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Structural health monitoring of CFRP airframe structures using fiber-optic-based strain mapping

机译:使用基于光纤的应变映射对CFRP机身结构进行结构健康监测

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This paper proposes structural health monitoring technology based on the strain mapping of composite airframestructures through their life cycles by FBG sensors. We carried out operational load tests of small-sized mockupspecimens of CFRP pressure bulkhead and measured the strain by FBG sensors. In addition, we confirmed strain changedue to stiffener debondings. Moreover, debonding detectability of FBG sensors were investigated through the strainmonitoring test of CFRP skin-stiffener panel specimens. As a result, the strain distribution varied with damageconfigurations. Moreover, the change in strain distribution measured by FBG sensors agrees well with numericalsimulation. These results demonstrate that FBG sensors can detect stiffener debondings with the dimension of 5mm incomposite airframe structures.© (2012) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
机译:本文提出了一种结构健康监测技术,该技术基于复合机体结构在整个生命周期中的应变映射,并使用FBG传感器进行了监测。我们对CFRP压力舱壁的小型样机进行了运行负载测试,并通过FBG传感器测量了应变。此外,我们确认了应变因加强筋剥离而改变。此外,通过CFRP皮肤加劲肋板样品的应变监测测试,研究了FBG传感器的脱胶检测能力。结果,应变分布随损伤构造而变化。此外,FBG传感器测得的应变分布变化与数值模拟非常吻合。这些结果表明FBG传感器可以检测到5mm的复合机体结构的加劲肋剥离。©(2012)COPYRIGHT光电仪器工程师协会(SPIE)。摘要的下载仅允许个人使用。

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