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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    Titel :

    MODULAR ATTACHMENT FOR LEADING AND TRAILING EDGE STRUCTURES


    Weitere Titelangaben:

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


    Beteiligte:
    HOLMES VERNON (Autor:in) / EVANS RODNEY (Autor:in)

    Erscheinungsdatum :

    2021-06-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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    Modular attachment for leading and trailing edge structures

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    Entrainment in Leading-Edge and Trailing Vortices

    Sforza, P. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007