COBALT-NICKEL BASE ALLOY AND METHOD OF MAKING AN ARTICLE THEREFROM
    2.
    发明申请
    COBALT-NICKEL BASE ALLOY AND METHOD OF MAKING AN ARTICLE THEREFROM 审中-公开
    钴镍基合金及其制备方法

    公开(公告)号:US20120312434A1

    公开(公告)日:2012-12-13

    申请号:US13156638

    申请日:2011-06-09

    IPC分类号: C22C30/00 C22F1/16

    CPC分类号: C22C19/07 C22C19/057 C22F1/10

    摘要: A high-temperature, high-strength, oxidation-resistant cobalt-nickel base alloy is disclosed. The alloy includes, in weight percent: about 3.5 to about 4.9% of Al, about 12.2 to about 16.0% of W, about 24.5 to about 32.0% Ni, about 6.5% to about 10.0% Cr, about 5.9% to about 11.0% Ta, and the balance Co and incidental impurities. A method of making an article having high-temperature strength, cyclic oxidation resistance and corrosion resistance is disclosed. The method includes forming a high-temperature, high-strength, oxidation-resistant cobalt-nickel base alloy as described herein; forming an article from the alloy; solution-treating the alloy by a solution heat treatment; and aging the alloy by providing at least one aging heat treatment at an aging temperature that is less than the gamma-prime solvus temperature, wherein the alloy is configured to form a continuous, protective, adherent oxide layer on an alloy surface upon exposure to a high-temperature oxidizing environment.

    摘要翻译: 公开了高温,高强度,耐氧化的钴镍基合金。 该合金包括重量百分比:约3.5至约4.9%的Al,约12.2至约16.0%的W,约24.5至约32.0%的Ni,约6.5%至约10.0%的Cr,约5.9%至约11.0% Ta,余量Co和杂质。 公开了制造具有高温强度,耐环氧化和耐腐蚀性的制品的方法。 该方法包括形成如本文所述的高温,高强度,耐氧化的钴镍基合金; 从合金制成制品; 通过固溶热处理对合金进行溶解处理; 并且通过在低于γ'溶质温度的老化温度下提供至少一种时效热处理来老化合金,其中该合金构造成在暴露于合金表面时在合金表面上形成连续的,保护性的粘附氧化物层 高温氧化环境。

    Nickel-Based Superalloys and Articles
    4.
    发明申请
    Nickel-Based Superalloys and Articles 审中-公开
    镍基超合金和制品

    公开(公告)号:US20110076180A1

    公开(公告)日:2011-03-31

    申请号:US12570654

    申请日:2009-09-30

    IPC分类号: C22C19/05 B22D27/04

    摘要: Rhenium-free nickel based alloys are provided. More particularly, the alloys comprise preferred levels and ratios of elements so as to achieve good high temperature strength of both gamma matrix phase and gamma prime precipitates, as well as good environmental resistance, without using rhenium. When cast and directionally solidified into single crystal form, the alloys exhibit creep and oxidation resistance substantially equivalent to or better than rhenium-bearing single-crystal alloys. Further, the alloys can be processed by directional solidification into articles in single crystal form or columnar structure comprising fine dendrite arm spacing, e.g., less than 400 μm, if need be, so that further improvements in mechanical properties in the articles can be seen.

    摘要翻译: 提供无铼镍基合金。 更具体地,合金包括优选的含量和元素比例,以便在不使用铼的情况下实现γ基质相和γ初始沉淀物的良好的高温强度以及良好的耐环境性。 当铸造和定向凝固成单晶形式时,合金具有基本上等于或优于含铼单晶合金的蠕变和抗氧化性能。 此外,如果需要,合金可以通过定向固化加工成单晶形状或柱状结构的制品,包括细小的枝晶臂间距,例如小于400μm,从而可以看到制品中机械性能的进一步改善。

    COBALT-NICKEL SUPERALLOYS, AND RELATED ARTICLES
    5.
    发明申请
    COBALT-NICKEL SUPERALLOYS, AND RELATED ARTICLES 有权
    钴镍超级合金及相关文章

    公开(公告)号:US20100291406A1

    公开(公告)日:2010-11-18

    申请号:US12465821

    申请日:2009-05-14

    IPC分类号: B32B15/01 C22C30/00

    摘要: A cobalt-nickel alloy composition is described, containing about 20% to about 28% cobalt; about 37% to about 46% nickel; at least about 6% chromium; aluminum; and at least one refractory metal. The total weight of cobalt, aluminum, and refractory metal in the composition is less than about 50% of the total weight of the composition. Moreover, the alloy composition comprises both a (Co, Ni)-gamma phase and an L12-structured (gamma prime) phase. Various components made from the cobalt-nickel alloy composition are also described. Examples include high-temperature machinery and devices, e.g., components of gas turbine engines.

    摘要翻译: 描述了钴镍合金组合物,其含有约20%至约28%的钴; 约37%至约46%的镍; 至少约6%的铬; 铝; 和至少一种难熔金属。 组合物中钴,铝和难熔金属的总重量小于组合物总重量的约50%。 此外,合金组成包括(Co,Ni) - γ相和L12结构(γ')相。 还描述了由钴 - 镍合金组合物制成的各种组分。 实例包括高温机械和设备,例如燃气涡轮发动机的部件。

    TURBINE AIRFOIL COMPONENT AND METHOD FOR MAKING
    6.
    发明申请
    TURBINE AIRFOIL COMPONENT AND METHOD FOR MAKING 有权
    涡轮机组件及制造方法

    公开(公告)号:US20120251330A1

    公开(公告)日:2012-10-04

    申请号:US13077475

    申请日:2011-03-31

    IPC分类号: F01D5/14 B22D25/02 B22D27/04

    摘要: A component such as a turbine bucket or blade, and method for making the component, are presented. One embodiment is an article that comprises an airfoil casting portion comprising a plurality of integral regions, wherein the plurality of integral regions comprises a single-crystalline region and a columnar-grained region. Another embodiment is a method for fabricating an article. The method comprises providing a quantity of molten metal; providing a mold defining an airfoil portion having an axial direction and a transverse direction, wherein the airfoil portion of the mold comprises a single-crystal growth region and a columnar growth region disposed along the transverse direction from the single crystal growth region; introducing the molten metal into the mold; and solidifying the metal such that a solidification front progresses in the axial direction to produce an airfoil casting portion comprising a single-crystalline region and a columnar-grained region.

    摘要翻译: 提出了诸如涡轮机桶或叶片的部件以及用于制造部件的方法。 一个实施例是一种制品,其包括包括多个整体区域的翼型铸造部分,其中所述多个整体区域包括单晶区域和柱状晶粒区域。 另一实施例是用于制造制品的方法。 该方法包括提供一定数量的熔融金属; 提供限定具有轴向方向和横向方向的翼型部的模具,其中所述模具的翼型部分包括单晶生长区域和沿着横向从单晶生长区域设置的柱状生长区域; 将熔融金属引入模具中; 并使金属固化,使得固化前沿轴向前进,以制造包括单晶区域和柱状晶粒区域的翼型铸造部分。

    Nickel-Based Superalloys and Articles
    7.
    发明申请
    Nickel-Based Superalloys and Articles 审中-公开
    镍基超合金和制品

    公开(公告)号:US20110076182A1

    公开(公告)日:2011-03-31

    申请号:US12571013

    申请日:2009-09-30

    IPC分类号: C22C19/05 B22D27/04

    CPC分类号: C22C19/057

    摘要: Rhenium-free nickel based alloys are provided. More particularly, the alloys comprise preferred levels and ratios of elements so as to achieve good high temperature strength of both gamma matrix phase and gamma prime precipitates, as well as good environmental resistance, without using rhenium. When cast and directionally solidified into single crystal form, the alloys exhibit creep resistance substantially equivalent to rhenium-bearing single-crystal alloys. Further, the alloys can be processed by directional solidification into articles in single crystal form or columnar structure comprising fine dendrite arm spacing, e.g., less than 400 μm, if need be, so that further improvements in mechanical properties in the articles can be seen.

    摘要翻译: 提供无铼镍基合金。 更具体地,合金包括优选的含量和元素比例,以便在不使用铼的情况下实现γ基质相和γ初始沉淀物的良好的高温强度以及良好的耐环境性。 当铸造和定向凝固成单晶形式时,合金具有基本上等同于含铼单晶合金的抗蠕变性。 此外,如果需要,合金可以通过定向固化加工成单晶形状或柱状结构的制品,包括细小的枝晶臂间距,例如小于400μm,从而可以看到制品中机械性能的进一步改善。