Thermal protection from effects of ice built up can be achieved by means of anti-icing or de-icing; two distinct types of anti-icing are total evaporative system and wet `run back' system; de-icing system allows ice to form on protected surface for short periods, after which ice is removed by application of heat to selected areas, in rotation; examples of de-icing systems are engine air intakes, leading edges of aerofoil surfaces, helicopter rotor blades and propeller blades; heating requirements and design calculations.


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    Title :

    Aircraft electrical ice protection systems


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1968


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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