Flexible Composite Films Made of EMAA- Na+ Ionomer: Evaluation of the Influence of Piezoelectric Particles on the Thermal and Mechanical Properties

Detalhes bibliográficos
Autor(a) principal: Tita, Sandra P. S.
Data de Publicação: 2022
Outros Autores: Magalhães, Fernão D., Paiva, Diana, Bertochi, Maria A. Z., Teixeira, Guilhermina F., Pires, Ana L., Pereira, André M., Tarpani, José R.
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://dx.doi.org/10.3390/polym14132755
http://hdl.handle.net/11449/241677
Resumo: Studies that aim to produce flexible films of composite materials based on ionomers-PZT, and volume fractions lower than 10% PZT, in order to monitor damage in aeronautical structures are seldom investigated. The growing emphasis on the use of polymers capable of self-healing after damage or activation by heating has motivated the application of self-healing ionomers as polymeric matrices in composites with piezoelectric particles aiming to monitor damage. Flexible composite films were developed based on the self-healing polymer matrix Surlyn® 8940 ionomer (DuPont™ —Wilmington, DE, USA) and PZT particles (connectivity 2-3) in volume fractions of 1, 3, 5 and 7%, with thickness around 50–100 µm. The choice of PZT volume fractions followed the preliminary requirement that establishes a final density, which is lower or at least close to the density of the materials used in aeronautical structures. Since the application of composites based on epoxy resin/carbon fibers has been increasing in the aeronautical segment, this material (with density lower than 1500 kg/m3) was chosen as a reference for the present work. Thus, due to self-healing (a characteristic of the matrix Surlyn® 8940) combined with recyclability, high flexibility and low thickness, the flexible composite films showed advantages to be applied on aeronautical structures, which present complex geometries and low-density materials. The manufactured films were characterized by SEM, XRD, DMA and mechanical tensile tests. The results were discussed mainly in terms of the volume fraction of PZT. X-ray diffraction patterns showed coexistent rhombohedral and tetragonal phases in the PZT particles-dispersed composite, which can potentialize the alignment of ferroelectric domains during polarization under strong electrical field, enhancing dielectric and piezoelectric properties toward sensing applications. DMA and tensile testing results demonstrated that the addition of PZT particles did not impair either dynamic or quasi-static mechanical performance of the flexible composite films. It was concluded that the PZT volume fraction should be lower than 3% because, for higher values, the molecular mobility of the polymer would suffer significant reductions. These findings, combined with the high flexibility and low density of the ceramic particle-filled thermoplastic polymer, render the developed flexible composite film a very promising candidate for strain and damage sensing in aeronautical structures.
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spelling Flexible Composite Films Made of EMAA- Na+ Ionomer: Evaluation of the Influence of Piezoelectric Particles on the Thermal and Mechanical Propertiesdamage sensorflexible composite filmsflexible polymer films-PZTionomersStudies that aim to produce flexible films of composite materials based on ionomers-PZT, and volume fractions lower than 10% PZT, in order to monitor damage in aeronautical structures are seldom investigated. The growing emphasis on the use of polymers capable of self-healing after damage or activation by heating has motivated the application of self-healing ionomers as polymeric matrices in composites with piezoelectric particles aiming to monitor damage. Flexible composite films were developed based on the self-healing polymer matrix Surlyn® 8940 ionomer (DuPont™ —Wilmington, DE, USA) and PZT particles (connectivity 2-3) in volume fractions of 1, 3, 5 and 7%, with thickness around 50–100 µm. The choice of PZT volume fractions followed the preliminary requirement that establishes a final density, which is lower or at least close to the density of the materials used in aeronautical structures. Since the application of composites based on epoxy resin/carbon fibers has been increasing in the aeronautical segment, this material (with density lower than 1500 kg/m3) was chosen as a reference for the present work. Thus, due to self-healing (a characteristic of the matrix Surlyn® 8940) combined with recyclability, high flexibility and low thickness, the flexible composite films showed advantages to be applied on aeronautical structures, which present complex geometries and low-density materials. The manufactured films were characterized by SEM, XRD, DMA and mechanical tensile tests. The results were discussed mainly in terms of the volume fraction of PZT. X-ray diffraction patterns showed coexistent rhombohedral and tetragonal phases in the PZT particles-dispersed composite, which can potentialize the alignment of ferroelectric domains during polarization under strong electrical field, enhancing dielectric and piezoelectric properties toward sensing applications. DMA and tensile testing results demonstrated that the addition of PZT particles did not impair either dynamic or quasi-static mechanical performance of the flexible composite films. It was concluded that the PZT volume fraction should be lower than 3% because, for higher values, the molecular mobility of the polymer would suffer significant reductions. These findings, combined with the high flexibility and low density of the ceramic particle-filled thermoplastic polymer, render the developed flexible composite film a very promising candidate for strain and damage sensing in aeronautical structures.Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)Materials Engineering Department Sao Carlos School of Engineering University of Sao Paulo, Av. João Dagnone, SPLEPABE—Laboratory for Process Engineering Environment Biotechnology and Energy Faculty of Engineering University of Porto, Rua Dr. Roberto FriasALiCE—Associate Laboratory in Chemical Engineering Faculty of Engineering University of Porto, Rua Dr. Roberto FriasDepartment of Biochemistry and Chemical Technology Chemistry Institute State University of Sao Paulo, SPLABEL/FC—Laboratory of Bio-electrocatalysis and Fuel Cells Institute of Chemistry Federal University of Goias (UFG), GODepartment of Physics and Astronomy Faculty of Science Institute of Physics of Advanced Materials Nanotechnology and Nanophotonics (IFIMUP) University of Porto, Rua do Campo Alegre, 687CAPES: 001CNPq: 140296/2016-6Universidade de São Paulo (USP)University of PortoFederal University of Goias (UFG)Tita, Sandra P. S.Magalhães, Fernão D.Paiva, DianaBertochi, Maria A. Z.Teixeira, Guilhermina F.Pires, Ana L.Pereira, André M.Tarpani, José R.2023-03-01T21:16:22Z2023-03-01T21:16:22Z2022-07-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articlehttp://dx.doi.org/10.3390/polym14132755Polymers, v. 14, n. 13, 2022.2073-4360http://hdl.handle.net/11449/24167710.3390/polym141327552-s2.0-85133820116Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengPolymersinfo:eu-repo/semantics/openAccess2023-03-01T21:16:22Zoai:repositorio.unesp.br:11449/241677Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462023-03-01T21:16:22Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv Flexible Composite Films Made of EMAA- Na+ Ionomer: Evaluation of the Influence of Piezoelectric Particles on the Thermal and Mechanical Properties
title Flexible Composite Films Made of EMAA- Na+ Ionomer: Evaluation of the Influence of Piezoelectric Particles on the Thermal and Mechanical Properties
spellingShingle Flexible Composite Films Made of EMAA- Na+ Ionomer: Evaluation of the Influence of Piezoelectric Particles on the Thermal and Mechanical Properties
Tita, Sandra P. S.
damage sensor
flexible composite films
flexible polymer films-PZT
ionomers
title_short Flexible Composite Films Made of EMAA- Na+ Ionomer: Evaluation of the Influence of Piezoelectric Particles on the Thermal and Mechanical Properties
title_full Flexible Composite Films Made of EMAA- Na+ Ionomer: Evaluation of the Influence of Piezoelectric Particles on the Thermal and Mechanical Properties
title_fullStr Flexible Composite Films Made of EMAA- Na+ Ionomer: Evaluation of the Influence of Piezoelectric Particles on the Thermal and Mechanical Properties
title_full_unstemmed Flexible Composite Films Made of EMAA- Na+ Ionomer: Evaluation of the Influence of Piezoelectric Particles on the Thermal and Mechanical Properties
title_sort Flexible Composite Films Made of EMAA- Na+ Ionomer: Evaluation of the Influence of Piezoelectric Particles on the Thermal and Mechanical Properties
author Tita, Sandra P. S.
author_facet Tita, Sandra P. S.
Magalhães, Fernão D.
Paiva, Diana
Bertochi, Maria A. Z.
Teixeira, Guilhermina F.
Pires, Ana L.
Pereira, André M.
Tarpani, José R.
author_role author
author2 Magalhães, Fernão D.
Paiva, Diana
Bertochi, Maria A. Z.
Teixeira, Guilhermina F.
Pires, Ana L.
Pereira, André M.
Tarpani, José R.
author2_role author
author
author
author
author
author
author
dc.contributor.none.fl_str_mv Universidade de São Paulo (USP)
University of Porto
Federal University of Goias (UFG)
dc.contributor.author.fl_str_mv Tita, Sandra P. S.
Magalhães, Fernão D.
Paiva, Diana
Bertochi, Maria A. Z.
Teixeira, Guilhermina F.
Pires, Ana L.
Pereira, André M.
Tarpani, José R.
dc.subject.por.fl_str_mv damage sensor
flexible composite films
flexible polymer films-PZT
ionomers
topic damage sensor
flexible composite films
flexible polymer films-PZT
ionomers
description Studies that aim to produce flexible films of composite materials based on ionomers-PZT, and volume fractions lower than 10% PZT, in order to monitor damage in aeronautical structures are seldom investigated. The growing emphasis on the use of polymers capable of self-healing after damage or activation by heating has motivated the application of self-healing ionomers as polymeric matrices in composites with piezoelectric particles aiming to monitor damage. Flexible composite films were developed based on the self-healing polymer matrix Surlyn® 8940 ionomer (DuPont™ —Wilmington, DE, USA) and PZT particles (connectivity 2-3) in volume fractions of 1, 3, 5 and 7%, with thickness around 50–100 µm. The choice of PZT volume fractions followed the preliminary requirement that establishes a final density, which is lower or at least close to the density of the materials used in aeronautical structures. Since the application of composites based on epoxy resin/carbon fibers has been increasing in the aeronautical segment, this material (with density lower than 1500 kg/m3) was chosen as a reference for the present work. Thus, due to self-healing (a characteristic of the matrix Surlyn® 8940) combined with recyclability, high flexibility and low thickness, the flexible composite films showed advantages to be applied on aeronautical structures, which present complex geometries and low-density materials. The manufactured films were characterized by SEM, XRD, DMA and mechanical tensile tests. The results were discussed mainly in terms of the volume fraction of PZT. X-ray diffraction patterns showed coexistent rhombohedral and tetragonal phases in the PZT particles-dispersed composite, which can potentialize the alignment of ferroelectric domains during polarization under strong electrical field, enhancing dielectric and piezoelectric properties toward sensing applications. DMA and tensile testing results demonstrated that the addition of PZT particles did not impair either dynamic or quasi-static mechanical performance of the flexible composite films. It was concluded that the PZT volume fraction should be lower than 3% because, for higher values, the molecular mobility of the polymer would suffer significant reductions. These findings, combined with the high flexibility and low density of the ceramic particle-filled thermoplastic polymer, render the developed flexible composite film a very promising candidate for strain and damage sensing in aeronautical structures.
publishDate 2022
dc.date.none.fl_str_mv 2022-07-01
2023-03-01T21:16:22Z
2023-03-01T21:16:22Z
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://dx.doi.org/10.3390/polym14132755
Polymers, v. 14, n. 13, 2022.
2073-4360
http://hdl.handle.net/11449/241677
10.3390/polym14132755
2-s2.0-85133820116
url http://dx.doi.org/10.3390/polym14132755
http://hdl.handle.net/11449/241677
identifier_str_mv Polymers, v. 14, n. 13, 2022.
2073-4360
10.3390/polym14132755
2-s2.0-85133820116
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Polymers
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.source.none.fl_str_mv Scopus
reponame:Repositório Institucional da UNESP
instname:Universidade Estadual Paulista (UNESP)
instacron:UNESP
instname_str Universidade Estadual Paulista (UNESP)
instacron_str UNESP
institution UNESP
reponame_str Repositório Institucional da UNESP
collection Repositório Institucional da UNESP
repository.name.fl_str_mv Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)
repository.mail.fl_str_mv
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