The invention provides a leading edge (1) for an airfoil of an aircraft comprising a leading plate (2) with a convex side (21) and a concave side (22), at least one container (3) filled with a non-Newtonian fluid, wherein the leading edge is configured to be secured to the torsion box (10) of the airfoil, the at least one container (3) being arranged between the concave side (22) of the leading plate (2) and the torsion box (10) of the airfoil. The invention also provides an airfoil comprising such leading edge and a method for assembling such leading edge.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    LEADING EDGE FOR AN AIRFOIL


    Weitere Titelangaben:

    VORDERKANTE FÜR EINE TRAGFLÄCHE
    BORD D'ATTAQUE POUR UN PROFIL AÉRODYNAMIQUE



    Erscheinungsdatum :

    2022-02-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Morphing airfoil leading edge

    GRIP ROBERT E / BROWN JOHN J / HARRISON NEAL A et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    MORPHING AIRFOIL LEADING EDGE

    GRIP ROBERT E / BROWN JOHN J / HARRISON NEAL A et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    MORPHING AIRFOIL LEADING EDGE

    ROBERT E GRIP / JOHN J BROWN / NEAL A HARRISON et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    Morphing airfoil leading edge

    BLAINE K RAWDON / JOHN C VASSBERG / ROBERT E GRIP et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    MORPHING AIRFOIL LEADING EDGE

    GRIP ROBERT E / BROWN JOHN J / HARRISON NEAL A et al. | Europäisches Patentamt | 2017

    Freier Zugriff