Distributed trailing edge wing flap systems are described. An example wing flap system for an aircraft includes a flap and an actuator. The flap is movable between a deployed position and a retracted position relative to a fixed trailing edge of a wing of the aircraft. The actuator is to move the flap relative to the fixed trailing edge. The actuator is hydraulically drivable via first pressurized hydraulic fluid to be supplied by a hydraulic system of the aircraft. The actuator is also hydraulically drivable via second pressurized hydraulic fluid to be supplied by a local power unit. The local power unit is selectively connectable to an electrical system of the aircraft. The electrical system is to power the local power unit to supply the second pressurized hydraulic fluid.


    Access

    Download


    Export, share and cite



    Title :

    DISTRIBUTED TRAILING EDGE WING FLAP SYSTEMS


    Contributors:

    Publication date :

    2019-07-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Distributed trailing edge wing flap systems

    HUYNH NEAL V | European Patent Office | 2021

    Free access

    DISTRIBUTED TRAILING EDGE WING FLAP SYSTEMS

    HUYNH NEAL V | European Patent Office | 2019

    Free access

    Distributed trailing edge wing flap systems

    HUYNH NEAL V | European Patent Office | 2021

    Free access

    DISTRIBUTED TRAILING EDGE WING FLAP SYSTEMS

    HUYNH NEAL V | European Patent Office | 2020

    Free access

    Distributed trailing edge wing flap systems

    HUYNH NEAL V | European Patent Office | 2020

    Free access