A dual primary deicing system for a rotary-wing aircraft, according to an exemplary aspect of the present disclosure includes, among other things, an electrothermal heating element system; and a controller in communication with said electrothermal heating element, said controller communicating a heating cycle to said electrothermal heating element system, said heating cycle defining a first electric pulse train associated with a main rotor blade assembly.


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    Title :

    DUAL-CHANNEL DEICING SYSTEM FOR A ROTARY WING AIRCRAFT


    Additional title:

    DOPPELKANALENTEISUNGSSYSTEM FÜR DREHFLÜGELFLUGZEUG
    SYSTEME DE DEGIVRAGE A DOUBLE PASSAGE POUR AERONEF A VOILURE TOURNANTE


    Contributors:

    Publication date :

    2017-03-08


    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 / H05B ELECTRIC HEATING , Elektrische Heizung



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