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

机译:空气耦合超声,利用兰姆波和超声验证在CFRP中进行损伤检测

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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,需要先进的无损检测(NDT)技术来检测几乎看不见的冲击损伤(BVID)。传统的无损检测方法基于手动或自动,使用带有水或凝胶耦合剂的超声换能器进行扫描,对于较大的区域而言非常耗时。超声波兰姆波对于飞机的结构健康监测(SHM)十分重要,作者和其他人先前已经对此应用进行了研究。兰姆波受到板状飞机结构的引导,对于SHM应用,可以使用一系列永久固定的嵌入式或表面安装的压电换能器(PZT)来通过使用兰姆波来监视较大的表面积。本文介绍了空气耦合超声换能器(ACT)和使用超声验证(USV)的兰姆波感测的新颖组合。 USV是由阿姆斯特丹大学和阿姆斯特丹应用科学大学联合开发的一种监测CFRP结构健康的分析程序。为了扫描较大的结构,不希望使用固定的换能器以避免探头和耦合剂之间的接触而损坏表面。 ACT可以通过使用空气作为耦合剂来克服这些问题。 ACT技术的发展现在允许在换能器和结构之间进行更高的能量传递,从而使该技术更易于用于航空航天应用。这项研究的目的是确定用于CFRP中损坏检测的最佳换能器参数,并确定在应用USV程序时是否可以将ACT用作PZT的替代品。具有可变频率,换能器类型,换能器与材料之间的距离,波模式和入射角等变量的实验设计(DOE)确定了具有最高灵敏度以检测损坏的参数。通过比较保真度和脉冲能量方法的损坏测试表明,基于测量值之间的差异,未损坏和损坏信号之间的百分比差异以及可以检测到损坏的时间窗口,使用能量方法可以最好地检测到损坏。由于可以在CFRP中检测到损坏,因此可以将ACT用作USV中PZT的替代方案。

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