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.


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    Title :

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


    Contributors:

    Publication date :

    2015-04-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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