Title
Design And Modeling Of A Five-Phase Aircraft Synchronous Generator With High Power Density
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. © 2012 IEEE.
Publication Date
12-17-2012
Publication Title
2012 IEEE Energy Conversion Congress and Exposition, ECCE 2012
Number of Pages
1878-1885
Document Type
Article; Proceedings Paper
Personal Identifier
scopus
DOI Link
https://doi.org/10.1109/ECCE.2012.6342583
Copyright Status
Unknown
Socpus ID
84870928387 (Scopus)
Source API URL
https://api.elsevier.com/content/abstract/scopus_id/84870928387
STARS Citation
Camarano, Tony; Wu, Thomas; Rodriguez, Samuel; Zumberge, Jon; and Wolff, Mitch, "Design And Modeling Of A Five-Phase Aircraft Synchronous Generator With High Power Density" (2012). Scopus Export 2010-2014. 4191.
https://stars.library.ucf.edu/scopus2010/4191