IMPROVED DAMAGE TOLERANT ALUMINUM 6XXX ALLOY
    1.
    发明授权
    IMPROVED DAMAGE TOLERANT ALUMINUM 6XXX ALLOY 失效
    具有改进的6XXX损伤性能铝合金

    公开(公告)号:EP0826072B1

    公开(公告)日:2003-07-02

    申请号:EP96913805.6

    申请日:1996-04-24

    IPC分类号: C22F1/04

    摘要: A method of producing an aluminum product having high formability, high fracture toughness, high strength and improved corrosion resistance, the method comprising: (a) providing stock including an aluminum base alloy consisting essentially of about 0.7 to 1.0 wt.% silicon, not more than about 0.3 wt.% iron, not more than about 0.5 wt.% copper, about 0.8 to 1.1 wt.% magnesium, about 0.3 to 0.4 wt.% manganese, and about 0.5 to 0.8 wt.% zinc, the remainder substantially aluminum, incidental elements and impurities; (b) homogenizing the stock; (c) hot rolling; (d) solution heat treating; (e) cooling by quenching; and (f) artificially aging to produce a T6 temper in the aluminum product. The figure shows ductility loss as a function of the amount of copper in alloys containing either manganese or chromium and zinc relative to alloy 6013.

    A METHOD OF MANUFACTURING ALUMINUM AIRCRAFT SHEET
    2.
    发明公开
    A METHOD OF MANUFACTURING ALUMINUM AIRCRAFT SHEET 失效
    一种制造铝合金飞机板的方法

    公开(公告)号:EP0817870A1

    公开(公告)日:1998-01-14

    申请号:EP96911294.0

    申请日:1996-03-20

    IPC分类号: C22F1 C22C21

    CPC分类号: C22C21/16 C22F1/057

    摘要: A method of producing an aluminum product comprising: providing stock including an aluminum alloy comprising about 4.0 to 4.4 wt.% copper, about 1.25 to 1.5 wt.% magnesium, about 0.35 to 0.5 wt.% manganese, not more than 0.12 wt.% silicon, not more than 0.08 wt.% iron, not more than 0.06 wt.% titanium, the remainder substantially aluminum, incidental elements and impurities; hot working the stock; annealing; cold rolling; solution heat treating; cooling; holding for at least 12 hours at room temperature; and cold working from about 4 % to 7 % thereby producing a product having increased strength and toughness properties. The figure shows composition-phase relations for an Al-Cu-Mg system at 930 °F.

    摘要翻译: 一种生产铝产品的方法,包括:提供包含铝合金的原料,所述铝合金包含约4.0-4.4重量%的铜,约1.25-1.5重量%的镁,约0.35-0.5重量%的锰,不超过0.12重量% 硅,不多于0.08重量%的铁,不多于0.06重量%的钛,其余基本上为铝,偶存元素和杂质; 热炒股票; 退火; 冷轧; 固溶热处理; 冷却; 在室温下保持至少12小时; 并且冷加工约4%至7%,从而生产具有增加的强度和韧性性能的产品。 该图显示了930°F时Al-Cu-Mg体系的组成相关系。

    ALUMINUM-MAGNESIUM-SCANDIUM ALLOYS WITH ZINC AND COPPER
    4.
    发明授权
    ALUMINUM-MAGNESIUM-SCANDIUM ALLOYS WITH ZINC AND COPPER 有权
    与锌的铜,铝,镁合金钪

    公开(公告)号:EP1212473B1

    公开(公告)日:2004-01-21

    申请号:EP00950416.8

    申请日:2000-08-02

    IPC分类号: C22C21/06

    CPC分类号: C22C21/06

    摘要: Al-Mg-Sc based alloys include additional elements selected from the group comprising Hf, Mn, Zr, Cu and Zn to improve their tensile properties. The alloys are preferably comprised of aluminum and, in wt.%, 1.0-8.0 % Mg, 0.05-0,6 % Sc, 0.05-0.20 % Hf and/or 0.05-0.20 % Zr, and 0.5-2.0 % Cu and/or 0.5-2.0 % Zn. In addition, 0.1-0.8 wt.% Mn may be added to the alloy to improve its strength characteristics further.

    IMPROVED DAMAGE TOLERANT ALUMINUM 6XXX ALLOY
    5.
    发明公开
    IMPROVED DAMAGE TOLERANT ALUMINUM 6XXX ALLOY 失效
    具有改进的6XXX损伤性能铝合金

    公开(公告)号:EP0826072A1

    公开(公告)日:1998-03-04

    申请号:EP96913805.0

    申请日:1996-04-24

    IPC分类号: C22C21 C22F1

    摘要: A method of producing an aluminum product having high formability, high fracture toughness, high strength and improved corrosion resistance, the method comprising: (a) providing stock including an aluminum base alloy consisting essentially of about 0.7 to 1.0 wt.% silicon, not more than about 0.3 wt.% iron, not more than about 0.5 wt.% copper, about 0.8 to 1.1 wt.% magnesium, about 0.3 to 0.4 wt.% manganese, and about 0.5 to 0.8 wt.% zinc, the remainder substantially aluminum, incidental elements and impurities; (b) homogenizing the stock; (c) hot rolling; (d) solution heat treating; (e) cooling by quenching; and (f) artificially aging to produce a T6 temper in the aluminum product. The figure shows ductility loss as a function of the amount of copper in alloys containing either manganese or chromium and zinc relative to alloy 6013.