Development of recyclable Fibre Metal Laminates (FML), their mechanical characterization and FE modelling, aiming at structural application in aeronautics
This study concerns with the optimisation of a fibre-reinforced composite material ply book and application to an aeronautical component. The presented material solution is a recyclable FML (Fibre Metal Laminate). Recyclable and structural PMCs (Polymeric Matrix Composites) developed up-to now...
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Format: | Article |
Language: | English |
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EDP Sciences
2021-01-01
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Series: | MATEC Web of Conferences |
Online Access: | https://www.matec-conferences.org/articles/matecconf/pdf/2021/18/matecconf_iceaf2021_01010.pdf |
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author | Bassi Stefano Scafe Matteo Leoni Enrico Mingazzini Claudio Bhatia Narayan Jatinder Rossi Andrea |
author_facet | Bassi Stefano Scafe Matteo Leoni Enrico Mingazzini Claudio Bhatia Narayan Jatinder Rossi Andrea |
author_sort | Bassi Stefano |
collection | DOAJ |
description | This study concerns with the optimisation of a fibre-reinforced composite material ply book and application to an aeronautical component. The presented material solution is a recyclable FML (Fibre Metal Laminate). Recyclable and structural PMCs (Polymeric Matrix Composites) developed up-to now in ENEA had to be improved to satisfy the high-demanding fire characteristics requirements in aeronautics, particularly for the case considered in ongoing project FireMat (www.firemat.it), namely a turbine-bonnet production. FireMat project objective is the combination of weight reduction and fire resistance, maximizing the use C2C recyclable, secondary and biomass derived raw materials. Aluminium layers were introduced inside the lamination, to act as oxygen barriers and improve fire-retardancy. FML were obtained starting from a fire-retardant biobased resin, which was associated with aeronautical grade basalt-derived mineral fabric, processed in the form of a prepreg and then coupled with aluminium foils. FE modelling was based on performed mechanical characterization of the single layers and inter- layer adhesive strength of the ply stack: a composite sandwich structure (including aluminium honeycomb) was optimised. |
first_indexed | 2024-12-17T21:03:01Z |
format | Article |
id | doaj.art-e77078ed5ec14624abb2fab43981c3c8 |
institution | Directory Open Access Journal |
issn | 2261-236X |
language | English |
last_indexed | 2024-12-17T21:03:01Z |
publishDate | 2021-01-01 |
publisher | EDP Sciences |
record_format | Article |
series | MATEC Web of Conferences |
spelling | doaj.art-e77078ed5ec14624abb2fab43981c3c82022-12-21T21:32:40ZengEDP SciencesMATEC Web of Conferences2261-236X2021-01-013490101010.1051/matecconf/202134901010matecconf_iceaf2021_01010Development of recyclable Fibre Metal Laminates (FML), their mechanical characterization and FE modelling, aiming at structural application in aeronauticsBassi Stefano0Scafe Matteo1Leoni Enrico2Mingazzini Claudio3Bhatia Narayan Jatinder4Rossi Andrea5CNR ISTECENEA SSPT-PROMAS-TEMAFENEA SSPT-PROMAS-TEMAFENEA SSPT-PROMAS-TEMAFConsorzio MUSP, Tecnopolo di PiacenzaConsorzio MUSP, Tecnopolo di PiacenzaThis study concerns with the optimisation of a fibre-reinforced composite material ply book and application to an aeronautical component. The presented material solution is a recyclable FML (Fibre Metal Laminate). Recyclable and structural PMCs (Polymeric Matrix Composites) developed up-to now in ENEA had to be improved to satisfy the high-demanding fire characteristics requirements in aeronautics, particularly for the case considered in ongoing project FireMat (www.firemat.it), namely a turbine-bonnet production. FireMat project objective is the combination of weight reduction and fire resistance, maximizing the use C2C recyclable, secondary and biomass derived raw materials. Aluminium layers were introduced inside the lamination, to act as oxygen barriers and improve fire-retardancy. FML were obtained starting from a fire-retardant biobased resin, which was associated with aeronautical grade basalt-derived mineral fabric, processed in the form of a prepreg and then coupled with aluminium foils. FE modelling was based on performed mechanical characterization of the single layers and inter- layer adhesive strength of the ply stack: a composite sandwich structure (including aluminium honeycomb) was optimised.https://www.matec-conferences.org/articles/matecconf/pdf/2021/18/matecconf_iceaf2021_01010.pdf |
spellingShingle | Bassi Stefano Scafe Matteo Leoni Enrico Mingazzini Claudio Bhatia Narayan Jatinder Rossi Andrea Development of recyclable Fibre Metal Laminates (FML), their mechanical characterization and FE modelling, aiming at structural application in aeronautics MATEC Web of Conferences |
title | Development of recyclable Fibre Metal Laminates (FML), their mechanical characterization and FE modelling, aiming at structural application in aeronautics |
title_full | Development of recyclable Fibre Metal Laminates (FML), their mechanical characterization and FE modelling, aiming at structural application in aeronautics |
title_fullStr | Development of recyclable Fibre Metal Laminates (FML), their mechanical characterization and FE modelling, aiming at structural application in aeronautics |
title_full_unstemmed | Development of recyclable Fibre Metal Laminates (FML), their mechanical characterization and FE modelling, aiming at structural application in aeronautics |
title_short | Development of recyclable Fibre Metal Laminates (FML), their mechanical characterization and FE modelling, aiming at structural application in aeronautics |
title_sort | development of recyclable fibre metal laminates fml their mechanical characterization and fe modelling aiming at structural application in aeronautics |
url | https://www.matec-conferences.org/articles/matecconf/pdf/2021/18/matecconf_iceaf2021_01010.pdf |
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