An assembly is provided for an aircraft propulsion system. This assembly includes a nacelle inlet structure (22) and a microwave system (80). The nacelle inlet structure extends circumferentially about a centerline (16). The nacelle inlet structure includes an exterior skin (78). The exterior skin includes dielectric material (82). The microwave system is configured to direct microwaves (88) 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


    Additional title:

    THERMISCHES VEREISUNGSSCHUTZSYSTEM MIT MIKROWELLENSYSTEM
    SYSTÈME ANTIGIVRAGE THERMIQUE COMPRENANT UN SYSTÈME À MICRO-ONDES


    Contributors:

    Publication date :

    2023-03-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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