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Fiber Bragg Gratings IT Techniques and Strain Gauge Validation for Strain Calculation on Aged Metal Specimens

机译:用于老化金属试样的应变计算的光纤布拉格光栅IT技术和应变计验证

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摘要

This paper studies the feasibility of calculating strains in aged F114 steel specimens with Fiber Bragg Grating (FBG) sensors and infrared thermography (IT) techniques. Two specimens have been conditioned under extreme temperature and relative humidity conditions making comparative tests of stress before and after aging using different adhesives. Moreover, a comparison has been made with IT techniques and conventional methods for calculating stresses in F114 steel. Implementation of Structural Health Monitoring techniques on real aircraft during their life cycle requires a study of the behaviour of FBG sensors and their wiring under real conditions, before using them for a long time. To simulate aging, specimens were stored in a climate chamber at 70 °C and 90% RH for 60 days. This study is framed within the Structural Health Monitoring (SHM) and Non Destructuve Evaluation (NDE) research lines, integrated into the avionics area maintained by the Aeronautical Technologies Centre (CTA) and the University of the Basque Country (UPV/EHU).
机译:本文研究了使用光纤布拉格光栅(FBG)传感器和红外热成像(IT)技术计算F114时效钢试样中应变的可行性。已经在极端温度和相对湿度条件下调节了两个样品,从而使用不同的粘合剂对老化前后的应力进行了对比测试。此外,已经对IT技术和用于计算F114钢中应力的常规方法进行了比较。在实际飞机的生命周期内实施结构健康监测技术需要对FBG传感器及其在真实条件下的接线的行为进行研究,然后再长期使用它们。为了模拟老化,将标本在70°C和90%RH的气候室内存放60天。这项研究是在结构健康监测(SHM)和非破坏性评估(NDE)研究领域内进行的,这些研究领域被整合到航空技术中心(CTA)和巴斯克地区大学(UPV / EHU)维护的航空电子领域。

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