clean sky smart fixed wing aircraft itd programme...casa, eurocopter, fraunhofer institute,...
TRANSCRIPT
TAKE OFF
Informationsveranstaltung
zu Ausschreibungen
nationaler und europäischer
Luftfahrtforschungsprogramme
Michel GOULAIN, SAGE
Project Officer
June 1st, 2010, Vienna
Clean SkySmart Fixed Wing Aircraft ITD
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SFWA-ITD Organisation and SetupSFWASFWA--ITD Organisation and SetupITD Organisation and Setup
CleanSky SFWA-ITD, Vienna 01st June 2010
3CleanSky SFWA-ITD, Vienna 01st June 2010
SFWA- ITD Participants and Global SharesSFWASFWA-- ITD Participants and Global SharesITD Participants and Global Shares
„ITD-Leaders“
� DLR
� ONERA
� INCAS -Cluster
� NL-Cluster
� QinetiQ
� RUAG
� Aernnova
Associate Partners
Partner
participation
based on Call
for Proposals
„CfP“
Partners
393M€ Total Budget
50% of Total Budget25% of Total Budget
25% of Total Budget
�Airbus
�SAAB
�Dassault
�EADS-CASA
�Thales
�Fraunhofer
�SAFRAN
�Rolls-Royce
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Key Technologies for SFWA Key Technologies for SFWA Key Technologies for SFWA
Innovative Powerplant Integration
� Technology Integration
� Large Scale Flight Demonstration
� Impact of airframe flow field on Propeller
design (acoustic, aerodynamic, vibration)
� Impact of open rotor configuration on
airframe (Certification capabilities, structure,
vibrations...)
� Innovative empennage design
Smart Wing Technologies
�Technology Development
�Technology Integration
� Large Scale Flight Demonstration
� Natural Laminar Flow (NLF)
� Hybrid Laminar Flow (HLF)
� Active and passive load control
� Novel enabling materials
� Innovative manufacturing scheme
SAGE ITD - CROR engine
SGO ITD - Systems for Green Operation
Input connecting to:
TE– SFWA technologies for a Green ATS
Output providing data to:
5Flight Demo Design
Technology IntegrationTechnology Development
SFWA3.5
Innovative Empenage
Airbus
SFWA- ITD Technology WBSSFWASFWA-- ITD Technology WBSITD Technology WBS
SFWA1:
Smart Wing Technology
SFWA2:
New Configuration
SFWA3: Flight Demonstration
SFWA 0:
SFWA1.2
Load Control
SFWA1.1
Flow Control
SFWA1.3
Integrated Flow & Load
Control Systems
NL-Cluster
Airbus
Airbus
Dassault
Airbus /
SAAB
SAAB
Airbus
SFWA2.1
Integration of Smart Wing
into OAD
Airbus
SFWA2.2
Integration of Other Smart
Components into OAD
Dassault
SFWA2.3
Interfaces & Technology
Assessment
Airbus
SFWA3.1
High Speed Smart Wing
Flight Demonstrator
Airbus
SFWA3.3
Innovative Engine Demonstrator
Flying Test Bed
Airbus
SFWA3.2
Low Speed Smart Wing
Flight Demonstrator
Dassault
SFWA3.4
Long Term Technology
Flight Demonstrator
Airbus
Flight Demonstration
Technologies enter at
TRL 2 or 3
SelectedTechnologies developed at
TRL 4
SelectedTechnologies integrated at TRL 4 or 5
Selectedtechnologies validated in large scale flight demos at TRL > 6
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The Smart Fixed Wing Aircraft ConceptsThe Smart Fixed Wing Aircraft ConceptsThe Smart Fixed Wing Aircraft Concepts
1. High Speed Demonstrator Passive (HSDP)
2. Low Speed Demonstrator (LSD)
3. Short Range Aircraft Concept (SRA)
4. Low Sweep Bizjet Concept (LSBJ)
5. High Speed Demonstrator Active (HSDA)
6. Long Range Aircraft Concept (LRA)
7. High Sweep Bizjet Concept (HSBJ)
8. CROR Engine Demo FTB
Demo
Demo
Demo
Demo ?
Paper
Paper
Paper
Paper
A major contribution to the maturing, integration and large scale demonstration of „Smart Fixed Wing Aircraft“ - technologies is delivered through eight „SFWA- Aircraft concepts“ by
� Defining or providing the operational environment to mature a technology to high TRLs
� Providing an evaluation platform
� Setting a scenario for a potential target application.
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SFWA ITD Flight Demonstrator OptionsSFWA ITD Flight Demonstrator OptionsSFWA ITD Flight 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: UAV
Option 2: Alpha-Jet
Option 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 2010
Status: Preferred solution
Selection(s) part of technology roadmap
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The SFWA- High Speed Demonstrator Passive (HSDP)The SFWAThe SFWA-- High Speed Demonstrator Passive (HSDP)High Speed Demonstrator Passive (HSDP)
Laminar Wing Ground testdemonstrator to address
structural, system and manufacturing aspects
Port wing
Laminar wing structure
concept option 2
Starboard wing
Laminar wing structure
concept option 1
Laminar Wing aerdynamic layout and performance
Smart Passive Laminar Flow Wing
� Design of an all new natural laminar wing
� Proof of natural laminar wing concept in wind tunnel tests
� Use of novel materials and structural concepts
� Exploitation of structural and system integration together
with tight tolerance / high quality manufacturing methods
in a large scale ground test demonstrator
� Large scale flight test demonstration of the laminar
wing in operational conditions
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SFWA-ITD HSDP preparation WorksharingSFWASFWA--ITD HSDP preparation ITD HSDP preparation WorksharingWorksharing
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SFWA-ITD Integration of the CROR Engine ConceptSFWASFWA--ITD Integration of the CROR Engine ConceptITD Integration of the CROR Engine Concept
CROR Aero -Acoustic experimental characterization
with / without pylon. Example of the RR - CROR
(Dream, Dowty Design)
CROR integration study for a full scale test
of a CROR engine on-board a modified Airbus A340-600 Flying Test Bed.
Innovative Power-Plant Integration
� Design of innovative CROR blades and pylon
� CROR installation effects: aero, noise, vibrations,
handling qualities
� CROR propeller kinematics, study of fragment
impact depending on size and propeller and
fuselage materials
� Structural technologies for armour and shielding
� Feasibility study of a full scale CROR engine in a
Flying Testbed Demonstration (FTB)
CROR design study with new blade and engine design
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SFWA-ITD Call for Proposal Topics OverviewSFWASFWA--ITD Call for Proposal Topics OverviewITD Call for Proposal Topics Overview
In the total project lifetime the SFWA-ITD expect to contribute in CleanSky Call for Proposals (CfP) on
�100 – 200 topics
�Total value of topics ~ 100M€
In the current calls Industry, Research Establishments and Universities are invited to check your interest and to reply upon
Call #2 – 2010 (30.March 2010 – 30.June 2010 (17:00))
�4 topics
�Total value of topics ~ 5.90M€
Call #3 – 2010 (28.April 2010 – 20.July 2010 (17:00))
�8 topics
�Total value of topics ~ 4.04M€
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0
0
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0
0
The Smart Fixed Wing Aircraft ConceptsThe Smart Fixed Wing Aircraft ConceptsThe Smart Fixed Wing Aircraft Concepts
1. High Speed Demonstrator Passive (HSDP)
2. Low Speed Demonstrator (LSD)
3. Short Range Aircraft Concept (SRA)
4. Low Sweep Bizjet Concept (LSBJ)
5. High Speed Demonstrator Active (HSDA)
6. Long Range Aircraft Concept (LRA)
7. High Sweep Bizjet Concept (HSBJ)
8. CROR Engine Demo FTB
9. Multiple Aircraft Concepts / Technology Streams
Demo
Demo
Demo
Demo ?
Paper
Paper
Paper
Paper
Topics 3rd CfP
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SFWA-ITD Call for Proposal Topics in Call#2 - 2010SFWASFWA--ITD Call for Proposal Topics in Call#2 ITD Call for Proposal Topics in Call#2 -- 20102010
SFWA High Speed Demonstrator Passive „HSDP“
SFWA Low Sweep Bizjet Concept „LSBJ“
SFWA CROR Engine Demo FTB
SFWA Application in different aircraft conceptsSFWA Low Speed Demonstrator„LSD“
Identification ITD - Area - Topic No. topics Value Start Date End Date
JTI-CS-SFWA-01 Area01 - Smart Wing TechnoilogyJTI-CS-2010-2-SFWA-01-021 MEMS accelerometer for wing behaviour measurement € 600.000 01.07.2010 28.06.2012
JTI-CS-2010-2-SFWA-01-022 MEMS gyrometer for wing behaviour measurement € 800.000 01.07.2010 01.04.2012
2 € 1.400.000
JTI-CS-SFWA-02 Area02 - New Configuration
0 0
JTI-CS-SFWA-03 Area03 - Flight DemonstratorJTI-CS-2010-2-SFWA-03-002 Starbord leading edge and upper cover design and manufacturing € 3.700.000 01.07.2010 01.12.2013
JTI-CS-2010-2-SFWA-03-003 Krueger flaps design and manufacture € 800.000 01.07.2010 01.12.2013
2 € 4.500.000
totals €: 4 € 5.900.000
For a complete description of the topics, please refer to the published text of the call in www.cleansky.eu
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The Smart Fixed Wing Aircraft ConceptsThe Smart Fixed Wing Aircraft ConceptsThe Smart Fixed Wing Aircraft Concepts
1. High Speed Demonstrator Passive (HSDP)
2. Low Speed Demonstrator (LSD)
3. Short Range Aircraft Concept (SRA)
4. Low Sweep Bizjet Concept (LSBJ)
5. High Speed Demonstrator Active (HSDA)
6. Long Range Aircraft Concept (LRA)
7. High Sweep Bizjet Concept (HSBJ)
8. CROR Engine Demo FTB
9. Multiple Aircraft Concepts / Technology Streams
Demo
Demo
Demo
Demo ?
Paper
Paper
Paper
Paper
Topics 2nd CfP
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SFWA-ITD Call for Proposal Topics in Call#3 2010SFWASFWA--ITD Call for Proposal Topics in Call#3 2010ITD Call for Proposal Topics in Call#3 2010
SFWA High Speed Demonstrator Passive „HSDP“
SFWA Low Sweep Bizjet Concept „LSBJ“
SFWA CROR Engine Demo FTB
SFWA Application in different aircraft conceptsSFWA Low Speed Demonstrator„LSD“
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CleanSky SFWA-ITD, Vienna 01st June 2010
JTI CleanSkyJTI CleanSkyJTI CleanSky
Vielen Dank für Ihre
Aufmerksamkeit
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CleanSky SFWA-ITD, Vienna 01st June 2010
JTI CleanSkyJTI CleanSkyJTI CleanSky
© 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
presentation is hereby granted freely provided the source is
recognized. No rights to modify the presentation are granted.