Aluminum-lithium alloys
    7.
    发明授权
    Aluminum-lithium alloys 失效
    铝 - 锂合金

    公开(公告)号:US5137686A

    公开(公告)日:1992-08-11

    申请号:US149802

    申请日:1988-01-28

    摘要: Disclosed is an aluminum base alloy suitable for forming into a wrought product having improved combinations of strength, corrosion resistance and fracture toughness. The alloy is comprised of 0.2 to 5.0 wt. % Li, 0.05 to 6.0 wt. % Mg, at least 2.45 wt. % Cu, 0.01 to 0.16 wt. % Zr, 0.05 to 12 wt. % Zn, 0.5 wt. % max. Fe, 0.5 wt. % max. Si, the balance aluminum and incidental impurities.

    摘要翻译: 公开了一种适合于形成具有改进的强度,耐腐蚀性和断裂韧性组合的锻造产品的铝基合金。 该合金由0.2〜5.0重量% %Li,0.05〜6.0重量% %Mg,至少2.45wt。 %Cu,0.01〜0.16wt。 %Zr,0.05〜12wt。 %Zn,0.5wt。 最大% Fe,0.5wt。 最大% Si,余量为铝和杂质。

    Aluminum alloy two-step aging method and article
    9.
    发明授权
    Aluminum alloy two-step aging method and article 失效
    铝合金两步老化方法及制品

    公开(公告)号:US4861391A

    公开(公告)日:1989-08-29

    申请号:US132889

    申请日:1987-12-14

    摘要: A method for thermally treating an article made from an aluminum alloy having a first temperature at which solute atoms cluster to yield nuclei for the formation and growth of strengthening precipitates, and a second higher temperature at which the strengthening precipitates dissolve. The method comprises: heating the article to allow substantially all soluble alloy components to enter into solution; rapidly cooling the article in a quenching medium; and precipitation hardening the article by aging at or below the first temperature for a few hours to several months; then aging above the first temperature and below the second temperature until desired strength is achieved. A method for imparting improved combinations of strength and fracture toughness to a solution heat treated-article which includes an aluminum-lithium alloy is also disclosed. This method comprises aging the article at one or more temperatures at or below a first temperature of about 93.degree. C. (200.degree. F.) for a few hours to several months; and further aging the article at one or more temperatures above the first temperature and below a second temperature of about 219.degree. C. (425.degree. F.) for at least about 30 minutes.

    Aluminum magnesium alloy product containing dispersoids
    10.
    发明授权
    Aluminum magnesium alloy product containing dispersoids 失效
    铝镁合金产品含有分散质

    公开(公告)号:US5624632A

    公开(公告)日:1997-04-29

    申请号:US381032

    申请日:1995-01-31

    IPC分类号: C22C21/06 C22C21/04

    CPC分类号: C22F1/047 C22C21/06

    摘要: An aluminum alloy product for use as a damage tolerant product for aerospace applications, including fuselage skin stock. The aluminum alloy composition contains about 3-7 wt % magnesium, about 0.03-0.2 wt % zirconium, about 0.2-1.2 wt % manganese, up to 0.15 wt % silicon and about 0.05-0.5 wt % of a dispersoid-forming element selected from the group consisting of: scandium, erbium, yttrium, gadolinium, holmium and hafnium, the balance being aluminum and incidental elements and impurities.

    摘要翻译: 一种铝合金产品,用作航空航天应用的耐损伤产品,包括机身皮肤原料。 铝合金组合物包含约3-7重量%的镁,约0.03-0.2重量%的锆,约0.2-1.2重量%的锰,至多0.15重量%的硅和约0.05-0.5重量%的选自以下的分散质形成元素: 由钪,铒,钇,钆,钬和铪组成的组,余量为铝和附带元素和杂质。