Title :
Computer evaluation of high-temperature aircraft A-C electrical system designs
Author :
Sollecito, W. E. ; Swann, D. A.
Author_Institution :
General Electric Company, Schenectady, N. Y.
Abstract :
This paper describes a design and analog computer study of a high-temperature aircraft a-c electrical system. The study includes an extensive, nonlinear representation of the a-c alternator and shows the effects of temperature, load, and regulator and exciter nonlinear behavior on system stability and transient performance. Torque-limiting techniques are evaluated and a computer approach for study of the reactive load division loop is developed.
Keywords :
Aircraft; Alternators; Computers; Limiting; System analysis and design; Temperature; Thermal stability;
Journal_Title :
American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
DOI :
10.1109/TAI.1960.6371608
