DocumentCode :
3302918
Title :
A high power density three phase AC-DC converter for more electric aircraft (MEA)
Author :
Singh, Amit K. ; Das, Pritam ; Panda, S.K.
Author_Institution :
Electr. & Comput. Eng., Nat. Univ. of Singapore, Singapore, Singapore
fYear :
2015
fDate :
1-5 June 2015
Firstpage :
1362
Lastpage :
1367
Abstract :
This paper presents matrix topology (3×1) based isolated three phase AC-DC converter suitable for aircraft systems. A novel modulation scheme based on Space Vector Modulation (SVM) is proposed to convert three phase line frequency AC into high frequency AC. The direct conversion of three phase line frequency AC into single phase high frequency AC removes the mandatory DC link capacitor which improves the power density and reliability of the system. Moreover, a variable frequency control is proposed for regulating the output voltage for different loading condition. The switching scheme for the converter is explained in detail and subsequently, the steady state analysis of converter is presented. An example converter of input 120 Vrms (3-phase), 400 Hz to output 28 V DC with an output power of 3.3 kW is designed. Comprehensive simulation is carried out using MATLAB Simulink and PSIM based software platform and results are discussed.
Keywords :
AC-DC power convertors; aircraft power systems; frequency control; voltage control; MEA; SVM; aircraft system; frequency 400 Hz; high power density converter; more electric aircraft; output voltage regulation; power 3.3 kW; single phase high frequency AC; space vector modulation; three phase AC-DC converter; variable frequency control; voltage 120 V; voltage 28 V; Aerospace electronics; Aircraft; Capacitors; Frequency conversion; Frequency modulation; Matrix converters; Switches;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Power Electronics and ECCE Asia (ICPE-ECCE Asia), 2015 9th International Conference on
Conference_Location :
Seoul
Type :
conf
DOI :
10.1109/ICPE.2015.7167956
Filename :
7167956
Link To Document :
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