Aircraft wings and aircraft comprising the same include at least one high-lift system(e.g., a high-lift flap) and an aerodynamic seal associated operatively with the high-lift system, the aerodynamic seal includes a non-planra angulated plate structure which has an outwardly extended planr section having a proximal edge joined to the at least one high-lift flap at the outboard and/or inboard ends thereof, and a downwardly extended planar section joined at an angle to a terminal edge of the outwardly extended planar section.
AERODYNAMIC SEALS TO REDUCE AERODYNAMIC NOISE ASSOCIATED WITH AIRCRAFT HIGH LIFT CONTROL SURFACES
AERODYNAMISCHE DICHTUNGEN ZUR VERMINDERUNG DES AERODYNAMISCHEN LÄRMS IN VERBINDUNG MIT HOCHAUFTRIEBSSTEUERFLÄCHEN VON FLUGZEUGEN
JOINTS AÉRODYNAMIQUES POUR RÉDUIRE LE BRUIT AÉRODYNAMIQUE ASSOCIÉ À DES SURFACES DE COMMANDE D'HYPERSUSTENTION D'AÉRONEF
2023-05-03
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
AERODYNAMIC SEALS TO REDUCE AERODYNAMIC NOISE ASSOCIATED WITH AIRCRAFT HIGH LIFT CONTROL SURFACES
European Patent Office | 2020
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