Example actuator assemblies (224) to deploy aircraft leading edge flaps and seals for aircraft leading edge flaps (202) are described herein. An example apparatus includes an aircraft flap (202) that is movable between a stowed position and a deployed position. The flap includes a top panel (308). A notch (372) is formed in the top panel and extends into a side of the top panel near a trailing edge (313) of the flap. The example apparatus also includes a seal (1000) coupled to the flap. The seal (1000) is movable to cover the notch (372) when the flap (202) is in the deployed position.


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    Titel :

    AIRCRAFT LEADING EDGE FLAP AND METHOD TO DEPLOY A LEADING EDGE FLAP


    Weitere Titelangaben:

    FLUGZEUGVORDERKANTENKLAPPE UND VERFAHREN ZUM AUSFAHREN EINER VORDERKANTENKLAPPE
    VOLET DE BORD D'ATTAQUE DE L'AVION ET MÉTHODE POUR DÉPLOYER UN VOLET DE BORD D'ATTAQUE


    Beteiligte:

    Erscheinungsdatum :

    14.02.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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