DocumentCode
3520112
Title
Full-bridge phase-shifted converter design for aircraft rectifier unit
Author
Luft, Sergey V. ; Khristolyubov, Aleksey A.
Author_Institution
Novosibirsk State Tech. Univ., Novosibirsk, Russia
fYear
2015
fDate
June 29 2015-July 3 2015
Firstpage
442
Lastpage
445
Abstract
Basic requirements for the aircraft converters besides the quality of electrical power conversion are minimizing the weight of the device and reducing the volume occupied by them. In particular, soft-switching topology are used to solve these problems. The method of soft-switching DC-DC converter design for controlled rectifier unit for aircraft is described in this paper. The design of 2 kW converter and the results of modeling in software PSIM are presented as an example.
Keywords
DC-DC power convertors; aircraft power systems; rectifiers; zero current switching; zero voltage switching; aircraft converters; aircraft rectifier unit; electrical power conversion; full-bridge phase-shifted converter design; power 2 kW; soft-switching DC-DC converter design; soft-switching topology; Aircraft; DC-DC power converters; Inductors; Magnetic resonance; Rectifiers; Soft switching; Switching frequency; aircraft; design procedure; soft-switching;
fLanguage
English
Publisher
ieee
Conference_Titel
Micro/Nanotechnologies and Electron Devices (EDM), 2015 16th International Conference of Young Specialists on
Conference_Location
Erlagol
ISSN
2325-4173
Print_ISBN
978-1-4673-6718-9
Type
conf
DOI
10.1109/EDM.2015.7184580
Filename
7184580
Link To Document