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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    Title :

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


    Additional title:

    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


    Contributors:

    Publication date :

    2024-02-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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