Transfer Characteristics of Brushless Aircraft Generator Systems
- 1 April 1964
- journal article
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Aerospace
- Vol. 2 (2), 913-928
- https://doi.org/10.1109/ta.1964.4319682
Abstract
This paper analyzes the rotating-rectifier type aircraft generator with its exciter and rectifier from the standpoint of its role as an element in a closed loop regulating system. It discusses the transfer characteristics of the brushless generator system in relation to its normal design parameters and its performance characteristics and presents data, largely in graphical form, for use in calculating the transfer characteristics. Further, it describes the very significant influence of the rectifier system on these characteristics.Keywords
This publication has 4 references indexed in Scilit:
- Behavior of Brushless Aircraft Generating SystemsIEEE Transactions on Aerospace, 1963
- Power factor of rectifiersTransactions of the American Institute of Electrical Engineers, Part II: Applications and Industry, 1958
- Analogue Computer Representations of Synchronous Generators in Voltage-Regulation Studies [includes discussion]Transactions of the American Institute of Electrical Engineers. Part III: Power Apparatus and Systems, 1956
- Analysis of Rectifier CircuitsTransactions of the American Institute of Electrical Engineers, 1944