Ice protection systems (50) for aircraft (10), and methods of their manufacture, where the ice protection system includes a metallic substance (36) applied to a nonconductive substructure of the external skin portion (34) at a leading edge (30) of an aircraft, an electrical power source, and a conductor circuit (56) electrically connecting the power source across the metallic substance. In particular, the metallic substance may be applied to a nonconductive substructure on an annular inlet surface of an aircraft nacelle lip skin, and a power source can be electrically connected across the metallic substance.


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    Titel :

    AIRCRAFT ICE PROTECTION SYSTEMS


    Weitere Titelangaben:

    EISSCHUTZSYSTEME FÜR FLUGZEUG
    SYSTÈMES DE PROTECTION CONTRE LE GIVRE POUR AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    2023-09-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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