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