Prototype autonomous deicing system for airplane includes network of electronic and electromechanical modules at various locations in wings and connected to central data-processing unit. Small, integrated solid-state device, using long coils installed under leading edge, exciting small vibrations to detect ice and larger vibrations to knock ice off. In extension of concept, outputs of vibration sensors and other sensors used to detect rivet-line fractures, fatigue cracks, and other potentially dangerous defects.


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    Titel :

    Autonomous Deicing System For Airplane Wing


    Beteiligte:
    Hickman, G. A. (Autor:in) / Gerardi, J. J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.10.1993



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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