Disclosed is a heated leading edge structure (15) for an aircraft (1), comprising a leading edge panel (17) having an outer surface (27) configured for contact with an ambient flow (28), and an inner surface (29) opposite the outer surface (27), and comprising a heater device (19) mounted to the inner surface (29) of the leading edge panel (17) for heating of the leading edge panel (17). The object to provide a simple, lightweight and cost-efficient leading edge structure that enables a simple, quick and efficient maintenance, is achieved in that the heater device (19) is mounted to the inner surface (29) of the leading edge panel (17) in a detachable manner.


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    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 :

    2024-08-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F03D Windkraftmaschinen , WIND MOTORS



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