jan 2011sfwa itd coordination jens könig airbus slide 1 smart fixed wing aircraft –itd cfp#8 info...
TRANSCRIPT
Jan 2011SFWA ITD Coordination Jens König Airbus Slide 1
Smart Fixed Wing Aircraft –ITD Smart Fixed Wing Aircraft –ITD
CfP#8 Info Day
Toulouse, 1st February 2011
Smart Fixed Wing Aircraft ITD
Jan 2011SFWA ITD Coordination Jens König Airbus Slide 2
ContentsContents
Overview SFWA ITD Structure Workpackages Partners Objectives Results Summary
Smart Fixed Wing Aircraft ITD
Jan 2011SFWA ITD Coordination Jens König Airbus Slide 3
Organisational StructureOrganisational Structure
SFWA-ITD
Airbus / SAAB
WP 1 Lead: Dassault
Smart Wing Technology
WP1.3 Lead: NL-Cluster Integrated Flow & Load Control Systems
WP1.2 Lead: AirbusLoad Control
WP1.1 Lead: AirbusFlow Control
WP 2 Lead: Saab
New Configuration
WP2.3 Lead: AirbusInterfaces & Technology Assessment
WP2.1 Lead: AirbusIntegration of Smart Winginto OAD
WP2.2 Lead: DassaultIntegration of Other Smart Components into OAD
WP 3 Lead: Airbus
Flight Demonstration
WP3.4 Lead: AirbusLong Term TechnologyFlight Demonstrator
WP3.1 Lead: AirbusHigh Speed Smart WingFlight Demonstrator
WP3.3 Lead: AirbusInnovative Engine Demo. Flying Test Bed
WP3.2 Lead: DassaultLow Speed Smart WingFlight Demonstrator
WP3.5 Lead: DassaultInnovative Empennage Large Demonstrator
WP3.6 Lead: AirbusALEAP Flight Test
Smart Fixed Wing Aircraft ITD
Jan 2011SFWA ITD Coordination Jens König Airbus Slide 4
SFWA ITD LeadershipSFWA ITD Leadership
The SFWA LeadershipSFWA-ITD counts 37 beneficiaries, i.e. leaders and partners with their
affiliates (Jan 2011)
8 SFWA ITD LeadersAirbus OperationsSaab ABDassault AviationEADS-CasaFraunhofer-Gesellschaft e.V.Rolls-RoyceSafran GroupThales Group
7 SFWA Associate partnersAernnova Aerospace DLR INCAS-ClusterNetherlands-ClusterOneraQinetiQRUAG Switzerland Ltd
Smart Fixed Wing Aircraft ITD
Jan 2011SFWA ITD Coordination Jens König Airbus Slide 5
Aircraft ConceptsAircraft Concepts
The aircraft concepts represent a “virtual” aircraft environment for maturing SFWA technologies. The concepts are:
High Speed Demonstrator Passive (HSDP) Low Speed Demonstrator (LSD) Short Range Aircraft Concept (SRA) Low Sweep Bizjet Concept (LSBJ) High Speed Demonstrator Active (HSDA) Long Range Aircraft Concept (LRA) High Sweep Bizjet Concept (HSBJ) CROR Engine Demo FTB
Smart Fixed Wing Aircraft ITD
Jan 2011SFWA ITD Coordination Jens König Airbus Slide 6
Technical PlanningTechnical Planning
Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4
2010 2011 2012 2013 2014 2015
Choice of flight test
vehicle
Feasibility PhasePreliminary Design
Detailed Design
Manufacturing
A/CChantier
Flight Test
Ground tests
CROR Demo -FTB
PDR
High Speed Demonstrator Passive (HSDP)
CDRCER
Low Speed Demo (LSD)
Flight Test
Manufacturing
A/CChantier
Detailed Design
Preliminary Design
PDR
CDR
Prel. Design
Detailed Design
Manufacturing
A/CChantier
Flight Test
Ground tests
PDR
CDR
Aircraft concepts – schedule 1/2
Smart Fixed Wing Aircraft ITD
Jan 2011SFWA ITD Coordination Jens König Airbus Slide 7
SFWA Concept ScheduleSFWA Concept Schedule
Aircraft concepts – schedule 2/2
Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4
2014 20152010 2011 2012 2013
CDR
Short Range Aircraft Concept(SRA)
Prel. Design
Low Sweep Bixjet Concept (LSBJ)
CER
Detailed Design
PDR
Conc Design
Prel. Design
Detailed Design
CDR
CER
PDR
High Sweep Bizjet Concept (HSBJ)
Conc Design
Prel. Design
Detailed Design
CDRPDR
CER
Evaluation
TRL6
TRL6
TRL6
Evaluation
Evaluation
Smart Fixed Wing Aircraft ITD
Jan 2011SFWA ITD Coordination Jens König Airbus Slide 8
Technology StreamsTechnology Streams
For bundling aircraft concept related technologies nine Technology Streams have been defined
Natural Laminar Flow (NLF) Hybrid Laminar Flow (HLFC) Innovative Control Surfaces (ICS) Fluidic Flow Control (FFC) Load Control Functions and architectures (LCFA) Buffet Control (BC) CROR Engine Integration (CROR-EI) Integration of innovative turbofan engines to bizjets (IITE) Advanced Flight Test Instrumentation
Smart Fixed Wing Aircraft ITD
Jan 2011SFWA ITD Coordination Jens König Airbus Slide 9
Technology Stream MatrixTechnology Stream Matrix
The Technology Streams define requirements & collect the respective RTD results from the Workpackages
Tec
hn
olo
gy
Str
eam
s
WP1 WP2 WP3
Workpackages & Tasks
Smart Fixed Wing Aircraft ITD
Jan 2011SFWA ITD Coordination Jens König Airbus Slide 10
Flight Demonstrator OptionsFlight Demonstrator Options
1. High Speed Flight DemonstratorObjective: Large scale flight test of passive and active flow and loads
control solutions on all new innovative wing concepts to validate low drag solutions at representative Mach and Reynolds Numbers. Envisaged to be used at least in two major phases of the project.
Option 1: UAVOption 2: Alpha-JetOption 3: Airbus A340 with modified wing
4. Long Term Technology Flight DemonstratorObjective: Validation of durability and robustness of Smart Wing technologies in
operational environment
Option 1: In Service Transport Aircraft
Option 2: Airbus A300 “Beluga”
Option 2: Airbus A320
3. Innovative Engine Demonstrator Flying TestbedObjective: Demonstrate viability of full scale innovative engine concept in operational
condition
Options under investigation
2. Low Speed Flight DemonstratorObjective: Validation flight testing of High Lift solution to support / enable the
innovative wing low drag concepts with a full scale demonstrator.
Option 1: Dassault Falcon
Option 2: Airbus A320
Selected in April 2009
Selection
scheduled for 2011
Preferred solution
Selection(s) part of
technology roadmap
Smart Fixed Wing Aircraft ITD
Jan 2011SFWA ITD Coordination Jens König Airbus Slide 11
Large Scale Flight Demo Impact of airframe flow field on
Propeller design Impact of open rotor
configuration on airframe Innovative empennage
design
SFWA output to Technology Evaluator SFWA output to Technology Evaluator
CleanSkyTechnology Evaluator
Smart Wing Technologies Technology Integration Large Scale Flight Demo
Natural Laminar Flow (NLF) Hybrid Laminar Flow (HLF) Active and passive load
control Novel enabling materials Innovative manufacturing
Smart Wing Technologies
Innovative Power Plant Integration
Input from System for Green Operation – ITD
Input from Sustainable & Green Engines – ITD
Smart Fixed Wing Aircraft ITD
Jan 2011SFWA ITD Coordination Jens König Airbus Slide 12
SFWA-ITD CfP Topics
In the total project lifetime the SFWA-ITD will contribute in CleanSky Call for Proposals (CfP) on
100 – 200 topics Total value of topics ~ 100M€
In the current call Industry, Research Establishments and Universities are invited to check your interest to reply to
12 topics Total value of topics 9.9M€
12 topics have been identified for Call-08: 5 topics refer to SMART WING TECHNOLOGY 4 topics refer to NEW CONFIGURATION 3 topics refer to FLIGHT DEMONSTRATION
Smart Fixed Wing Aircraft ITD
Jan 2011SFWA ITD Coordination Jens König Airbus Slide 13
SFWA-ITD Call 8 Topics
Smart Fixed Wing Aircraft ITD
Jan 2011SFWA ITD Coordination Jens König Airbus Slide 14
DisclaimerDisclaimer
© 2010 by the CleanSky Leading Partners: Airbus, AgustaWestland, Alenia Aeronautica, Dassault Aviation, EADS-CASA, Eurocopter, Fraunhofer Institute, Liebherr-Aerospace, Rolls-Royce, Saab AB,
Safran Thales and the European Commission.
Permission to copy, store electronically, or disseminate this presen-tation is hereby granted freely provided the source is recognized. No
rights to modify the presentation are granted.