The application of advanced composites and of modern metal processing methods is discussed from the point of view of a European manufacturer, mainly focussed on utility and commuter aircraft in the 15 to 30 Pax category.Examples are the Dornier 228 commuter aircraft and two programs for fuselage and laminar wing technology development. A tooling and production concept for the manufacturing of integrally stiffened CFRP shells is presented.Special attention is to be given to the interiors. Early coordination between airframe and systems designers can lead to considerable cost savings.


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    Titel :

    Structures Technology of Modern General Aviation Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Rostan, Eberhard (Autor:in) / Uhse, Wolfgang (Autor:in)

    Kongress:

    General Aviation Aircraft Meeting and Exposition ; 1987



    Erscheinungsdatum :

    01.05.1987




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Structures technology of modern general aviation aircraft

    Uhse, W. / Rostan, E. | Tema Archiv | 1987


    Modern Wing Technology for General Aviation Aircraft

    M. Lotz / B. Huinink / W. Haberland et al. | NTIS | 1977


    Bonded Aircraft Structures for General Aviation

    Steiner, Norman F. | SAE Technical Papers | 1970


    Technology assessment of advanced general aviation aircraft

    Hurkamp, C. H. / Johnston, W. M. / Wilson, J. H. | NTRS | 1971


    Technology Assessment of Advanced General Aviation Aircraft

    Hurkamp, C. H. / Johnston, W. M. / Wilson, J. H. | NTRS | 1971