Disclosed is an aerodynamic sealing (1) as well as a wing (23) for an aircraft comprising such sealing (1). The sealing (1) comprises: an elastic first sealing wall (5) extending between a first bottom edge (13) and a first tip edge (15); an elastic second sealing wall (7) extending between a second bottom edge (17) and a second tip edge (19), and extending convergent with respect to the first sealing wall (5), so that the first and second sealing walls (5, 7) are joined together at their first and second tip edges (15, 19) to form a tip line (21); a bottom element (9) connecting the first bottom edge (13) to the second bottom edge (17), wherein the bottom element (9) is joined to both the first sealing wall (5) and the second sealing wall (7); and a plurality of stiffening elements (11) connecting the first sealing wall (5) to the second sealing wall (7) between the tip line (21) and the bottom element (9), wherein the stiffening elements (11) are spaced apart from one another and joined to both the first sealing wall (5) and the second sealing wall (7).
AERODYNAMIC SEALING AND WING FOR AN AIRCRAFT COMPRISING SUCH SEALING
AERODYNAMISCHE DICHTUNG UND FLÜGEL FÜR EIN FLUGZEUG MIT SOLCH EINER DICHTUNG
JOINT D'ÉTANCHÉITÉ AÉRODYNAMIQUE ET AILE POUR AÉRONEF COMPRENANT UN TEL JOINT D'ÉTANCHÉITÉ
2018-11-07
Patent
Electronic Resource
English
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