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7E13059

CreAting NonconventionAl Laminates

Public support

  • Provider

    Ministry of Education, Youth and Sports

  • Programme

  • Call for proposals

    FP7-AAT-2012-RTD-1

  • Main participants

    Výzkumný a zkušební letecký ústav, a.s.

  • Contest type

    RP - Co-financing of EC programme

  • Contract ID

    MSMT-42111/2013

Alternative language

  • Project name in Czech

    CreAting NonconventionAl Laminates

  • Annotation in Czech

    The purpose of the CANAL project is to develop new Non-Conventional Laminate (NCL) configurations using Dry Fibre Placement (DFP) and the establishment of engineering tools to ensure implementation of the technology in the aerospace industry and other industries, such as automotive that can benefit from rapid and cost effective production of complex shaped and high-performance composite parts. Whereas up to now composite laminates usually consist of only 90, 0 and +/-45 degree layers, the development ofAutomated Fibre Placement technology has opened possibilities to divert from this limiting step in design and manufacturing. Currently, no non-conventional laminates are known to be implemented in the industry, though research has shown promising results in virtual analysis and coupon testing. Variable stiffness laminates with curved fibre paths show an increase in buckling loads, as well as tailoring of natural frequencies for both panels and cylinders. Straight-fibre laminates with dispersed fibre angles show a promise for improved damage tolerance. A so-called AP-PLY multidirectional weave pattern can improve damage tolerance for any stacking sequence. Whereas for large aircraft manufacturers like Airbus and Boeing it almost seems default to use composites and a high level of automated fabrication with e.g. AFP, it is also lucrative for the small aircraft industry and the transport industry in general. Both weight and cost reduction can be achieved using automated composite manufacturing like AFP.Further material cost reduction are achieved through use of dry fibres instead of more costly prepregs, in combination with Liquid Composite Moulding instead of costly autoclave curing. The reduction in weight and cost supported by novel non-conventional design and dry fibre placement and LCM manufacturing technique will further facilitate and speed up the introduction of composite lightweight structures in aerospace and other transport industries.

Scientific branches

  • R&D category

    AP - Applied research

  • CEP classification - main branch

    JU - Aeronautics, aerodynamics, aeroplanes

  • CEP - secondary branch

  • CEP - another secondary branch

  • OECD FORD - equivalent branches <br>(according to the <a href="http://www.vyzkum.cz/storage/att/E6EF7938F0E854BAE520AC119FB22E8D/Prevodnik_oboru_Frascati.pdf">converter</a>)

    20304 - Aerospace engineering

Completed project evaluation

  • Provider evaluation

    U - Uspěl podle zadání (s publikovanými či patentovanými výsledky atd.)

  • Project results evaluation

    Following the condition that the candidate of financial contribution was evaluated and afterwards selected by international provider in accordance with the rules of the program the Ministry of Education, Youth ans Sports does not realize the evaluation of project results. The project is evaluated only after its approval by an international provider.

Solution timeline

  • Realization period - beginning

    Sep 1, 2013

  • Realization period - end

    Aug 31, 2016

  • Project status

    U - Finished project

  • Latest support payment

    Feb 26, 2016

Data delivery to CEP

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

  • Data delivery code

    CEP17-MSM-7E-U/01:1

  • Data delivery date

    Jun 20, 2017

Finance

  • Total approved costs

    2,137 thou. CZK

  • Public financial support

    2,137 thou. CZK

  • Other public sources

    0 thou. CZK

  • Non public and foreign sources

    0 thou. CZK