The invention relates to a method for manufacturing a thin sheet having a thickness of 0.5 to 3.3 mm and an essentially non-recrystallized structure made of aluminum-based alloy.


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    Title :

    Thin sheets made of an aluminium-copper-lithium alloy for producing airplane fuselages


    Contributors:
    BES BERNARD (author) / CHEVY JULIETTE (author) / EBERL FRANK (author)

    Publication date :

    2019-12-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    C22F CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS OR NON-FERROUS ALLOYS , Verändern der physikalischen Struktur von Nichteisenmetallen oder Nichteisenlegierungen / B64C AEROPLANES , Flugzeuge / C22C Legierungen , ALLOYS



    Aluminium-copper-lithium alloy sheets for producing aeroplane fuselages

    CHEVY JULIETTE / BES BERNARD / EBERL FRANK et al. | European Patent Office | 2015

    Free access

    THIN SHEETS MADE OF ALUMINIUM-COPPER-LITHIUM ALLOY FOR AIRCRAFT FUSELAGE MANUFACTURE

    DAVO GUTIERREZ MARIA BELEN / PEGUET LIONEL / SAFRANY JEAN-SYLVESTRE et al. | European Patent Office | 2020

    Free access

    Shaping of airplane fuselages for minimum drag

    DODBELE, S. / VAN DAM, C. / HOLMES, B. | AIAA | 1986


    Shaping of airplane fuselages for minimum drag

    DODBELE, S. S. / VAN DAM / C. P. et al. | AIAA | 1987