可替换电极触发真空开关及其在雷击电流分量A发电机中的应用

Sun Jinru, Y. Xueling, X. Wenjun, C. Jingliang
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引用次数: 0

摘要

雷电会对飞行器造成严重的破坏,雷电直接效应试验对航天器材料研究、飞行器结构设计具有重要意义,但测量技术和专用试验装置的限制已成为技术瓶颈。雷电直接效应试验的雷电电流分量由A分量(初跨)、B分量(中间电流)、C分量(持续电流)和D分量(重击)组成。雷电电流分量A和D可由RLC电路和撬棍电路两种类型产生。传统的RLC电路产生长时间脉冲电流波的效率相对较低。为了解决这一问题,本文设计研究了一种可更换电极触发真空开关,并在此基础上设计了一种产生雷电电流分量a的高效撬棍电路。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Replaceable electrodes triggered vacuum switch and its application in lightning current component A generator
Lightning can cause severe damage to aircraft, lightning direct effect test is very important for research of spacecraft material, design of structure of aircraft, but the limitation of the measuring technology and special test apparatus has become the technical bottleneck. Lightning current components for lightning direct effect test consist of component A (initial strode), component B (Intermediate current), component C (Continuing current) and component D (Restrike). Lightning current components A and D can be produced by the type of RLC circuit and crowbar circuit. The efficiency of the conventional RLC circuit in generating long duration time impulse current wave is relative low. To solve this problem, a replaceable electrodes triggered vacuum switch is designed and researched and then a high efficiency crowbar circuit which produces lightning current component A is designed in this paper.
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