Abstract
THE performance of 208/120-volt 400-cycle constant-frequency aircraft electric power systems under abnormal conditions resulting from synchronizing disturbances, loss of field excitation, and short circuits is described. As a basis for this study, tests were made on 40-kva alternators, to determine their electrical parameters. The values of these parameters expressed in per unit are listed in Table I.
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Schedule a callMore From: Transactions of the American Institute of Electrical Engineers, Part II: Applications and Industry
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