01 - Aircraft and Systems Integration
HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS
Y. Fefermann¹, C. Maury¹, C. Level¹, K. Zarati¹, J.-P. Salanne¹, C. Pornet¹, B. Thoraval¹, A.T. Isikveren¹; ¹SAFRAN S.A., France
This paper shall discuss design and integration considerations involved when utilizing hybrid-electric motive power systems for fixed-wing commuter transport aircraft. The primary aim of deploying hybrid-electric technologies to aircraft is to seek pragmatic, appropriately projected engineering solutions in meeting aggressive emissions and noise targets declared by the EC, NASA, IATA and ICAO.