F. Ciccarelli, L. P. D. Noia, S. Hamasaki, R. Rizzo
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Thermal Analysis of DAB Converter Core used in Hybrid Aircraft Propulsion System
The interest in the hybrid electric aircraft propulsion is increasing. Different goals must be guaranteed for a correct performance of an electric propulsion system for aircraft: reliability, low weights, performance in critical conditions. The paper is focused on the thermal analysis of the medium/high frequency core transformers used for the coupling between the battery storage system and the electric motor in electric aircrafts. A multi-physics simulation is carried out to solve the transient thermal problem for the transformer during electrical assisted phase of the aircraft.
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