在类似机身的测试装置上处理由高浪涌电流测试产生的测试数据

R. Caldecott, O. Altay, S. Sebo, D. Schweickart, J. Horwath, L. Walko
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引用次数: 1

摘要

在一个高压和一个大电流的两个实验室中,各种金属试验圆柱体受到高达15 kA的电流脉冲,用于模拟飞机对高瞬态电流和电压的敏感性。在测试过程中记录浪涌电流和相应的dB/dt时间函数(B为磁通密度)。该项目涉及飞机在瞬态(即浪涌)电流(如雷击)情况下的电磁(EM)兼容性能。本文逐步回顾了浪涌电流和dB/dt测试数据的处理,并举例说明了所有步骤。对测试数据进行处理,使测试结果的电磁兼容性评估成为可能。测试结果的评估提供了飞机机身内部区域瞬态电磁场相关量的大小和波形信息,这些量会导致机载电子设备受到电磁干扰。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Processing test data generated by high surge current tests on a fuselage-like test setup
In two laboratories, one high voltage and the other one high current, various metal test cylinders were subjected to current pulses, up to 15 kA for the simulation of aircraft susceptibility to high transient currents and voltages. Surge current and corresponding dB/dt time functions were recorded during the tests (B is the magnetic flux density). The project is related to the electromagnetic (EM) compatibility performance of an aircraft in case of transient (i.e., surge) currents, such as lightning strokes. The paper reviews (step-by-step) the processing of surge current and dB/dt test data, and illustrates all steps with examples. Processing the test data makes the EM compatibility evaluation of the test results possible. Evaluation of the test results gives information on the magnitude and wave shape of transient EM field related quantities in the internal area of the fuselage of an aircraft that result in EM interference with on-board electronics.
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