inverse mapping from input space (signals) to target space (damage classes). Starting from the well-established Structural Health Monitoring (SHM) technologies, a network of distributed sensors embedded throughout the structure could be used for real-time structural monitoring and data acquisition. Structural data will constitute an enormous amount of information that can be adequately filtered with the help of specific DNNs designed and trained for the structural context and aimed to classify and identify significant parameters. The authors have collaborated for some years to collect wave propagation signals through experimental tests and validated numerical models of healthy and damaged composite structures, and developed machine learning algorithms (mainly dense and convolutional neural networks) aimed at signal classification and analysis for damage detection and localization. This paper presents a brief review of relevant works about SHM employing Machine Learning methodologies and summarizes the most promising approaches developed during the last years jointly by the two research groups and presents a critical analysis of obtained results and subsequent future activities.

查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
通过波传播信号分析复合材料面板分层检测的机器学习算法:回顾、经验和结果
性能是航空航天飞行器的主要关注点,要求结构更安全,消耗尽可能少。复合材料甚至取代了初级航空航天结构中的铝合金,以更轻的组件实现更高的性能。然而,随机事件(如低速撞击)可能会导致损伤,这种损伤通常比金属更危险,而且大多不可见。飞机的疲劳设计采用损伤容限(DT)方法,但复合材料结构的断裂机制和失效传播预测更具挑战性。因此,对于这些类型的结构来说,DT 方法仍然成本高昂。只有通过昂贵的实验测试,并通过应用散射系数(由于其原始估算的不确定性)来大幅降低容许应力水平和维护间隔,才能实现这一目标。结构健康监测(SHM)系统主要处理传感器化结构,提供与其 "负载和健康状态 "相关的信号,以减少维护和重量。与此同时,基于战略工程标准的深度神经网络(DNN)的使用可能是一种有效和高效的分析工具,以促进更快的数据分析和分类。例如,在飞机维护领域,这种方法可以更快地了解飞机/机队情况或预测故障。基于深度学习的网络可在不同的抽象层次自动提取特征。利用神经网络的通用函数逼近特性,它可以学习从输入空间(信号)到目标空间(损坏类别)的反映射。从成熟的结构健康监测(SHM)技术出发,嵌入整个结构的分布式传感器网络可用于实时结构监测和数据采集。结构数据将构成海量信息,可借助针对结构环境设计和训练的特定 DNN 进行充分过滤,并对重要参数进行分类和识别。多年来,作者们通过实验测试和验证健康和受损复合结构的数值模型,合作收集波传播信号,并开发了机器学习算法(主要是密集神经网络和卷积神经网络),旨在对信号进行分类和分析,以进行损伤检测和定位。本文简要回顾了采用机器学习方法进行 SHM 的相关工作,总结了两个研究小组在过去几年中联合开发的最有前途的方法,并对取得的成果和未来的活动进行了批判性分析。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
Progress in Aerospace Sciences
Progress in Aerospace Sciences 工程技术-工程:宇航
CiteScore
20.20
自引率
3.10%
发文量
41
审稿时长
5 months
期刊介绍: "Progress in Aerospace Sciences" is a prestigious international review journal focusing on research in aerospace sciences and its applications in research organizations, industry, and universities. The journal aims to appeal to a wide range of readers and provide valuable information. The primary content of the journal consists of specially commissioned review articles. These articles serve to collate the latest advancements in the expansive field of aerospace sciences. Unlike other journals, there are no restrictions on the length of papers. Authors are encouraged to furnish specialist readers with a clear and concise summary of recent work, while also providing enough detail for general aerospace readers to stay updated on developments in fields beyond their own expertise.
期刊最新文献
Retro-propulsion in rocket systems: Recent advancements and challenges for the prediction of aerodynamic characteristics and thermal loads A definition, conceptual framework, and pathway towards sustainable aviation Robotic manipulators for in-orbit servicing and active debris removal: Review and comparison Editorial Board Compressible vortex loops and their interactions
×
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
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 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 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1