An anti-icing/de-icing system for an airfoil structure having multiple layers is provided and includes a thermal article, wherein the thermal article is embedded within the airfoil structure to be located between the multiple layers. The thermal article includes a first terminal end, a second terminal end and a thermal expanded mesh material which connects the first terminal end with the second terminal end, and wherein the thermal expanded mesh material is configured to have at least one predetermined resistance between the first terminal end and the second terminal end.


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    Title :

    Anti-icing/de-icing system and method


    Contributors:

    Publication date :

    2021-12-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse




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