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dc.creatorVeiga Suárez, Fernandoes_ES
dc.creatorBhujangrao, Trunales_ES
dc.creatorSuárez, Alfredoes_ES
dc.creatorAldalur, Eideres_ES
dc.creatorGoenaga, Igores_ES
dc.creatorGil Hernández, Danieles_ES
dc.date.accessioned2023-01-17T09:15:25Z
dc.date.available2023-01-17T09:15:25Z
dc.date.issued2022
dc.identifier.citationVeiga, F., Bhujangrao, T., Suárez, A., Aldalur, E., Goenaga, I., & Gil-Hernandez, D. (2022). Validation of the Mechanical Behavior of an Aeronautical Fixing Turret Produced by a Design for Additive Manufacturing (DfAM). Polymers, 14(11), 2177. https://doi.org/10.3390/polym14112177en
dc.identifier.issn2073-4360
dc.identifier.urihttps://hdl.handle.net/2454/44582
dc.description.abstractThe design of parts in such critical sectors as the manufacturing of aeronautical parts is awaiting a paradigm shift due to the introduction of additive manufacturing technologies. The manufacture of parts designed by means of the design-oriented additive manufacturing methodology (DfAM) has acquired great relevance in recent years. One of the major gaps in the application of these technologies is the lack of studies on the mechanical behavior of parts manufactured using this methodology. This paper focuses on the manufacture of a turret for the clamping of parts for the aeronautical industry. The design of the lightened turret by means of geometry optimization, the manufacture of the turret in polylactic acid (PLA) and 5XXX series aluminum alloy by means of Wire Arc Additive Manufacturing (WAAM) technology and the analysis by means of finite element analysis (FEA) with its validation by means of a tensile test are presented. The behavior of the part manufactured with both materials is compared. The conclusion allows to establish which are the limitations of the part manufactured in PLA for its orientation to the final application, whose advantages are its lower weight and cost. This paper is novel as it presents a holistic view that covers the process in an integrated way from the design and manufacture to the behaviour of the component in use.en
dc.description.sponsorshipThis project has received funding from the ELKARTEK program of the Basque Government (Project VIRTUA3D, under Contract nº KK-2022/00025) and HAZITEK (Project ADDHOC, under Contract nº ZL-2022/00665).en
dc.format.mimetypeapplication/pdfen
dc.language.isoengen
dc.publisherMDPIen
dc.relation.ispartofPolymers 2022, 14, 2177en
dc.rights© 2022 by the authors. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) licenseen
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectAdditive manufacturingen
dc.subjectAeronautical fixtureen
dc.subjectDfAMen
dc.subjectWAAMen
dc.titleValidation of the mechanical behavior of an aeronautical fixing turret produced by a design for additive manufacturing (DfAM)en
dc.typeArtículo / Artikuluaes
dc.typeinfo:eu-repo/semantics/articleen
dc.date.updated2023-01-17T09:09:15Z
dc.contributor.departmentIngenieríaes_ES
dc.contributor.departmentIngeniaritzaeu
dc.rights.accessRightsAcceso abierto / Sarbide irekiaes
dc.rights.accessRightsinfo:eu-repo/semantics/openAccessen
dc.identifier.doi10.3390/polym14112177
dc.relation.publisherversionhttps://doi.org/10.3390/polym14112177
dc.type.versionVersión publicada / Argitaratu den bertsioaes
dc.type.versioninfo:eu-repo/semantics/publishedVersionen


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© 2022 by the authors. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license
Except where otherwise noted, this item's license is described as © 2022 by the authors. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license

El Repositorio ha recibido la ayuda de la Fundación Española para la Ciencia y la Tecnología para la realización de actividades en el ámbito del fomento de la investigación científica de excelencia, en la Línea 2. Repositorios institucionales (convocatoria 2020-2021).
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