DocumentCode :
3009838
Title :
A Three-Phase Delta Switch Rectifier for More Electric Aircraft Applications Employing a Novel PWM Current Control Concept
Author :
Hartmann, M. ; Miniboeck, J. ; Kolar, J.W.
Author_Institution :
Power Electron. Syst. Lab., Swiss Fed. Inst. of Technol., Zurich
fYear :
2009
fDate :
15-19 Feb. 2009
Firstpage :
1633
Lastpage :
1640
Abstract :
In the course of the more electric aircraft program active three-phase rectifiers in the power range of 5 kW are required. A comparison with other rectifier topologies shows that the three-phase Delta-switch rectifier (comprising three Delta-connected bidirectional switches) is well suited for this application. The system is analyzed using space vector calculus and a novel PWM current controller concept is presented, where all three phases are controlled simultaneously; the analysis shows that the proposed concept yields optimized switching sequences. To facilitate the rectifier design, analytical relationships for calculating the power components average and rms current ratings are derived. Furthermore, a laboratory prototype with an output power of 5 kW is realized. Measurements taken from this prototype confirm the operation of the proposed current controller. Finally, initial EMI-measurements of the system are also presented.
Keywords :
PWM rectifiers; aircraft power systems; electric current control; EMI-measurements; PWM current control; aircraft power system; electric aircraft applications; power 5 kW; space vector calculus; switching sequences; three phase control; three-phase delta switch rectifier; Aerospace control; Aircraft; Control systems; Electric current control; Functional analysis; Prototypes; Pulse width modulation; Rectifiers; Switches; Topology;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Applied Power Electronics Conference and Exposition, 2009. APEC 2009. Twenty-Fourth Annual IEEE
Conference_Location :
Washington, DC
ISSN :
1048-2334
Print_ISBN :
978-1-4244-2811-3
Electronic_ISBN :
1048-2334
Type :
conf
DOI :
10.1109/APEC.2009.4802887
Filename :
4802887
Link To Document :
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