DocumentCode :
1264025
Title :
Protection Devices for Aircraft Electrical Power Distribution Systems: State of the Art
Author :
Izquierdo, D. ; Barrado, A. ; Raga, C. ; Sanz, M. ; Lázaro, A.
Author_Institution :
EADS, Univ. Carlos III de Madrid, Leganés, Spain
Volume :
47
Issue :
3
fYear :
2011
fDate :
7/1/2011 12:00:00 AM
Firstpage :
1538
Lastpage :
1550
Abstract :
The development of all electric aircraft (AEC) has provided new opportunities in the field of electronic devices and power electronics. One of the most interesting areas is focused on the protection devices field and the management of the loads by means of the solid state power controllers (SSPC). This is mainly due to the great increase of these devices in the electrical power distribution system architectures used in the new airplanes such as A380 and B787. This paper presents a survey of conventional and future trends of protection devices in onboard platforms. Moreover a virtual test bench is developed in order to analyze the potential problems that could appear by using SSPC in new onboard platforms. In addition an experimental validation with commercial SSPC and its model are presented.
Keywords :
aircraft power systems; electric control equipment; power distribution protection; power electronics; aircraft electrical power distribution systems; all electric aircraft; electronic devices; power electronics; protection devices; solid state power controllers; Aerospace electronics; Aircraft; Aircraft manufacture; Circuit faults; Power electronics; Solids; Wires;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.2011.5937248
Filename :
5937248
Link To Document :
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