DocumentCode :
3151545
Title :
Electrical generation and distribution for the more electric aircraft
Author :
Avery, C.R. ; Burrow, S.G. ; Mellor, P.H.
Author_Institution :
Univ. of Bristol, Bristol
fYear :
2007
fDate :
4-6 Sept. 2007
Firstpage :
1007
Lastpage :
1012
Abstract :
The aircraft industry is developing the more electric aircraft (MEA) with an ultimate goal of distributing only electrical power across the airframe. The replacement of existing systems with electric equivalents has, and will continue to, significantly increase the electrical power requirement. This has created a need for the enhancement of generation capacity and changes to distribution systems. The higher powers will push distribution voltages higher in order to limit conduction losses and reduce cable size, and hence weight. A power electronic interface may be required to regulate generator output into the distributed power form.
Keywords :
aircraft; electric vehicles; power distribution; MEA; distribution systems capacity; electric aircraft; electrical distribution; electrical generation; power electronic interface; Aerospace electronics; Aircraft propulsion; Control systems; Distributed power generation; Engines; Power distribution; Power electronics; Power generation; Synchronous generators; Turbines; Aircraft Distribution; Aircraft Generation; More Electric Aircraft;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Universities Power Engineering Conference, 2007. UPEC 2007. 42nd International
Conference_Location :
Brighton
Print_ISBN :
978-1-905593-36-1
Electronic_ISBN :
978-1-905593-34-7
Type :
conf
DOI :
10.1109/UPEC.2007.4469088
Filename :
4469088
Link To Document :
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