A HIGH STRENGTH, HEAT TREATABLE ALUMINUM ALLOY
    1.
    发明申请
    A HIGH STRENGTH, HEAT TREATABLE ALUMINUM ALLOY 审中-公开
    高强度,热处理铝合金

    公开(公告)号:WO2008005852A2

    公开(公告)日:2008-01-10

    申请号:PCT/US2007/072513

    申请日:2007-06-29

    CPC classification number: C22C21/10 C22C21/08

    Abstract: A high strength aluminum alloy is suitable for ultra thick gauge wrought product. The alloy can have 6 to 8 wt % zinc, 1 to 2 wt % magnesium, and dispersoid forming elements such as Zr, Mn, Cr, Ti, and /or Sc with the balance made of aluminum and incidental elements and/or impurities. The alloy is suitable for many uses, including in moulds for injection-molded plastics.

    Abstract translation: 高强度铝合金适用于超厚锻造产品。 该合金可以具有6至8重量%的锌,1至2重量%的镁和分散质形成元素如Zr,Mn,Cr,Ti和/或Sc,余量由铝和附带的元素和/或杂质构成。 该合金适用于许多用途,包括用于注模塑料的模具。

    HIGH STRENGTH, HEAT TREATABLE AL-ZN-MG ALUMINIUM ALLOY
    2.
    发明申请
    HIGH STRENGTH, HEAT TREATABLE AL-ZN-MG ALUMINIUM ALLOY 审中-公开
    高强度,热处理AL-ZN-MG铝合金

    公开(公告)号:WO2008005852A3

    公开(公告)日:2008-04-17

    申请号:PCT/US2007072513

    申请日:2007-06-29

    CPC classification number: C22C21/10 C22C21/08

    Abstract: A high strength aluminum alloy. is suitable for ultra thick gauge wrought product. The alloy can have 6 to 8 wt % zinc, 1 to 1.9 wt % magnesium, wherein Mg is present in an amount from (0.2 2m,- 0.3) wt. % to (0.2 Zm + 0.3) wt. %, and dispersoid forming elements such as Zr, Mn, Cr, Ti, and /or Sc with the balance made of aluminum and incidental elements and/or impurities. The alloy is suitable for many uses, including in moulds for injection-molded plastics.

    Abstract translation: 高强度铝合金。 适用于超厚规格锻造产品。 该合金可以具有6至8重量%的锌,1至1.9重量%的镁,其中Mg以(0.2-2μm,-0.3)重量%的量存在。 %至(0.2Zm + 0.3)wt。 %,以及分散相形成元素如Zr,Mn,Cr,Ti和/或Sc,余量由铝和附带元素和/或杂质构成。 该合金适用于许多用途,包括用于注模塑料的模具。

    AL-ZN-CU-MG ALUMINUM BASE ALLOYS AND METHODS OF MANUFACTURE AND USE
    3.
    发明申请
    AL-ZN-CU-MG ALUMINUM BASE ALLOYS AND METHODS OF MANUFACTURE AND USE 审中-公开
    AL-ZN-CU-MG铝基合金及其制造和使用方法

    公开(公告)号:WO2006086534A3

    公开(公告)日:2006-09-28

    申请号:PCT/US2006004541

    申请日:2006-02-10

    CPC classification number: C22C21/10 C22F1/053

    Abstract: A rolled or forged Al-Zn-Cu-Mg aluminum-based alloy wrought product having a thickness from 2 to 10 inches. The product has been treated by solution heat-treatment, quenching and aging, and the product comprises (in weight-%) :Zn 6.2 - 7.2, Mg 1.5 - 2.4, Cu 1.7 - 2.1. Fe 0 - 0.13, Si 0 - 0.10, Ti 0 - 0.06, Zr 0.06 - 0.13, Cr 0 - 0.04, Mn 0 - 0.04, impurities and other incidental elements = 0.05 each. Alloys per se and aircraft and aerospace uses, as well as methods of making products are also disclosed.

    Abstract translation: 轧制或锻造的厚度为2至10英寸的Al-Zn-Cu-Mg铝基合金锻造产品。 该产品已经通过溶液热处理,淬火和老化处理,产物包含(重量%):Zn 6.2-7.2,Mg 1.5-2.4,Cu 1.7-2.1。 Fe 0-0.13,Si0-0.10,Ti0-0.06,Zr 0.06-0.13,Cr0-0.04,Mn0-0.04,杂质和其他附带元素各0.05。 还公开了合金本身以及飞机和航空航天用途以及制造产品的方法。

    AL- ZN-CU-MG ALUMINUM BASE ALLOYS AND METHODS OF MANUFACTURE AND USE
    4.
    发明申请
    AL- ZN-CU-MG ALUMINUM BASE ALLOYS AND METHODS OF MANUFACTURE AND USE 审中-公开
    AL-ZN-CU-MG铝基合金及其制造和使用方法

    公开(公告)号:WO2006086534A2

    公开(公告)日:2006-08-17

    申请号:PCT/US2006/004541

    申请日:2006-02-10

    CPC classification number: C22C21/10 C22F1/053

    Abstract: A rolled or forged Al-Zn-Cu-Mg aluminum-based alloy wrought product having a thickness from 2 to 10 inches. The product has been treated by solution heat-treatment, quenching and aging, and the product comprises (in weight-%) :Zn 6.2 - 7.2, Mg 1.5 - 2.4, Cu 1.7 - 2.1. Fe 0 - 0.13, Si 0 - 0.10, Ti 0 - 0.06, Zr 0.06 - 0.13, Cr 0 - 0.04, Mn 0 - 0.04, impurities and other incidental elements ≤ 0.05 each. Alloys per se and aircraft and aerospace uses, as well as methods of making products are also disclosed.

    Abstract translation: 轧制或锻造的厚度为2至10英寸的Al-Zn-Cu-Mg铝基合金锻造产品。 该产品已经通过溶液热处理,淬火和老化处理,产物包含(重量%):Zn 6.2-7.2,Mg 1.5-2.4,Cu 1.7-2.1。 Fe 0-0.13,Si0-0.10,Ti0-0.06,Zr 0.06-0.13,Cr0-0.04,Mn0-0.04,杂质和其他附带元素各0.05。 还公开了合金本身以及飞机和航空航天用途以及制造产品的方法。

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