An aircraft wing trailing edge section assembly is disclosed having an upper skin structure providing an upper external aerodynamic trailing edge surface, a lower skin structure providing a lower external aerodynamic trailing edge surface, and a movement mechanism including a first portion attached to an internal surface of the upper skin structure, a second portion attached to an internal surface of the lower skin structure, and a rotationally mounted connector member connected between the first and second portions, such that rotational movement of the connector member causes simultaneous movement of both first and second portions and therefore both upper and lower skin structures, such that the camber of the trailing edge section is changed. An aircraft wing section assembly, an aircraft and methods of operating an aircraft are disclosed.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft wing trailing edge section assembly


    Contributors:

    Publication date :

    2024-01-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT WING TRAILING EDGE SECTION ASSEMBLY

    KELLY PETER / KELLY MARK SHAUN / ALEXANDER STUART STRACHAN | European Patent Office | 2022

    Free access

    An aircraft wing trailing edge section assembly

    PETER KELLY / MARK SHAUN KELLY / STUART ALEXANDER | European Patent Office | 2022

    Free access

    AN AIRCRAFT WING TRAILING EDGE SECTION ASSEMBLY

    European Patent Office | 2021

    Free access

    Aircraft wing, trailing edge high lift assembly and aircraft

    SCHLIPF BERNHARD / HAUNERT JAN | European Patent Office | 2024

    Free access

    Aircraft wing, trailing edge high lift assembly and aircraft

    ANDREANI LUCI / KRAY DENNIS | European Patent Office | 2023

    Free access