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Magnetostrictive Sensors for Composite Damage Detection and Wireless Structural Health Monitoring

机译:用于复合材料损伤检测和无线结构健康监测的磁致伸缩传感器

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摘要

The efficacy of magnetostrictive ribbon actuators as aerospace composites impact damage detectors has been investigated through finite-element modeling and experimental studies, investigating both the sensitivity of magnetostrictive ribbons embedded and surface mounted using the tensile and three-point bending tests. From the modeling, it was found that the surface-mounted ribbons increased Young's modulus of the system compared to the composite alone but caused the ribbons to delaminate from the surface before failure. The embedded ribbons did not appear to affect the structural properties of the composite, which was observed through the three-point bending tests carried out. From the impact damage tests, it was determined that the ribbons had to be embedded two-ply below the surface to measure impact energies greater than 1.6 J. For surface-mounted ribbons, damages of 1.6 J to the surface could be detected and pinpointed for two ribbons 10 mm apart. We also demonstrate in a simple way how a two-ribbon scheme may be used to determine the damage position in the tested sample, which may be extended for wireless sensing.
机译:通过有限元建模和实验研究,研究了磁致伸缩带驱动器作为航空航天复合材料冲击损伤检测器的功效,并通过拉伸和三点弯曲试验研究了嵌入和表面安装的磁致伸缩带的灵敏度。通过建模,发现与单独的复合材料相比,表面安装的碳带增加了系统的杨氏模量,但导致碳带在破坏前从表面脱层。通过执行的三点弯曲测试可以观察到,嵌入的条带似乎不会影响复合材料的结构性能。根据冲击损伤测试,确定必须将色带嵌入表面之下两层,以测量大于1.6 J的冲击能量。对于表面安装的色带,可以检测到1.6 J的表面损伤,并精确定位两根色带,相距10毫米。我们还以简单的方式演示了如何使用两个功能区的方案来确定测试样品中的损坏位置,该位置可以扩展为无线传感。

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