A heater mat assembly for a blade using an electrical current is provided including a first heating element region configured to generate a first amount of heat using the electrical current and disposed at a first region of the heater mat assembly. A second heating element region extends form the first heating element region and is configured to generate a second amount of heat using the electrical current. The second amount of heat is different than the first amount of heat.


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    Titel :

    HEATING DESIGN FOR ROTORCRAFT BLADE DE-ICING AND ANTI-ICING


    Beteiligte:
    ZHAO WENPING (Autor:in) / CHAUDHRY ZAFFIR A (Autor:in) / WANG JINLIANG (Autor:in) / NGUYEN DEAN (Autor:in)

    Erscheinungsdatum :

    2018-03-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



    HEATING DESIGN FOR ROTORCRAFT BLADE DE-ICING AND ANTI-ICING

    ZHAO WENPING / CHAUDHRY ZAFFIR A / WANG JINLIANG et al. | Europäisches Patentamt | 2016

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