By Topic

Analysis of load transfer oscillations in parallel aircraft A-C electric power systems

Sign In

Cookies must be enabled to login.After enabling cookies , please use refresh or reload or ctrl+f5 on the browser for the login options.

Formats Non-Member Member
$33 $13
Learn how you can qualify for the best price for this item!
Become an IEEE Member or Subscribe to
IEEE Xplore for exclusive pricing!
close button

puzzle piece

IEEE membership options for an individual and IEEE Xplore subscriptions for an organization offer the most affordable access to essential journal articles, conference papers, standards, eBooks, and eLearning courses.

Learn more about:

IEEE membership

IEEE Xplore subscriptions

1 Author(s)
H. A. Kahle ; Jack & Heintz, Inc., Cleveland, Ohio

THE PURPOSE of this paper is to investigate a method by which the performance of parallel aircraft a-c generator systems may be predicted, and to define boundaries for the characteristics of generator, regulator, constant-speed drive, and real and reactive load division circuit (LDC) which will guarantee satisfactory parallel operation. The method will be restricted to the analysis of load transfer oscillations in parallel generator systems. Its advantage is that only one generator system need be considered in order to investigate parallel operation and load transfer oscillations; this is because a parallel electric power system is symmetrical with respect to the voltage bus connecting the parallel generators.

Published in:

Transactions of the American Institute of Electrical Engineers, Part II: Applications and Industry  (Volume:79 ,  Issue: 1 )