The patent relates to an apparatus that improves external load modal damping, provides the pilot command control augmentation of the load, and minimizes pilot induced oscillation, and is universally adaptable to a wide variety of helicopters. The apparatus contemplates rigid pendants which damp load motion in response to a sensor.


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    Titel :

    External Load Stabilization Apparatus


    Beteiligte:
    J. H. Smith (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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