Electro-Impulse De-Icing (EIDI) is a method of ice removal by sharp blows delivered by a transient electromagnetic field. Detailed results are given for studies of the electrodynamic phenomena. Structural dynamic tests and computations are described. Also reported are ten sets of tests at NASA's Icing Research Tunnel and flight tests by NASA and Cessna Aircraft Company. Fabrication of system components are described and illustrated. Fatigue and electromagnetic interference tests are reported. Here, the necessary information for the design of an EIDI system for aircraft is provided.


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    Titel :

    Electro-Impulse De-Icing Testing Analysis and Design


    Beteiligte:
    G. W. Zumwalt (Autor:in) / R. L. Schrag (Autor:in) / W. D. Bernhart (Autor:in) / R. A. Friedberg (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    352 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Electro-impulse de-icing testing analysis and design

    Zumwalt, G. W. / Schrag, R. L. / Bernhart, W. D. et al. | NTRS | 1988


    Designing an electro-impulse de-icing system

    ZUMWALT, G. / FRIEDBERG, R. | AIAA | 1986



    Electro-impulse de-icing of aircraft engine inlets

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