DocumentCode
1476218
Title
Selenium power rectifiers for A-C aircraft systems
Author
Embry, Alvin L.
Author_Institution
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 substantially 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 step-down transformers and voltage-regulating equipment, are described in this paper. Ratings vary from 100 to 800 amperes.
Keywords
Aircraft; Alternators; Cooling; Inductors; Rectifiers; Regulators; Voltage control;
fLanguage
English
Journal_Title
Electrical Engineering
Publisher
ieee
ISSN
0095-9197
Type
jour
DOI
10.1109/EE.1945.6441222
Filename
6441222
Link To Document