DocumentCode :
3576892
Title :
Power converter topologies for a high performance transformer rectifier unit in aircraft applications
Author :
Vieira, Jose Luiz F. ; Oliver, Jesus A. ; Alou, Pedro ; Cobos, Jose A.
Author_Institution :
Dept. de Eng. Eletr., Univ. Fed. do Espirito Santo - UFES, Vitoria, Brazil
fYear :
2014
Firstpage :
1
Lastpage :
8
Abstract :
This paper presents some power converter architectures and circuit topologies, which can be used to achieve the requirements of the high performance transformer rectifier unit in aircraft applications, mainly as: high power factor with low THD, high efficiency and high power density. The voltage and the power levels demanded for this application are: three-phase line-to-neutral input voltage of 115 or 115VAC rms (360-800Hz), output voltage of 28VDC or 270VDC (new grid value) and the output power up to tens of kilowatts.
Keywords :
aircraft power systems; avionics; harmonic distortion; power convertors; power factor; power transformers; rectifying circuits; aircraft applications; circuit topology; frequency 360 Hz to 800 Hz; high performance transformer rectifier unit; high power density; high power factor; low THD; power converter topology; three-phase line-to-neutral input voltage; voltage 115 V; voltage 270 V; voltage 28 V; Aerospace electronics; Aircraft; Bridge circuits; Density measurement; Power system measurements; Rectifiers; Topology;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Industry Applications (INDUSCON), 2014 11th IEEE/IAS International Conference on
Print_ISBN :
978-1-4799-5550-3
Type :
conf
DOI :
10.1109/INDUSCON.2014.7059403
Filename :
7059403
Link To Document :
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