DocumentCode
1026758
Title
Selenium Power Rectifiers for A-C Aircraft Systems
Author
Embry, Alvin L.
Author_Institution
Design engineer, Tungar and metallic rectifier section, lighting engineering division, General Electric Company, West Lynn, Mass.
Volume
64
Issue
8
fYear
1945
Firstpage
596
Lastpage
600
Abstract
Increasing electric-power requirements for large aircraft have brought about the introduction of a-c power systems. Two major systems have been developed. In the first power is generated at variable frequency and converted to direct current; in the second power is generated at sub-stantially constant frequency, and both a-c and d-c power are used. In both systems selenium rectifiers can be used as converters. Rectifier units developed to supply 28.5-volt regulated d-c power, which include stepdown transformers and voltage-regulating equipment, are described in this paper. Ratings vary from 100 to 800 amperes.
Keywords
Aircraft; Conductors; Design engineering; Frequency measurement; Induction generators; Instruments; Power generation; Power systems; Rectifiers; Time measurement;
fLanguage
English
Journal_Title
American Institute of Electrical Engineers, Transactions of the
Publisher
ieee
ISSN
0096-3860
Type
jour
DOI
10.1109/T-AIEE.1945.5059183
Filename
5059183
Link To Document