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Application of active structural health monitoring technique to aircraft fuselage structures

机译:主动结构健康监测技术在飞机机身结构中的应用

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Abstract: Damage identification of complex structures can beperformed using an Active Structural Health MonitoringSystem (ASHMS) utilizing an array of piezoceramic (PZT)sensor- actuators and an electromechanical impedanceanalyzer. Based on the theory of electromechanicalimpedance for surface-bonded collocatedsensor-actuators, the system provides the means ofimplementing effective Non-Destructive-Evaluationhealth monitoring to a structure at any point in itslife cycle. When integrated into a structure, the ASHMScan identify the location and extent of damage througha statistical analysis algorithm which compares theelectromechanical admittance of the structure's currentcondition with the structure's `baseline' conditionover a defined frequency range. This paper presents amodel independent method of structure damageidentification based on statistical analysis of thechanges in the electromechanical impedance of thestructural response. Using a small section of anairplane fuselage with free-free boundary conditions asthe test structure, a prototype system has beensuccessfully developed which automatically measures andcollects the electromechanical admittance data from anarray of transducers. The measurement system developedcan apply large voltages to the PZT transducers, whileaccurately determining the spectral and harmonicinformation of the frequency range of interestresulting in an increase in the measurement sensitivityand the area monitored by a single transducer. Thesystem can accurately measure and collect large amountsof structural information with a limited number oftransducers in a very short period of time. Thepost-analysis of the measured structural variation canbe performed with the advanced signal processingalgorithm presented herein within seconds of datacollection. The results show a remarkable accuracy ofdamage location identification for a complex structure.The basic research conducted so far indicates that theASHMS and associated processing techniques have apromising potential for health monitoring of realcomplex structures.!5
机译:摘要:可以使用主动结构健康监测系统(ASHMS),利用压电陶瓷(PZT)传感器-执行器阵列和机电阻抗分析仪,对复杂结构进行损伤识别。基于表面结合的并置传感器-执行器的机电阻抗理论,该系统提供了对结构生命周期中任何时刻进行有效无损评估健康监控的方法。当集成到结构中时,ASHMScan通过统计分析算法确定损坏的位置和程度,该算法将结构的当前条件的机电导纳与结构在指定频率范围内的“基线”条件进行比较。本文基于对结构响应的机电阻抗变化的统计分析,提出了一种独立于模型的结构损伤识别方法。通过使用一小部分具有自由边界条件的飞机机身作为测试结构,成功开发了一个原型系统,该系统可以自动测量并收集来自一系列换能器的机电导纳数据。开发的测量系统可以向PZT传感器施加较大的电压,同时准确确定感兴趣频率范围的频谱和谐波信息,从而提高测量灵敏度和单个传感器监视的面积。该系统可以在很短的时间内用数量有限的传感器准确地测量和收集大量的结构信息。可以在数据收集的几秒钟内使用本文介绍的高级信号处理算法对测量的结构变化进行后分析。结果表明,复杂结构的损伤位置识别具有非凡的准确性。到目前为止进行的基础研究表明,ASHMS和相关的处理技术对于真实的复杂结构的健康状况监测具有广阔的前景。5

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