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Characterization of Hidden Corrosion In Multilayer Aircraft Structures Using Transient Eddy-Current NDE

机译:瞬态涡流NDE表征多层飞机结构中的隐藏腐蚀

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摘要

Previous research [1–4] has demonstrated that transient eddy-current (EC) techniques have significant advantages for the nondestructive evaluation (NDE) of hidden corrosion in multilayer aircraft structures when compared with conventional EC NDE. By sampling the time-domain response to a step or pulsed excitation using a high-speed digitiser, the probe response is effectively captured over a wide range of frequencies within a single measurement of only a few milliseconds duration, giving a very significant performance advantage over swept-frequency methods. In addition, direct measurement of the transient magnetic field (eg. using a Hall effect device), rather than the voltage induced in a pickup coil, allows transient EC NDE to probe more deeply into a multilayer structure compared to conventional EC techniques, giving improved sensitivity to deeply buried defects including hidden corrosion [1, 2, 5].
机译:先前的研究[1-4]已证明,与传统的EC NDE相比,瞬态涡流(EC)技术对于多层飞机结构中的隐藏腐蚀的无损评估(NDE)具有明显的优势。通过使用高速数字化仪对阶跃或脉冲激励的时域响应进行采样,可以在仅几毫秒持续时间的单次测量中在很宽的频率范围内有效捕获探头响应,与之相比,具有非常显着的性能优势扫频方法。另外,直接测量瞬态磁场(例如使用霍尔效应器件),而不是拾取线圈中感应的电压,使瞬态EC NDE与常规EC技术相比能够更深入地探查多层结构,从而提供了改进对深埋缺陷(包括隐藏腐蚀)的敏感性[1、2、5]。

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