A high-lift trailing edge flap system for an aircraft wing unit is provided. In the high-lift trailing edge flap system, the backward movement and the inclination of the trailing edge flap (2) in the extended position are dissociated in order to allow for the incorporation of an actuating mechanism (11, 12, 14, 15) into a wing (1) in the stowed position.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HIGH-LIFT TRAILING EDGE FLAP SYSTEM FOR AN AIRCRAFT WING UNIT


    Beteiligte:

    Erscheinungsdatum :

    15.04.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    High-lift trailing edge flap system for an aircraft wing unit

    GUERING BERNARD | Europäisches Patentamt | 2017

    Freier Zugriff

    Morphing Trailing Edge Flap for High Lift Wing

    Di Matteo, Natalia / Guo, Shijun | AIAA | 2011


    Morphing Trailing Edge Flap for High Lift Wing

    Di Matteo, N. / Guo, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011


    Aircraft wing, trailing edge high lift assembly and aircraft

    ANDREANI LUCI / KRAY DENNIS | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft wing, trailing edge high lift assembly and aircraft

    SCHLIPF BERNHARD / HAUNERT JAN | Europäisches Patentamt | 2024

    Freier Zugriff