Superplastic aluminium alloy sheets
    2.
    发明授权
    Superplastic aluminium alloy sheets 失效
    超塑性铝合金板材

    公开(公告)号:US4618382A

    公开(公告)日:1986-10-21

    申请号:US660126

    申请日:1984-10-12

    IPC分类号: C22F1/053 C22F1/057 C22C21/00

    摘要: Sheets of high strength superplastic Al--Zn--Mg alloys or Al--Cu alloys which having a maximum grain size below 30 .mu.m on average are described. These alloy sheets are obtained by a method which is characterized by keeping a homogenized and hot worked ingot of the alloy at two different temperatures for sufficient times whereby a fine grain structure is formed in the alloy to impart superplasticity to the alloy.

    摘要翻译: 描述了平均具有低于30μm的最大粒度的高强度超塑性Al-Zn-Mg合金或Al-Cu合金的片材。 这些合金板通过以下方法获得:其特征在于,将合金的均质化和热加工锭保持在两个不同的温度下足够的时间,由此在合金中形成细晶粒结构以赋予合金超塑性。

    High strength heat treatable 7000 series aluminum alloy of excellent
corrosion resistance and a method of producing thereof
    3.
    发明授权
    High strength heat treatable 7000 series aluminum alloy of excellent corrosion resistance and a method of producing thereof 失效
    具有优异耐腐蚀性的高强度可热处理7000系列铝合金及其制造方法

    公开(公告)号:US6048415A

    公开(公告)日:2000-04-11

    申请号:US55906

    申请日:1998-04-07

    CPC分类号: C22F1/053

    摘要: A heat treatable 7000 series aluminum alloy has a micro-structure with a crystal grain size of 45 .mu.m or less and an aspect ratio (longitudinal/long transverse ratio of crystal grain) of preferably 4 or less, whereby its corrosion resistance is improved outstandingly by applying a solution heat treatment and hardening and subsequently, applying an aging treatment at 100 to 145.degree. C. for 5 to 50 hr, a reversion treatment at 140 to 195.degree. C. for 0.5 to 30 hr. and a re-aging treatment at 100 to 145.degree. C. for 5 to 50 hr. to thereby make an electroconductivity to 38-40 IACS %, and render the micro-structure so as to have a minimum distance for the .eta. phase on the crystal grain boundary of 20 nm or more and a maximum size for the .eta.' phase in the crystal grain of 20 nm or less.

    摘要翻译: 可热处理的7000系铝合金具有晶粒尺寸为45μm以下的微结构,纵横比(晶粒的纵横比)优选为4以下,耐腐蚀性显着提高 通过进行固溶热处理和硬化,然后在100〜145℃下进行5〜50小时的时效处理,在140〜195℃下反复处理0.5〜30小时。 并在100〜145℃下进行5〜50小时的再老化处理。 从而使电导率达到38-40IACS%,并使微结构具有在20nm以上的晶界上的eta相的最小距离,以及在 20nm以下的晶粒。

    Heat treatable Al alloys excellent in fracture touchness, fatigue
characteristic and formability
    4.
    发明授权
    Heat treatable Al alloys excellent in fracture touchness, fatigue characteristic and formability 失效
    耐热处理铝合金,断裂接触性,疲劳特性和成型性优良

    公开(公告)号:US5759302A

    公开(公告)日:1998-06-02

    申请号:US513395

    申请日:1995-08-10

    摘要: There is provided Al alloys which have improved and excellent fracture toughness and fatigue characteristic and improved formability, and which can be suitably used for transportation machines, such as aircraft, railway vehicles, general mechanical parts and the like. The Al alloy contains 1 to 8% (% by weight, the same is true for the following) of Cu, containing one or more selected from a group comprising 0.4 to 0.8% of Mn, 0.15 to 0.3% of Cr, 0.05 to 0.1% of Zr and 0.1 to 2.5% of Mg, Fe and Si each being less than 0.1%, a distance between constituents being more than 85 .mu.m, and having a micro-structure fulfilling at least one of the following (a) to (c): (a) the size of Al--Mn dispersoids is 4000 .ANG. or more, (b) the size of Al--Cr dispersoids is 1000 .ANG. or more, and (c) the size of Al--Zr dispersoids is 300 .ANG. or more.

    摘要翻译: 提供了具有改进且优异的断裂韧性和疲劳特性和改进的成型性的Al合金,并且可以适用于诸如飞机,铁路车辆,通用机械零件等的运输机器。 Al合金含有1〜8%(以下相同的Cu),含有选自Mn:0.4〜0.8%,Cr:0.15〜0.3%,Cr:0.05〜0.1的一种或多种 Zr和0.1〜2.5%的Mg,Fe和Si各自小于0.1%,组分之间的距离大于85μm,并且具有满足以下(a)至( c):(a)Al-Mn分散体的尺寸为4000或更大,(b)Al-Cr分散体的尺寸为1000或更大,(c)Al-Zr分散体的尺寸为300或 更多。