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A user interface damage detection technique based on a multiparameter methodology

机译:一种基于多游ameter方法的用户界面损伤检测技术

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Structural Health Monitoring (SHM) based on ultrasonic guided waves is able to assess the health of complex structures, improving maintenance strategies and overall performances of an aircraft. However, wave propagation analysis in composite structures is quite complex for effective damage identification. To alleviate such difficulties, various parametric information can be simultaneously extracted from propagating waves in view of a more effective detection of damage. A multi-parameter approach is indeed able to detect and localize impact induced damages with an increasing probability of detection. Experimental tests and numerical simulations have been used in combination to improve the methodology. The formers are oriented to optimize the single parameter methodology whose effectiveness and issues have been already investigated. The latter are mostly oriented to evaluate the effectiveness of a multi-parameter approach in view of an increasing probability of detection of the system. Finally, the management of large amount of data is optimized developing a graphic user interface aimed to easily post-process measurements and simulation data and quickly investigate several implemented techniques.
机译:基于超声波引导波的结构健康监测(SHM)能够评估复杂结构的健康,提高飞机的维护策略和整体性能。然而,复合结构中的波传播分析对于有效损害识别非常复杂。为了减轻这种困难,考虑到更有效地检测损坏,可以同时提取各种参数信息。多参数方法确实能够通过增加的检测概率来检测和定位影响造成的损坏。实验测试和数值模拟已组合使用以改善方法。成型器面向优化已经调查了其有效性和问题的单一参数方法。鉴于对系统的检测概率的增加,后者主要取向以评估多参数方法的有效性。最后,优化了大量数据的管理开发了旨在容易地后测量和仿真数据的图形用户界面,并快速调查几种实现的技术。

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