An adjustable fixed structure attachment system 200 for an aircraft wing, the attachment system 200 including a bracket 210 having: 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.


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    Titel :

    MODULAR ATTACHMENT FOR LEADING AND TRAILING EDGE STRUCTURES


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

    Erscheinungsdatum :

    16.04.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Modular attachment for leading and trailing edge structures

    RODNEY EVANS / VERNON HOLMES | Europäisches Patentamt | 2020

    Freier Zugriff

    Modular attachment for leading and trailing edge structures

    RODNEY EVANS / VERNON HOLMES | Europäisches Patentamt | 2020

    Freier Zugriff

    MODULAR ATTACHMENT FOR LEADING AND TRAILING EDGE STRUCTURES

    HOLMES VERNON / EVANS RODNEY | Europäisches Patentamt | 2021

    Freier Zugriff