The following conclusions can be drawn: Several product forms and alloys are available; p=1.7-1.9 g cm(exp-3 ). Advanced alloys with good mechanical/technological properties are available. More than 33% increase in specific strength is possible and some alloys with symmetry under tension/compression. HT alloys are applicable until 200 deg C. Fatigue strength (Kt=1.0, R=0.1) is 150-220 MPa. Flammability issue is under discussion between Airbus and the FAA. Intrinsic corrosion behavior of alloys has improved. Green surface protection systems are evaluated, dependent upon alloy. Forming is possible under elevated temperatures. FSW and LBW works well and results in good properties. Buckling behavior of stiffened panels is comparable to aluminium.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    AEROMAG - magnesium suitable for aeronautic applications?


    Beteiligte:

    Erschienen in:

    Light Metal Age ; 67 , 3 ; 34-39


    Erscheinungsdatum :

    2009


    Format / Umfang :

    6 Seiten, 15 Bilder, 2 Tabellen, 3 Quellen



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    AEROMAG - Magnesium suitable for aeronautic applications?

    Hombergsmeier, Elke | Tema Archiv | 2009


    Magnesium alloys in new aeronautic equipment

    Zeumer, N. | Tema Archiv | 1998


    Structural Batteries for Aeronautic Applications

    Kühnelt, Helmut / Beutl, Alexander / Jiang, Qixiang et al. | Springer Verlag | 2025

    Freier Zugriff

    Aeronautic proposals

    Engineering Index Backfile | 1928


    AERONAUTIC CRAFT

    PERFILOV ALEKSANDR ALEKSANDROVICH | Europäisches Patentamt | 2018

    Freier Zugriff