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


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    Title :

    ACTUATOR ASSEMBLIES TO DEPLOY AIRCRAFT LEADING EDGE FLAPS AND SEALS FOR AIRCRAFT LEADING EDGE FLAPS


    Contributors:

    Publication date :

    2018-12-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    ACTUATOR ASSEMBLIES TO DEPLOY AIRCRAFT LEADING EDGE FLAPS AND SEALS FOR AIRCRAFT LEADING EDGE FLAPS

    JOHNSON PATTERSON / SAKURAI SEIYA / SANTINI GREGORY M et al. | European Patent Office | 2023

    Free access

    ACTUATOR ASSEMBLIES TO DEPLOY AIRCRAFT LEADING EDGE FLAPS AND SEALS FOR AIRCRAFT LEADING EDGE FLAPS

    PATTERSON JOHNSON / SAKURAI SEIYA / GREGORY M SANTINI et al. | European Patent Office | 2019

    Free access

    Actuator assemblies to deploy aircraft leading edge flaps and seals for aircraft leading edge flaps

    JOHNSON PATTERSON / SAKURAI SEIYA / SANTINI GREGORY M et al. | European Patent Office | 2019

    Free access

    Leading-Edge Flaps and Variable Camber

    Emerald Group Publishing | 1953


    Leading-edge flaps and variable camber

    Engineering Index Backfile | 1953