Clean Sky Smart Fixed Wing Aircraft ITD programme...CASA, Eurocopter, Fraunhofer Institute,...

TAKE OFF

Informationsveranstaltung

zu Ausschreibungen

nationaler und europäischer

Luftfahrtforschungsprogramme

Michel GOULAIN, SAGE

Project Officer

June 1st, 2010, Vienna

Clean SkySmart Fixed Wing Aircraft ITD

2

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


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



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.


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


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


SFWA-ITD HSDP preparation WorksharingSFWASFWA--ITD HSDP preparation ITD HSDP preparation WorksharingWorksharing


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


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€

12

0

0

4


0

0










9. Multiple Aircraft Concepts / Technology Streams

Demo

Demo

Demo

Demo ?

Paper

Paper

Paper

Paper

Topics 3rd CfP

4

13


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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1

1

2


2

2










9. Multiple Aircraft Concepts / Technology Streams

Demo

Demo

Demo

Demo ?

Paper

Paper

Paper

Paper

Topics 2nd CfP

8


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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JTI CleanSkyJTI CleanSkyJTI CleanSky

Vielen Dank für Ihre

Aufmerksamkeit

17


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.

Clean Sky Smart Fixed Wing Aircraft ITD programme...CASA, Eurocopter, Fraunhofer Institute,...

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