Lightning protection system consisting of two layers of aluminum foil separated by layer of dielectric material protects graphite/epoxy composite structures on aircraft. Protective layer is secondarily applied lightning protection system, prime advantage of which is nullification of thermal and right angle effect of lightning arc attachment to graphite/epoxy laminate.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Lightning Protection for Composite Aircraft Structures


    Beteiligte:
    Olson, G. O. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1985-01-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    LIGHTNING PROTECTION FOR ADVANCED COMPOSITE AIRCRAFT STRUCTURES

    Woodrum, G. T. | SAE Technical Papers | 1970



    Lightning strike dispersion for composite aircraft structures

    SCHMIDT RYAN | Europäisches Patentamt | 2019

    Freier Zugriff

    LIGHTNING STRIKE DISPERSION FOR COMPOSITE AIRCRAFT STRUCTURES

    SCHMIDT RYAN | Europäisches Patentamt | 2024

    Freier Zugriff

    LIGHTNING STRIKE DISPERSION FOR COMPOSITE AIRCRAFT STRUCTURES

    SCHMIDT RYAN | Europäisches Patentamt | 2017

    Freier Zugriff