The large use of electrified aircraft vehicles requires the development of high performance and reliable electric drives. Furthermore, fault tolerant performance plays an important role and control strategies for common faults inherent in the application should be developed. The paper refers to the use Surface Permanent Magnet Synchronous Motors (SPMSM) for the electric propulsion of unmanned aerial vehicles. A numerical approach is proposed for the analysis of the effects of an imbalance of the propellers on the operations and features of the used motors. The results obtained are compared with those deriving from conventional types of eccentricity.
Evaluation of the Effects of Propeller Imbalance on PM Motors for Aircraft Electric Propulsion / Brando, G.; Dannier, A.; Pizzo, A. D.; Di Noia, L. P.. - (2023), pp. 1-6. (Intervento presentato al convegno 2023 IEEE International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles and International Transportation Electrification Conference, ESARS-ITEC 2023 tenutosi a ita nel 2023) [10.1109/ESARS-ITEC57127.2023.10114907].
Evaluation of the Effects of Propeller Imbalance on PM Motors for Aircraft Electric Propulsion
Brando G.;Dannier A.;Pizzo A. D.;Di Noia L. P.
2023
Abstract
The large use of electrified aircraft vehicles requires the development of high performance and reliable electric drives. Furthermore, fault tolerant performance plays an important role and control strategies for common faults inherent in the application should be developed. The paper refers to the use Surface Permanent Magnet Synchronous Motors (SPMSM) for the electric propulsion of unmanned aerial vehicles. A numerical approach is proposed for the analysis of the effects of an imbalance of the propellers on the operations and features of the used motors. The results obtained are compared with those deriving from conventional types of eccentricity.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
