The paper presents a preliminary design structure of an electric propulsion system and associated control management unit for a small twin-seater aircraft. This is part of a larger research project that involves design, simulation, and flight test of a piloted vehicle equipped with a single engine powered by a combination of fuel cells and batteries. The innovative aspects of this applied research project, make it the first full European effort to all-electric propelled air vehicle.
Design of an All-Electric Propulsion System and Control Management for a General Aviation Aircraft
INNOCENTI, MARIO
Primo
Project Administration
;POLLINI, LORENZOPenultimo
Validation
;SANI, LUCAUltimo
Data Curation
2009-01-01
Abstract
The paper presents a preliminary design structure of an electric propulsion system and associated control management unit for a small twin-seater aircraft. This is part of a larger research project that involves design, simulation, and flight test of a piloted vehicle equipped with a single engine powered by a combination of fuel cells and batteries. The innovative aspects of this applied research project, make it the first full European effort to all-electric propelled air vehicle.File in questo prodotto:
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