05 - Propulsion
STUDY OF HYBRIDISATION SCENARIOS FOR TURBOPROP AIRCRAFT IN THE GENERAL AVIATION SEGMENT
F. Lutz¹, J. Jézégou¹, M. Budinger², A. Reysset²; ¹ISAE-SUPAERO, France ;²INSA Toulouse, France
This paper explores the feasibility of the hybridisation of turboprop aircraft in the General Aviation segment. Because of the long lifetime of CO2 in the atmoshpere, designs using current electric technologies are investigated to assess the reductions in terms of cumulated emissions. Two aircraft and their most common routes are studied to obtain commercially realistic hybridised versions.