Aeronautics Research 2002 - 2006 projects

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48 1. Wing deformation studies, 2. Propeller deformation studies, 3. Helicopter studies, 4. Surface fl ow measurements, 5. High lift structures, 6. Industrial fl ight testing. Results The expected results of the project are reliable optical measurement techniques performed in-fl ight for certifi cation as well as for research purposes. This project will demonstrate only the general feasibility of the measurement techniques, since not all possible application can be tested. In particular, the goal of AIM is to use of the following measurement techniques for in-fl ight investigations: – Image Pattern Correlation Technique (IPCT) for the measurement of local deformations of e.g. wing, aileron and fl ap and with help of Quantitative Video Technique (QVT) for the determination of local propeller and rotor deformations, – Particle Image Velocimetry (PIV) for the measurement of a velocity fl ow fi eld of a vortex and velocity fi elds in high lift confi gurations, – Background Oriented Schlieren method (BOS) for the measurement of the density gradients of a fl ow fi eld and therefore to determine the position and strength of spatial vortex fi laments, – Light detection and ranging (LIDAR) for the measurement of a velocity fl ow fi eld of a vortex, – Pressure Sensitive Paint (PSP) for the measurement of surface pressures, – Infrared Technique (IRT) for the measurement of surface heat distributions.
Acronym: AIM Name of proposal: Advanced In-Flight Measurement Techniques Contract number: AST5-CT2006-030827 Instrument: STP Total cost: 3 538 526 € EU contribution: 2 000 000 € Call: FP6-2005-Aero-1 Starting date: 01.11.2006 Ending date: 31.10.2009 Duration: 36 months Objective: Competitiveness Research domain: Aerodynamics Website: http://aim.dlr.de Coordinator: Dr. Falk Klinge Deutsches Zentrum für Luft- und Raumfahrt e. V. Bunsenstrasse 10 Linder Höhe DE 37073 Göttingen E-mail: falk.klinge@dlr.de Tel: +49 (0) 551 709 2471 Fax: +49 (0) 551 709 2830 EC Offi cer: R. Denos Partners: Airbus France FR Eurocopter Deutschland DE EUROCOPTER S.A.S. FR PIAGGIO AERO INDUSTRIES S.p.A. IT EVEKTOR, spol. s r.o. CZ Stichting Nationaal Lucht- en Ruimtevaartlaboratorium NL Offi ce National d`Etudes et de Recherches Aérospatiales FR Cranfi eld University UK Moscow Power Engineering Institute (Technical University) RU Flughafengesellschaft Braunschweig mbH DE 49
Page 1 and 2: PROJECT SYNOPSES ��
Page 3 and 4: EUROPEAN COMMISSION Aeronautics Res
Page 5: During the Sixth Framework Programm
Page 9 and 10: Aeronautics and air transport in Eu
Page 11 and 12: ��
Page 13 and 14: Main research areas Aeronautics res
Page 15 and 16: Call 1A 12/2002 €243 m Call 2A 12
Page 17: i.e. the average EC funding per pro
Page 21 and 22: Strengthening Competitiveness Table
Page 23 and 24: Improving Aircraft Safety and Secur
Page 25: Support Actions EASN II European Ae
Page 28 and 29: 26 Strengthening Competitiveness Sa
Page 30 and 31: 28 Partners: Aero Vodochody a.s. CZ
Page 32 and 33: 30 for different payloads, such as
Page 34 and 35: 32 Strengthening Competitiveness PL
Page 36 and 37: A topology optimisationbased design
Page 38 and 39: 36 Strengthening Competitiveness Si
Page 40 and 41: 38 Acronym: SimSAC Name of proposal
Page 42 and 43: 40 The goal of the project is to sh
Page 44 and 45: 42 Strengthening Competitiveness TI
Page 46 and 47: 44 Acronym: TIMECOP-AE Name of prop
Page 48 and 49: Image Pattern Correlation Technique
Page 52 and 53: 50 Strengthening Competitiveness AV
Page 54 and 55: 52 Acronym: AVERT Name of proposal:
Page 56 and 57: 54 Description of work In order to
Page 58 and 59: 56 Strengthening Competitiveness NO
Page 60 and 61: 58 Acronym: NODESIM-CFD Name of pro
Page 62 and 63: KATnet II matrix structure 60 Other
Page 64 and 65: 62 Strengthening Competitiveness DI
Page 66 and 67: 64 Acronym: DIANA Name of proposal:
Page 68 and 69: 66 MINERVAA project in the context
Page 70 and 71: 68 Strengthening Competitiveness CO
Page 72 and 73: 70 Acronym: COSEE Name of proposal:
Page 74 and 75: Deployment view of DIANA Project Ar
Page 76 and 77: 74 Fundación Robotiker ES SELEX Co
Page 78 and 79: 76 The main SEAT objectives can be
Page 80 and 81: 78 Strengthening Competitiveness MO
Page 82 and 83: 80 Research domain: Electric & Mech
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Page 86 and 87: 84 NEFS RTD work will support the s
Page 88 and 89: 86 The element group of a multi-poi
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Page 92 and 93: 90 High-integrated new cladding hea
Page 94 and 95: 92 Strengthening Competitiveness RA
Page 96 and 97: 94 SMD engineer examining a test co
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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
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Visualisation of calculation result
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122 © Rolls-Royce, 2007 Strengthen
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124 Acronym: PREMECCY Name of propo
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126 reduced parts consumption, and
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128 Strengthening Competitiveness N
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130 - Design and development of a s
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132 Creep test facility Strengtheni
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134 Acronym: ATLLAS Name of proposa
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136 high-altitude fl ight is techni
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138
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140 - Experimental results for vali
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142 NEWAC - Innovative combustors w
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144 Aachen University of Technology
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146 From these studies, and combine
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148 Description of work Improving E
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150 Acronym: ERAT Name of proposal:
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152 which will take results from pr
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Link between modelling and measurem
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156 - improvement of acoustic desig
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158 Improving Environmental Impact
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160 Acronym: MIME Name of proposal:
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162 - investigate key enabling issu
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164 National Research & Development
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166 View of a vibration and damage
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Folded core composite structural el
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170 Initial folding patterns to be
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172 Improving Aircraft Safety and S
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176 WP2: Specifications and require
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180 Acronym: VULCAN Name of proposa
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182 - SP3 focuses on innovative mul
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184 - the lack of basic teaching ma
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SICOM: a decision-support tool 186
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190 Acronym: SUPERSKYSENSE Name of
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192 age Assessment System) for in-f
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194 Acronym: ILDAS Name of proposal
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196 Electromechanical redundant act
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Single particle measurement princip
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202 - Certifi cation requirement fo
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204 Validation resources - demonstr
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206 Acronym: SOFIA Name of proposal
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208 sure) module for MANPADS jammin
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210
Page 214 and 215:
212 Acronym: ART Name of proposal:
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214 EMMA2 Validation is split into
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SINBAD: system overview 216 Increas
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218 Acronym: SINBAD Name of proposa
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SKY Scanner simulations - protected
Page 224 and 225:
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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Page 238 and 239:
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
Page 250 and 251:
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
Page 256 and 257:
Levels of maturity of ATM concepts
Page 258 and 259:
256 Acronym: CAATS-II Name of propo
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258 Work Packages and interdependen
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Page 264 and 265:
262 Acronym: EP3 Name of proposal:
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Page 268 and 269:
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
Page 306 and 307:
304 STREP ABiTAS Advanced Bonding T
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306 CATS Contract-based Air Transpo
Page 310 and 311:
308 GOAHEAD Generation of Advanced
Page 312 and 313:
310 NODESIM-CFD Non-Deterministic S
Page 314 and 315:
312 TIMECOP-AE Toward Innovative Me
Page 316 and 317:
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
Page 328 and 329:
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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