Validation of the mechanical behavior of an aeronautical fixing turret produced by a design for additive manufacturing (DfAM)

Veiga Suárez, Fernando; Bhujangrao, Trunal; Suárez, Alfredo; Aldalur, Eider; Goenaga, Igor; Gil Hernández, Daniel

Publication:
Validation of the mechanical behavior of an aeronautical fixing turret produced by a design for additive manufacturing (DfAM)

dc.contributor.author	Veiga Suárez, Fernando
dc.contributor.author	Bhujangrao, Trunal
dc.contributor.author	Suárez, Alfredo
dc.contributor.author	Aldalur, Eider
dc.contributor.author	Goenaga, Igor
dc.contributor.author	Gil Hernández, Daniel
dc.contributor.department	Ingeniería	es_ES
dc.contributor.department	Ingeniaritza	eu
dc.date.accessioned	2023-01-17T09:15:25Z
dc.date.available	2023-01-17T09:15:25Z
dc.date.issued	2022
dc.date.updated	2023-01-17T09:09:15Z
dc.description.abstract	The 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.sponsorship	This 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.mimetype	application/pdf	en
dc.identifier.citation	Veiga, 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/polym14112177	en
dc.identifier.doi	10.3390/polym14112177
dc.identifier.issn	2073-4360
dc.identifier.uri	https://academica-e.unavarra.es/handle/2454/44582
dc.language.iso	eng	en
dc.publisher	MDPI	en
dc.relation.ispartof	Polymers 2022, 14, 2177	en
dc.relation.publisherversion	https://doi.org/10.3390/polym14112177
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) license	en
dc.rights.accessRights	Acceso abierto / Sarbide irekia	es
dc.rights.accessRights	info:eu-repo/semantics/openAccess	en
dc.rights.uri	http://creativecommons.org/licenses/by/4.0/
dc.subject	Additive manufacturing	en
dc.subject	Aeronautical fixture	en
dc.subject	DfAM	en
dc.subject	WAAM	en
dc.title	Validation of the mechanical behavior of an aeronautical fixing turret produced by a design for additive manufacturing (DfAM)	en
dc.type	Artículo / Artikulua	es
dc.type	info:eu-repo/semantics/article	en
dc.type.version	Versión publicada / Argitaratu den bertsioa	es
dc.type.version	info:eu-repo/semantics/publishedVersion	en
dspace.entity.type	Publication
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