An aircraft airflow modification device 301, comprising: at least one resiliently deformable base member 305; and at least one resiliently deformable flap member 303 that extends from the resiliently deformable base member 305, wherein deformation of the resiliently deformable base member 305 from a first state to a second state results in corresponding deformation of the resiliently deformable flap member 303 from a first state to a second state.


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    Title :

    AIRCRAFT AIRFLOW MODIFICATION DEVICE AND VORTEX GENERATOR ARRANGEMENT FOR AN AIRCRAFT


    Additional title:

    FLUGZEUGLUFTSTROMMODIFIZIERUNGSVORRICHTUNG UND WIRBELGENERATORANORDNUNG FÜR EIN FLUGZEUG
    DISPOSITIF DE MODIFICATION D'ÉCOULEMENT D'AIR D'UN AÉRONEF ET DISPOSITIF DE GÉNÉRATION DE TOURBILLONS POUR UN AÉRONEF


    Contributors:

    Publication date :

    2020-01-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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