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A review on the development and properties of continuous fiber/epoxy/aluminum hybrid composites for aircraft structures

dc.contributor.authorBotelho, Edson Cocchieri [UNESP]
dc.contributor.authorSilva, Rogério Almeida
dc.contributor.authorPardini, Luiz Cláudio
dc.contributor.authorRezende, Mirabel Cerqueira
dc.contributor.institutionCTA
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.contributor.institutionEmpresa Brasileira de Aeronáutica - EMBRAER
dc.date.accessioned2014-05-27T11:21:54Z
dc.date.available2014-05-27T11:21:54Z
dc.date.issued2006-07-01
dc.description.abstractWeight reduction and improved damage tolerance characteristics were the prime drivers to develop new family of materials for the aerospace/ aeronautical industry. Aiming this objective, a new lightweight Fiber/ Metal Laminate (FML) has been developed. The combination of metal and polymer composite laminates can create a synergistic effect on many properties. The mechanical properties of FML shows improvements over the properties of both aluminum alloys and composite materials individually. Due to their excellent properties, FML are being used as fuselage skin structures of the next generation commercial aircrafts. One of the advantages of FML when compared with conventional carbon fiber/epoxy composites is the low moisture absorption. The moisture absorption in FML composites is slower when compared with polymer composites, even under the relatively harsh conditions, due to the barrier of the aluminum outer layers. Due to this favorable atmosphere, recently big companies such as EMBRAER, Aerospatiale, Boing, Airbus, and so one, starting to work with this kind of materials as an alternative to save money and to guarantee the security of their aircrafts.en
dc.description.affiliationDivisão de Materiais Instituto de Aeronáutica e Espaço CTA, São José dos Campos, São Paulo
dc.description.affiliationFatigue and Aeronautic Material Research Group Department of Material and Technology UNESP, Guaratingueta, Sao Paulo
dc.description.affiliationDepartamento de Engenharia Mecânica e Aeronáutica ITA CTA, São José dos Campos, 12228-904 São Paulo
dc.description.affiliationEmpresa Brasileira de Aeronáutica - EMBRAER, São José dos Campos, 12228-904 São Paulo
dc.description.affiliationUnespFatigue and Aeronautic Material Research Group Department of Material and Technology UNESP, Guaratingueta, Sao Paulo
dc.format.extent247-256
dc.identifierhttp://dx.doi.org/10.1590/S1516-14392006000300002
dc.identifier.citationMaterials Research, v. 9, n. 3, p. 247-256, 2006.
dc.identifier.doi10.1590/S1516-14392006000300002
dc.identifier.file2-s2.0-33750506111.pdf
dc.identifier.issn1516-1439
dc.identifier.lattes4378078337343660
dc.identifier.orcid0000-0001-8338-4879
dc.identifier.scieloS1516-14392006000300002
dc.identifier.scopus2-s2.0-33750506111
dc.identifier.urihttp://hdl.handle.net/11449/68952
dc.language.isoeng
dc.relation.ispartofMaterials Research
dc.relation.ispartofjcr1.103
dc.relation.ispartofsjr0,398
dc.rights.accessRightsAcesso aberto
dc.sourceScopus
dc.subjectComposite materials
dc.subjectFiber metal laminate
dc.subjectMechanical properties
dc.subjectAluminum alloys
dc.subjectEpoxy resins
dc.subjectLaminated composites
dc.subjectPolymers
dc.subjectAircraft structures
dc.subjectContinuous hybrid composites
dc.subjectSynergistic effect
dc.subjectAircraft materials
dc.titleA review on the development and properties of continuous fiber/epoxy/aluminum hybrid composites for aircraft structuresen
dc.typeArtigo
dcterms.licensehttp://www.scielo.br/revistas/mr/iaboutj.htm
dspace.entity.typePublication
unesp.author.lattes4378078337343660[1]
unesp.author.orcid0000-0001-8338-4879[1]
unesp.campusUniversidade Estadual Paulista (UNESP), Faculdade de Engenharia, Guaratinguetápt
unesp.departmentMateriais e Tecnologia - FEGpt

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