A fairing attachment system for a wing of an aircraft includes a high lift support structure configured to movably support a high-lift airfoil element of a wing of an aircraft relative to the wing. The system includes a fairing device extending in a lengthwise direction, configured to provide an aerodynamic housing of the high lift support structure when attached to a surface of the wing, and an adjustable attachment element configured to attach the fairing device to the high lift support structure. The adjustable attachment element is longitudinally extending and adjustable in length to compensate for tolerances of the high lift support structure relative to the wing during assembly. An aircraft wing includes the fairing attachment system. The fairing attachment system is used in a method for mounting a fairing device to a wing of an aircraft.


    Access

    Download


    Export, share and cite



    Title :

    FAIRING ATTACHMENT SYSTEM FOR A WING OF AN AIRCRAFT, AIRCRAFT WING AND METHOD FOR MOUNTING A FAIRING DEVICE


    Contributors:

    Publication date :

    2023-11-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge




    Aircraft wing and wing tip device with fairing

    ERIC WILDMAN / MATT HARDING / ALAN HADDRELL | European Patent Office | 2019

    Free access

    Aircraft wing and wing tip device with fairing

    European Patent Office | 2017

    Free access

    Rotor wing fairing of composite wing aircraft

    YU LEI / WU WENHUA / TU MENGLEI et al. | European Patent Office | 2021

    Free access

    AIRCRAFT WING FAIRING DRIVE ASSEMBLY SYSTEM AND METHOD

    European Patent Office | 2023

    Free access