DocumentCode
230212
Title
Control of a three-sources-power-net for More Electric Aircraft application including a fuel-cell-APU
Author
Hasic, Edin ; Gerling, Dieter
Author_Institution
Dept. of Electr. Drives & Actuators, Univ. der Bundeswehr, Munich, Germany
fYear
2014
fDate
22-25 Oct. 2014
Firstpage
2785
Lastpage
2789
Abstract
In this paper a power net for More Electric Aircraft application with three power sources is presented. In extension to the Two-Generators-Concept where two synchronous generators are mounted on one turbine a fuel cell APU is connected in parallel to the 270 VDC power net. The aim is to control the power of the two generators and the fuel cell in order to obtain a stable voltage on the power net busbar.
Keywords
aircraft control; aircraft power systems; busbars; fuel cell vehicles; machine control; power control; synchronous generators; voltage control; fuel cell APU; more electric aircraft application; power net busbar; power sources; synchronous generators; three-sources-power-net control; two-generators-concept; voltage 270 V; voltage stability; Aircraft; Commutation; Fuel cells; Generators; Load modeling; Rectifiers; Transfer functions;
fLanguage
English
Publisher
ieee
Conference_Titel
Electrical Machines and Systems (ICEMS), 2014 17th International Conference on
Conference_Location
Hangzhou
Type
conf
DOI
10.1109/ICEMS.2014.7013972
Filename
7013972
Link To Document