Publication:
Modeling of cutting force and final thickness for low stiffness 2024-T3 aluminum alloy part milling considering its geometry and fixtures

dc.contributor.authorCasuso, Mikel
dc.contributor.authorRubio Mateos, Antonio
dc.contributor.authorVeiga Suárez, Fernando
dc.contributor.authorLamikiz, Aitzol
dc.contributor.departmentIngenieríaes_ES
dc.contributor.departmentIngeniaritzaeu
dc.date.accessioned2023-03-27T10:35:33Z
dc.date.available2023-03-27T10:35:33Z
dc.date.issued2022
dc.date.updated2023-03-27T10:28:08Z
dc.description.abstractThe aeronautic industry is facing many challenges regarding the lifetime, weight and accuracy that aircraft skins must comply to meet stringent structural and aerodynamic requirements. Currently, mechanical milling of aircraft skin parts of 2024-T3 aluminum alloy is displacing the highly pollutant chemical milling. Consequently, flexible and reconfigurable vacuum holding fixtures are being increasingly employed, because they are adaptable to several part geometries, but, since their rigidity is extremely reduced, the low stiffness of parts limits severely their deployment. Aiming to harness the full potential of these holding systems for aluminum alloy skin parts, a complete analysis of final thickness achieved and cutting force is developed. Thin floor parts of different geometries are pocket milled, simply screwed at their corners, emulating a skin part supported by four vacuum cups. Process forces are continuously monitored, and final thickness is measured. It has been proven that the reduction of mass and stiffness during milling causes a corresponding reduction of the natural frequencies of the parts. Also, as long as natural frequencies are not excited, final thickness error is almost constant and not affected by the tool position, but only by the initial geometry and fixtures distribution of the part. Additionally, a new cutting force model for skin parts is empirically calculated. Unlike models designed for fully supported parts, this model is designed for skins held in flexible fixtures. It has a relative error of 5.6% and it allows to optimize the trajectory, geometry and support distribution, thus boosting the use of flexible fixtures.en
dc.description.sponsorshipFinancial support from the Basque Government under the ELKARTEK Program (EKOHEGAZ project, grant number KK-2021/00092) is gratefully acknowledged by the authors.en
dc.format.mimetypeapplication/pdfen
dc.identifier.citationCasuso, M., Rubio-Mateos, A., Veiga, F., Lamikiz, A. (2022) Modeling of cutting force and final thickness for low stiffness 2024-T3 aluminum alloy part milling considering its geometry and fixtures. Journal of Materials Research and Technology, 21, 2416-2427. https://doi.org/10.1016/j.jmrt.2022.10.070.en
dc.identifier.doi10.1016/j.jmrt.2022.10.070
dc.identifier.issn2238-7854
dc.identifier.urihttps://academica-e.unavarra.es/handle/2454/44958
dc.language.isoengen
dc.publisherElsevieren
dc.relation.ispartofJournal of Materials Research and Technology 2022 ; 21: 2416-2427en
dc.relation.publisherversionhttps://doi.org/10.1016/j.jmrt.2022.10.070
dc.rights© 2022 The Author(s). This is an open access article under the CC BY-NC-ND license.en
dc.rights.accessRightsAcceso abierto / Sarbide irekiaes
dc.rights.accessRightsinfo:eu-repo/semantics/openAccessen
dc.rights.urihttp:// creativecommons.org/licenses/by-nc-nd/4.0/
dc.subjectAA 2024 T3 aluminum alloyen
dc.subjectForce modelingen
dc.subjectThin flooren
dc.subjectThin parts millingen
dc.titleModeling of cutting force and final thickness for low stiffness 2024-T3 aluminum alloy part milling considering its geometry and fixturesen
dc.typeArtículo / Artikuluaes
dc.typeinfo:eu-repo/semantics/articleen
dc.type.versionVersión publicada / Argitaratu den bertsioaes
dc.type.versioninfo:eu-repo/semantics/publishedVersionen
dspace.entity.typePublication
relation.isAuthorOfPublication2b7b0dc3-53e2-4710-b104-17eea797eeff
relation.isAuthorOfPublication.latestForDiscovery2b7b0dc3-53e2-4710-b104-17eea797eeff

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