Universal circuit breaker for aeronautic testing application

In this paper, a universal circuit breaker for aeronautic testing is proposed. The aim of the work is to discuss the design and simulations of a circuit breaker that can work with a low/high and AC/DC voltage source. Furthermore, the breaker can work in single or three phase mode synchronizing more devices. Thanks to the high performance DSP installed on board and the general purpose protection system algorithm, the device enables all protective devices used on aircraft to be emulated.

[1]  Detlef Schulz,et al.  Implementation of a Solid-State Power Controller for High-Voltage DC Grids in Aircraft , 2015 .

[2]  G. Rubino,et al.  Electrical Power Center with energy management capability for aeronautical applications , 2016, 2016 International Symposium on Power Electronics, Electrical Drives, Automation and Motion (SPEEDAM).

[3]  F. C. Lee,et al.  Modeling and stability analysis of a DC power system with solid state power controllers , 1996, Proceedings of Applied Power Electronics Conference. APEC '96.

[4]  W. Liu,et al.  A novel high current solid state power controller , 2005, 31st Annual Conference of IEEE Industrial Electronics Society, 2005. IECON 2005..

[5]  S. N. Friedman Solid-state power controllers for the next generation , 1992, Proceedings of the IEEE 1992 National Aerospace and Electronics Conference@m_NAECON 1992.

[6]  Douglas C. Hopkins,et al.  High current and thermal transient design of a SiC SSPC for aircraft application , 2011, 2011 Twenty-Sixth Annual IEEE Applied Power Electronics Conference and Exposition (APEC).

[7]  P. Zumel,et al.  Protection devices for aircraft electrical power distribution systems: a survey , 2008, 2008 34th Annual Conference of IEEE Industrial Electronics.

[8]  J. J. Simon State of the art in solid state power controller for aeronautical application , 2002 .