A fairing attachment system for a wing of an aircraft comprises a high lift support structure (11) configured for movable supporting a high-lift airfoil element (17) of a wing (10) of an aircraft relative to the wing (10), a fairing device (12) extending in a lengthwise direction (X), configured for providing an aerodynamic housing of the high lift support structure (11) when attached to a surface (13) of the wing (10), and an adjustable attachment element configured for attachment of the fairing device (12) to the high lift support structure (11). The adjustable attachment element (14) is longitudinally extending and adjustable in length in order to compensate tolerances of the high lift support structure (11) relative to the wing (10) during assembly. An aircraft wing comprises the fairing attachment system. The fairing attachment system is used in a method for mounting a fairing device (12) to a wing (10) of an aircraft.
FAIRING ATTACHMENT SYSTEM FOR A WING OF AN AIRCRAFT, AIRCRAFT WING AND METHOD FOR MOUNTING A FAIRING DEVICE
VERKLEIDUNGSBEFESTIGUNGSSYSTEM FÜR EIN FLUGZEUG, FLUGZEUGFLÜGEL UND VERFAHREN ZUR MONTAGE EINER VERKLEIDUNGSVORRICHTUNG
SYSTÈME DE FIXATION DE CARÉNAGE POUR UNE AILE D'UN AÉRONEF, AILE D'AÉRONEF ET PROCÉDÉ DE MONTAGE D'UN DISPOSITIF DE CARÉNAGE
2023-11-01
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2023
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