Electrospun piezoelectric polymer nanofiber layers for enabling in situ measurement in high-performance composite laminates

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dc.contributor.author Lotfian, Saeid
dc.contributor.author Giraudmaillet, Claire
dc.contributor.author Yoosefinejad, Ata
dc.contributor.author Thakur, Vijay Kumar
dc.contributor.author Hamed, Yazdani Nezhad
dc.date.accessioned 2018-09-04T09:08:33Z
dc.date.available 2018-09-04T09:08:33Z
dc.date.issued 2018-08-09
dc.identifier.citation Saeid Lotfian, Claire Giraudmaillet, Ata Yoosefinejad, et al., Electrospun piezoelectric polymer nanofiber layers for enabling in situ measurement in high-performance composite laminates. ACS Omega, Volume 3, Issue 8, pp8891-8902 en_UK
dc.identifier.issn 2470-1343
dc.identifier.uri https://doi.org/10.1021/acsomega.8b00940
dc.identifier.uri https://dspace.lib.cranfield.ac.uk/handle/1826/13455
dc.description.abstract This article highlights the effects from composite manufacturing parameters on fiber-reinforced composite laminates modified with layers of piezoelectric thermoplastic nanofibers and a conductive electrode layer. Such modifications have been used for enabling in situ deformation measurement in high-performance aerospace and renewable energy composites. Procedures for manufacturing high-performance composites are well-known and standardized. However, this does not imply that modifications via addition of functional layers (e.g., piezoelectric nanofibers) while following the same manufacturing procedures can lead to a successful multifunctional composite structure (e.g., for enabling in situ measurement). This article challenges success of internal embedment of piezoelectric nanofibers in standard manufacturing of high-performance composites via relying on composite process specifications and parameters only. It highlights that the process parameters must be revised for manufacturing of multifunctional composites. Several methods have been used to lay up and manufacture composites such as electrospinning the thermoplastic nanofibers, processing an inter digital electrode (IDE) made by conductive epoxy–graphene resin, and prepreg autoclave manufacturing aerospace grade laminates. The purpose of fabrication of IDE was to use a resin type (HexFlow RTM6) for the conductive layer similar to that used for the composite. Thereby, material mismatch is avoided and the structural integrity is sustained via mitigation of downgrading effects on the interlaminar properties. X-ray diffraction, Fourier transform infrared spectroscopy, energy dispersive X-ray spectroscopy, and scanning electron microscopy analyses have been carried out in the material characterization phase. Pulsed thermography and ultrasonic C-scanning were used for the localization of conductive resin embedded within the composite laminates. This study also provides recommendations for enabling internally embedded piezoelectricity (and thus health-monitoring capabilities) in high-performance composite laminates. en_UK
dc.language.iso en en_UK
dc.publisher American Chemical Society en_UK
dc.rights Attribution 4.0 International *
dc.rights.uri http://creativecommons.org/licenses/by/4.0/ *
dc.subject Carbon-based materials en_UK
dc.subject Composites en_UK
dc.subject Crystal structure en_UK
dc.subject Diffraction en_UK
dc.subject Electric properties en_UK
dc.subject Epoxy resins en_UK
dc.subject Fibers en_UK
dc.subject Fluoropolymers en_UK
dc.subject Mechanical properties en_UK
dc.subject Piezoelectricity and Thermoelectricity en_UK
dc.subject Polymer morphology en_UK
dc.subject Solid state electrochemistry en_UK
dc.subject Spectra en_UK
dc.subject Thermal properties en_UK
dc.title Electrospun piezoelectric polymer nanofiber layers for enabling in situ measurement in high-performance composite laminates en_UK
dc.type Article en_UK


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