A heated leading-edge structure (2) for an aircraft is proposed, comprising a leading edge panel (4) having an outer surface (6) configured to be contacted by an ambient flow, and an inner surface (8) opposite the outer surface (6), a rear panel (10) arranged at least partially arranged in a distance to the inner surface (8), a closed chamber (20) inside the leading-edge structure (2), a heating device (22) attached inside the chamber (20), and an air conveying device (24) in fluid communication with the heating device (22), wherein the air conveying device (24) is configured to convey air from inside the chamber (20) through the heating device (22) to be heated and returned to the chamber (20), such that a circulating flow of heated air is created inside the chamber (20).


    Access

    Download


    Export, share and cite



    Title :

    HEATED LEADING-EDGE STRUCTURE FOR AN AIRCRAFT


    Additional title:

    BEHEIZTE VORDERKANTENSTRUKTUR FÜR EIN FLUGZEUG
    STRUCTURE DE BORD D'ATTAQUE CHAUFFÉ POUR AÉRONEF


    Contributors:

    Publication date :

    2024-05-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Heated leading edge structure for aircraft

    SCHLIPF BERNHARD / LORENZ FLORIAN | European Patent Office | 2024

    Free access

    HEATED LEADING EDGE STRUCTURE FOR AN AIRCRAFT

    SCHLIPF BERNHARD / HUBER ALEXANDER / STÖVEN TIMO | European Patent Office | 2024

    Free access

    Heated leading edge structure for an aircraft

    SCHLIPF BERNHARD / HUBER ALEXANDER / STÖVEN TIMO | European Patent Office | 2023

    Free access

    HEATED LEADING EDGE STRUCTURE FOR AN AIRCRAFT

    SCHLIPF BERNHARD / HUBER ALEXANDER / STÖVEN TIMO | European Patent Office | 2022

    Free access

    HEATED LEADING-EDGE STRUCTURE FOR AN AIRCRAFT

    SCHLIPF BERNHARD / LORENZ FLORIAN | European Patent Office | 2024

    Free access