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