Abstract
This paper proposes a new design of high-temperature starter-generator with external rotor to be installed on high pressure shaft of aircraft engine to implement More Electrical Engine concept. The basic materials to make this starter-generator were selected and justified. Multi-criteria optimization of the developed design was performed using a genetic algorithm and Pareto method. The optimum (in Pareto terms) active length and thickness of permanent magnets of starter-generator were selected as a result of the optimization. Using the obtained dimensions allowed reducing the weight of the designed starter-generator by 10 kg relative to a base option at constant thermal loads. Multidisciplinary computer simulation was performed on the basis of the optimum geometric dimensions, which proved performance efficiency of the design.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
