Show simple item record

dc.contributor.authorVeiga, Fernando
dc.contributor.authorBhujangrao, Trunal
dc.contributor.authorSuárez, Alfredo
dc.contributor.authorAldalur, Eider
dc.contributor.authorGoenaga, Igor
dc.contributor.authorGil-Hernandez, Daniel
dc.date.accessioned2022-09-12T12:43:00Z
dc.date.available2022-09-12T12:43:00Z
dc.date.issued2022-05-27
dc.identifier.citationVeiga, Fernando, Trunal Bhujangrao, Alfredo Suárez, Eider Aldalur, Igor Goenaga, and Daniel Gil-Hernandez. 2022. "Validation of the Mechanical Behavior of an Aeronautical Fixing Turret Produced by a Design for Additive Manufacturing (DfAM)" Polymers 14, no. 11: 2177. https://doi.org/10.3390/polym14112177en
dc.identifier.urihttp://hdl.handle.net/11556/1402
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 useen
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.language.isoengen
dc.publisherMultidisciplinary Digital Publishing Institute (MDPI)en
dc.rightsAttribution 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/*
dc.titleValidation of the Mechanical Behavior of an Aeronautical Fixing Turret Produced by a Design for Additive Manufacturing (DfAM)en
dc.typearticleen
dc.identifier.doi10.3390/polym14112177en
dc.rights.accessRightsopenAccessen
dc.subject.keywordsAeronautical fixtureen
dc.subject.keywordsWAAMen
dc.subject.keywordsDfAMen
dc.subject.keywordsAdditive manufacturingen
dc.identifier.essn2073-4360en
dc.issue.number11en
dc.journal.titlePolymersen
dc.page.initial2177en
dc.volume.number14en


Files in this item

Thumbnail

    Show simple item record

    Attribution 4.0 InternationalExcept where otherwise noted, this item's license is described as Attribution 4.0 International