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

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 acquire...

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Autores: Veiga Suárez, Fernando, Bhujangrao, Trunal, Suárez, Alfredo, Aldalur, Eider, Goenaga, Igor, Gil Hernández, Daniel
Tipo de recurso: artículo
Estado:Versión publicada
Fecha de publicación:2022
País:España
Institución:Universidad Pública de Navarra
Repositorio:Academica-e. Repositorio Institucional de la Universidad Pública de Navarra
OAI Identifier:oai:academica-e.unavarra.es:2454/44582
Acceso en línea:https://hdl.handle.net/2454/44582
Access Level:acceso abierto
Palabra clave:Additive manufacturing
Aeronautical fixture
DfAM
WAAM
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spelling Validation of the mechanical behavior of an aeronautical fixing turret produced by a design for additive manufacturing (DfAM)Veiga Suárez, FernandoBhujangrao, TrunalSuárez, AlfredoAldalur, EiderGoenaga, IgorGil Hernández, DanielAdditive manufacturingAeronautical fixtureDfAMWAAMThe 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.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).MDPIIngenieríaIngeniaritza2022info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionapplication/pdfhttps://hdl.handle.net/2454/44582reponame:Academica-e. Repositorio Institucional de la Universidad Pública de Navarrainstname:Universidad Pública de NavarraInglés© 2022 by the authors. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) licensehttps://creativecommons.org/licenses/by/4.0/info:eu-repo/semantics/openAccessoai:academica-e.unavarra.es:2454/445822026-06-17T12:41:47Z
dc.title.none.fl_str_mv Validation of the mechanical behavior of an aeronautical fixing turret produced by a design for additive manufacturing (DfAM)
title Validation of the mechanical behavior of an aeronautical fixing turret produced by a design for additive manufacturing (DfAM)
spellingShingle Validation of the mechanical behavior of an aeronautical fixing turret produced by a design for additive manufacturing (DfAM)
Veiga Suárez, Fernando
Additive manufacturing
Aeronautical fixture
DfAM
WAAM
title_short Validation of the mechanical behavior of an aeronautical fixing turret produced by a design for additive manufacturing (DfAM)
title_full Validation of the mechanical behavior of an aeronautical fixing turret produced by a design for additive manufacturing (DfAM)
title_fullStr Validation of the mechanical behavior of an aeronautical fixing turret produced by a design for additive manufacturing (DfAM)
title_full_unstemmed Validation of the mechanical behavior of an aeronautical fixing turret produced by a design for additive manufacturing (DfAM)
title_sort Validation of the mechanical behavior of an aeronautical fixing turret produced by a design for additive manufacturing (DfAM)
dc.creator.none.fl_str_mv Veiga Suárez, Fernando
Bhujangrao, Trunal
Suárez, Alfredo
Aldalur, Eider
Goenaga, Igor
Gil Hernández, Daniel
author Veiga Suárez, Fernando
author_facet Veiga Suárez, Fernando
Bhujangrao, Trunal
Suárez, Alfredo
Aldalur, Eider
Goenaga, Igor
Gil Hernández, Daniel
author_role author
author2 Bhujangrao, Trunal
Suárez, Alfredo
Aldalur, Eider
Goenaga, Igor
Gil Hernández, Daniel
author2_role author
author
author
author
author
dc.contributor.none.fl_str_mv Ingeniería
Ingeniaritza
dc.subject.none.fl_str_mv Additive manufacturing
Aeronautical fixture
DfAM
WAAM
topic Additive manufacturing
Aeronautical fixture
DfAM
WAAM
description 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.
publishDate 2022
dc.date.none.fl_str_mv 2022
dc.type.none.fl_str_mv info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
format article
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dc.identifier.none.fl_str_mv https://hdl.handle.net/2454/44582
url https://hdl.handle.net/2454/44582
dc.language.none.fl_str_mv Inglés
language_invalid_str_mv Inglés
dc.rights.none.fl_str_mv https://creativecommons.org/licenses/by/4.0/
info:eu-repo/semantics/openAccess
rights_invalid_str_mv https://creativecommons.org/licenses/by/4.0/
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv MDPI
publisher.none.fl_str_mv MDPI
dc.source.none.fl_str_mv reponame:Academica-e. Repositorio Institucional de la Universidad Pública de Navarra
instname:Universidad Pública de Navarra
instname_str Universidad Pública de Navarra
reponame_str Academica-e. Repositorio Institucional de la Universidad Pública de Navarra
collection Academica-e. Repositorio Institucional de la Universidad Pública de Navarra
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