A wing arrangement for an aircraft is disclosed including a wing having a base section with a first end portion, which is adapted to be secured to the fuselage of an aircraft, and an opposite second end portion, and a tip section with a third end portion and an opposite fourth end portion. The third end portion is pivotably connected to the second end portion such that the tip section (9) is selectively pivotable about a tip section pivot axis between a deployed position and a folded position in which the spanwise length of the wing is smaller than in the deployed position. An actuating system including an actuator and coupled between the base section and the tip section such that the actuator is operable to selectively move the tip section between the deployed position and the folded position. The actuating system includes at least one first component arranged and adapted to move upon operating the actuator.


    Access

    Download


    Export, share and cite



    Title :

    WING ARRANGEMENT FOR AN AIRCRAFT


    Contributors:
    WEDER PAUL (author) / DEGE SASKIA (author) / JEGMINAT SVENJA (author)

    Publication date :

    2019-12-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    WING ARRANGEMENT FOR AN AIRCRAFT

    WINKELMANN CHRISTOPH / ELLMERS WILFRIED / BRIANCOURT STEPHEN et al. | European Patent Office | 2018

    Free access

    Wing arrangement for an aircraft

    WINKELMANN CHRISTOPH / ELLMERS WILFRIED / BRIANCOURT STEPHEN et al. | European Patent Office | 2021

    Free access

    Aircraft wing or tail arrangement

    JAMES BROWN | European Patent Office | 2025

    Free access

    Wing arrangement for an aircraft and aircraft

    DEGE SASKIA | European Patent Office | 2022

    Free access

    Wing arrangement for an aircraft

    WEDER PAUL / DEGE SASKIA / JEGMINAT SVENJA | European Patent Office | 2022

    Free access