Corrosion and grain growth resistant aluminum alloy
    2.
    发明授权
    Corrosion and grain growth resistant aluminum alloy 有权
    耐腐蚀和耐晶粒生长的铝合金

    公开(公告)号:US06503446B1

    公开(公告)日:2003-01-07

    申请号:US09616015

    申请日:2000-07-13

    IPC分类号: C22C2100

    CPC分类号: C22C21/00

    摘要: An aluminum alloy composition includes controlled amounts of iron, manganese, zinc, zirconium, vanadium, and titanium to effectively inhibit grain growth during exposure to elevated temperatures while maintaining extrudability and corrosion resistance. The composition is especially adapted for use as micro-multivoid tubing for brazed heat exchanger applications and has a post-braze grain structure that is more resistant to intergranular corrosion so as to reduce or eliminate heat exchanger failures during service.

    摘要翻译: 铝合金组合物包括受控量的铁,锰,锌,锆,钒和钛,以在保持可挤出性和耐腐蚀性的同时在高温下有效抑制晶粒生长。 该组合物特别适合用作钎焊热交换器应用的微多孔管,并且具有更好地抵抗晶间腐蚀的后钎焊晶粒结构,以便在使用期间减少或消除热交换器故障。

    High strength, high toughness aluminum-copper-magnesium-type aluminum
alloy
    3.
    发明授权
    High strength, high toughness aluminum-copper-magnesium-type aluminum alloy 失效
    高强度,高韧性的铝 - 铜 - 镁型铝合金

    公开(公告)号:US5593516A

    公开(公告)日:1997-01-14

    申请号:US481578

    申请日:1995-06-07

    IPC分类号: C22C21/16

    CPC分类号: C22C21/16

    摘要: An aluminum-based alloy composition having improved combinations of strength and fracture toughness consists essentially of 2.5-5.5 percent copper, 0.10-2.30 percent magnesium, with minor amounts of grain refining elements, dispersoid additions and impurities and the balance aluminum. The amounts of copper and magnesium are controlled such that the solid solubility limit for these elements in aluminum is not exceeded. The inventive alloy composition may also include 0.10-1.00 percent silver for improved mechanical properties. The alloys are useful as high strength, high fracture toughness components for aircraft and aerospace structural parts.

    摘要翻译: 具有改进的强度和断裂韧性组合的铝基合金组合物基本上由2.5-5.5%的铜,0.10-2.30%的镁,少量的晶粒细化元素,分散质添加剂和杂质以及余量的铝组成。 控制铜和镁的量使得不超过这些元素在铝中的固溶度极限。 本发明的合金组合物还可以包括0.10-1.00%的银以改善机械性能。 该合金可用作飞机和航空航天结构部件的高强度,高断裂韧性部件。

    High strength, high toughness aluminum-copper-magnesium-type aluminum
alloy
    4.
    发明授权
    High strength, high toughness aluminum-copper-magnesium-type aluminum alloy 失效
    高强度,高韧性的铝 - 铜 - 镁型铝合金

    公开(公告)号:US5376192A

    公开(公告)日:1994-12-27

    申请号:US937935

    申请日:1992-08-28

    IPC分类号: C22C21/16 C22C21/00

    CPC分类号: C22C21/16

    摘要: An aluminum-based alloy composition having improved combinations of strength and fracture toughness consists essentially of 2.5-5.5 percent copper, 0.10-2.30 percent magnesium, with minor amounts of grain refining elements, dispersoid additions and impurities and the balance aluminum. The amounts of copper and magnesium are controlled such that the solid solubility limit for these elements in aluminum is not exceeded. The inventive alloy composition may also include 0.10-1.00 percent silver for improved mechanical properties. The alloys are useful as high strength, high fracture toughness components for aircraft and aerospace structural parts.

    摘要翻译: 具有改进的强度和断裂韧性组合的铝基合金组合物基本上由2.5-5.5%的铜,0.10-2.30%的镁,少量的晶粒细化元素,分散质添加剂和杂质以及余量的铝组成。 控制铜和镁的量使得不超过这些元素在铝中的固溶度极限。 本发明的合金组合物还可以包括0.10-1.00%的银以改善机械性能。 该合金可用作飞机和航空航天结构部件的高强度,高断裂韧性部件。

    Aluminum alloys with optimum combinations of formability, corrosion resistance, and hot workability, and methods of use

    公开(公告)号:US06656296B2

    公开(公告)日:2003-12-02

    申请号:US10225378

    申请日:2002-08-20

    IPC分类号: C22F104

    CPC分类号: C22C21/00 F28F21/08

    摘要: An aluminum alloy article containing the alloying amounts of iron, silicon, manganese, titanium, and zinc has controlled levels of iron and manganese to produce an alloy article that combines excellent corrosion resistant with good formability. The alloy article composition employs a controlled ratio of manganese to iron and controlled total amounts of iron and manganese to form intermetallic compounds in the final alloy article. The electrolytic potential of the intermetallic compounds match the aluminum matrix of the article to minimize corrosion. The levels of iron and manganese are controlled so that the intermetallic compounds are present in a volume fraction that allows the alloy article to be easily formed. The aluminum alloy composition is especially adapted for extrusion processes, and tubing that are used in heat exchanger applications.

    Method of making high strength, high toughness
aluminum-copper-magnesium-type aluminum alloy
    6.
    发明授权
    Method of making high strength, high toughness aluminum-copper-magnesium-type aluminum alloy 失效
    制造高强度,高韧性的铝 - 铜 - 镁型铝合金的方法

    公开(公告)号:US5512112A

    公开(公告)日:1996-04-30

    申请号:US267069

    申请日:1994-06-27

    IPC分类号: C22C21/16 C22F1/04 C22C21/12

    CPC分类号: C22C21/16

    摘要: A process for producing an aluminum-based alloy composition having improved combinations of strength and fracture toughness. The process includes casting an ingot consisting essentially of 2.5-5.5 percent copper, 0.10-2.30 percent magnesium, with minor amounts of grain refining elements, dispersoid additions and impurities and the balance aluminum. The amounts of copper and magnesium are controlled such that the solid solubility limit for these elements in aluminum is not exceeded. The alloy composition also includes 0.10-1.00 percent silver for improved mechanical properties. The ingot, in accordance with the inventive process, is homogenized and worked to produce a product. The product is solution heat treated to obtain a saturated solid solution and then aged to develop an improved combination of high strength and fracture toughness.

    摘要翻译: 一种具有改善的强度和断裂韧性组合的铝基合金组合物的制造方法。 该方法包括铸造基本上由2.5-5.5%的铜,0.10-2.30%的镁,少量的晶粒细化元素,分散质添加物和杂质以及余量的铝组成的锭。 控制铜和镁的量使得不超过这些元素在铝中的固溶度极限。 合金组成还包括0.10-1.00%的银,用于改善机械性能。 将锭按照本发明的方法进行均质化并加工成产品。 将产品进行固溶热处理以获得饱和固溶体,然后老化以形成高强度和断裂韧性的改进组合。

    Aluminum alloys with optimum combinations of formability, corrosion resistance, and hot workability, and methods of use
    7.
    发明授权
    Aluminum alloys with optimum combinations of formability, corrosion resistance, and hot workability, and methods of use 有权
    具有成型性,耐腐蚀性和热加工性的最佳组合的铝合金和使用方法

    公开(公告)号:US06458224B1

    公开(公告)日:2002-10-01

    申请号:US09564053

    申请日:2000-05-03

    IPC分类号: C22C2100

    CPC分类号: C22C21/00 F28F21/08

    摘要: An aluminum alloy article containing the alloying amounts of iron, silicon, manganese, titanium, and zinc has controlled levels of iron and manganese to produce an alloy article that combines excellent corrosion resistant with good formability. The alloy article composition employs a controlled ratio of manganese to iron and controlled total amounts of iron and manganese to form intermetallic compounds in the final alloy article. The electrolytic potential of the intermetallic compounds match the aluminum matrix of the article to minimize corrosion. The levels of iron and manganese are controlled so that the intermetallic compounds are present in a volume fraction that allows the alloy article to be easily formed. The aluminum alloy composition is especially adapted for extrusion processes, and tubing that are used in heat exchanger applications.

    摘要翻译: 含有铁,硅,锰,钛和锌的合金量的铝合金制品控制了铁和锰的含量,从而生产出具有优良耐腐蚀性和良好成型性的合金制品。 合金制品组合物采用锰与铁的控制比例,并控制铁和锰的总量,以在最终的合金制品中形成金属间化合物。 金属间化合物的电解电位与制品的铝基体相匹配,以使腐蚀最小化。 控制铁和锰的含量,使得金属间化合物以允许合金制品容易形成的体积分数存在。 铝合金组合物特别适用于挤出工艺,以及用于热交换器应用的管材。

    Delaying final stretching for improved aluminum alloy plate properties
    8.
    发明授权
    Delaying final stretching for improved aluminum alloy plate properties 失效
    延期最终拉伸改善铝合金板的性能

    公开(公告)号:US5273594A

    公开(公告)日:1993-12-28

    申请号:US816682

    申请日:1992-01-02

    IPC分类号: C22F1/00 C22F1/04 C22F1/057

    CPC分类号: C22F1/057 C22F1/04

    摘要: The present invention provides a method for improving aluminum alloy plate product properties by delaying final stretching of the plate product. During processing of the product, a time interval or intentional delay is provided between the final cold rolling step and the final stretching step. By delaying the final stretching procedure, an aluminum alloy plate product is provided with an improved fracture toughness without significant decrease in strength values. The method of intentionally delaying final stretching is particularly adapted for 2000 series aluminum alloys.

    摘要翻译: 本发明提供了通过延迟板产品的最终拉伸来提高铝合金板产品性能的方法。 在产品的加工过程中,在最后的冷轧步骤和最后的拉伸步骤之间提供时间间隔或有意的延迟。 通过延迟最终拉伸程序,铝合金板产品具有改进的断裂韧性,而强度值没有显着降低。 有意延迟最终拉伸的方法特别适用于2000系列铝合金。