Hot stamping of aerospace aluminium alloys: Automotive technologies for the aeronautics industry

dc.contributor.authorAtxaga, G.
dc.contributor.authorArroyo, A.
dc.contributor.authorCanflanca, B.
dc.contributor.institutionEXTREMAT
dc.contributor.institutionPROMETAL
dc.contributor.institutionSG
dc.date.issued2022-09
dc.descriptionPublisher Copyright: © 2022 The Society of Manufacturing Engineers
dc.description.abstractThis paper proposes the use of the hot stamping process that provides ready to use parts for the obtention of aircraft components as an alternative manufacturing technology to e.g. machined parts. The development has been focused on the study of the high temperature formability of aluminium alloys. The feasibility of hot forming the AA2198 aluminium‑lithium alloy into complex shapes component has been studied. A wide experimental campaign has been carried out to set up the optimum hot stamping process parameters. In addition, forming trials with different geometries (omega and B-pillar shapes) have also been performed and, after the corresponding heat treatment, material properties have been recovered. Simulations of the hot stamping process have been carried out with Pamstamp® 2G software. These results have been correlated with the ones obtained in the experimental campaign. As a final step of the development, a demonstrator corresponding to a wing rib has been successfully manufactured. Characterization carried out to the prototype indicate specifications are fulfilled.en
dc.description.sponsorshipThe study presented in this paper was carried out in the frame of OUTCOME project within Airframe ITD of Clean Sky 2 Programme. The project received funding from the Clean Sky 2 Joint Undertaking (JU) under ITD Airframe Grant Agreement for Members. The JU received support from the European Union's Horizon 2020 (H2020) research and innovation programme and the Clean Sky 2 JU members other than the Union. The authors want to acknowledge Airbus Defence and Space S.A.U for providing the design of the developed prototype, Aernnova Aerospace S.A.U for OUTCOME project coordination and facilitator and fruitful technical discussions and RIB-ON Consortium for developing and building the die and final manufacturing of the wing ribs. The study presented in this paper was carried out in the frame of OUTCOME project within Airframe ITD of Clean Sky 2 Programme. The project received funding from the Clean Sky 2 Joint Undertaking (JU) under ITD Airframe Grant Agreement for Members. The JU received support from the European Union's Horizon 2020 (H2020) research and innovation programme and the Clean Sky 2 JU members other than the Union.
dc.description.statusPeer reviewed
dc.format.extent11
dc.identifier.citationAtxaga , G , Arroyo , A & Canflanca , B 2022 , ' Hot stamping of aerospace aluminium alloys : Automotive technologies for the aeronautics industry ' , Journal of Manufacturing Processes , vol. 81 , pp. 817-827 . https://doi.org/10.1016/j.jmapro.2022.07.032
dc.identifier.doi10.1016/j.jmapro.2022.07.032
dc.identifier.issn1526-6125
dc.identifier.otherresearchoutputwizard: 11556/1388
dc.identifier.urlhttp://www.scopus.com/inward/record.url?scp=85134880880&partnerID=8YFLogxK
dc.language.isoeng
dc.relation.ispartofJournal of Manufacturing Processes
dc.relation.projectIDAirbus Defence and Space S.A.U
dc.relation.projectIDHorizon 2020 Framework Programme, H2020, 945521
dc.relation.projectIDEuropean Commission, EC
dc.rightsinfo:eu-repo/semantics/restrictedAccess
dc.subject.keywordsAeronautics
dc.subject.keywordsAl-li alloys
dc.subject.keywordsAluminium
dc.subject.keywordsFE process modeling
dc.subject.keywordsHot forming
dc.subject.keywordsHot stamping
dc.subject.keywordsAluminium
dc.subject.keywordsAl-li alloys
dc.subject.keywordsHot stamping
dc.subject.keywordsHot forming
dc.subject.keywordsAeronautics
dc.subject.keywordsFE process modeling
dc.subject.keywordsStrategy and Management
dc.subject.keywordsManagement Science and Operations Research
dc.subject.keywordsIndustrial and Manufacturing Engineering
dc.subject.keywordsSDG 9 - Industry, Innovation, and Infrastructure
dc.subject.keywordsProject ID
dc.subject.keywordsinfo:eu-repo/grantAgreement/EC/H2020/945521/EU/AIRFRAME ITD/GAM-2020-AIR
dc.subject.keywordsinfo:eu-repo/grantAgreement/EC/H2020/945521/EU/AIRFRAME ITD/GAM-2020-AIR
dc.subject.keywordsFunding Info
dc.subject.keywordsThe study presented in this paper was carried out in the frame of_x000D_ OUTCOME project within Airframe ITD of Clean Sky 2 Programme. The_x000D_ project received funding from the Clean Sky 2 Joint Undertaking (JU)_x000D_ under ITD Airframe Grant Agreement for Members. The JU received_x000D_ support from the European Union's Horizon 2020 (H2020) research and_x000D_ innovation programme and the Clean Sky 2 JU members other than the_x000D_ Union._x000D_ The authors want to acknowledge Airbus Defence and Space S.A.U_x000D_ for providing the design of the developed prototype, Aernnova Aero-_x000D_ space S.A.U for OUTCOME project coordination and facilitator and_x000D_ fruitful technical discussions and RIB-ON Consortium for developing_x000D_ and building the die and final manufacturing of the wing ribs
dc.subject.keywordsThe study presented in this paper was carried out in the frame of_x000D_ OUTCOME project within Airframe ITD of Clean Sky 2 Programme. The_x000D_ project received funding from the Clean Sky 2 Joint Undertaking (JU)_x000D_ under ITD Airframe Grant Agreement for Members. The JU received_x000D_ support from the European Union's Horizon 2020 (H2020) research and_x000D_ innovation programme and the Clean Sky 2 JU members other than the_x000D_ Union._x000D_ The authors want to acknowledge Airbus Defence and Space S.A.U_x000D_ for providing the design of the developed prototype, Aernnova Aero-_x000D_ space S.A.U for OUTCOME project coordination and facilitator and_x000D_ fruitful technical discussions and RIB-ON Consortium for developing_x000D_ and building the die and final manufacturing of the wing ribs
dc.titleHot stamping of aerospace aluminium alloys: Automotive technologies for the aeronautics industryen
dc.typejournal article
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