A multilayer structure for deicing an aircraft airfoil component includes an electrically and thermally insulating bottom layer formed in a defined pattern, preferably directly on the aircraft airfoil component, an electrothermal middle layer of electrically resistant heater element arrays formed in the defined pattern on the electrically and thermally insulating bottom layer, and a thermally conductive and electrically insulating top layer encapsulating the electrically and thermally insulating bottom layer and the electrothermal middle layer of electrically resistant heater element arrays. The multilayer structure may be directly applied to the airfoil component by direct writing/additive manufacturing, which may be done with the assistance of a multi-axis robot.


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    Title :

    MULTILAYER STRUCTURE FOR DEICING AN AIRCRAFT AIRFOIL COMPONENT AND METHOD OF MANUFACTURE THEREOF


    Additional title:

    MEHRSCHICHTIGE STRUKTUR ZUR ENTEISUNG EINER FLUGZEUGTRAGFLÄCHENKOMPONENTE UND VERFAHREN ZU DEREN HERSTELLUNG
    STRUCTURE MULTICOUCHE POUR LE DÉGIVRAGE D'UN COMPOSANT D'AILE D'AÉRONEF ET SON PROCÉDÉ DE FABRICATION


    Contributors:

    Publication date :

    2019-11-27


    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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