Modelling and designing cryogenic hydrogen tanks for future aircraft applications

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dc.identifier.uri http://dx.doi.org/10.15488/3366
dc.identifier.uri http://www.repo.uni-hannover.de/handle/123456789/3396
dc.contributor.author Winnefeld, Christopher
dc.contributor.author Kadyk, Thomas
dc.contributor.author Bensmann, Boris
dc.contributor.author Krewer, Ulrike
dc.contributor.author Hanke-Rauschenbach, Richard
dc.date.accessioned 2018-05-23T07:46:37Z
dc.date.available 2018-05-23T07:46:37Z
dc.date.issued 2018
dc.identifier.citation Winnefeld, C.; Kadyk, T.; Bensmann, B.; Krewer, U.; Hanke-Rauschenbach, R.: Modelling and designing cryogenic hydrogen tanks for future aircraft applications. In: Energies 11 (2018), Nr. 1, 105. DOI: https://doi.org/10.3390/en11010105
dc.description.abstract In the near future, the challenges to reduce the economic and social dependency on fossil fuels must be faced increasingly. A sustainable and efficient energy supply based on renewable energies enables large-scale applications of electro-fuels for, e.g., the transport sector. The high gravimetric energy density makes liquefied hydrogen a reasonable candidate for energy storage in a light-weight application, such as aviation. Current aircraft structures are designed to accommodate jet fuel and gas turbines allowing a limited retrofitting only. New designs, such as the blended-wing-body, enable a more flexible integration of new storage technologies and energy converters, e.g., cryogenic hydrogen tanks and fuel cells. Against this background, a tank-design model is formulated, which considers geometrical, mechanical and thermal aspects, as well as specific mission profiles while considering a power supply by a fuel cell. This design approach enables the determination of required tank mass and storage density, respectively. A new evaluation value is defined including the vented hydrogen mass throughout the flight enabling more transparent insights on mass shares. Subsequently, a systematic approach in tank partitioning leads to associated compromises regarding the tank weight. The analysis shows that cryogenic hydrogen tanks are highly competitive with kerosene tanks in terms of overall mass, which is further improved by the use of a fuel cell. © 2018 by the authors. eng
dc.language.iso eng
dc.publisher Basel : MDPI AG
dc.relation.ispartofseries Energies 11 (2018), Nr. 1
dc.rights CC BY 4.0
dc.rights.uri https://creativecommons.org/licenses/by/4.0/
dc.subject Aviation eng
dc.subject Energy storage eng
dc.subject Fuel tanks eng
dc.subject Hydrogen storage eng
dc.subject Proton-exchange membrane fuel cell eng
dc.subject Aircraft manufacture eng
dc.subject Airframes eng
dc.subject Aviation eng
dc.subject Combustion eng
dc.subject Cryogenics eng
dc.subject Energy storage eng
dc.subject Fighter aircraft eng
dc.subject Flexible wings eng
dc.subject Fossil fuels eng
dc.subject Fuel cells eng
dc.subject Fuel storage eng
dc.subject Gas turbines eng
dc.subject Hydrogen eng
dc.subject Hydrogen storage eng
dc.subject Proton exchange membrane fuel cells (PEMFC) eng
dc.subject Tanks (containers) eng
dc.subject Aircraft applications eng
dc.subject Aircraft structure eng
dc.subject Flexible integration eng
dc.subject Gravimetric energy densities eng
dc.subject Large-scale applications eng
dc.subject Renewable energies eng
dc.subject Storage densities eng
dc.subject Storage technology eng
dc.subject Fuel tanks eng
dc.subject.ddc 620 | Ingenieurwissenschaften und Maschinenbau ger
dc.title Modelling and designing cryogenic hydrogen tanks for future aircraft applications
dc.type article
dc.type Text
dc.relation.issn 1996-1073
dc.relation.doi https://doi.org/10.3390/en11010105
dc.bibliographicCitation.issue 1
dc.bibliographicCitation.volume 11
dc.bibliographicCitation.firstPage 105
dc.description.version publishedVersion
tib.accessRights frei zug�nglich


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