This document presents the results of an FAA investigation to determine the effects of using de-icing, as opposed to anti-icing, in aircraft turbine engine inlets. A literature search was conducted. Ice protection equipment technology was assessed. This report describes the icing/de-icing process, discusses de-ice system operation and performance and ice detector characteristics, and presents a method for determining the effects of the de-icing process on the turbine engine and its associated induction system. Keywords: Aircraft icing, De-icing systems, Ice detectors, Anti-icing. (MJM)


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    Titel :

    De-Icing of Aircraft Turbine Engine Inlets


    Beteiligte:
    H. A. Rosenthal (Autor:in) / D. O. Nelepovitz (Autor:in) / H. M. Rockholt (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    72 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    De-icing of aircraft turbine engine inlets

    Rosenthal, H.A. / Nelepovitz, D.O. / Rockholt, H.M. | Tema Archiv | 1988


    Electro-impulse de-icing of aircraft engine inlets

    NELEPOVITZ, D. / ROSENTHAL, H. | AIAA | 1986


    Computational icing analysis for aircraft inlets

    SCHUSTER, E. / FISHER, M. / GAMBILL, J. | AIAA | 1992


    Water droplet impingement on airfoils and aircraft engine inlets for icing analysis

    Papadakis, Michael / Elangovan, R. / Freund, George A., Jr. et al. | NTRS | 1991


    Test and analysis of electro-impulse de-icing systems in turbine engine inlets

    NELEPOVITZ, DON / ROSENTHAL, HERMAN / ROCKHOLT, HEATHER | AIAA | 1988