DocumentCode
3213139
Title
Improving aircraft engine operability through electric system design and operation
Author
Norman, Patrick J. ; Galloway, Stuart J. ; Burt, Graeme M. ; Hill, Jason E.
Author_Institution
University of Strathclyde, UK
fYear
2010
fDate
19-21 April 2010
Firstpage
1
Lastpage
5
Abstract
With modern passenger aircraft requiring greater levels of electrical power to supply the novel technologies employed, the potential for interaction between the aircraft engine and electrical system is greatly increased. There is therefore a strong requirement to develop a thorough appreciation of the interrelationships governing the behaviour of the integrated system such that undesirable modes of operation may be avoided, and, in the longer term, globally optimised engine-electrical system designs may be produced. This paper presents the findings of a number of investigative studies conducted on a high fidelity, integrated aircraft engine and electrical power system simulation tool. These studies assess the effectiveness of a variety of electrical system design and operation methods in optimising the behaviour of the aircraft engine, whilst illustrating key trends in the behaviour of the integrated system.
Keywords
Aircraft electrical systems; power offtakes;
fLanguage
English
Publisher
iet
Conference_Titel
Power Electronics, Machines and Drives (PEMD 2010), 5th IET International Conference on
Conference_Location
Brighton, UK
Type
conf
DOI
10.1049/cp.2010.0046
Filename
5523768
Link To Document