Ice protection systems for aircraft, and methods of their manufacture, where the ice protection system includes a metallic substance applied to a nonconductive substructure of the external skin portion at a leading edge of an aircraft, an electrical power source, and a conductor circuit 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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    Title :

    AIRCRAFT ICE PROTECTION SYSTEMS


    Contributors:

    Publication date :

    2020-01-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H05B ELECTRIC HEATING , Elektrische Heizung



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