An aircraft wing 101 or tail arrangement (figure 8) is provided comprising an aircraft wing tip portion T or tail fin (T, figure 8), and one or more outlets 102- 116 for the delivery of anti-icing fluid to a surface of the aircraft wing tip portion or tail fin. The anti-icing system may also be applicable to folding wing tips.


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    Titel :

    Aircraft wing or tail arrangement


    Beteiligte:
    JAMES BROWN (Autor:in)

    Erscheinungsdatum :

    09.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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