An aircraft includes a heat absorbent material carried by an airfoil susceptible to ice buildup and a transmitter spaced apart from the heat absorbent material. A method includes the process of transmitting the heat energy from the transmitter to the heat absorbent material that in turn warms the airfoil to break apart ice buildup. The heat absorbent material may include a first heat absorbent material secured to a suction surface of the airfoil, and a second heat absorbent material secured to a pressure surface of the airfoil.


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    Titel :

    ROTOR BLADE DE-ICING SYSTEM


    Weitere Titelangaben:

    SYSTEME DE DEGIVRAGE DE PALES DE ROTOR L


    Beteiligte:
    MCCOLLOUGH JAMES M (Autor:in) / AUBERT ROGER (Autor:in)

    Erscheinungsdatum :

    2016-02-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Rotor blade de-icing system

    MCCOLLOUGH JAMES M / AUBERT ROGER | Europäisches Patentamt | 2015

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    INVESTIGATION OF ACTIVE TWIST ROTOR FOR BLADE DE-ICING

    Schulz, M. / Riemenschneider, J. / American Helicopter Society | British Library Conference Proceedings | 2013