A sealing strip for sealing a gap between convexly curved aerodynamic surface elements of an aircraft such that the sealing strip has a convexly curved outer side, the sealing strip having a profile with a mid-seal section and welting sections, wherein the welting sections are arranged at end portions of the profile for fixing the sealing strip at the aerodynamic surface elements and protrude on an inner side from the mid-seal section, wherein the mid-seal section is arranged between the welting sections, wherein at least one stringer-type stiffening structure is provided on the inner side of the mid-seal section. Further, a control surface arrangement, a wing and an aircraft comprising such a sealing strip.


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    Titel :

    SEALING STRIP, CONTROL SURFACE ARRANGEMENT, AIRCRAFT WING AND AIRCRAFT


    Beteiligte:
    SCHLIPF BERNHARD (Autor:in) / LORENZ FLORIAN (Autor:in)

    Erscheinungsdatum :

    03.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16J Kolben , PISTONS / B64C AEROPLANES , Flugzeuge



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