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dc.contributor.authorGalarza, Nekane
dc.contributor.authorRubio, Benjamin
dc.contributor.authorBERECIARTUA PÉREZ, ARANZAZU
dc.contributor.authorLozano, Ivan
dc.contributor.authorGascón, Jaime
dc.contributor.authorAtxaga, Garbiñe
dc.contributor.authorPEREZ, JOSE
dc.date.accessioned2020-07-28T15:03:39Z
dc.date.available2020-07-28T15:03:39Z
dc.date.issued2020-07
dc.identifier.citationGalarza, Nekane, Benjamin Rubio, ARANZAZU BERECIARTUA PÉREZ, Ivan Lozano, Jaime Gascón, Garbiñe Atxaga, and JOSE PEREZ. “ANÁLISIS DE TÉCNICAS DE VISIÓN ARTIFICIAL Y ULTRASONIDOS PARA LA INSPECCIÓN EN SERVICIO DE PIEZAS AERONAÚTICAS PRODUCIDAS POR FABRICACIÓN ADITIVA.” DYNA INGENIERIA E INDUSTRIA 95, no. 4 (2020): 371–375. doi:10.6036/9622.en
dc.identifier.issn0012-7361en
dc.identifier.urihttp://hdl.handle.net/11556/958
dc.description.abstractBionic Aircraft is a project founded under the framework H2020 and it is a result of a need to reduce emissions due to the impact of the growth of the aviation industry. The introduction of Additive Layer Manufacturing (ALM) to produce some metal aircraft parts is considered as an opportunity to address this issue. This technology allows to produce ultra-lightweight and highly complex parts (so-called "bionic parts"). One of the actions to consider in the project is the development of new Non-Destructive Technologies (NDT) strategies to inspect, in-service, parts produced by ALM made of Al-based alloys. This need arises because, ALM processes for these alloys are at low maturity level (Technology Readiness Level - TRL1) and hence, no proven and certified NDT methods are yet developed. Moreover, in-service inspection of aeronautic bionic parts involves challenges like the uncertainty of the inner inspection of a layered material, the lack of accessibility (the part is attached to the aircraft fuselage), and the unexpected defects under in-service conditions, something still under study. The objective of this work is to assess the inspection, in-service, of this kind of parts, by selecting and customizing the most suitable NDT methods, according to the type and maximum tolerable damage sizes estimated by a fatigue life prediction evaluation.en
dc.description.sponsorshipWe would like to thank European Commission for partially financing this research. The developments have been done in the project BIONIC AIRCRAFT, contract No: H2020-MG-2015-690689, under the H2020 framework programme.en
dc.language.isoengen
dc.publisherPublicaciones Dyna Slen
dc.titleON THE ANALYSIS OF COMPUTER VISION AND ULTRASOUND BASED TECHNIQUES FOR THE IN-SERVICE INSPECTION OF AERONAUTICS PARTS PRODUCED BY ADDITIVE LAYER MANUFACTURING (ALM)en
dc.title.alternativeANÁLISIS DE TÉCNICAS DE VISIÓN ARTIFICIAL Y ULTRASONIDOS PARA LA INSPECCIÓN EN SERVICIO DE PIEZAS AERONAÚTICAS PRODUCIDAS POR FABRICACIÓN ADITIVAen
dc.typearticleen
dc.identifier.doi10.6036/9622en
dc.relation.projectIDinfo:eu-repo/grantAgreement/EC/H2020/690689/EU/Increasing resource efficiency of aviation through implementation of ALM technology and bionic design in all stages of an aircraft life cycle/Bionic Aircraften
dc.rights.accessRightsopenAccessen
dc.subject.keywordsComputer visiónen
dc.subject.keywordsUltrasounden
dc.subject.keywordsAdditive manufacturingen
dc.subject.keywordsCracks and defects detectionen
dc.identifier.essn1989-1490en
dc.issue.number4en
dc.journal.titleDYNA INGENIERIA E INDUSTRIAen
dc.page.final375en
dc.page.initial371en
dc.volume.number95en


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