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 :
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