WASIS
Composite fuselage section Wafer Design Approach for Safety Increasing in Worst Case Situations and Joints Minimizing
| Coordinatore | FUNDACION CIDAUT
Organization address
address: PLAZA VICENTE ALEIXANDRE CAMPOS 2 PQ TECNOLOGICO DE BOECILLO 209 contact info |
| Nazionalità Coordinatore | Spain [ES] |
| Sito del progetto | http://www.wasis.eu |
| Totale costo | 4˙339˙301 € |
| EC contributo | 3˙239˙763 € |
| Programma | FP7-TRANSPORT
Specific Programme "Cooperation": Transport (including Aeronautics) |
| Code Call | FP7-AAT-2010-RTD-1 |
| Funding Scheme | CP-FP |
| Anno di inizio | 2011 |
| Periodo (anno-mese-giorno) | 2011-01-01 - 2014-12-31 |
Partecipanti
| # | ||||
|---|---|---|---|---|
| 1 |
FUNDACION CIDAUT
Organization address
address: PLAZA VICENTE ALEIXANDRE CAMPOS 2 PQ TECNOLOGICO DE BOECILLO 209 contact info |
ES (VALLADOLID) | coordinator | 463˙607.00 |
| 2 |
CIRCOMP GMBH
Organization address
address: MARIE CURIE STRASSE 11 contact info |
DE (KAISERSLAUTERN) | participant | 424˙200.00 |
| 3 |
INEGI - INSTITUTO DE CIENCIA E INOVACAO EM ENGENHARIA MECANICA E ENGENHARIA INDUSTRIAL
Organization address
address: RUA DR ROBERTO FRIAS 400 contact info |
PT (PORTO) | participant | 412˙523.50 |
| 4 |
INSTITUT FUER VERBUNDWERKSTOFFE GMBH
Organization address
address: ERWIN-SCHROEDINGER-STRASSE GEB 58 contact info |
DE (KAISERSLAUTERN) | participant | 401˙700.00 |
| 5 |
NATIONAL AEROSPACE UNIVERSITY KHARKIV AVIATION INSTITUTE NAMED BY N ZUKOVSKIY
Organization address
address: CHKALOVA STR 17 contact info |
UA (KHARKIV) | participant | 339˙500.00 |
| 6 |
UNIVERSITY OF PATRAS
Organization address
address: UNIVERSITY CAMPUS RIO PATRAS contact info |
EL (RIO PATRAS) | participant | 280˙680.00 |
| 7 |
NETCOMPOSITES LIMITED
Organization address
address: BRIDGE WAY 4A BROOM BUSINESS PARK contact info |
UK (CHESTERFIELD) | participant | 236˙510.28 |
| 8 |
ELEMENT MATERIALS TECHNOLOGY HITCHIN LIMITED
Organization address
address: WILBURY WAY contact info |
UK (HITCHIN HERTS) | participant | 186˙158.50 |
| 9 |
PIAGGIO AERO INDUSTRIES SPA
Organization address
address: Viale Castro Pretorio 116 contact info |
IT (ROMA) | participant | 178˙839.00 |
| 10 |
MATERIALS ENGINEERING RESEARCH LABORATORY LIMITED
Organization address
address: Wilbury Way contact info |
UK (HITCHIN - HERTS) | participant | 166˙336.61 |
| 11 |
AOES Group BV - Advanced Operations and Engineering Services Group BV
Organization address
address: Huygensstraat 34 contact info |
NL (Noordwijk) | participant | 136˙108.11 |
| 12 |
COMITE EUROPEEN DE NORMALISATION
Organization address
address: Avenue Marnix 17 contact info |
BE (BRUXELLES) | participant | 13˙600.00 |
| 13 |
COMAT COMPOSITE MATERIALS GMBH
Organization address
address: MARIE CURIE STRASSE 1 contact info |
DE (KAISERSLAUTERN) | participant | 0.00 |
| 14 |
CORVUS-AIRCRAFT SPORTREPULOGEP GYARTO ES SZOLGALTATO KORLATOLT TARSASAG
Organization address
address: II KORZET 35 contact info |
HU (BALLOSZOG) | participant | 0.00 |
Mappa
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Obiettivo del progetto (Objective)
'Aeronautics is a key asset for the future of Europe, but nowadays the industry has to face the challenge of “More Affordable, Safer, Cleaner and Quieter” while at the same time accounting for a demand that will triple over the next 20 years. WASIS project aims to rise to this challenge with the development of a composite fuselage structure based on the lattice stiffening concept, optimizing geometrical and mass properties of transition zones of fuselage structural joints. Project overall concept is focused on simultaneous meeting environmental demands and rising safety coupled with design and manufacturing cost-efficiency improvement.
The lattice approach allows composites to obtain more efficient mechanical behaviour, reducing weight and optimizing structure performance, which will be proved by comparative simulations against other approaches. This will be combined with specially designed semi-loop and micro-pin joining elements to provide the ability of innovative non-regular lattice structure manufacturing, save aircraft weight, avoid fuselage section weakening due to cutting reinforcement fibres.
Furthermore, the structure will also be developed to better withstand worst situation loadings, assessing safety through the large adoption of simulation and virtual testing from the very first design stages to analyze explosions and material damping. Developed innovative fuselage section design will be merged with high-productive filament winding technology to reduce manufacturing costs and time, and samples will be manufactured in order to prove how the different concepts fit together. Complete testing of the samples will be applied to prove the wafer approach. As a result of this project integrated approach – sufficient fuselage weight savings, manufacturing cost/time efficiency and safety increasing are to be achieved.'