Conceptual design of operation strategies for hybrid electric aircraft
Conceptual design of operation strategies for hybrid electric aircraft
Ambitious targets to reduce emissions caused by aviation in the light of an expected ongoing rise of the air transport demand in the future drive the research of propulsion systems with lower CO2 emissions. Regional hybrid electric aircraft (HEA) powered by conventional gas turbines and battery powered electric motors are investigated to test hybrid propulsion operation strategies. Especially the role of the battery within environmentally friendly concepts with significantly reduced carbon footprint is analyzed. Thus, a new simulation approach for HEA is introduced. The main findings underline the importance of choosing the right power-to-energy-ratio of a battery according to the flight mission. The gravimetric energy and power density of the electric storages determine the technologically feasibility of hybrid concepts. Cost competitive HEA configurations are found, but do not promise the targeted CO2 emission savings, when the well-to-wheel system is regarded with its actual costs. Sensitivity studies are used to determine external levers that favor the profitability of HEA
Hoelzen, J.
07fbc2ba-510c-4ccb-a82b-11b67e032861
Liu, Y.
621975c3-5440-4f2c-b313-4e724228220d
Bensmann, Boris
0360e6e1-6ddf-4434-9217-35f4f3576be8
Winnefeld, C.
7cd55c3d-bfbf-4b5f-a2e1-abd89f0a058f
Elham, A.
676043c6-547a-4081-8521-1567885ad41a
Friedrichs, Jens
8f603506-d21c-4aa4-9fde-8f426e1bef4f
Hanke-Rauschenbach, Richard
25eeb898-a5de-4aef-b603-4ac8c9041e56
16 January 2018
Hoelzen, J.
07fbc2ba-510c-4ccb-a82b-11b67e032861
Liu, Y.
621975c3-5440-4f2c-b313-4e724228220d
Bensmann, Boris
0360e6e1-6ddf-4434-9217-35f4f3576be8
Winnefeld, C.
7cd55c3d-bfbf-4b5f-a2e1-abd89f0a058f
Elham, A.
676043c6-547a-4081-8521-1567885ad41a
Friedrichs, Jens
8f603506-d21c-4aa4-9fde-8f426e1bef4f
Hanke-Rauschenbach, Richard
25eeb898-a5de-4aef-b603-4ac8c9041e56
Hoelzen, J., Liu, Y., Bensmann, Boris, Winnefeld, C., Elham, A., Friedrichs, Jens and Hanke-Rauschenbach, Richard
(2018)
Conceptual design of operation strategies for hybrid electric aircraft.
Energies, 11 (1), [217].
(doi:10.3390/en11010217).
Abstract
Ambitious targets to reduce emissions caused by aviation in the light of an expected ongoing rise of the air transport demand in the future drive the research of propulsion systems with lower CO2 emissions. Regional hybrid electric aircraft (HEA) powered by conventional gas turbines and battery powered electric motors are investigated to test hybrid propulsion operation strategies. Especially the role of the battery within environmentally friendly concepts with significantly reduced carbon footprint is analyzed. Thus, a new simulation approach for HEA is introduced. The main findings underline the importance of choosing the right power-to-energy-ratio of a battery according to the flight mission. The gravimetric energy and power density of the electric storages determine the technologically feasibility of hybrid concepts. Cost competitive HEA configurations are found, but do not promise the targeted CO2 emission savings, when the well-to-wheel system is regarded with its actual costs. Sensitivity studies are used to determine external levers that favor the profitability of HEA
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Accepted/In Press date: 12 January 2018
Published date: 16 January 2018
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Local EPrints ID: 470421
URI: http://eprints.soton.ac.uk/id/eprint/470421
ISSN: 1996-1073
PURE UUID: 9cacaaca-ba6b-4399-be63-6557908b830b
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Date deposited: 10 Oct 2022 16:57
Last modified: 16 Mar 2024 21:27
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Author:
J. Hoelzen
Author:
Y. Liu
Author:
Boris Bensmann
Author:
C. Winnefeld
Author:
Jens Friedrichs
Author:
Richard Hanke-Rauschenbach
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