Conference paper Open Access

A challenge for next A/C Fuselage: New Hybrid Thermoplastic Material, Testing activities definition

Antonietta Mormone; Marco Raffone; Salvatore Russo


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  <identifier identifierType="DOI">10.5281/zenodo.3819812</identifier>
  <creators>
    <creator>
      <creatorName>Antonietta Mormone</creatorName>
      <affiliation>Leonardo Aircraft Division, Viale dell'Aeronautica, SNC, 80038 Naples, Italy</affiliation>
    </creator>
    <creator>
      <creatorName>Marco Raffone</creatorName>
      <affiliation>Leonardo Aircraft Division, Viale dell'Aeronautica, SNC, 80038 Naples, Italy</affiliation>
    </creator>
    <creator>
      <creatorName>Salvatore Russo</creatorName>
      <affiliation>Leonardo Aircraft Division, Viale dell'Aeronautica, SNC, 80038 Naples, Italy</affiliation>
    </creator>
  </creators>
  <titles>
    <title>A challenge for next A/C Fuselage: New Hybrid Thermoplastic Material, Testing activities definition</title>
  </titles>
  <publisher>Zenodo</publisher>
  <publicationYear>2018</publicationYear>
  <dates>
    <date dateType="Issued">2018-09-04</date>
  </dates>
  <resourceType resourceTypeGeneral="ConferencePaper"/>
  <alternateIdentifiers>
    <alternateIdentifier alternateIdentifierType="url">https://zenodo.org/record/3819812</alternateIdentifier>
  </alternateIdentifiers>
  <relatedIdentifiers>
    <relatedIdentifier relatedIdentifierType="DOI" relationType="IsVersionOf">10.5281/zenodo.3819811</relatedIdentifier>
    <relatedIdentifier relatedIdentifierType="URL" relationType="IsPartOf">https://zenodo.org/communities/nhyte-h2020</relatedIdentifier>
  </relatedIdentifiers>
  <rightsList>
    <rights rightsURI="https://creativecommons.org/licenses/by/4.0/legalcode">Creative Commons Attribution 4.0 International</rights>
    <rights rightsURI="info:eu-repo/semantics/openAccess">Open Access</rights>
  </rightsList>
  <descriptions>
    <description descriptionType="Abstract">&lt;p&gt;A new hybrid thermoplastic concept patented by Leonardo allows to obtain a material that can be processed at temperature lower than usual thermoplastic resin processing temperature without any problem concerning the crystallinity. The high-performing hybrid material based on commercial PEEK-Carbon Fiber prepreg with the addition of amorphous (PEI) films overcomes the disadvantage of high/narrow processing parameters window and allows to take full advantage of prepreg material automated lamination, essential to make thermoplastic parts economically convenient respect to thermoset ones. Thus the new concept answers to the needs to have reduced weight and consequently reduced fuel consumptions and emissions on aircraft, as well as reduced manufacturing and operational costs. The preliminary tests performed on the new hybrid material showed good results, the goal of this work is to define an extensive mechanical test campaign to elaborate on material structural properties and validate static and dynamic behaviour of structural parts for next A/C fuselage.&lt;/p&gt;</description>
  </descriptions>
  <fundingReferences>
    <fundingReference>
      <funderName>European Commission</funderName>
      <funderIdentifier funderIdentifierType="Crossref Funder ID">10.13039/501100000780</funderIdentifier>
      <awardNumber awardURI="info:eu-repo/grantAgreement/EC/H2020/723309/">723309</awardNumber>
      <awardTitle>New Hybrid Thermoplastic Composite Aerostructures manufactured by Out of Autoclave Continuous Automated Technologies</awardTitle>
    </fundingReference>
  </fundingReferences>
</resource>
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