A leading edge structure (11) for a flow control system of an aircraft (1), including a leading edge panel (13) that surrounds a plenum (17), wherein the leading edge panel (13) has a first side portion (21), a second side portion (27), an inner surface (33) and an outer surface (37), wherein the leading edge panel (13) having micro pores (45) forming a fluid connection between the plenum (17) and the ambient flow (39), wherein a first air inlet/outlet device (49) is arranged in the first side portion (21) and a second air inlet outlet/device (51) is arranged in the second side portion (27), fluidly connected to the plenum (17), and wherein the first air inlet/outlet device (49) comprises a pivotable first door (55) and the second air inlet outlet/device (51) comprises a pivotable second door (61).


    Access

    Download


    Export, share and cite



    Title :

    Leading edge structure for a flow control system of an aircraft


    Contributors:

    Publication date :

    2024-06-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Leading edge structure for a flow control system of an aircraft

    BERTOLINI IVANO / GIAQUINTO STEFANO / WELZ SEBASTIAN et al. | European Patent Office | 2024

    Free access

    LEADING EDGE STRUCTURE FOR A FLOW CONTROL SYSTEM OF AN AIRCRAFT

    BERTOLINI IVANO / GIAQUINTO STEFANO / WELZ SEBASTIAN et al. | European Patent Office | 2023

    Free access

    Leading edge structure for a flow control system of an aircraft

    HECK CHRISTIAN | European Patent Office | 2022

    Free access

    Leading edge structure for a flow control system of an aircraft

    BÜSCHER ALEXANDER | European Patent Office | 2021

    Free access

    LEADING EDGE STRUCTURE FOR A FLOW CONTROL SYSTEM OF AN AIRCRAFT

    BÜSCHER ALEXANDER | European Patent Office | 2022

    Free access