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Induced effects of lightning on a composite airframe Establishment of simplified coupling figures for various cable protection means

机译:闪电对各种电缆保护装置的简化耦合图的复合机架建立的诱导效应

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This paper deals with the protection of composite aircraft against the induced effects of lightning. The ins and outs of the protection architecture are depicted from a technical standpoint as well as from an industrial standpoint. A specific attention is paid to the determination of simplified coupling figures which objective is to cover the induction per linear meter of cable harness. Different figures are established for several cable installation principles: cables unprotected or shielded with various means like metallic sleeves, raceways or drain cables. The paper presents why and how such figures can be of interest for an aircraft manufacturer or an integrator of complex components. A method to obtain these figures from computational modelling is also presented with comparison to experimental data.
机译:本文涉及保护复合飞机对闪电诱导效果的保护。 保护架构的INS和OUTS从技术角度以及从工业立场中描绘。 特别注意的是确定简化的耦合图的确定,目的是覆盖每个线性仪表的诱导电缆线束。 建立不同的图为几个电缆安装原理:电缆不受保护或屏蔽各种手段,如金属套管,滚道或漏极电缆。 本文介绍了为什么对飞机制造商或复杂组件的集成商的感兴趣的原因以及这些数字。 与实验数据相比,还介绍了从计算建模中获得这些图的方法。

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