closing of clean sky 1 sfwa-itd blade project. sfwa... · sfwa-itd blade project by daniel kierbel...
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Closing of Clean Sky 1 SFWA-ITD
BLADE project by Daniel KIERBEL (AIRBUS SAS)
Brussels 21st & 22nd March 2017
Innovation takes off
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Aircraft DPM
CS Event Brussels – 21st & 22nd March 2017
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Laminar technology
Up to 8% Aircraft drag reduction potential at Mach 0.75 vs. a turbulent wing
Up to 4,6% fuel burn saving on 800 NM mission
Mastering aerodynamic instability => laminar/turbulent transition
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What influences the existence of a natural laminar flow on an industrial wing ?
Leading edge and wing contamination: insects, grease, de-icing fluids, scratches, dents, erosion, dust, …
Atmospheric disturbances
Acoustic disturbances and vibrations
Wing global deformation
Wing local deformation
Joint & filler deformation
Fastener head deformation
System integration
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16 European key partners
500 Contributors
6500 Parts
123 Flight Test Hours planned
2000 Parameters to capture
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Wing Architectures
Starboard wing Port wing
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Design Freeze
alibration Plate
Infrared Camera 1
Infrared Camera 2
Trailing Cone Tube
Flow Cone Cameras
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Advanced FTI Technologies
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Components Manufacturing
Integration
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Wing Assembly Start
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Latest Achievements
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SFWA-ITD Consortium Confidential
©2014 by the Clean Sky Leading Partners: Airbus, Agusta Westland, Alenia Aermacchi, Dassault Aviation, EADS-CASA, Fraunhofer Institute, Liebbherr-Aerospace, Rolls-Royce, Saab AB, Safran, Thales & 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.
SFWA-ITD:CS closing event 21 & 22 March 2017,
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