THERMAL protection from the effects of ice built up can be achieved by means of anti-icing or de icing. Most aircraft structures are de-iced since this consumes considerably less power, but in some cases it is essential that the surface be anti-iced, (e.g. engine intakes, where ice ingestion to the engine is unacceptable and any formation of ice must therefore be prevented).


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    Title :

    Aircraft Electrical Ice Protection Systems


    Contributors:


    Publication date :

    1968-07-01


    Size :

    2 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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