session-6-3-Prof-Mirko-Hornung

More documents

Recommendations

Info

Parallel Hybrid (A/C Level) Hybrid-electric propulsion system with 4 propulsors 2 conventional gas turbines 2 electrically powered ducted fans No direct coupling between different energy carriers/propulsion systems Battery supplied electric system used as assistance system Expected advantages Downsizing of gas turbines Electric cruise capability Increased operational behavior compared to integrated parallel hybrid topologies No coupling of propulsors Alle Rechte bei / All rights with Bauhaus Luftfahrt e-Flight Forum - Beijing 2017, 9.11.2017 Slide 8
Hybridization Strategy Electric support given by constant thrust split between conventional and electric supplied propulsors over the entire mission Normalized power profile used to determine fuel and battery demand Aircraft level assessment performed with the help of trade factors Alle Rechte bei / All rights with Bauhaus Luftfahrt e-Flight Forum - Beijing 2017, 9.11.2017 Slide 9
Page 1 and 2: (Hybrid) Electric Transport Aircraf
Page 3 and 4: Agenda Universally Electric Aircraf
Page 5 and 6: Benchmarking Ce-Liner Aircraft Prop
Page 7: Basic Approaches to Hybrid Electric
Page 11 and 12: Initial Aircraft Level Results and
Page 13 and 14: The Cloud of MIPH Concepts MIPH app
Page 15 and 16: MIPH: Electric Motor Sizing Sizing
Page 17 and 18: MIPH: Design Block Fuel Assessment
Page 19 and 20: Agenda Universally Electric Aircraf
Page 21 and 22: Fuselage Fan Propulsion System Inte
Page 23 and 24: Synergistic Propulsion-Airframe Int

session-6-3-Prof-Mirko-Hornung

Create successful ePaper yourself

Delete template?

Save as template?