Heat-resistant nickel-based alloy excellent in weldability
    1.
    发明授权
    Heat-resistant nickel-based alloy excellent in weldability 失效
    耐热镍基合金,焊接性优良

    公开(公告)号:US5882586A

    公开(公告)日:1999-03-16

    申请号:US899587

    申请日:1997-07-24

    IPC分类号: C22C19/05

    CPC分类号: C22C19/056

    摘要: A heat-resistant nickel-based alloy having excellent welding properties, said nickel-based alloy consisting essentially of, in terms of wt. %, 0.05 to 0.25% of C, 18 to 25% of Cr, 15 to 25% of Co, at least one selected from the group consisting of up to 3.5% of Mo and 5 to 10% of W, with W+1/2Mo being 5 to 10%, 1.0 to 5.0% of Ti, 1.0 to 4.0% of Al, 0.5 to 4.5% of Ta, 0.2 to 3.0% of Nb, 0.005 to 0.10% of Zr, 0.001 to 0.01% of B and the balance being Ni and unavoidable impurities, wherein the (Al+Ti) content and the (W+1/2Mo) content are within the range surrounded by the lines connecting points A (Al+Ti: 5%, W+1/2Mo: 10%), B (Al+Ti: 5%, W+1/2Mo: 5%), C (Al+Ti: 7%, W+1/2Mo: 5%), and D (Al+Ti: 7%, W+1/2Mo: 10%) excluding the line A-B in FIG. 1. Another alloy has substantially the same composition as described above except that the Cr content is 10 to 20% and the (Al+Ti) content and the (W+1/2Mo) content are within the range surrounded by the lines connecting points A, B, E (Al+Ti: 4%, W+1/2Mo: 5%), F (Al+Ti: 4%, W+1/2Mo: 0.5%), G (Al+Ti: 7%, W+1/2Mo: 0.5%) and D, excluding the line A-B-E, in FIG. 1.

    摘要翻译: 一种具有优异焊接性能的耐热镍基合金,所述镍基合金基本上以重量计。 ,0.05〜0.25%的C,18〜25%的Cr,15〜25%的Co,至少1种选自高达3.5%的Mo和5〜10%的W,W + E,fra 1/2 + EE Mo为5〜10%,Ti为1.0〜5.0%,Al为1.0〜4.0%,Ta为0.5〜4.5%,Nb为0.2〜3.0%,Zr为0.005〜0.10% 0.001〜0.01%的B,余量为Ni和不可避免的杂质,其中(Al + Ti)含量和(W ++ E,fra 1/2 + EE Mo)含量在连接点 A(Al + Ti:5%,W ++ E,fra 1/2 + EE Mo:10%),B(Al + Ti:5%,W ++ E,fra 1/2 + EE Mo: ),C(Al + Ti:7%,W ++ E,fra 1/2 + EE Mo:5%)和D(Al + Ti:7%,W ++ E, :10%),不包括图1中的线AB。 另一种合金具有与上述基本相同的组成,不同之处在于Cr含量为10〜20%,(Al + Ti)含量和(W ++ E,fra 1/2 + EE Mo)含量在 连接点A,B,E(Al + Ti:4%,W ++ E,fra 1/2 + EE Mo:5%),F(Al + Ti:4%,W ++ E ,1/2 + EE Mo:0.5%),G(Al + Ti:7%,W ++ E,fra 1/2 + EE Mo:0.5%)和D,不包括线ABE。 1。

    Process for the heat treatment of a Ni-base heat-resisting alloy
    2.
    发明授权
    Process for the heat treatment of a Ni-base heat-resisting alloy 有权
    镍基耐热合金热处理工艺

    公开(公告)号:US06132535A

    公开(公告)日:2000-10-17

    申请号:US428785

    申请日:1999-10-28

    IPC分类号: C22C19/05 C22F1/10

    摘要: Provided is a process for improving alloy properties which can improve the high-temperature ductility of a Ni-base heat-resisting alloy while maintaining its excellent high-temperature strength and weldability. Specifically, it relates to a process for the heat treatment of a Ni-base heat-resisting alloy having a specific composition which comprises the steps of subjecting the alloy to a first-stage solution treatment by keeping it at a specific temperature for a specific period of time; cooling the alloy to a second-stage solution treatment temperature at a specific cooling rate; subjecting the alloy to a second-stage solution treatment by keeping it at a specific temperature for a specific period of time; cooling the alloy rapidly to room temperature at a specific cooling rate; subjecting the alloy to a stabilizing treatment by keeping it at a specific temperature for a specific period of time; cooling the alloy rapidly to room temperature at a specific cooling rate; and subjecting the alloy to an aging treatment by keeping it at a specific temperature for a specific period of time.

    摘要翻译: 提供了一种提高合金性能的方法,其可以在保持其优异的高温强度和可焊性的同时提高Ni基耐热合金的高温延展性。 具体而言,涉及具有特定组成的Ni基耐热合金的热处理方法,该方法包括以下步骤:使合金进行第一阶段固溶处理,将其保持在特定温度下一段特定的时间 的时间 以合适的冷却速度将合金冷却至第二阶段固溶处理温度; 通过将合金保持在特定温度一段时间来对合金进行第二阶段溶液处理; 以合适的冷却速度将合金快速冷却至室温; 通过将合金保持在特定温度一段特定的时间来对合金进行稳定处理; 以合适的冷却速度将合金快速冷却至室温; 并通过将其保持在特定温度一段时间来对合金进行时效处理。

    High temperature corrosion-resistant and abrasion-resistant coating member, and manufacturing method thereof
    9.
    发明授权

    公开(公告)号:US06423432B1

    公开(公告)日:2002-07-23

    申请号:US09438724

    申请日:1999-11-11

    IPC分类号: B32B1500

    摘要: A high temperature corrosion-resistant and abrasion-resistant coated member or part which is suitable for use under a severe high temperature corrosive and severe abrasive environment and in flying particles, and a manufacturing method thereof are provided. A manufacturing method of a high temperature corrosion-resistant and abrasion-resistant coated member wherein an Al diffusion and infiltration treatment is performed after a chromium carbide coating has been applied onto the surface of a base material, or wherein a chromium carbide coating layer whose outside surface is an Al diffusion layer is formed on the surface of the base material, and a gas turbine blade comprising the above member are provided.

    摘要翻译: 提供适用于严酷的高温腐蚀性和严重的磨蚀环境和飞粒子的高温耐腐蚀和耐磨涂层的部件或部件及其制造方法。 一种高耐蚀耐磨涂层构件的制造方法,其中在将碳化铬涂层施加到基材的表面上之后进行Al扩散和渗透处理,或者其外部的碳化铬涂层 表面是在基材的表面上形成Al扩散层,并且设置包括上述构件的燃气轮机叶片。