Research on Switching Technology of Aviation 270V DC System

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Abstract:

In this article, large capacitor charging and discharging experimental system is utilized to generate 270V DC-current by pre-charging to the large capacitor and discharging. Interrupter switching experiments of 540A, 1800A are done in aviation environment, and results of arcing breakdown manner are analyzed and explained. The experiment results indicate that 270V DC-current and arc in aviation environment can be broken by the way of using IGBT in appropriate time; In aviation environment, the breaking capability can be improved, and arcing breaking manner can be used to estimate the arc time constant by several experiments.

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442-445

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March 2015

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© 2015 Trans Tech Publications Ltd. All Rights Reserved

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[1] Chen-Weihua: Research on The Structure and Simulation Technique for Aircraft 270V HVDC Power Supply System(NUAA, 2010. DOI: 10. 7666/d. y1811091. ), pp.15-17.

Google Scholar

[2] Zheng-Zhanfeng, Zou-Jiyan, Dong-Enyuan: DC interrupter and DC circuit breaker (Dalian University of technology, Dalian 2014).

Google Scholar

[3] Mei-Jun, Zhang-Jianying, Hu-Minqiang: Structure and Analysis Of a Hybrid Current Limiting Circuit Breaker Based on IGBT Soft Switching (High Voltage Device, 2004).

Google Scholar

[4] Xu-Guoshun, Jiang-Zhuangxian, Zhuang-Jingwu: A New DC Vacuum Current Limitting Circuit Breaker and Its Dielectric Recovery Characteristics(Transactions of China Electrotechnical Society, 2013).

Google Scholar

[5] Zhou-Wandi, Wei-Xiaoguang, Gao-Chong: Thyristor Based Hybrid Arc-less High Voltage Direct Current Circuit Breaker (Proceedings of the CSEE, 2014).

Google Scholar

[6] Wang-Qiping: Electrical Arc Theory(China Machine Press, 1982), pp.223-224.

Google Scholar