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Evaluation methods of out-of-autoclave epoxy prepreg working life used in aerospace application

dc.contributor.authorde Faria Gonzales Leal, Tanila Penteado [UNESP]
dc.contributor.authorde Paula Santos, Luis Felipe [UNESP]
dc.contributor.authorLeali Costa, Michelle [UNESP]
dc.contributor.authorBotelho, Edson Cocchieri [UNESP]
dc.contributor.institutionEmbraer
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)
dc.contributor.institutionInstituto de Pesquisas Tecnológicas do Estado de São Paulo-IPT
dc.date.accessioned2025-04-29T20:16:00Z
dc.date.issued2024-01-01
dc.description.abstractPrepregs are highly dependent on the resin, its chemical composition, and physical properties. Resin is the perishable part of prepreg materials and usually requires controlled storage, otherwise, its processability and properties may be affected. Oven curing prepregs are recognized to have longer life out of the freezer than those designed to cure in autoclave, and one of them, prepreg 2511, is the focus of this research. Prepreg 2511 has a formal out-time limit of 28 days at clean room environment (23°C/50% relative humidity), and 24 months shelf life, when frozen at −18°C, while common prepreg designed to be cured in autoclave, usually have 15 days of out-time and 12 months of shelf-life. It is known that the real shelf life and out time of epoxy-based materials tends to be longer than suppliers’ recommendation. Aiming to assess 2511 performance after those 28 days of exposure to clean room ambient, during and after 24 months in freezer; the material was exposed to this environmental condition for more than 28 days and tested periodically using different methods, including, Differential Scanning Calorimeter, High-Performance Liquid Chromatography tack, among others. In resume, the goal of this research was to identify 2511 longest out life without losing its properties and which of the tests used during these experiments would be more sensitive to capture its aging.en
dc.description.affiliationResearch and Development Materials Engineering Department Embraer, São Paulo
dc.description.affiliationMaterials and Technology Department School of Science and Engineering São Paulo State University (UNESP)
dc.description.affiliationLightweight Structures Laboratory – LEL Instituto de Pesquisas Tecnológicas do Estado de São Paulo-IPT
dc.description.affiliationUnespMaterials and Technology Department School of Science and Engineering São Paulo State University (UNESP)
dc.format.extent1784-1797
dc.identifierhttp://dx.doi.org/10.1080/10426914.2024.2334679
dc.identifier.citationMaterials and Manufacturing Processes, v. 39, n. 12, p. 1784-1797, 2024.
dc.identifier.doi10.1080/10426914.2024.2334679
dc.identifier.issn1532-2475
dc.identifier.issn1042-6914
dc.identifier.scopus2-s2.0-85189608461
dc.identifier.urihttps://hdl.handle.net/11449/309591
dc.language.isoeng
dc.relation.ispartofMaterials and Manufacturing Processes
dc.sourceScopus
dc.subjectout life
dc.subjectOut-of-autoclave prepreg
dc.subjectphysical-chemical properties
dc.subjectthermal properties
dc.subjectthermosetting resin
dc.titleEvaluation methods of out-of-autoclave epoxy prepreg working life used in aerospace applicationen
dc.typeArtigopt
dspace.entity.typePublication

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