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Automated fatigue crack detection for structural health monitoring of metallic aerospace structures

Automated fatigue crack detection for structural health monitoring of metallic aerospace structures
用于金属航空航天结构结构健康监测的自动疲劳裂纹检测
批准号:
1943540
负责人:
金额:
$0.0万
依托单位:
依托单位国家:
英国
项目类别:
Studentship
财政年份:
2017
资助国家:
英国
项目状态:
已结题
起止时间:
2017 至 --

项目摘要

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中文摘要
翻译
结构健康监测(SHM)提供了在整个使用寿命期间实时监测结构的能力,以确保其安全运行。这种技术有可能大大节省维护和维修成本,同时提高安全性。由于这个原因,目前航空航天、能源、运输和基础设施部门对SHM技术有着重大的技术拉动作用。声发射(AE)是一种被动SHM技术,能够通过检测结构损伤增长时释放的少量能量来实时监测大型结构。然而,与许多SHM技术一样,声发射技术需要操作员对数据进行解释,并且在复杂结构中不太可靠,这被视为工业实施的最大障碍。由于测量噪声、系统知识的缺乏、操作条件的可变性等导致的不确定性的存在,使这个问题变得更加具有挑战性。具备信号处理、多元统计、新颖性检测、不确定性分析等方面的技能。这项工作的目的是开发数据处理方法,允许自动检测铝吊架的疲劳裂纹。这将包括准确定位损伤、从断裂信号中分离无关噪声、新颖性检测和特征提取等技术。开发的技术将通过广泛的实验疲劳测试计划得到支持和验证,申请人将获得声发射监测和实验测试方面的专业知识。开发的技能也将广泛适用于监测一系列结构以外的最初的航空航天重点。支持文档。
英文摘要
Structural health monitoring (SHM) offers the ability to monitor structures, in real time, throughout their service lives to ensure they are safe for operation. Such technology has the potential to provide significant savings in maintenance and repair costs whilst increasing safety. For this reason there is currently a significant technology pull through for SHM techniques by the aerospace, energy, transport and infrastructure sectors. Acoustic emission (AE) is a passive SHM technique that is able to globally monitor large structures in real-time by detecting small amounts of energy that are released when damage grows in a structure. However, like many SHM techniques acoustic emission requires operator interpretation of data and can be less reliable in complex structures, which is seen as the greatest barrier to industrial implementation. This problem is made all the more challenging by the presence of uncertainty which results from measurement noise, lack of system knowledge, variability in operating conditions, etc. The applicant will develop excellent skills in signal processing, multi-variate statistics, novelty detection and uncertainty analysis. The aim of the work is to develop data processing methodologies that allow the automated detection of fatigue cracking in aluminium hangers. This will include techniques for accurate location of damage, the separation of extraneous noise from fracture signals, novelty detection and feature extraction. The developed techniques will be supported and validated by an extensive experimental fatigue testing programme, where the applicant will gain expertise in acoustic emission monitoring and experimental testing. The developed skills will also be widely applicable to the monitoring of a range of structures outside the initial aerospace focus. Supporting Documentation.
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DOI: 10.1016/j.ymssp.2020.106801
发表时间: 2020-08-01
期刊: MECHANICAL SYSTEMS AND SIGNAL PROCESSING
影响因子: 8.4
作者: [Purcell,Frederick A. F., Eaton,Mark, Pullin,Rhys]
通讯作者: Pullin,Rhys
海外基金