System architectures for thermal management of hybrid-electric aircraft - FutPrInt50

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dc.contributor.authorAffonso Jr., Walter
dc.contributor.authorTavares, Renata T.
dc.contributor.authorBarbosa, Felipe R.
dc.contributor.authorGandolfi, Ricardo
dc.contributor.authordos Reis, Ricardo J. N.
dc.contributor.authorda Silva, Carlos R. I.
dc.contributor.authorKipouros, Timoleon
dc.contributor.authorLaskaridis, Panagiotis
dc.contributor.authorBalaghi Enalou, Hossein
dc.contributor.authorChekin, Andrei
dc.contributor.authorKukovinets, Aleksey
dc.contributor.authorGubernatorov, Konstantin
dc.contributor.authorRavikovich, Yury
dc.contributor.authorIvanov, Nikolay
dc.contributor.authorPonyaev, Leonid
dc.contributor.authorHolobtsev, Dmitry
dc.date.accessioned2022-03-01T11:52:06Z
dc.date.available2022-03-01T11:52:06Z
dc.date.issued2022-02-15
dc.description.abstractElectric and Hybrid-Electric Aircraft (HEA) propulsion system designs shall bring challenges at aircraft and systems level, mainly in propulsion, electric and thermal management systems (TMS). The electrification of the propulsion system relies on large and high-power electrical equipment (e.g., electrical motors, converters, power electronics, batteries, and others) that dissipate heat at a rate at least one order of magnitude higher than conventional propulsion aircraft systems. As a result, high impacts on weight, drag and power consumption of the TMS/cooling systems at the aircraft level are expected. This paper proposes potential technologies to perform the thermal management of future electric and HEA, in the context of FUTPRINT50 project. For each technology, relevant aspects such as its integration to aircraft, safety, operational and maintenance impacts, certification, technologies readiness level (TRL) and the latest research works are analysed. A quantitative comparison of the several technologies is also proposed considering weight, volume, electric power consumption, pneumatic air flow and cooling air flow per cooling effect. Lastly, we present a set of potential TMS architectures for HEA.en_UK
dc.description.sponsorshipEuropean Union funding: 875551en_UK
dc.identifier.citationAffonso W, Tavares RT, Barbosa FR, et al., (2022) System architectures for thermal management of hybrid-electric aircraft - FutPrInt50. In: International Conference on Innovation in Aviation & Space to the Satisfaction of the European Citizens (11th EASN 2021), 1-3 September 2021, Virtual event, IOP Conference Series: Materials Science and Engineering, Volume 1226, Article number 012062en_UK
dc.identifier.eissn1757-899X
dc.identifier.issn1757-8981
dc.identifier.urihttps://doi.org/10.1088/1757-899X/1226/1/012062
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/17614
dc.language.isoenen_UK
dc.publisherIOPen_UK
dc.rightsAttribution 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/*
dc.titleSystem architectures for thermal management of hybrid-electric aircraft - FutPrInt50en_UK
dc.typeConference paperen_UK

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