Transcript SFWA ITD - Clean Sky

Smart Fixed Wing Aircraft –ITD
CfP#8 Info Day
Toulouse, 1st February 2011
SFWA ITD Coordination Jens König Airbus
Slide 1
Jan 2011
Contents
Smart Fixed Wing Aircraft ITD
 Overview
 SFWA ITD Structure
 Workpackages
 Partners
 Objectives
 Results
 Summary
SFWA ITD Coordination Jens König Airbus
Slide 2
Jan 2011
Organisational Structure
Smart Fixed Wing Aircraft ITD
SFWA-ITD
Airbus / SAAB
WP 1 Lead: Dassault
WP 2 Lead: Saab
WP 3 Lead: Airbus
Smart Wing Technology
New Configuration
Flight Demonstration
WP1.1 Lead: Airbus
Flow Control
WP2.1 Lead: Airbus
Integration of Smart Wing
into OAD
WP3.1 Lead: Airbus
High Speed Smart Wing
Flight Demonstrator
WP1.2 Lead: Airbus
Load Control
WP2.2 Lead: Dassault
Integration of Other Smart
Components into OAD
WP3.2 Lead: Dassault
Low Speed Smart Wing
Flight Demonstrator
WP1.3 Lead: NL-Cluster Integrated
Flow & Load Control Systems
WP2.3 Lead: Airbus
Interfaces & Technology
Assessment
WP3.3 Lead: Airbus
Innovative Engine Demo. Flying
Test Bed
WP3.4 Lead: Airbus
Long Term Technology
Flight Demonstrator
WP3.5 Lead: Dassault
Innovative Empennage Large
Demonstrator
WP3.6 Lead: Airbus
ALEAP Flight Test
SFWA ITD Coordination Jens König Airbus
Slide 3
Jan 2011
SFWA ITD Leadership
Smart Fixed Wing Aircraft ITD
The SFWA Leadership
SFWA-ITD counts 37 beneficiaries, i.e. leaders and partners with their
affiliates (Jan 2011)
 8 SFWA ITD Leaders
 7 SFWA Associate partners
 Airbus Operations
 Aernnova Aerospace
 Saab AB
 DLR
 Dassault Aviation
 INCAS-Cluster
 EADS-Casa
 Netherlands-Cluster
 Fraunhofer-Gesellschaft e.V.
 Onera
 Rolls-Royce
 QinetiQ
 Safran Group
 RUAG Switzerland Ltd
 Thales Group
SFWA ITD Coordination Jens König Airbus
Slide 4
Jan 2011
Aircraft Concepts
Smart Fixed Wing Aircraft ITD
 The aircraft concepts represent a “virtual” aircraft
environment for maturing SFWA technologies. The
concepts are:
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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
SFWA ITD Coordination Jens König Airbus
Slide 5
Jan 2011
Technical Planning
Smart Fixed Wing Aircraft ITD
Aircraft concepts – schedule 1/2
2010
Q1
Q2
2011
Q3
Q4
Q1
Q2
2012
Q3
Q4
Q1
Q2
2013
Q3
Q4
Q1
Q2
2014
Q3
Q4
Q1
Q2
Q3
2015
Q4
Q1
Q2
Q3
Q4
Prel. Design
Detailed Design
High Speed
Demonstrator
Passive (HSDP)
Manufacturing
PDR
A/CChantie
r
Ground tests
CDR
Flight
Test
Feasibility Phase
Preliminary Design
Detailed Design
Manufacturing
CROR Demo FTB
CER
PDR
CDR
A/CChantie
r
Ground tests
Flight
Test
Preliminary Design
Low Speed Demo
(LSD)
Detailed
Design
Choice of
flight test
vehicle
SFWA ITD Coordination Jens König Airbus
Manufacturing
A/CChantie
r
PDR
CDR
Slide 6
Flight
Test
Jan 2011
SFWA Concept Schedule
Smart Fixed Wing Aircraft ITD
Aircraft concepts – schedule 2/2
2010
Q1
Q2
2011
Q3
Q4
Q1
Q2
Q3
2012
Q4
Q1
Q2
Q3
2013
Q4
Q1
Q2
Q3
2014
Q4
Q1
Q2
Q3
2015
Q4
Q1
Q2
Q3
Q4
Prel. Design
Detailed Design
Short Range
Aircraft Concept
(SRA)
Evaluation
CER
PDR
CDR
TRL6
Conc Design
Low Sweep
Bixjet Concept
(LSBJ)
Prel. Design
Detailed Design
CER
Evaluation
PDR
CDR
High Sweep
Bizjet Concept
(HSBJ)
TRL6
Conc Design
Prel. Design
Detailed Design
Evaluation
CER
PDR
SFWA ITD Coordination Jens König Airbus
CDR
Slide 7
TRL6
Jan 2011
Technology Streams
Smart Fixed Wing Aircraft ITD
 For bundling aircraft concept related technologies
nine Technology Streams have been defined
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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
SFWA ITD Coordination Jens König Airbus
Slide 8
Jan 2011
Technology Stream Matrix
Smart Fixed Wing Aircraft ITD
The Technology Streams define requirements & collect
the respective RTD results from the Workpackages
WP2
WP3
Technology Streams
WP1
Workpackages & Tasks
SFWA ITD Coordination Jens König Airbus
Slide 9
Jan 2011
Flight Demonstrator Options
Smart Fixed Wing Aircraft ITD
1. High Speed Flight Demonstrator
Objective: 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
2. Low Speed Flight Demonstrator
Objective: 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
3. Innovative Engine Demonstrator Flying Testbed
Objective: Demonstrate viability of full scale innovative engine concept in operational
condition
Options under investigation
4. Long Term Technology Flight Demonstrator
Objective: 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
SFWA ITD Coordination Jens König Airbus
Slide 10
Jan 2011
SFWA output to Technology Evaluator
Smart Fixed Wing Aircraft ITD
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Smart Wing Technologies
Technology Integration
Large Scale Flight Demo
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Natural Laminar Flow (NLF)
Hybrid Laminar Flow (HLF)
Active and passive load control
Novel enabling materials
Innovative manufacturing
Smart Wing
Technologies
Input from System for
Green Operation – ITD
CleanSky
Technology
Evaluator
 Large Scale Flight Demo
Input from Sustainable &
Green Engines – ITD
SFWA ITD Coordination Jens König Airbus
Innovative Power
Plant Integration
 Impact of airframe flow field on
Propeller design
 Impact of open rotor
configuration on airframe
 Innovative empennage
design
Slide 11
Jan 2011
SFWA-ITD CfP Topics
Smart Fixed Wing Aircraft ITD
 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
SFWA ITD Coordination Jens König Airbus
Slide 12
Jan 2011
SFWA-ITD Call 8 Topics
Smart Fixed Wing Aircraft ITD
SFWA ITD Coordination Jens König Airbus
Slide 13
Jan 2011
Disclaimer
Smart Fixed Wing Aircraft ITD
© 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.
SFWA ITD Coordination Jens König Airbus
Slide 14
Jan 2011