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Air-coupled ultrasound for damage detection in CFRP using Lamb waves and ultrasonic verification

机译:使用LAMB波和超声验证的CFRP中的空气耦合超声波检测

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Modern aircraft consist of Carbon Fiber Reinforced Polymer (CFRP) structures and require advanced nondestructive testing (NDT) techniques to detect barely visible impact damage (BVID). Conventional NDT methods, based on manual, or automated, scanning with ultrasonic transducers with water or gel couplant are time consuming for larger areas. Ultrasonic Lamb waves are of interest for structural health monitoring (SHM) of aircraft and have been investigated previously for this application by the authors and others. Lamb waves are guided by the plate-like aircraft structure and for SHM applications an array of permanently fixed embedded or surface-mounted piezoelectric transducers (PZTs) can be used to monitor large surface areas by using Lamb waves. This paper describes the novel combination of air-coupled ultrasound transducers (ACTs) and Lamb wave sensing using ultrasonic verification (USV). USV is an analysis procedure of monitoring the structural health of CFRP, developed jointly by the University of Amsterdam and the University of Applied Sciences, Amsterdam. For the scanning of larger structures, fixed transducers are not desirable to avoid damage to the surface by contact between the probe head and the couplant. ACTs can overcome these problems by using air as a couplant. Developments in ACT technology now allow much higher energy transfer between the transducer and the structure, making the technology more accessible for aerospace applications. The objectives of this research were to determine the optimum transducer parameters for damage detection in CFRP and to determine if ACTs can be used as alternative for PZTs when applying the USV procedure. A Design Of Experiments (DOE) with the variables frequency, type of transducer, distance between the transducer and the material, wave mode and angle of incidence determined the parameters with the highest sensitivity to detect damage. A damage test comparing the fidelity and pulse energy methods showed that damage can be detected best with the energy method based on the variances between the measurements, difference in percentage between undamaged and damaged signals and time windows in which damage can be detected. Because damage can be detected in CFRP, ACTs can be used as alternative for PZTs in USV.
机译:现代飞机由碳纤维增强聚合物(CFRP)结构组成,需要先进的非破坏性测试(NDT)技术来检测几乎可见的冲击损伤(BVID)。常规NDT方法基于手动或自动化,用带有水或凝胶耦合剂的超声换能器扫描较大区域的耗时。超声羔羊波对于飞机的结构健康监测(SHM)感兴趣,并且先前已经通过作者和其他人进行了调查。羊波由板状飞行器结构和SHM应用引导,永久固定的嵌入或表面安装的压电换能器(PZT)的阵列可用于通过使用羊光波监测大的表面区域。本文介绍了使用超声验证(USV)的空气耦合超声换能器(Acts)和羊振波感测的新颖组合。 USV是监测CFRP结构健康的分析程序,由阿姆斯特丹大学和应用科学大学,阿姆斯特丹共同发展。为了扫描较大的结构,不希望通过探头和耦合剂之间的接触避免损坏表面的固定换能器。通过使用空气作为耦合剂,可以克服这些问题。 ACT技术的发展现已允许换能器和结构之间的能量转移更高,使技术更容易获得航空航天应用。该研究的目标是确定CFRP中损伤检测的最佳换能器参数,并在应用USV过程时可以用作PZTS的替代物。实验(DOE)与变量频率,换能器的类型,换能器与材料之间的距离,波模式和入射角确定具有最高敏感性的参数,以检测损坏。比较验证和脉冲能量方法的损伤测试表明,基于测量之间的差异,能量方法可以最佳地检测到损坏,未损坏的信号和时间窗之间的百分比差异,可以检测到损坏。由于在CFRP中可以检测到损坏,因此可以用作USV中PZTS的替代品。

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