Optimized thermal management for high-power electric machines
Aircraft power demand is growing, due to the introduction of new onboard systems requiring additional power, and to aircraft size/range increase. Concurrently, concern for the impact of aviation on global warming is increasing. Thus, interest in hybrid/electric propulsion for aircraft is increasing. The introduction of this type of propulsion system introduces challenges to be faced, such as the thermal management of electrical machines. The present work focuses on the design of a novel TMS (thermal management system) for the thermal control of an advanced electric machine developed for a future much more electric aircraft.