Title :
Aircraft Electric Power-Supply System
Author_Institution :
Commercial engineer, selenium rectifier division, for the Federal Telephone and Radio Corporation, East Newark, N. J.
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 manufacture; Alternators; Batteries; Cooling; Humidity; Power generation; Power transformers; Rectifiers; Temperature; Testing;
Journal_Title :
American Institute of Electrical Engineers, Transactions of the
DOI :
10.1109/T-AIEE.1943.5058621