DocumentCode :
1563809
Title :
Analysis and comparison of diode rectifier units suitable for aerospace applications
Author :
Clark, Therese ; Chivite-Zabalza, F.J. ; Forsyth, A.J. ; Barnes, M.
Author_Institution :
Univ. of Manchester, Manchester
fYear :
2008
Firstpage :
602
Lastpage :
606
Abstract :
The importance of power quality increases as more electric systems are introduced on aircraft. This paper compares the common mode and harmonic performance of four suitable multi-pulse diode rectifiers to give a better understanding of the performance tradeoffs of each system. This is achieved by simulating and assessing the effects of imbalance in the phase shifting transformers, voltage harmonics and negative sequence imbalance in the supply on CMV, line currents and Total Harmonic Current Distortion (THDI). This paper concludes that zero sequence harmonic distortion has the largest impact on the magnitude of CMV and a negligible effect on THDI. It is found that the DC link voltage is affected negligibly by harmonic distortion, negative sequence supply imbalance and inductive imbalance in the phase shifting transformers. Higher pulse number circuits tend to have a lower harmonic distortion and lower CMV providing the higher pulse number is not achieved by extending a lower pulse number converter using voltage injection techniques.
Keywords :
aircraft power systems; harmonic distortion; power convertors; power supply quality; power transformers; rectifiers; aerospace applications; aircraft; diode rectifier; multipulse diode rectifiers; phase shifting transformers; power quality; pulse number converter; total harmonic current distortion; voltage harmonics; voltage injection techniques; zero sequence harmonic distortion; Common-Mode Voltage; Multi-Pulse Circuits; Power Quality; Rectifiers;
fLanguage :
English
Publisher :
iet
Conference_Titel :
Power Electronics, Machines and Drives, 2008. PEMD 2008. 4th IET Conference on
Conference_Location :
York
ISSN :
0537-9989
Print_ISBN :
978-0-86341-900-3
Type :
conf
Filename :
4528909
Link To Document :
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