Method of manufacturing aluminum aircraft sheet
    1.
    发明授权
    Method of manufacturing aluminum aircraft sheet 失效
    制造铝飞机板的方法

    公开(公告)号:US5938867A

    公开(公告)日:1999-08-17

    申请号:US824555

    申请日:1997-03-25

    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 at 725-875.degree. F.; 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.

    摘要翻译: 一种生产铝产品的方法,包括提供包含约4.0至4.4wt。 %铜,约1.25至1.5wt。 %镁,约0.35至0.5wt。 %锰,不超过0.12wt。 %硅,不大于0.08wt。 %铁,不超过0.06重量% %钛,余量基本为铝,附带元素和杂质; 热点库存; 退火725-875°F。 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%,从而产生具有增强的强度和韧性的产品。

    High Strength Aluminum Alloys and Process for Making the Same
    2.
    发明申请
    High Strength Aluminum Alloys and Process for Making the Same 有权
    高强度铝合金及其制造方法

    公开(公告)号:US20110150696A1

    公开(公告)日:2011-06-23

    申请号:US12980874

    申请日:2010-12-29

    IPC分类号: C22C21/10

    CPC分类号: C22C21/10

    摘要: High strength aluminum alloys based on the Al—Zn—Mg—Cu alloy system preferably include high levels of zinc and copper, but modest levels of magnesium, to provide increased tensile strength without sacrificing toughness. Preferred ranges of the elements include by weight, 8.5-10.5% Zn, 1.4-1.85% Mg, 2.25-3.0% Cu and at least one element from the group Zr, V, or Hf not exceeding about 0.5%, the balance substantially aluminum and incidental impurities. In addition, small amounts of scandium (0.05-0.30%) are also preferably employed to prevent recrystallization. During formation of the alloys, homogenization, solution heat treating and artificial aging processes are preferably employed.

    摘要翻译: 基于Al-Zn-Mg-Cu合金系统的高强度铝合金优选包括高水平的锌和铜,但适度的镁,以提供增加的拉伸强度而不牺牲韧性。 元素的优选范围包括8.5-10.5%的Zn,1.4-1.85%的Mg,2.25-3.0%的Cu和至少一种来自Zr,V或Hf的元素不超过约0.5%,余量基本上为铝 和杂质。 此外,还优选使用少量钪(0.05-0.30%)以防止重结晶。 在合金形成期间,优选使用均化,固溶热处理和人造时效处理。

    Aluminum-copper-magnesium-manganese alloy useful for aircraft
applications
    3.
    发明授权
    Aluminum-copper-magnesium-manganese alloy useful for aircraft applications 失效
    用于飞机应用的铝 - 铜 - 镁 - 锰合金

    公开(公告)号:US5897720A

    公开(公告)日:1999-04-27

    申请号:US768801

    申请日:1996-12-18

    申请人: Ralph C. Dorward

    发明人: Ralph C. Dorward

    IPC分类号: C22C21/16 C22F1/057 C22F1/04

    CPC分类号: C22C21/16 C22F1/057

    摘要: A product comprising an aluminum base alloy including about 3.8 wt. % copper, about 1.2 wt. % magnesium, about 0.3 to 0.6 wt. % manganese, not more than about 0.15 wt. % silicon, not more than about 0.12 wt. % iron, not more than about 0.1 wt. % titanium, the remainder substantially aluminum, incidental elements and impurities, the product having at least 5% improvement over 2024 alloy in fracture toughness, fatigue crack growth rate, corrosion resistance, and formability properties.

    摘要翻译: 一种包含铝基合金的产品,其包含约3.8重量% %铜,约1.2重量% %镁,约0.3-0.6wt。 %锰,不大于约0.15wt。 %硅,不大于约0.12wt。 %铁,不超过约0.1wt。 %钛,余量基本上为铝,偶然元素和杂质,该产品的断裂韧性,疲劳裂纹扩展速率,耐腐蚀性和成形性均优于2024合金,提高至少5%。

    High strength aluminum alloys and process for making the same
    4.
    发明授权
    High strength aluminum alloys and process for making the same 有权
    高强度铝合金及其制造方法

    公开(公告)号:US09410229B2

    公开(公告)日:2016-08-09

    申请号:US12980874

    申请日:2010-12-29

    IPC分类号: C22C21/10

    CPC分类号: C22C21/10

    摘要: High strength aluminum alloys based on the Al—Zn—Mg—Cu alloy system preferably include high levels of zinc and copper, but modest levels of magnesium, to provide increased tensile strength without sacrificing toughness. Preferred ranges of the elements include by weight, 8.5-10.5% Zn, 1.4-1.85% Mg, 2.25-3.0% Cu and at least one element from the group Zr, V, or Hf not exceeding about 0.5%, the balance substantially aluminum and incidental impurities. In addition, small amounts of scandium (0.05-0.30%) are also preferably employed to prevent recrystallization. During formation of the alloys, homogenization, solution heat treating and artificial aging processes are preferably employed.

    摘要翻译: 基于Al-Zn-Mg-Cu合金系统的高强度铝合金优选包括高水平的锌和铜,但适度的镁,以提供增加的拉伸强度而不牺牲韧性。 元素的优选范围包括8.5-10.5%的Zn,1.4-1.85%的Mg,2.25-3.0%的Cu和至少一种来自Zr,V或Hf的元素不超过约0.5%,余量基本上为铝 和杂质。 此外,还优选使用少量钪(0.05-0.30%)以防止重结晶。 在合金形成期间,优选使用均化,固溶热处理和人造时效处理。

    Aluminum-magnesium-scandium alloys with zinc and copper
    5.
    发明授权
    Aluminum-magnesium-scandium alloys with zinc and copper 有权
    具有锌和铜的铝 - 镁 - 钪合金

    公开(公告)号:US6139653A

    公开(公告)日:2000-10-31

    申请号:US372979

    申请日:1999-08-12

    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.

    摘要翻译: Al-Mg-Sc基合金包括选自Hf,Mn,Zr,Cu和Zn的另外的元素以改善其拉伸性能。 合金优选由铝组成,以重量计。 %,1.0-8.0%Mg,0.05-0.6%Sc,0.05-0.20%Hf和/或0.05-0.20%Zr,以及0.5-2.0%Cu和/或0.5-2.0%Zn。 另外,0.1-0.8wt。 可以将Mn添加到合金中以进一步提高其强度特性。

    High strength aluminum alloys and process for making the same
    6.
    发明申请
    High strength aluminum alloys and process for making the same 审中-公开
    高强度铝合金及其制造方法

    公开(公告)号:US20100180988A1

    公开(公告)日:2010-07-22

    申请号:US12591956

    申请日:2009-12-04

    IPC分类号: C22F1/053

    CPC分类号: C22C21/10 C22F1/053

    摘要: High strength aluminum alloys based on the Al—Zn—Mg—Cu alloy system preferably include high levels of zinc and copper, but modest levels of magnesium, to provide increased tensile strength without sacrificing toughness. Preferred ranges of the elements include by weight, 8.5-10.5% Zn, 1.4-1.85% Mg, 2.25-3.0% Cu and at least one element from the group Zr, V, or Hf not exceeding about 0.5%, the balance substantially aluminum and incidental impurities. In addition, small amounts of scandium (0.05-0.30%) are also preferably employed to prevent recrystallization. During formation of the alloys, homogenization, solution heat treating and artificial aging processes are preferably employed.

    摘要翻译: 基于Al-Zn-Mg-Cu合金系统的高强度铝合金优选包括高水平的锌和铜,但适度的镁,以提供增加的拉伸强度而不牺牲韧性。 元素的优选范围包括8.5-10.5%的Zn,1.4-1.85%的Mg,2.25-3.0%的Cu和至少一种来自Zr,V或Hf的元素不超过约0.5%,余量基本上为铝 和杂质。 此外,还优选使用少量钪(0.05-0.30%)以防止重结晶。 在合金形成期间,优选使用均化,固溶热处理和人造时效处理。

    Production of high quality machinable tolling plate using brazing sheet
scrap
    7.
    发明授权
    Production of high quality machinable tolling plate using brazing sheet scrap 失效
    生产高品质可加工的收割板,采用钎焊片材废料

    公开(公告)号:US6004409A

    公开(公告)日:1999-12-21

    申请号:US12010

    申请日:1998-01-22

    摘要: The present invention is a process to use aluminum alloy scrap to manufacture high quality machinable tooling plate. This is an new use for this scrap which has heretofore been used in lower quality products. The tooling plate thus made has superior properties when machined as it produces smaller chips and/or a limited of spirals from the plate. Large chips and long spirals create problems and a smaller chip greatly facilitates the machining operation.

    摘要翻译: 本发明是使用铝合金废料来制造高品质可加工工具板的方法。 这是迄今为止在低质量产品中使用的这种废料的新用途。 如此制造的加工板在加工时具有优异的性能,因为它从板产生较小的切屑和/或限制的螺旋。 大芯片和长螺旋产生问题,较小的芯片极大地促进了加工操作。

    Aluminum alloy having improved damage tolerant characteristics
    8.
    发明授权
    Aluminum alloy having improved damage tolerant characteristics 失效
    具有改善的耐损伤特性的铝合金

    公开(公告)号:US5888320A

    公开(公告)日:1999-03-30

    申请号:US803718

    申请日:1997-02-21

    申请人: Ralph C. Dorward

    发明人: Ralph C. Dorward

    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 at a temperature ranging from about 950.degree. to 1050.degree. F. for a time period ranging from about 2 to 20 hours; (c) hot rolling at a temperature ranging from about 750.degree. to 950.degree. F. will increase; (d) solution heat treating at a temperature ranging from about 1000.degree. to 1080.degree. F. for a time period ranging from about 5 minutes to one hour; (e) cooling by quenching at a rate of about 1000.degree. F./second to a temperature of 100.degree. F. or lower; and (f) artificially aging by reheating to a temperature ranging from about 300.degree. to 400.degree. F. for a time period ranging from about 2 to 20 hours to produce a T6 temper in the aluminum product.

    摘要翻译: 一种生产具有高成形性的高断裂韧性,高强度和改善的耐腐蚀性的铝产品的方法,所述方法包括:(a)提供包含基本上由约0.7至1.0wt。 %硅,不大于约0.3wt。 %铁,不大于约0.5wt。 %铜,约0.8〜1.1wt。 %镁,约0.3至0.4wt。 %锰,和约0.5至0.8wt。 %锌,其余基本为铝,附带元素和杂质; (b)在大约950°至1050°F的温度范围内将原料匀化约2至20小时; (c)在约750°至950°F的温度下进行热轧。 (d)在约1000°至1080°F的温度下固溶热处理约5分钟至1小时; (e)通过以约1000°F /秒的速度淬火冷却到100°F或更低的温度; 和(f)通过再加热至约300-400°F的温度约2至20小时,从而在铝产品中产生T6回火而人为老化。