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.

    Les ailes d'aéronef et l'aéronef le comprenant comprennent au moins un système hypersustentateur (par exemple, un volet hypersustentateur) et un joint aérodynamique associé fonctionnellement au système hypersustentateur, le joint aérodynamique comprenant une structure de plaque angulaire non plane qui dispose d'une section plane étendue vers l'extérieur ayant un bord proximal relié au ou aux volets hypersustentateurs au niveau des extrémités extérieures et/ou intérieures de celui-ci, et une section plane s'étendant vers le bas jointe à un angle par rapport à un bord terminal de la section plane étendue vers l'extérieur.


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    Title :

    AERODYNAMIC SEALS TO REDUCE AERODYNAMIC NOISE ASSOCIATED WITH AIRCRAFT HIGH LIFT CONTROL SURFACES


    Additional title:

    JOINTS AÉRODYNAMIQUES POUR RÉDUIRE LE BRUIT AÉRODYNAMIQUE ASSOCIÉ À DES SURFACES DE COMMANDE D'HYPERSUSTENTION D'AÉRONEF



    Publication date :

    2020-06-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    AERODYNAMIC SEALS TO REDUCE AERODYNAMIC NOISE ASSOCIATED WITH AIRCRAFT HIGH LIFT CONTROL SURFACES

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    LIVERSAGE DAVID / CREW DARREN | European Patent Office | 2019

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    Aerodynamic seals

    LIVERSAGE DAVID / CREW DARREN | European Patent Office | 2022

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    Aerodynamic Noise Sources on Aircraft High Lift Slats and Flaps

    Smith, Malcolm / Chow, Stephen | AIAA | 2003


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    DAVID LIVERSAGE / DARREN CREW | European Patent Office | 2021

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