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SYNERGIES AND TRADE-OFFS IN HYBRID PROPULSION SYSTEMS THROUGH PHYSICS-BASED ELECTRICAL COMPONENT MODELLING

Bermperis, Dimitios (författare)
Mälardalens universitet,Framtidens energi
Ntouvelos, E. (författare)
Aristotle University of Thessaloniki, Thessaloniki, Greece
Kavvalos, Mavroudis (författare)
Mälardalens universitet,Framtidens energi
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Vouros, Stavros (författare)
Mälardalens universitet,Innovation och produktrealisering
Kyprianidis, Konstantinos (författare)
Mälardalens universitet,Framtidens energi
Kalfas, A. I. (författare)
Aristotle University of Thessaloniki, Thessaloniki, Greece
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 (creator_code:org_t)
American Society of Mechanical Engineers (ASME), 2023
2023
Engelska.
Ingår i: Proc. ASME Turbo Expo. - : American Society of Mechanical Engineers (ASME). - 9780791886939
  • Konferensbidrag (refereegranskat)
Abstract Ämnesord
Stäng  
  • Hybrid-electric propulsion is recognized as one of the enabling technologies for reducing aviation’s environmental impact. In this work a serial/parallel hybrid configuration of a 19-passenger commuter aircraft is investigated. Two underwing-mounted turboprop engines are connected to electrical branches via generators. One rear fuselage-mounted electrically driven ducted fan is coupled with an electric motor and respective electrical branch. A battery system completes the selected architecture. Consistency in modelling accuracy of propulsion systems is aimed for by development of an integrated framework. A multi-point synthesis scheme for the gas turbine and electric fan is combined with physics-based analytical modelling for electrical components. Influence of turbomachinery and electrical power system design points on the integrated power system is examined. An opposing trend between electrical and conventional powertrain mass is driven by electric fan design power. Power system efficiency improvements in the order of 2% favor high-power electric fan designs. A trade-off in electrical power system mass and performance arises from oversizing of electrical components for load manipulation. Branch efficiency improvements of up to 3% imply potential to achieve battery mass reduction due to fewer transmission losses in mission-significant segments. A threshold system voltage of 1kV, yielding 32% mass reduction of electrical branches and performance improvements of 1-2%, is defined. Above the indicated threshold, benefits are limited, and system design complexity increases unfavorably. This work sets the foundation for interpreting mission-level electrification outcomes that are driven by interactions on the integrated power system. Areas of conflicting interests and synergistic opportunities are highlighted for optimal conceptual design of hybrid powertrains.

Ämnesord

TEKNIK OCH TEKNOLOGIER  -- Maskinteknik -- Energiteknik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Mechanical Engineering -- Energy Engineering (hsv//eng)

Nyckelord

Conceptual design
Economic and social effects
Efficiency
Electric loads
Environmental impact
Environmental technology
Machine design
Systems analysis
Efficiency improvement
Electric fans
Electrical components
Electrical power system
Fan designs
Integrated Power Systems
Mass reduction
Performance
Physics-based
Trade off
Electric power transmission

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