Liquid Hydrogen Storage Tank Virtual Crashworthiness Design Exploration for Civil Aircraft

Civil aviation industry is researching for alternative fuel energy sources to substitute current hydrocarbon-based aviation fuels. Carbon free emissions flights could be achieved with fuels like Hydrogen either through combustion or via electricity producing fuel cells. It is of great importance to...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of physics. Conference series 2024-02, Vol.2692 (1), p.12049
Hauptverfasser: Gallois, A, Giannopoulos, I K, Theotokoglou, E E
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue 1
container_start_page 12049
container_title Journal of physics. Conference series
container_volume 2692
creator Gallois, A
Giannopoulos, I K
Theotokoglou, E E
description Civil aviation industry is researching for alternative fuel energy sources to substitute current hydrocarbon-based aviation fuels. Carbon free emissions flights could be achieved with fuels like Hydrogen either through combustion or via electricity producing fuel cells. It is of great importance to explore the airframe designs to house Hydrogen in its cryogenic liquified state. The objective of the study herein was to provide a conceptual qualitative analysis related to the crashworthiness behaviour of civil aircraft carrying liquid Hydrogen fuel storage tanks. The design parameters of interest were the storage tank location in the airframe, the structural energy absorption following crash landing scenarios and the structural deformation of the structure surrounding the tanks, penetrating the survival space of the occupants. Several structural design arrangements were proposed and compared. Simulation results indicated that the optimal location for the fuel storage greatly depends on the actual aircraft layout as well as on the future civil aircraft airworthiness requirements that are still under development for that type of fuel energy source.
doi_str_mv 10.1088/1742-6596/2692/1/012049
format Article
fullrecord <record><control><sourceid>proquest_iop_j</sourceid><recordid>TN_cdi_proquest_journals_2924353863</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2924353863</sourcerecordid><originalsourceid>FETCH-LOGICAL-c359t-8ed787bb8dabe07323410aa1cd10d4fc907d7b2b033a8284eec49b3d09119cf03</originalsourceid><addsrcrecordid>eNqFkF9LwzAUxYsoOKefwYBvwmz-dE3yOOp0ykBh0wdfQtqkW2ZtuqRV9-1tqUwEwftyL9xzzr38guAcwSsEGQsRjfAoHvM4xDHHIQohwjDiB8Fgvzncz4wdByfebyAkbdFB8DI328YoMNspZ1e6BIvaOrnSYCnLV_BsXN3IAiRO-vWHdfXalNp7cK29WZVg-lkVrbo2tgS5dSAx76YAE-MyJ_P6NDjKZeH12XcfBk8302UyG80fbu-SyXyUkTGvR0wrymiaMiVTDSnBJEJQSpQpBFWUZxxSRVOcth9LhlmkdRbxlCjIEeJZDskwuOhzK2e3jfa12NjGle1JgTmOyJiwmLQq2qsyZ713OheVM2_S7QSCogMpOkSiwyU6kAKJHmTrJL3T2Oon-n_X5R-u-8dk8VsoKpWTL13Vg4E</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2924353863</pqid></control><display><type>article</type><title>Liquid Hydrogen Storage Tank Virtual Crashworthiness Design Exploration for Civil Aircraft</title><source>IOP Publishing Free Content</source><source>Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals</source><source>IOPscience extra</source><source>Alma/SFX Local Collection</source><source>Free Full-Text Journals in Chemistry</source><creator>Gallois, A ; Giannopoulos, I K ; Theotokoglou, E E</creator><creatorcontrib>Gallois, A ; Giannopoulos, I K ; Theotokoglou, E E</creatorcontrib><description>Civil aviation industry is researching for alternative fuel energy sources to substitute current hydrocarbon-based aviation fuels. Carbon free emissions flights could be achieved with fuels like Hydrogen either through combustion or via electricity producing fuel cells. It is of great importance to explore the airframe designs to house Hydrogen in its cryogenic liquified state. The objective of the study herein was to provide a conceptual qualitative analysis related to the crashworthiness behaviour of civil aircraft carrying liquid Hydrogen fuel storage tanks. The design parameters of interest were the storage tank location in the airframe, the structural energy absorption following crash landing scenarios and the structural deformation of the structure surrounding the tanks, penetrating the survival space of the occupants. Several structural design arrangements were proposed and compared. Simulation results indicated that the optimal location for the fuel storage greatly depends on the actual aircraft layout as well as on the future civil aircraft airworthiness requirements that are still under development for that type of fuel energy source.</description><identifier>ISSN: 1742-6588</identifier><identifier>EISSN: 1742-6596</identifier><identifier>DOI: 10.1088/1742-6596/2692/1/012049</identifier><language>eng</language><publisher>Bristol: IOP Publishing</publisher><subject>Aircraft ; Aircraft reliability ; Airframes ; Alternative fuels ; Aviation ; Aviation fuel ; Crash landing ; Crashworthiness ; Design parameters ; Energy absorption ; Energy sources ; Fuel cells ; Fuel storage ; Fuel tanks ; Hydrogen ; Hydrogen fuels ; Hydrogen storage ; Impact strength ; Liquid hydrogen ; Qualitative analysis ; Storage tanks ; Structural design</subject><ispartof>Journal of physics. Conference series, 2024-02, Vol.2692 (1), p.12049</ispartof><rights>Published under licence by IOP Publishing Ltd</rights><rights>Published under licence by IOP Publishing Ltd. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c359t-8ed787bb8dabe07323410aa1cd10d4fc907d7b2b033a8284eec49b3d09119cf03</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://iopscience.iop.org/article/10.1088/1742-6596/2692/1/012049/pdf$$EPDF$$P50$$Giop$$Hfree_for_read</linktopdf><link.rule.ids>314,780,784,27924,27925,38868,38890,53840,53867</link.rule.ids></links><search><creatorcontrib>Gallois, A</creatorcontrib><creatorcontrib>Giannopoulos, I K</creatorcontrib><creatorcontrib>Theotokoglou, E E</creatorcontrib><title>Liquid Hydrogen Storage Tank Virtual Crashworthiness Design Exploration for Civil Aircraft</title><title>Journal of physics. Conference series</title><addtitle>J. Phys.: Conf. Ser</addtitle><description>Civil aviation industry is researching for alternative fuel energy sources to substitute current hydrocarbon-based aviation fuels. Carbon free emissions flights could be achieved with fuels like Hydrogen either through combustion or via electricity producing fuel cells. It is of great importance to explore the airframe designs to house Hydrogen in its cryogenic liquified state. The objective of the study herein was to provide a conceptual qualitative analysis related to the crashworthiness behaviour of civil aircraft carrying liquid Hydrogen fuel storage tanks. The design parameters of interest were the storage tank location in the airframe, the structural energy absorption following crash landing scenarios and the structural deformation of the structure surrounding the tanks, penetrating the survival space of the occupants. Several structural design arrangements were proposed and compared. Simulation results indicated that the optimal location for the fuel storage greatly depends on the actual aircraft layout as well as on the future civil aircraft airworthiness requirements that are still under development for that type of fuel energy source.</description><subject>Aircraft</subject><subject>Aircraft reliability</subject><subject>Airframes</subject><subject>Alternative fuels</subject><subject>Aviation</subject><subject>Aviation fuel</subject><subject>Crash landing</subject><subject>Crashworthiness</subject><subject>Design parameters</subject><subject>Energy absorption</subject><subject>Energy sources</subject><subject>Fuel cells</subject><subject>Fuel storage</subject><subject>Fuel tanks</subject><subject>Hydrogen</subject><subject>Hydrogen fuels</subject><subject>Hydrogen storage</subject><subject>Impact strength</subject><subject>Liquid hydrogen</subject><subject>Qualitative analysis</subject><subject>Storage tanks</subject><subject>Structural design</subject><issn>1742-6588</issn><issn>1742-6596</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><sourceid>O3W</sourceid><sourceid>ABUWG</sourceid><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><recordid>eNqFkF9LwzAUxYsoOKefwYBvwmz-dE3yOOp0ykBh0wdfQtqkW2ZtuqRV9-1tqUwEwftyL9xzzr38guAcwSsEGQsRjfAoHvM4xDHHIQohwjDiB8Fgvzncz4wdByfebyAkbdFB8DI328YoMNspZ1e6BIvaOrnSYCnLV_BsXN3IAiRO-vWHdfXalNp7cK29WZVg-lkVrbo2tgS5dSAx76YAE-MyJ_P6NDjKZeH12XcfBk8302UyG80fbu-SyXyUkTGvR0wrymiaMiVTDSnBJEJQSpQpBFWUZxxSRVOcth9LhlmkdRbxlCjIEeJZDskwuOhzK2e3jfa12NjGle1JgTmOyJiwmLQq2qsyZ713OheVM2_S7QSCogMpOkSiwyU6kAKJHmTrJL3T2Oon-n_X5R-u-8dk8VsoKpWTL13Vg4E</recordid><startdate>20240201</startdate><enddate>20240201</enddate><creator>Gallois, A</creator><creator>Giannopoulos, I K</creator><creator>Theotokoglou, E E</creator><general>IOP Publishing</general><scope>O3W</scope><scope>TSCCA</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>H8D</scope><scope>HCIFZ</scope><scope>L7M</scope><scope>P5Z</scope><scope>P62</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope></search><sort><creationdate>20240201</creationdate><title>Liquid Hydrogen Storage Tank Virtual Crashworthiness Design Exploration for Civil Aircraft</title><author>Gallois, A ; Giannopoulos, I K ; Theotokoglou, E E</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c359t-8ed787bb8dabe07323410aa1cd10d4fc907d7b2b033a8284eec49b3d09119cf03</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Aircraft</topic><topic>Aircraft reliability</topic><topic>Airframes</topic><topic>Alternative fuels</topic><topic>Aviation</topic><topic>Aviation fuel</topic><topic>Crash landing</topic><topic>Crashworthiness</topic><topic>Design parameters</topic><topic>Energy absorption</topic><topic>Energy sources</topic><topic>Fuel cells</topic><topic>Fuel storage</topic><topic>Fuel tanks</topic><topic>Hydrogen</topic><topic>Hydrogen fuels</topic><topic>Hydrogen storage</topic><topic>Impact strength</topic><topic>Liquid hydrogen</topic><topic>Qualitative analysis</topic><topic>Storage tanks</topic><topic>Structural design</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Gallois, A</creatorcontrib><creatorcontrib>Giannopoulos, I K</creatorcontrib><creatorcontrib>Theotokoglou, E E</creatorcontrib><collection>IOP Publishing Free Content</collection><collection>IOPscience (Open Access)</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>Advanced Technologies &amp; Aerospace Collection</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>Aerospace Database</collection><collection>SciTech Premium Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Advanced Technologies &amp; Aerospace Database</collection><collection>ProQuest Advanced Technologies &amp; Aerospace Collection</collection><collection>Publicly Available Content Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><jtitle>Journal of physics. Conference series</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Gallois, A</au><au>Giannopoulos, I K</au><au>Theotokoglou, E E</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Liquid Hydrogen Storage Tank Virtual Crashworthiness Design Exploration for Civil Aircraft</atitle><jtitle>Journal of physics. Conference series</jtitle><addtitle>J. Phys.: Conf. Ser</addtitle><date>2024-02-01</date><risdate>2024</risdate><volume>2692</volume><issue>1</issue><spage>12049</spage><pages>12049-</pages><issn>1742-6588</issn><eissn>1742-6596</eissn><abstract>Civil aviation industry is researching for alternative fuel energy sources to substitute current hydrocarbon-based aviation fuels. Carbon free emissions flights could be achieved with fuels like Hydrogen either through combustion or via electricity producing fuel cells. It is of great importance to explore the airframe designs to house Hydrogen in its cryogenic liquified state. The objective of the study herein was to provide a conceptual qualitative analysis related to the crashworthiness behaviour of civil aircraft carrying liquid Hydrogen fuel storage tanks. The design parameters of interest were the storage tank location in the airframe, the structural energy absorption following crash landing scenarios and the structural deformation of the structure surrounding the tanks, penetrating the survival space of the occupants. Several structural design arrangements were proposed and compared. Simulation results indicated that the optimal location for the fuel storage greatly depends on the actual aircraft layout as well as on the future civil aircraft airworthiness requirements that are still under development for that type of fuel energy source.</abstract><cop>Bristol</cop><pub>IOP Publishing</pub><doi>10.1088/1742-6596/2692/1/012049</doi><tpages>7</tpages><oa>free_for_read</oa></addata></record>
fulltext fulltext
identifier ISSN: 1742-6588
ispartof Journal of physics. Conference series, 2024-02, Vol.2692 (1), p.12049
issn 1742-6588
1742-6596
language eng
recordid cdi_proquest_journals_2924353863
source IOP Publishing Free Content; Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals; IOPscience extra; Alma/SFX Local Collection; Free Full-Text Journals in Chemistry
subjects Aircraft
Aircraft reliability
Airframes
Alternative fuels
Aviation
Aviation fuel
Crash landing
Crashworthiness
Design parameters
Energy absorption
Energy sources
Fuel cells
Fuel storage
Fuel tanks
Hydrogen
Hydrogen fuels
Hydrogen storage
Impact strength
Liquid hydrogen
Qualitative analysis
Storage tanks
Structural design
title Liquid Hydrogen Storage Tank Virtual Crashworthiness Design Exploration for Civil Aircraft
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-22T17%3A42%3A04IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_iop_j&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Liquid%20Hydrogen%20Storage%20Tank%20Virtual%20Crashworthiness%20Design%20Exploration%20for%20Civil%20Aircraft&rft.jtitle=Journal%20of%20physics.%20Conference%20series&rft.au=Gallois,%20A&rft.date=2024-02-01&rft.volume=2692&rft.issue=1&rft.spage=12049&rft.pages=12049-&rft.issn=1742-6588&rft.eissn=1742-6596&rft_id=info:doi/10.1088/1742-6596/2692/1/012049&rft_dat=%3Cproquest_iop_j%3E2924353863%3C/proquest_iop_j%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2924353863&rft_id=info:pmid/&rfr_iscdi=true