An aircraft wing 200 comprises a Krueger flap 215 with an anti-icing system. The anti-icing system comprises a conduit 201 that is configured to provide hot air to an interior surface of the leading edge of the wing 200. The conduit 201 of the anti-icing system structurally supports at least part of the weight of the Krueger flap 215 by means of a support bracket 230. The flap is actuated by a drive shaft 223.


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    Titel :

    Aircraft wing with anti-icing system and Krueger flap


    Beteiligte:

    Erscheinungsdatum :

    2021-05-19


    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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