Aeronautics Research 2002 - 2006 projects

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170 Initial folding patterns to be investigated will be V-form zigzag geometry, which gives an open cellular structure. The key to the design of improved cellular materials is modelling and simulation. Methods will be developed based on cell micromodels for optimising cell geometries, together with homogenised models and multiscale code developments for impact modelling in larger sandwich structures. The structural case selected for study is foreign object impact damage from impactors such as bird strikes on CM panels and tyre rubber or runway debris impacts on CHC twin-skinned structures. Structural tests will focus on gas gun and drop tower impact tests on generic structures. Validation studies will assess the technology developments, verify the simulation and design methods by detailed comparison of impact damage predictions with test results, and fi nally make recommendations for aircraft designers. CELPACT will conclude with fi nal assessment reports and design guides for aircraft industry users, the ‘Road map to application’ reports and a fi nal workshop. Results CELPACT will provide new technologies for airframes which will facilitate novel aircraft confi gurations. They will be based on advanced twin-walled structural concepts, using advanced composite and metallic cellular structures as core materials and leading to structural weight reduction in airframes. New advanced manufacturing processes will be developed and refi ned for cellular metal structures using selected laser melting technology, and for continuous fabrication of folded hybrid composite core structures. Concepts will be demonstrated for lightweight structures with improved impact resistance. These material developments have strong potential outside the aerospace industry such as fi lter technology and medical implants for CM structures, and boat hull and vehicle structures for CHC materials. New design methods for advanced sandwich structures will be validated, based on new simulation tools which combine multiscale modelling with microscale cell models. They may be used to optimise structural concepts for improved behaviour under complex load systems such as impact and crash loads.
Acronym: CELPACT Name of proposal: Cellular Structures for Impact Performance Contract number: AST5-CT-2006-031038 Instrument: STP Total cost: 3 109 000 € EU contribution: 2 430 000 € Call: FP6-2005-Aero-1 Starting date: 01.09.2006 Ending date: 31.08.2009 Duration: 36 months Objective: Safety & Security Research domain: Accident Prevention Coordinator: Dr Johnson Alastair Deutsches Zentrum für Luft- und Raumfahrt eV Institute of Structures and Design Pfaffenwaldring 38-40 DE 70569 Stuttgart E-mail: alastair.johnson@dlr.de Tel: +49 (0)711 6862 297 Fax: +49 (0)711 6862 227 EC Offi cer: P. Perez-Illana Partners: University of Liverpool UK The Chancellor, Master and Scholars of the University of Oxford UK Laboratory of Technology and Strength of Materials GR Aachen University DE ENS Cachan FR University of Stuttgart DE Brno University of Technology CZ ATECA FR Airbus Deutschland GmbH DE EADS CCR FR EADS Deutschland GmbH DE Alma Consulting Group S.A.S. FR 171
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PROJECT SYNOPSES ��
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EUROPEAN COMMISSION Aeronautics Res
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During the Sixth Framework Programm
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Aeronautics and air transport in Eu
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Main research areas Aeronautics res
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Call 1A 12/2002 €243 m Call 2A 12
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i.e. the average EC funding per pro
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Strengthening Competitiveness Table
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Improving Aircraft Safety and Secur
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Support Actions EASN II European Ae
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26 Strengthening Competitiveness Sa
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28 Partners: Aero Vodochody a.s. CZ
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30 for different payloads, such as
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32 Strengthening Competitiveness PL
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A topology optimisationbased design
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36 Strengthening Competitiveness Si
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38 Acronym: SimSAC Name of proposal
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40 The goal of the project is to sh
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42 Strengthening Competitiveness TI
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44 Acronym: TIMECOP-AE Name of prop
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Image Pattern Correlation Technique
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48 1. Wing deformation studies, 2.
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50 Strengthening Competitiveness AV
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52 Acronym: AVERT Name of proposal:
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54 Description of work In order to
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56 Strengthening Competitiveness NO
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58 Acronym: NODESIM-CFD Name of pro
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KATnet II matrix structure 60 Other
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62 Strengthening Competitiveness DI
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64 Acronym: DIANA Name of proposal:
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66 MINERVAA project in the context
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68 Strengthening Competitiveness CO
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70 Acronym: COSEE Name of proposal:
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Deployment view of DIANA Project Ar
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74 Fundación Robotiker ES SELEX Co
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76 The main SEAT objectives can be
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78 Strengthening Competitiveness MO
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80 Research domain: Electric & Mech
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82 Strengthening Competitiveness NE
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84 NEFS RTD work will support the s
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86 The element group of a multi-poi
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88 Strengthening Competitiveness FA
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90 High-integrated new cladding hea
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92 Strengthening Competitiveness RA
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94 SMD engineer examining a test co
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96 Strengthening Competitiveness MA
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98 Acronym: MAGFORMING Name of prop
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100 6. manufacture, CAE design and
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102 Strengthening Competitiveness S
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104 Acronym: SENARIO Name of propos
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106 fi nal assembly of components a
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Surface Treatment and Monitoring, A
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110 Results The outputs of this pro
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112 Strengthening Competitiveness A
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114 Acronym: AUTOW Name of proposal
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116 The innovations can be summaris
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118 Strengthening Competitiveness T
Page 122 and 123: Visualisation of calculation result
Page 124 and 125: 122 © Rolls-Royce, 2007 Strengthen
Page 126 and 127: 124 Acronym: PREMECCY Name of propo
Page 128 and 129: 126 reduced parts consumption, and
Page 130 and 131: 128 Strengthening Competitiveness N
Page 132 and 133: 130 - Design and development of a s
Page 134 and 135: 132 Creep test facility Strengtheni
Page 136 and 137: 134 Acronym: ATLLAS Name of proposa
Page 138 and 139: 136 high-altitude fl ight is techni
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Page 142 and 143: 140 - Experimental results for vali
Page 144 and 145: 142 NEWAC - Innovative combustors w
Page 146 and 147: 144 Aachen University of Technology
Page 148 and 149: 146 From these studies, and combine
Page 150 and 151: 148 Description of work Improving E
Page 152 and 153: 150 Acronym: ERAT Name of proposal:
Page 154 and 155: 152 which will take results from pr
Page 156 and 157: Link between modelling and measurem
Page 158 and 159: 156 - improvement of acoustic desig
Page 160 and 161: 158 Improving Environmental Impact
Page 162 and 163: 160 Acronym: MIME Name of proposal:
Page 164 and 165: 162 - investigate key enabling issu
Page 166 and 167: 164 National Research & Development
Page 168 and 169: 166 View of a vibration and damage
Page 170 and 171: Folded core composite structural el
Page 174 and 175: 172 Improving Aircraft Safety and S
Page 178 and 179: 176 WP2: Specifications and require
Page 182 and 183: 180 Acronym: VULCAN Name of proposa
Page 184 and 185: 182 - SP3 focuses on innovative mul
Page 186 and 187: 184 - the lack of basic teaching ma
Page 188 and 189: SICOM: a decision-support tool 186
Page 192 and 193: 190 Acronym: SUPERSKYSENSE Name of
Page 194 and 195: 192 age Assessment System) for in-f
Page 196 and 197: 194 Acronym: ILDAS Name of proposal
Page 198 and 199: 196 Electromechanical redundant act
Page 202 and 203: Single particle measurement princip
Page 204 and 205: 202 - Certifi cation requirement fo
Page 206 and 207: 204 Validation resources - demonstr
Page 208 and 209: 206 Acronym: SOFIA Name of proposal
Page 210 and 211: 208 sure) module for MANPADS jammin
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Page 214 and 215: 212 Acronym: ART Name of proposal:
Page 216 and 217: 214 EMMA2 Validation is split into
Page 218 and 219: SINBAD: system overview 216 Increas
Page 220 and 221: 218 Acronym: SINBAD Name of proposa
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SKY Scanner simulations - protected
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222 Increasing Operational Capacity
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224 Acronym: SPADE-2 Name of propos
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226 - proven wake vortex detection
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228 - WP1: Goal setting of desired
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230 Acronym: RESET Name of proposal
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Integration of different aeronautic
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236 Following the stated technical
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238 Figure 2: SWIM prototype - phys
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240 Acronym: SWIM-SUIT Name of prop
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242 1 Enhanced MTCD 2 ATC Auto-pilo
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246 lite as a powerful enabler of s
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248 The Contract of Objectives asse
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250 iFLY work structure Increasing
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252 - Assess the A3 operation on sa
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Levels of maturity of ATM concepts
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256 Acronym: CAATS-II Name of propo
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258 Work Packages and interdependen
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262 Acronym: EP3 Name of proposal:
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266 Acronym: STAR Name of proposal:
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268 introduced in order to further
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270 Support Actions USE HAAS Study
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272 Acronym: USE HAAS Name of propo
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A thermoplane airship 274 Thermopla
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276 Support Actions AeroSME VI Supp
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278 Acronym: AeroSME VI Name of pro
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280 During this process, much empha
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282 multidisciplinary database is a
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284
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286 Project Offi cer Jean-Luc March
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288
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290 AIDA Aggressive Intermediate Du
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292 CoJeN Computation of Coaxial Je
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294 FASTWing CL Foldable, Adaptable
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296 MESEMA Magnetoelastic Energy Sy
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298 SENARIO Advanced sensors and no
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300 VERDI Virtual Engineering for R
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302 FLYSAFE Airborne Integrated Sys
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304 STREP ABiTAS Advanced Bonding T
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306 CATS Contract-based Air Transpo
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308 GOAHEAD Generation of Advanced
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310 NODESIM-CFD Non-Deterministic S
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312 TIMECOP-AE Toward Innovative Me
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314 ACA4-CT-2005-012213 ASAS-TN2 Ai
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316 ASA3-CT_2004-511045 AeroSME V S
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318 AST3-CT-2003-502832 WEL-AIR Dev
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320 AST3-CT-2004-502895 REMFI Rear
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322 AST4-CT-2005-516103 SMIST Struc
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324 AST5-CT-2006-030779 ENFICA - FC
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326 AST5-CT-2006-030874 MAGPI Main
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328 FP6-2003-AERO-1- 561131-ICE ICE
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330
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332 Air France 191 Air France Consu
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334 AustroControl 260 Autofl ug Gmb
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336 Civil Aviation Authority of Chi
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338 DSNA / Centre En Route de la Na
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340 Eurocopter Deutschland GmbH 32,
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342 Hexcel Reinforcements 112 Hispa
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344 Instytut Obrobki Plastycznej (M
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346 Lufthansa Technik AG 191, 207 L
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348 Oxsensis Ltd 125 Palbam Metal W
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350 SCITEK Consultants Ltd 141 SEA
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352 Stridsberg Powertrain AB 82, 19
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354 TLS Technik GmbH & Co Spezialpu
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356 University of Patras - Mechanic
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358 WS Atkins Consultants Limited 5
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360 BULGARIA Mr MILANOV Evgeni Bulg
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362 Mr BENTZINGER Peter PT-Luftfahr
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364 Ms MCKENZIE Finella National Ph
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366 LITHUANIA Mr LAPIENIS Saulius A
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368 Mr THORSHAUG Niels Peter Resear
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370 Mr. MELNIKOV Vladimir JSC Unit
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European Commission Luxembourg: Off
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Aeronautics Research in the Sixth F
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Aeronautics Research 2002 - 2006 projects

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