Analysis and Optimization for Winding Topology of Multiphase High Power DC Generator in Future Hybrid Electric Propulsion Aircraft
Author:
Affiliation:
1. Nanjing University of Aeronautics and Astronautics,Center for More-Electric-Aircraft Power Systems,Nanjing,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10343527/10343421/10344389.pdf?arnumber=10344389
Reference8 articles.
1. Technology for the more and all electric aircraft of the future
2. Review of Electric Machines in More-/Hybrid-/Turbo-Electric Aircraft
3. Multimegawatt synchronous generators for airborne applications: A review
4. Maximum Torque per Ampere Control with Inductance and Field Current Estimation for Wound-Rotor Synchronous Starter/Generator
5. Initial Rotor Position Estimation Method for Aircraft Three-Stage Starter/Generator Based on Self-Injected Harmonic Signal
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