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