ALASCA
Advanced Lattice Structures for Composite Airframes
| Coordinatore | DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV
Organization address
address: Linder Hoehe contact info |
| Nazionalità Coordinatore | Germany [DE] |
| Totale costo | 3˙431˙752 € |
| EC contributo | 1˙350˙260 € |
| Programma | FP7-TRANSPORT
Specific Programme "Cooperation": Transport (including Aeronautics) |
| Code Call | FP7-AAT-2010-RTD-RUSSIA |
| Funding Scheme | CP-FP |
| Anno di inizio | 2010 |
| Periodo (anno-mese-giorno) | 2010-12-01 - 2013-11-30 |
Partecipanti
| # | ||||
|---|---|---|---|---|
| 1 |
DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV
Organization address
address: Linder Hoehe contact info |
DE (KOELN) | coordinator | 513˙641.00 |
| 2 |
TECHNISCHE UNIVERSITEIT DELFT
Organization address
address: Stevinweg 1 contact info |
NL (DELFT) | participant | 251˙100.00 |
| 3 |
AIRBUS DEFENCE AND SPACE GMBH
Organization address
address: WILLY MESSERSCHMITT STRASSE 1 contact info |
DE (OTTOBRUNN) | participant | 226˙350.00 |
| 4 |
UNIVERSITY OF LEEDS
Organization address
address: WOODHOUSE LANE contact info |
UK (LEEDS) | participant | 194˙400.00 |
| 5 |
SMR ENGINEERING & DEVELOPMENT SA
Organization address
address: Rue Dufour 109 b contact info |
CH (BIENNE) | participant | 95˙850.00 |
| 6 |
AIRBUS OPERATIONS GMBH
Organization address
address: Kreetslag 10 contact info |
DE (HAMBURG) | participant | 47˙742.36 |
| 7 |
AIRBUS OPERATIONS SAS
Organization address
address: ROUTE DE BAYONNE 316 contact info |
FR (TOULOUSE) | participant | 21˙176.64 |
| 8 |
Central Research Institute for Special Machine Building
Organization address
address: Zavodskaya contact info |
RU ("Khotkovo, Moscow Region") | participant | 0.00 |
| 9 |
FEDERAL STATE UNITARY ENTERPRISE THE CENTRAL AEROHYDRODYNAMIC INSTITUTE NAMED AFTER PROF. N.E. ZHUKOVSKY
Organization address
address: Zhukovsky str 1 contact info |
RU (ZHUKOVSKY) | participant | 0.00 |
| 10 |
MENDELEYEV UNIVERSITY OF CHEMICAL TECHNOLOGY OF RUSSIA
Organization address
address: MIUSSKAYA SQUARE 9 contact info |
RU (Moscow) | participant | 0.00 |
| 11 |
NIK-SAMARA OOO
Organization address
address: AERODROMNAYA STREET 45 OFFICE 703 contact info |
RU (Samara) | participant | 0.00 |
| 12 |
NON-STATE EDUCATIONAL INSTITUTION EDUCATIONAL SCIENTIFIC AND EXPERIMENTAL CENTER OF MOSCOW INSTITUTE OF PHYSICS AND TECHNOLOGY
Organization address
address: INSTITUTSKY PEREULOK 9 contact info |
RU ("DOLGOPRUDNY, MOSCOW") | participant | 0.00 |
| 13 |
SCIENTIFIC AND PRODUCTION ENTERPRISE RADAR-MMS OAO
Organization address
address: NOVOSELKOVSKAYA ULICA 37 contact info |
RU (St. Petersburg) | participant | 0.00 |
Mappa
Word cloud
Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.
Obiettivo del progetto (Objective)
'The ALaSCA project focuses on maximum weight and cost reduction significant in airframes by developing manufacture-optimized lattice fuselage structures fulfilling fundamental aspects of airworthiness. The idea behind the ALaSCA project is to perform a comprehensive investigation starting with the beneficial geodesic design well-proven in space technology and transferring it to composite aircraft fuselage designs. The main objectives of this research programme are: a) Maximum weight and cost reduction by using lattice designs for fuselage structures. b) Development of manufacture-optimized lattice designs satisfying airworthiness requirements. c) Verification of airworthiness by manufacture and testing of representative lattice components.
Since structural requirements and boundary conditions in rocket technology are quite different from those in aircraft fuselage design, the scope of this project covers the specific aspects of design, sizing, manufacture and testing of lattice structures that follow from aircraft requirements. The objectives will only be achieved when solutions to the following issues in terms of lay-out, design, sizing, manufacture, and testing are found: a) Pro-lattice aircraft configurations for maximum weight and cost savings b) Aircraft specific components treated in the lattice fuselage design. c) Lattice elements, i.e. examination in the aircraft-specific detailed design of loads from impact and internal pressure.
Applying the above-mentioned methodology, the objectives will be achieved by main innovations in the following areas: a) Structural concepts for long service-life periods b) Design and dimensioning of cut-out surround structures c) Optimized floor-barrel interface. d) Barrel-barrel interface. e) Aircraft configurations reducing the demand for large cut-outs and interfaces in lattice fuselage sections. f) Process chain: preliminary design, sizing, detailed design, manufacturing, testing, validation, cost and weight analysis.'
Introduzione (Teaser)
Reductions in weight translate to important decreases in costs and emissions for the aerospace industry. Adaptation of successful space technology to produce novel fuselage architectures promises to make a significant contribution to the cause.