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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    Titel :

    Aircraft Electrical Ice Protection Systems


    Beteiligte:
    Foster, R.A. (Autor:in)


    Erscheinungsdatum :

    1968-07-01


    Format / Umfang :

    2 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Aircraft electrical ice protection systems

    Foster, R.A. | Engineering Index Backfile | 1968


    Control Systems for Aircraft Electrical Ice Protection

    Gauld, J.E.A. | Emerald Group Publishing | 1968


    PROTECTION OF ELECTRICAL SYSTEMS ON MILITARY AIRCRAFT

    Lusk, R. J. | SAE Technical Papers | 1945


    Aircraft electrical Systems

    Pallett, Edwin H. J. / Pallett, E. H. J. | TIBKAT | 1987


    Aircraft electrical systems

    Pallett, Edwin H. J. | SLUB | 1986