An aircraft structural component having an upwardly- or downwardly-extending portion, such as a wing tip or tail fin, comprising one or more outlets for the delivery of anti-icing fluid to a first surface of the aircraft structural component. Anti-icing fluid is delivered through an outlet located at or near the tip of the upwardly-extending portion, or the base of the downwardly-extending portion. The anti-icing fluid thus delivered may, under the influence of gravity, run down the surface of the component, thereby providing the surface of the component with anti-icing fluid.


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    Titel :

    AIRCRAFT WING OR TAIL ARRANGEMENTS


    Beteiligte:
    BROWN JAMES (Autor:in)

    Erscheinungsdatum :

    03.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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