Various methods for eliminating static charge were evaluated on basis of data derived from field tests; active and passive corona discharge systems were installed in H-37 aircraft for evaluation; active system provided adequate control of aircraft charge potential; system was designed to maintain automatically near-zero charge and tested; in hover attitude, at altitude of 25 ft, aircraft charge was reduced to zero in 5 sec, and thereafter maintained within predetermined limits; residual charge voltage, measured with respect to ground, was on order of +300 v.


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    Titel :

    Automatic control of static electricity for helicopters


    Weitere Titelangaben:

    Am Helicopter Soc -- J


    Beteiligte:
    Tona, C.J. (Autor:in) / Hayman, R.A. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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