Design and Modeling of a Five-Phase Aircraft Synchronous Generator With High Power Density
Document Type
Article
Publication Date
11-10-2012
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Abstract
This paper presents a methodology for the design and modeling of a five-phase aircraft synchronous generator with high-power density. A new method was recently proposed for a more accurate model of the air-gap of a salient pole rotor through expanding the inverse of an effective air-gap function for three-phase synchronous generators. This approach is adapted to the five-phase case here, with some modifications to the derivations. Five-phase decoupling direct-quadrature theory is reviewed and presented as the basis for linear modeling of the five-phase synchronous machine. Following the procedure for a three-phase design with five-phase considerations, a 200 kVA high power density synchronous generator with 12 krpm rotational velocity is obtained. Finally, the design is verified using finite element method software.
Repository Citation
Camarano, T.,
Wu, T.,
Rodriguez, S.,
Zumberge, J.,
& Wolff, M.
(2012). Design and Modeling of a Five-Phase Aircraft Synchronous Generator With High Power Density. 2012 IEEE Energy Conversion Congress and Exposition, ECCE 2012, 1878-1885.
https://corescholar.libraries.wright.edu/mme/677
DOI
10.1109/ECCE.2012.6342583
