An aircraft wing includes a groove extending along a length between a forward extremity and an aft extremity. A forward segment of the groove extends upwardly to the forward extremity. The forward extremity is a highest point of the groove. A flap carriage is mounted to the groove and displaceable therealong. A flap is pivotably attached to the flap carriage to define a flap pivot axis about which the flap is rotatable. The flap is displaceable with the flap carriage. An actuator has an arm being extendable between an extended position and a retracted position to displace the flap carriage along the groove. The flap carriage in the retracted position being disposed in the forward segment of the groove and the flap being rotated about the flap pivot axis to position the flap trailing edge in negative flap deployment.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT WING WITH DEPLOYABLE FLAP


    Contributors:

    Publication date :

    2019-12-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT WING WITH DEPLOYABLE FLAP

    ILIESCU VLAD | European Patent Office | 2019

    Free access

    AIRCRAFT WING WITH DEPLOYABLE FLAP

    ILIESCU VLAD | European Patent Office | 2021

    Free access

    Aircraft wing with deployable flap

    ILIESCU VLAD | European Patent Office | 2021

    Free access

    Variable deployable wing flap

    NEIL JOHN LYONS / JAMES ALDERMAN | European Patent Office | 2020

    Free access

    Deployable wing for an aircraft

    KEAVNEY THOMAS E / BAUER ROBERT E | European Patent Office | 2020

    Free access