An airfoil extension for a wing of an aircraft, the airfoil extension including an upper surface wall and a lower surface wall, the upper surface wall and the lower surface wall defining between them a profile of the airfoil extension. A structural reinforcement is disposed along the leading edge of the airfoil extension. The profile of the airfoil is configured to be modified in response to flight conditions (e.g., aerodynamic pressures acting on the upper surface wall and the lower surface wall) experienced by, on, and/or at the airfoil extension.
EXTENSION DE VOILURE POUR UNE AILE D'AERONEF
AEROFOIL EXTENSION FOR AN AIRCRAFT WING
TRAGFLÄCHENERWEITERUNG FÜR EINEN FLÜGEL EINES LUFTFAHRZEUGS
28.10.2020
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
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