Deployment system for adjusting a leading edge high lift device, in particular a slat, between a retracted position, in which, in use, the high lift device is retracted with respect to an airfoil, and at least one deployed position, in which, in use, the high lift device is deployed with respect to the airfoil, comprising at least one actuation unit that is configured to actuate the high lift device between the retracted position and the at least one deployed position, at least one guidance unit that is configured to guide the high lift device during adjustment between the retracted position and the at least one deployed position along an adjustment path, wherein the guidance unit is independent from the actuation unit.


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    Title :

    Deployment System for an Airfoil High Lift Leading Edge Device



    Publication date :

    2020-01-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Deployment system for an airfoil high lift leading edge device

    EVERAERT BOB ARMAND HENRI / VERVLIET ANTOON MARCEL / VAN KEMENADE GEERT ROGER GREET | European Patent Office | 2023

    Free access

    DEPLOYMENT SYSTEM FOR AN AIRFOIL HIGH LIFT LEADING EDGE DEVICE

    EVERAERT BOB ARMAND HENRI / VERVLIET ANTOON MARCEL / VAN KEMENADE GEERT ROGER GREET | European Patent Office | 2021

    Free access

    Aeroacoustic Study of Airfoil Leading Edge High-Lift Devices

    Andreou, Christodoulos / Graham, Will / Shin, Ho-Chul | AIAA | 2006


    Leading-edge slat optimization for maximum airfoil lift

    Olson, Lawrence E. / McGowan, Phillip R. / Guest, Clayton J. | TIBKAT | 1979


    GUIDANCE ASSEMBLY FOR AN AIRFOIL LEADING EDGE HIGH-LIFT DEVICE CARRIER TRACK

    VERVLIET ANTOON MARCEL / PAULUS IVO PETER MARIE / VERHUIZEN ALEXANDER JEAN M et al. | European Patent Office | 2021

    Free access