The Hercules/NASA Advanced Composite Technology (ACT) program will demonstrate the low cost potential of the automated fiber placement process. The Hercules fiber placement machine was developed for cost effective production of composite aircraft structures. The process uses a low cost prepreg tow material form and achieves equivalent laminate properties to structures fabricated with prepreg tape layup. Fiber placement demonstrations planned for the Hercules/NASA program include fabrication of stiffened test panels which represent crown, keel, and window belt segments of a typical transport aircraft fuselage.


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    Titel :

    Advanced fiber placement of composite fuselage structures


    Beteiligte:


    Erscheinungsdatum :

    1991-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Advanced TOW Placement of Composite Fuselage Structure

    R. L. Anderson / C. G. Grant | NTIS | 1992


    Advanced tow placement of composite fuselage structure

    Anderson, Robert L. / Grant, Carroll G. | NTRS | 1992


    Advanced Composite Fuselage Technology

    Ilcewicz, L. B. / Smith, P. J. / Horton, R. E. et al. | British Library Conference Proceedings | 1992