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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Advanced Fiber Placement of Composite Fuselage Structures


    Beteiligte:
    R. L. Anderson (Autor:in) / C. G. Grant (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Advanced fiber placement of composite fuselage structures

    Anderson, Robert L. / Grant, Carroll G. | NTRS | 1991


    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