DocumentCode
1557530
Title
A Doubly Salient Starter/Generator With Two-Section Twisted-Rotor Structure for Potential Future Aerospace Application
Author
Chen, Zhihui ; Wang, Huizhen ; Yan, Yangguang
Author_Institution
Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
Volume
59
Issue
9
fYear
2012
Firstpage
3588
Lastpage
3595
Abstract
The starter/generator is one key technology for the more electric/all electric aircraft. The wound-field doubly salient starter/generator supplies good prospect in the aircraft application. The doubly salient starter/generator prototype is modeled for simulation. The electromotive force (EMF) waveforms obtained from simulation are validated by the experiments. Based on the EMF waveforms of the machine, the standard three-step control algorithm is derived. When the rotor runs at high speed, the advanced angle control (AAC) method is adopted to get enough torque. The simulation and experiment results with two different control strategies are compared. The AAC scheme can increase the average torque by 62.7% at 3600 r/min. To reduce the torque ripples, the two-section twisted-rotor structure is adopted. The analysis shows that the two-section twisted-rotor structure helps to reduce the torque ripple coefficient by more than 50%. The two-section twisted-rotor structure is also helpful to reduce the output dc voltage ripple.
Keywords
aircraft; angular velocity control; electric generators; electric potential; electric vehicles; finite element analysis; rotors; starting; torque control; AAC method; EMF waveforms; advanced angle control method; control strategies; electric aircraft; electromotive force waveforms; output DC voltage ripple; potential future aerospace application; standard three-step control algorithm; torque ripple coefficient; two-section twisted-rotor structure; wound-field doubly salient starter-generator; Electromagnetic scattering; Finite element methods; Generators; Rotors; Torque; Windings; Doubly salient machines; electromotive force (EMF); finite-element methods (FEMs); torque ripple coefficient; two-section twisted-rotor structure;
fLanguage
English
Journal_Title
Industrial Electronics, IEEE Transactions on
Publisher
ieee
ISSN
0278-0046
Type
jour
DOI
10.1109/TIE.2011.2159951
Filename
5892883
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