Disclosed is an adjustable fixed structure attachment system (200) for an aircraft wing, the attachment system (200) comprising a bracket (210), comprising: a wall (212) for connection to a wing box, a protrusion (214) protruding from the wall (212), and a slot (216) extending through the protrusion (214), wherein the slot (216) has a height and a width, and a bush (220) having a bore (222) extending therethrough for receipt of a pin, wherein the bush (222) is insertable into the slot (216) and dimensioned relative to the slot (216) so that the bush (220) is substantially immovable in a width-wise direction of the slot (216), and is moveable in a height-wise direction of the slot (216) to thereby vary a position of the bush (220) within the slot (216). Also disclosed are fixed structure attachment arrangements for aircraft wings, modular aircraft wing portions, leading or trailing edge attachment systems for aircraft wings, and aircraft.


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    Title :

    MODULAR ATTACHMENT FOR LEADING AND TRAILING EDGE STRUCTURES


    Additional title:

    MODULARER AUFSATZ FÜR VORDER- UND HINTERKANTENSTRUKTUREN
    FIXATION MODULAIRE POUR STRUCTURES DE BORD D'ATTAQUE ET DE FUITE


    Contributors:

    Publication date :

    2021-06-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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    Modular attachment for leading and trailing edge structures

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