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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    Title :

    Aircraft wing or tail arrangement


    Contributors:
    JAMES BROWN (author)

    Publication date :

    2025-04-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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