Transcript Diapositive 1 - MCI Stockholm

Flygteknik 2010
The CleanSky “Smart Fixed Wing Aircraft
Integrated Technology Demonstrator” (SFWA-ITD):
Saab’s participation in Clean Sky and our
contribution to a laminar wing development
Stockholm, 18 oktober 2010
Thomas. Hellström (Saab)
The CleanSky “Smart Fixed Wing Aircraft
Integrated Technology Demonstrator”
Presentation Content
 Introduction
 SFWA-ITD key objectives
 SFWA-ITD large ground and flight demonstrators
 Saab Participation in CleanSky and actual status of work
 Conclusion
Flygteknik
2010
Stockholm,
18.okt.
2010
Flygteknik
2010
Stockholm
18 okt.
2010
CleanSky key features
Joint Technology Initiative (JTI) „Clean Sky“

New instrument in European Commission Frame Programme FP7

Single Frame Demonstrator R&T program for „Greening of the Air Traffic
System“

Representing the European large civil aero-industry

1.6 B€ programme budget out of 4.6 B€ Aero R&T in FP7

7 years runtime

Annual update of workplan, annual „Grant Agreement“

Run via a dedicated „Joint Undertaking“ (JU)
Flygteknik
Flygteknik2010
2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010
The CleanSky “Smart Fixed Wing Aircraft
Integrated Technology Demonstrator”
Flygteknik
Flygteknik2010
2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010
SFWA-ITD participants and global shares
„ITD-Leaders“
Associate Partners
 DLR
 ONERA
•
•
•
•
•
•
•
•
Airbus
SAAB
Dassault
EADS-CASA
Thales
Fraunhofer
SAFRAN
Rolls-Royce
 INCAS
 NL-Cluster
 QinetiQ
 RUAG
 Aernnova
25% of Total Budget
Partner
participation
based on Call
for Proposals
„CfP“
50% of Total Budget
25% of Total Budget
393M€ Total Budget
Flygteknik
Flygteknik2010
2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010
The CleanSky “Smart Fixed Wing Aircraft
Integrated Technology Demonstrator”
Presentation Content
 Introduction
 SFWA-ITD key objectives
 SFWA-ITD large ground and flight demonstrators

Saab Participation in CleanSky and actual status of work
 Conclusion
Flygteknik
Flygteknik2010
2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010
Mature technologies to achieve
ACARE ambitious targets
 50% cut in CO2 emissions
Aircraft manufacturers 20-25%
Engine manufacturers
15-20%
Technologies are key towards
ACARE targets, but can only
deploy their benefits through smart
integration
ACARE: Advisory Council for Aeronautics Research in Europe
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Stockholm 18
18.okt.
okt. 2010
2010
Operations
5-10%
Air Traffic Management
Key Smart Fixed Wing Aircraft technologies
Smart Wing Technologies
Input connecting to:
Technology Development
SAGE ITD – CROR engine
SGO –
Technology Integration
Systems for Green
Operation
 Large Scale Flight Demonstration
 Natural Laminar Flow (NLF)
 Hybrid Laminar Flow (HLF)
 Active and passive load control
Innovative Powerplant Integration
 Novel enabling materials
 Technology Integration
 Innovative manufacturing scheme
 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
Output providing data to:
TE– SFWA technologies for a
Green ATS
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2010
Aerodynamic drag reduction through
laminar flow
Schematic Representation
V at boundary-layer
edge
V at boundary-layer edge
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2010
Potential of using laminarity to reduce the
aerodynamic drag
Potential drag reductions through
the application of laminarity
 Wing
 Tail
 Nacelles
Flygteknik
Flygteknik2010
2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010
The CleanSky “Smart Fixed Wing Aircraft
Integrated Technology Demonstrator”
Presentation Content
 Introduction
 SFWA-ITD key objectives
 SFWA-ITD large ground and flight demonstrators

Saab Participation in CleanSky and actual status of work
 Conclusion
Flygteknik
Flygteknik2010
2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010
SFWA flight demonstrator options
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2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010
SFWA- High Speed Demonstrator Passive
(HSDP)
Smart Passive Laminar Flow Wing

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


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
Port wing
Starboard wing
Laminar wing structure
concept option 2
Laminar wing structure
concept option 1
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2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010
Smart Wing flight test instrumentation
Flygteknik
Flygteknik2010
2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010
The CleanSky “Smart Fixed Wing Aircraft
Integrated Technology Demonstrator”
Presentation Content
 Introduction
 SFWA-ITD key objectives
 SFWA-ITD large ground and flight demonstrators

Saab Participation in CleanSky and actual status of work
 Conclusion
Flygteknik
Flygteknik2010
2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010
The CleanSky ; Saab Participation

Saab AB focus on design, development and manufacturing of a
complex and innovative wing with natural laminar flow properties.

Saab participation in SFWA:






Co leader of SFWA together with Airbus
Leader of WP2
Partner to Airbus in the design process of the SRA wing incl systems and actuators
Responsible for design, development and manufacturing of the upper skin panel with
integrated leading edge. It is a unique, optimized and fully integrated composite part
Partner to Airbus in the flying demonstrators, Wing FTB and CROR FTB
CROR Engine Pylon TE (design & manufacturing incl optimization of acoustic
characteristics
Upper wing skin
Flying demonstrator activites Engine Pylon trailing edge
with integrated leading edge
Flygteknik
Flygteknik2010
2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010
The CleanSky “Smart Fixed Wing Aircraft
Integrated Technology Demonstrator”


Saab AB’s focus in SGO is to design and develop energy efficient
systems, integration of energy management systems and to develop
trajectory optimisation concepts to be able to fly “green trajectories”
during the full mission.
Saab participation in SGO:



WP leader and developer of on-board mission and trajectory optimisation concepts
to reduce the amount of emissions and the perceived noise
WP leader of Thermal Management. Saab will develop a Thermal Management
function that will manage and minimize the thermal peak loads of an more/all electric
aircraft in order to reduce system size and fuel consumption.
Design and development of a low power electro-mechanical de-icing system for an
all electrical aircraft. The system design will be validated in a flight test on a A320
aircraft
Thermal Management system
Low power Electro-Mechanical deicing system
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2010 Stockholm,
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18.okt.
okt. 2010
2010
Mission and Trajectory Optimisation
system
Worksharing to design and build the “HSDP”
Smart Wing demonstrator
Wing Tip: Aernnova
Integrated upper cover (SAAB)
Aileron structure (INCAS)
Integrated upper cover with structural
concept (SAAB)
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Flygteknik2010
2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010
The CleanSky “Smart Fixed Wing Aircraft
Integrated Technology Demonstrator”
• Assembly
– Due to the tight surface
requirement, limited
numbers of joint and fasteners
through surface is allowed
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2010 Stockholm,
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18.okt.
okt. 2010
2010
This document and the information contained herein is the property of Saab AB and must not be used, disclosed or altered without Saab AB prior written consent.
Saab status of design and build the “HSDP”
Smart Wing demonstrator
 Test/Trial Panel
 A test/trial panel has been manufactured
and is used for several purposes, i.e.
evaluation design concepts, tooling,
surface measurement etc.
2m
2m
 Complexity
 The panel combines
several advanced design
principles into an fully
integrated solution, cocured in one step.
 Fulfilling very challenging
requirements regarding
surface quality
Sub spar
Stringer
Spar Cap
Rib feet
Flygteknik
2010 Stockholm,
18.okt.
2010 – 23 September 2010
SFWA WP3.1-3
Integration
Review
Port side Upper Cover & Leading Edge
20
This document and the information contained herein is the property of Saab AB and must not be used, disclosed or altered without Saab AB prior written consent.
Saab status of design and build the “HSDP”
Smart Wing demonstrator
 More comprehensive measurements
of surface and to be conducted
 Complex integration
 Lightning Strike
protection
 Integrated nose with
small radii
 Co-cured all-in-one
 Spring back
 Good laminat quality
Flygteknik
2010 Stockholm,
18.okt.
2010 – 23 September 2010
SFWA WP3.1-3
Integration
Review
Port side Upper Cover & Leading Edge
21
The CleanSky “Smart Fixed Wing Aircraft
Integrated Technology Demonstrator”
•
Final Manufacturing concept
– Final product will be much longer, more complex
– Test panel has proven tooling concept
– Test panel has proven surface quality can be very good
– Design principles has been proven
9m
Flygteknik2010
2010 Stockholm,
Stockholm 18
okt. 2010
Flygteknik
18.okt.
2010
The CleanSky “Smart Fixed Wing Aircraft
Integrated Technology Demonstrator”
Presentation Content
 Introduction
 SFWA-ITD key objectives
 SFWA-ITD large ground and flight demonstrators
 Actual status of work and planning selected demonstrators
 Conclusion
Flygteknik
Flygteknik2010
2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010
Aeronautics priority R&T in CleanSky
CLEANSKY
is of major importance for European Aeronautics R&T
to fulfil on the ambitious targets of ACARE
The special priority R&T needs for large commercial Aircraft are
covered in SFWA-ITD
• by developing an all new smart low drag wing
• by integration of innovative power plants
• through large, representative flight test demonstration
• engaging a wide range of partners from all over Europe
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Flygteknik2010
2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010
Aeronautics priority R&T in CleanSky
© 2008 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.
Flygteknik
Flygteknik2010
2010 Stockholm,
Stockholm 18
18.okt.
okt. 2010
2010