An assembly is provided for an aircraft propulsion system. This assembly includes a nacelle inlet structure and a microwave system. The nacelle inlet structure extends circumferentially about a centerline. The nacelle inlet structure includes an exterior skin. The exterior skin includes dielectric material. The microwave system is configured to direct microwaves to the dielectric material for melting and/or preventing ice accumulation on the exterior skin.


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    Title :

    THERMAL ANTI-ICING SYSTEM WITH MICROWAVE SYSTEM


    Contributors:

    Publication date :

    2021-05-06


    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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