Methodology for developing a hybrid power plant with an electromechanical energy converter and a permanent magnet generator

Abstract

The article presents a comprehensive methodology for designing hybrid propulsion systems for advanced aircraft, based on the use of high-efficiency electromechanical energy converters with permanent magnets. A comparative analysis of the circuit solutions for propulsion systems, as well as Russian and foreign developments, is conducted. The article also demonstrates the experience of implementing an integrated propulsion system in the field of aviation electric machines. Special attention is given to the determination of primary parameters, the optimization of electromechanical characteristics, and the integration aspects of creating hybrid propulsion systems. The article presents the results of experimental studies that confirm the advantages of the proposed solutions and identify issues for further research. doi 10.54708/19926502_2026_30111131