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Simulation Tools for a Fiber-Optic Based Structural Health Monitoring System

机译:基于光纤的结构健康监测系统的仿真工具

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摘要

Probability of detection(POD)graphics allow for a change from qualitative to quantitative assessment for every damage detection system,and as such it is a main request for conventional non-destructive testing(NDT) techniques.Its availability can greatly help towards the industrialization of the corresponding Structural health mo-nitoring(SHM)system.But having in mind that for SHM systems the sensors are at fixed positions,and the lo-cation of a potential damage would change its detectability.Consequently robust simulation tools are required to obtain the model assisted probability of detection(MAPOD)which is needed to validate the SHM system.This tool may also help for the optimization of the sensor distribution,and finally will allow a probabilistic risk manage-ment.INDEUS,simulation of ultrasonic waves SHM system,was a main milestone in this direction.This article deals with the simulation tools for a strain based SHM system,using fiber optic sensors(FOS).FOS are essen-tially strain/temperature sensors,either with multi-point or with distributed sensing.The simulation tool includes the finite element model(FEM)for the original and damaged structure,and algorithms to compare the strain data at the pre-established sensors locations,and from this comparison to extract information about damage occurrence and location. The study has been applied to the structure of an all-composite unmanned aircraft vehicle(UAV)now under construction,designed at Universidad Politecnica de Madrid for the inspection of electrical utilities networks.Dis-tributed sensing optical fibers were internally bonded at the fuselage and wing.Routine inspection is planned to be done with the aircraft at the test bench by imposing known loads.From the acquired strain data,damage occur-rence may be calculated as slight deviations from the baselines.This is a fast inspection procedure without requi-ring trained specialists,and it would allow for detection of hidden damages.Simulation indicates that stringer par-tial debondings are detected before they become critical,while small delaminations as those produced by barely vis-ible impact damages would require a prohibited number of sensing lines.These simulation tools may easily be ap-plied to any other complex structure,just by changing the FEM models.From these results it is shown how a fiber optic based SHM system may be used as a reliable damage detection procedure.
机译:检测概率(POD)图形允许改变对每个损坏检测系统的定量评估的变化,因此它是传统的非破坏性测试(NDT)技术的主要请求。可用性可以极大地帮助实现工业化相应的结构健康Mo-niriting(Shm)系统。请记住,对于SHM系统,传感器处于固定位置,并且潜在损坏的LO阳离子将改变其可检测性。需要进行稳健的仿真工具来获得用于验证SHM系统所需的检测的模型辅助概率(MAPOD)。该工具还可以帮助优化传感器分布,最后将允许概率风险管理.Indeus,超声波SHM系统的仿真,仿真。这方面是一个主要的里程碑。这篇文章处理基于SHM系统的模拟工具,使用光纤传感器(FOS).FOS是埃森 - 故障/温度传感器,具有多点或具有分布式感应的。模拟工具包括用于原始和损坏结构的有限元模型(FEM),以及将在预先建立的传感器位置进行比较的算法,以及从这比较的算法提取有关损坏发生和位置的信息。该研究已应用于现在正在建设的全综合无人驾驶飞机(UAV)的结构,该研究在MadiTecnica de Madrid中设计,用于检查电气公用事业网络。DIS-触发的光纤在机身内部粘合和计划通过施加已知的负载,计划在测试台上在试验台上进行检查。从获取的应变数据,可能会计算出与基线的略微偏差。这是一个快速检查程序,没有戒指训练有素的专家,它将允许检测隐藏的损伤。刺激指示在它们变得关键之前检测到斯特林格划分的剥离,而小分层是由几乎没有受到影响损害所产生的小分层需要禁止的传感线数。这些模拟工具可以很容易地将Applied与任何其他复杂的结构相比,只需改变有限元模型即可。通过这些结果显示出来W光纤基SHM系统可用作可靠的损坏检测过程。

著录项

  • 来源
    《南京航空航天大学学报(英文版)》 |2018年第2期|219-225|共7页
  • 作者单位

    Laboratory for Composites & Smart Structures,Department of Aeronautics,Polytechnic University of Madrid,Spain;

    Laboratory for Composites & Smart Structures,Department of Aeronautics,Polytechnic University of Madrid,Spain;

    Laboratory for Composites & Smart Structures,Department of Aeronautics,Polytechnic University of Madrid,Spain;

    Laboratory for Composites & Smart Structures,Department of Aeronautics,Polytechnic University of Madrid,Spain;

    Laboratory for Composites & Smart Structures,Department of Aeronautics,Polytechnic University of Madrid,Spain;

  • 收录信息 中国科学引文数据库(CSCD);中国科技论文与引文数据库(CSTPCD);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 无线电中继通信、微波通信;
  • 关键词

  • 入库时间 2022-08-18 02:01:03
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