DocumentCode :
1443866
Title :
Aircraft electric power-supply system
Author :
Yarmack, J. E.
Author_Institution :
Federal Telephone and Radio Corporation, East Newark, N. J.
Volume :
62
Issue :
10
fYear :
1943
Firstpage :
655
Lastpage :
658
Abstract :
An ever increasing demand for electric power in aircraft has been felt for some time. The necessity of using an electric storage battery started the practice of accompanying it with a d-c generator, first of low current and voltage capacity, later of 50-ampere 12-volt rating, and for the past few years of 200-ampere 24-volt output. In the largest four-engine aircraft, even four generators of maximum capacity do not furnish ample electric energy. Experiments have proved so far that generation of a-c power and application of lightweight transformers, together with its conversion to direct current by means of selenium rectifiers, is entirely a reliable and practical way of attaining large, trouble-free electric plant capacity in aircraft. The subsequent pages and illustrations portray the current progress made with lightweight power transformers and rectifiers in the a-c — d-c aircraft systems. They also represent at least a partial answer to the questions raised by Lieutenant Colonel Holliday1 when he discussed problems of applications of electric power in aircraft two years ago.
Keywords :
Aircraft; Alternators; Cooling; Power transformer insulation; Rectifiers; Temperature; Windings;
fLanguage :
English
Journal_Title :
Electrical Engineering
Publisher :
ieee
ISSN :
0095-9197
Type :
jour
DOI :
10.1109/EE.1943.6435960
Filename :
6435960
Link To Document :
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