A Doubly Salient Starter/Generator With Two-Section Twisted-Rotor Structure for Potential Future Aerospace Application

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) wavefo...

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Published inIEEE transactions on industrial electronics (1982) Vol. 59; no. 9; pp. 3588 - 3595
Main Authors Chen, Zhihui, Wang, Huizhen, Yan, Yangguang
Format Journal Article
LanguageEnglish
Published New York IEEE 01.09.2012
The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subjects
Aircraft components
Computer simulation
Control algorithms
Doubly salient machines
Electric potential
Electromagnetic scattering
electromotive force (EMF)
Finite element methods
finite-element methods (FEMs)
Generators
Ripples
Rotors
Starters
Studies
Torque
torque ripple coefficient
two-section twisted-rotor structure
Waveforms
Windings
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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.
AbstractList 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.
Author Zhihui Chen
Yangguang Yan
Huizhen Wang
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  surname: Yan
  fullname: Yan, Yangguang
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SubjectTerms Aircraft components
Computer simulation
Control algorithms
Doubly salient machines
Electric potential
Electromagnetic scattering
electromotive force (EMF)
Finite element methods
finite-element methods (FEMs)
Generators
Ripples
Rotors
Starters
Studies
Torque
torque ripple coefficient
two-section twisted-rotor structure
Waveforms
Windings
Title A Doubly Salient Starter/Generator With Two-Section Twisted-Rotor Structure for Potential Future Aerospace Application
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