DocumentCode
1307171
Title
Solid-state switching for aircraft electric systems
Author
Dickey, Lee D. ; Jones, Clyde M.
Author_Institution
LTV Aerospace Corporation
Volume
7
Issue
11
fYear
1970
Firstpage
73
Lastpage
79
Abstract
An aircraft electric system designed around a solid-state approach offers many potential advantages over an electromechanical counterpart. These include higher reliability, longer life, more ruggedness, more versatility, and better compatibility. To achieve these advantages, however, it is not merely sufficient to replace electromechanical components with their solid-state equivalents. Here is one approach that has been tested in the laboratory and in aircraft during the past ten years¿with success. Included is a report on an advanced system undergoing evaluation.
Keywords
Aerospace control; Aerospace electronics; Aircraft; Circuit breakers; Power semiconductor switches; Power system protection; Solid state circuits; Switching circuits; Voltage; Wiring;
fLanguage
English
Journal_Title
Spectrum, IEEE
Publisher
ieee
ISSN
0018-9235
Type
jour
DOI
10.1109/MSPEC.1970.5213040
Filename
5213040
Link To Document