DocumentCode :
1088963
Title :
Higher voltage aircraft power systems
Author :
Cotton, I. ; Nelms, A.
Author_Institution :
Univ. of Manchester, Manchester
Volume :
23
Issue :
2
fYear :
2008
Firstpage :
25
Lastpage :
32
Abstract :
Modern aircraft designs are focused on minimising the use of engine bleed air, eliminating gearboxes, and reducing the reliance on hydraulic systems. Instead, many of these mechanical systems will be replaced with electrical versions. The increasing amounts of electrical power that will be shipped through an aircraft means that it is increasingly difficult to rely on low voltage power systems owing to voltage drop and weight constraints. This discusses the challenges that relate to the safe use of higher voltage systems within aircraft.
Keywords :
aircraft power systems; high-voltage techniques; higher voltage aircraft power systems; low voltage power systems; voltage drop; Air gaps; Aircraft propulsion; Breakdown voltage; Cotton; Engines; Low voltage; Mechanical systems; Power demand; Power system reliability; Power systems;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems Magazine, IEEE
Publisher :
ieee
ISSN :
0885-8985
Type :
jour
DOI :
10.1109/MAES.2008.4460728
Filename :
4460728
Link To Document :
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