Damaged panels do not fail catastrophically when fabricated this way. Isogrid stiffener formed in slotted silicon-rubber tool. At grid intersections, slots offset to prevent excessive buildup of composite material and widened to give room for overlapping filaments to spread when compressed. Following total failure of skin, isogrid stiffener still carries 350 kN/m (2,000 1b/in.) and remains intact.


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    Titel :

    Continuous-Filament Isogrid Composite Panel


    Beteiligte:
    Williams, J. G. (Autor:in) / Palmer, R. J. (Autor:in) / Tucci, A. T. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.04.1985



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Filament winding of composite isogrid structures

    British Library Online Contents | 2014



    Isogrid structures

    KEY, J. / SLYSH, P. / DYER, J. et al. | AIAA | 1975


    Results of graphite-polyimide isogrid panel testing

    Hyer, M. W. / Douglas, D. O. | NTRS | 1977


    ISOGRID STIFFENING ELEMENTS

    DUPONT ANTHONY A | Europäisches Patentamt | 2018

    Freier Zugriff