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).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HEATED LEADING-EDGE STRUCTURE FOR AN AIRCRAFT


    Weitere Titelangaben:

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


    Beteiligte:
    LORENZ FLORIAN (Autor:in) / SCHLIPF BERNHARD (Autor:in)

    Erscheinungsdatum :

    22.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    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 | Europäisches Patentamt | 2024

    Freier Zugriff

    HEATED LEADING EDGE STRUCTURE FOR AN AIRCRAFT

    SCHLIPF BERNHARD / HUBER ALEXANDER / STÖVEN TIMO | Europäisches Patentamt | 2024

    Freier Zugriff

    Heated leading edge structure for an aircraft

    SCHLIPF BERNHARD / HUBER ALEXANDER / STÖVEN TIMO | Europäisches Patentamt | 2023

    Freier Zugriff

    HEATED LEADING EDGE STRUCTURE FOR AN AIRCRAFT

    SCHLIPF BERNHARD / HUBER ALEXANDER / STÖVEN TIMO | Europäisches Patentamt | 2022

    Freier Zugriff

    HEATED LEADING-EDGE STRUCTURE FOR AN AIRCRAFT

    SCHLIPF BERNHARD / LORENZ FLORIAN | Europäisches Patentamt | 2024

    Freier Zugriff