An approach to show the potential to improve aircraft fuselages with the application of a multi-disciplinary design philosophy is discussed. It is found that aluminum is the common metal being used in all the aircraft for the design purposes. This evolution of the aluminum airplane structure has led to the current over-optimized stiffened skin structure. It is also found that both the combination of composite materials with the sandwich concept is very attractive and both thermosets and thermoplastic polymers can be applied for airplanes.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Multi-disciplinary design philosophy for aircraft fuselages. Part I


    Beteiligte:
    Beukers, A. (Autor:in) / Van Tooren, M.J.L. (Autor:in) / De Jong, T. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2005


    Format / Umfang :

    9 Seiten, 4 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    AIRCRAFT FUSELAGES

    DETERT BRUCE RAYMOND | Europäisches Patentamt | 2016

    Freier Zugriff

    AIRCRAFT FUSELAGES

    DETERT BRUCE RAYMOND | Europäisches Patentamt | 2017

    Freier Zugriff

    Aircraft fuselages

    DETERT BRUCE RAYMOND | Europäisches Patentamt | 2015

    Freier Zugriff

    Aircraft fuselages

    DETERT BRUCE RAYMOND | Europäisches Patentamt | 2020

    Freier Zugriff

    Aircraft fuselages

    DETERT BRUCE RAYMOND | Europäisches Patentamt | 2017

    Freier Zugriff