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Generation of controlled delaminations in composites using symmetrical laser shock configuration

机译:使用对称激光冲击配置在复合材料中生成受控分层

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摘要

Structural Health Monitoring (SHM) is defined as the process of implementing a damage identification strategy for aerospace, civil and mechanical engineering infrastructures. SHM can be organized into five main steps: detection, localization, classification, quantification and prognosis. Our work considers SHM quantification level and in particular the evaluation of the severity of delamination-type damage in CFRP composite laminates. Prior to quantification algorithms implementation, it is important to properly prepare the supports on which algorithms will be tested. Teflon inserts and conventional impacts are commonly used techniques to generate or simulate delaminations. However, with such rudimentary techniques it is difficult to generate controlled delamination-type damage in a realistic way. In the present work, we investigate symmetrical laser shock approach, as a new method to calibrate delaminations in composites. By tuning the time delay between the two laser beams and laser energy, through thickness damage position and severity can respectively be adjusted. The effect of multiple contiguous laser impacts was also investigated. Post-mortem analyses using A-scan and C-scan testing as well as penetrant testing were performed in order to characterize laser impact induced damage. Results are encouraging and demonstrate the high potential of symmetrical laser shock for damage calibration in both size and location. (C) 2017 Elsevier Ltd. All rights reserved.
机译:结构健康监测(SHM)被定义为对航空航天,土木和机械工程基础设施实施损害识别策略的过程。 SHM可以分为五个主要步骤:检测,定位,分类,量化和预后。我们的工作考虑了SHM的量化水平,尤其是CFRP复合材料层压板中分层型损坏严重程度的评估。在实施量化算法之前,重要的是正确准备要在其上测试算法的支持物。铁氟龙插件和常规冲击是生成或模拟分层的常用技术。然而,利用这种基本技术,很难以现实的方式产生受控的分层型损坏。在当前的工作中,我们研究对称的激光冲击方法,作为一种校准复合材料分层的新方法。通过调节两个激光束之间的时间延迟和激光能量,可以分别调节厚度损伤的位置和严重性。还研究了多个连续激光冲击的影响。使用A扫描和C扫描测试以及渗透测试进行了事后分析,以表征激光冲击引起的损坏。结果令人鼓舞,并证明了对称激光冲击在尺寸和位置上进行损伤校准的巨大潜力。 (C)2017 Elsevier Ltd.保留所有权利。

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