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Development of a prototype test system for certification of curved fuselage panels

dc.creatorJiménez, Migueles
dc.creatorCabrera, R.es
dc.creatorArmario, J.L.es
dc.creatorGraciani Díaz, Enriquees
dc.creatorEstefani Morales, Alejandroes
dc.creatorMuñoz, Kirsaes
dc.creatorGarcía, Eduardo Higuerases
dc.creatorParís Carballo, Federicoes
dc.date.accessioned2021-03-09T15:42:33Z
dc.date.available2021-03-09T15:42:33Z
dc.date.issued2021-01
dc.identifier.citationJiménez, M., Cabrera, R., Armario, J.L., Graciani Díaz, E., Estefani Morales, A., Muñoz, K.,...,París Carballo, F. (2021). Development of a prototype test system for certification of curved fuselage panels. En 10th EASN International Conference on Innovation in Aviation and Space to the Satisfaction of the European Citizens, IOP Conference Series: Materials Science and Engineering, Vol. 1024, Issue 1,(012081), Virtual, Online: IOP Publishing Ltd.
dc.identifier.issn1757-8981es
dc.identifier.urihttps://hdl.handle.net/11441/105812
dc.descriptionVolume 1024, Issue 1 Article number 012081es
dc.description.abstractA prototype test system with capacity to reproduce combined loads representative of real loading cases of a curved fuselage panel has been developed. This prototype test system allows the structural validation of curved fuselage panels to be accomplished. The developed system is able to apply combined mechanical and pressurization loading states under quasi-static and dynamic loading conditions. It has been designed using CAD models and calculated with the aid of Finite Element models to ensure its integrity. A data acquisition system synchronized with a control system enables real time monitoring of test parameters.es
dc.description.sponsorshipHorizonte 2020 (Unión Europea) CS2-AIR-GAM-2014-2015-01es
dc.formatapplication/pdfes
dc.format.extent8 p.es
dc.language.isoenges
dc.publisherIOP Publishing Ltdes
dc.relation.ispartof10th EASN International Conference on Innovation in Aviation and Space to the Satisfaction of the European Citizens, (2021), IOP Conference Series: Materials Science and Engineering, Vol. 1024, Issue 1, pp. 012081.
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 Internacional*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/*
dc.subjectAircraft Propulsiones
dc.subjectFly by Wire Controles
dc.subjectBlended-wing-body Configurationses
dc.titleDevelopment of a prototype test system for certification of curved fuselage panelses
dc.typeinfo:eu-repo/semantics/conferenceObjectes
dcterms.identifierhttps://ror.org/03yxnpp24
dc.type.versioninfo:eu-repo/semantics/publishedVersiones
dc.rights.accessRightsinfo:eu-repo/semantics/openAccesses
dc.contributor.affiliationUniversidad de Sevilla. Departamento de Mecánica de Medios Continuos y Teoría de Estructurases
dc.relation.projectIDCS2-AIR-GAM-2014-2015-01es
dc.relation.publisherversionhttps://iopscience.iop.org/article/10.1088/1757-899X/1024/1/012081es
dc.identifier.doi10.1088/1757-899X/1024/1/012081es
dc.contributor.groupUniversidad de Sevilla. TEP-131: Elasticidad y Resistencia de Materialeses
dc.publication.initialPage012081es
dc.eventtitle10th EASN International Conference on Innovation in Aviation and Space to the Satisfaction of the European Citizens,es
dc.eventinstitutionVirtual, Onlinees

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