An assembly (20) is provided for a structure. This assembly (20) composite skin (26) includes a composite skin (26) and a thermal anti-icing system (24). The composite skin (26) extends between an exterior surface (28) and an interior surface (34). The thermal anti-icing system (24) includes a susceptor (36) and a waveguide (44A, 44B). The susceptor (36) and the waveguide (44A, 44B) are integrated into the composite skin (26) between the exterior surface (28) and the interior surface (34). The waveguide (44A, 44B) is configured to direct microwaves to the susceptor (36) for melting and/or preventing ice accumulation on the exterior surface (28).


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    Title :

    INTEGRATED MICROWAVE THERMAL ANTI-ICING SYSTEM


    Additional title:

    INTEGRIERTES MIKROWELLENTHERMISCHES ENTEISUNGSSYSTEM
    SYSTÈME ANTIGIVRAGE THERMIQUE INTÉGRÉ À MICRO-ONDES


    Contributors:

    Publication date :

    2023-01-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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