Nickel-base single-crystal superalloys, method for manufacturing the
same, and gas turbine parts prepared therefrom
    2.
    发明授权
    Nickel-base single-crystal superalloys, method for manufacturing the same, and gas turbine parts prepared therefrom 有权
    镍基单晶超级合金,其制造方法和由其制备的燃气轮机部件

    公开(公告)号:US6159314A

    公开(公告)日:2000-12-12

    申请号:US261230

    申请日:1999-03-03

    CPC分类号: C22F1/10

    摘要: The invention relates to a nickel-base single-crystal superalloy applied to parts for industrial gas turbine or the like such as turbine rotor blade and stator blade which are used at high temperatures, a method for manufacturing the same, and gas turbine parts prepared from such nickel-base single-crystal superalloys, and more particularly the invention provides a nickel-base single-crystal superalloy consisting essentially of, in percentages by weight, 5% to 10% cobalt, 4.7% to 6% chromium, more than 2.0% to less than 3.5% molybdenum, 7.5% to 10% tungsten, 5% to 6% aluminum, 0.1% to 2% titanium, 4% to 5.5% tantalum, 1% to 4% rhenium, 0.01% to 0.2% hafnium, the balance being nickel and incidental impurities, which is excellent in high-temperature strength and high-temperature corrosion resistance, and further excellent in structural stability even in a long time use.

    摘要翻译: 本发明涉及一种应用于工业燃气轮机等部件的镍基单晶超合金,例如在高温下使用的涡轮转子叶片和定子叶片,其制造方法,以及由 这种镍基单晶超合金,更具体地说,本发明提供了一种镍基单晶超合金,主要由重量百分比为5%至10%的钴,4.7%至6%的铬,大于2.0% 至少于3.5%的钼,7.5%至10%的钨,5%至6%的铝,0.1%至2%的钛,4%至5.5%的钽,1%至4%的铼,0.01%至0.2%的铪, 余量为镍和附带杂质,其耐高温性和耐高温腐蚀性优异,即使长时间使用也具有优异的结构稳定性。

    Nickel-based single crystal alloy and a method of manufacturing the same
    4.
    发明授权
    Nickel-based single crystal alloy and a method of manufacturing the same 有权
    镍基单晶合金及其制造方法

    公开(公告)号:US06755921B2

    公开(公告)日:2004-06-29

    申请号:US10139352

    申请日:2002-05-07

    IPC分类号: C22C1905

    摘要: The present inventions offer a nickel-based single crystal alloy which has a high strength, is easy in conducting the solution heat treatment, hardly gives a harmful phase and is resistant to corrosion at high temperature. A nickel-based single crystal alloy is offered where the composition consists of 7-15 of Co, 0.1-4 of Cr, 1-4 of Mo, 4-7 of W, 5.5-6.5 of Al, 5-7 of Ta, 4-5.5 of Re, 0-0.5 each of Hf and V, and 0-2 each of Ti and Nb in terms of % by weight and residual part substantially consists of Ni wherein said alloy may contain unavoidable impurities.

    摘要翻译: 本发明提供了一种具有高强度的镍基单晶合金,易于进行固溶热处理,几乎不产生有害相,并且耐高温腐蚀。 提供了一种镍基单晶合金,其中组成由7-15个Co,0.1-4个Cr,1-4个Mo,4-7个W,5.5-6.5个Al,5-7个Ta, 4.5的Re,0-0.5的Hf和V,以及Ti和Nb的0-2以重量%计,剩余部分基本上由Ni组成,其中所述的合金可能含有不可避免的杂质。

    Ni-BASED SINGLE CRYSTAL SUPERALLOY AND COMPONENT OBTAINED FROM THE SAME
    6.
    发明申请
    Ni-BASED SINGLE CRYSTAL SUPERALLOY AND COMPONENT OBTAINED FROM THE SAME 审中-公开
    镍基单晶超级合金及其成分

    公开(公告)号:US20110142714A1

    公开(公告)日:2011-06-16

    申请号:US13000815

    申请日:2009-06-26

    IPC分类号: C22C19/05 C22C30/00

    CPC分类号: C22C19/057

    摘要: Provided is an Ni-based single crystal superalloy wherein the ingredients have a composition containing, as ratio by mass, from 5.0% by mass to 7.0% by mass of Al, from 4.0% by mass to 8.0% by mass of Ta, from 0% by mass to 2.0% by mass of Mo, from 3.0% by mass to 8.0% by mass of W, from 3.0% by mass to 8.0% by mass of Re, from 0% by mass to 0.50% by mass of Hf, from 3.0% by mass to 7.0% by mass of Cr, from 0% by mass to 9.9% by mass of Co and from 1.0% by mass to 10.0% by mass of Ru, with the balance of Ni and inevitable impurities. The alloy prevents TCP phase precipitation at high temperatures, therefore having improved strength at high temperatures and having oxidation resistance at high temperatures.The above-mentioned first-generation alloy CMSX-2 and second-generation alloy CMSX-4 are, though comparable thereto in point of creep strength at low temperatures, inferior to third-generation alloys in point of creep strength at high temperatures, since a large quantity of eutectic γ′-phase remains therein even after high-temperature solution treatment.

    摘要翻译: 本发明提供一种Ni基单晶超耐热合金,其中成分具有以质量比计含有5.0质量%至7.0质量%的Al,4.0质量%至8.0质量%的Ta,0 以质量计2.0质量%,3.0质量%〜8.0质量%的W,3.0质量%〜8.0质量%的Re,0质量%〜0.50质量%的Hf, 从3.0质量%至7.0质量%的Cr,0质量%至9.9质量%的Co和1.0质量%至10.0质量%的Ru,余量为Ni和不可避免的杂质。 该合金防止高温下的TCP相沉淀,因此在高温下具有改善的强度并且在高温下具有抗氧化性。 上述第一代合金CMSX-2和第二代合金CMSX-4尽管与低温下的蠕变强度相当,但在高温下的蠕变强度方面比第三代合金低,因为 即使在高温溶液处理后,仍存在大量的共晶γ'相。

    Ni-Base Superalloy, Method for Producing the Same, and Turbine Blade or Turbine Vane Components
    9.
    发明申请
    Ni-Base Superalloy, Method for Producing the Same, and Turbine Blade or Turbine Vane Components 有权
    镍基超合金,其制造方法以及涡轮叶片或涡轮叶片组件

    公开(公告)号:US20100226779A1

    公开(公告)日:2010-09-09

    申请号:US12225254

    申请日:2007-03-16

    摘要: A Ni-base superalloy having a chemical composition comprising Cr: 3.0-5.0 wt %, Co: 5.0-10.0 wt %, Mo: 0.5-3.0 wt %, W: 8.0-10.0 wt %, Ta: 5.0-8.0 wt %, Nb: 3.0 wt % or less, Al: 4.5-6.0 wt %, Ti: 0.1-2.0 wt %, Re: more than 3.0-4.0 wt %, Ru: 0.2-4.0 wt %, Hf: 0.01-0.2 wt %, and the balance being Ni and unavoidable impurities, a method for producing the same, and turbine blade or turbine vane components are disclosed. The Ni-base superalloy has high creep strength and textural stability under high temperature environment, and is excellent in applicability to turbine blade or turbine vane components of large-sized gas turbines.

    摘要翻译: 具有Cr:3.0-5.0重量%,Co:5.0-10.0重量%,Mo:0.5-3.0重量%,W:8.0-10.0重量%,Ta:5.0-8.0重量%的化学组成的Ni基超合金, Nb:3.0重量%以下,Al:4.5〜6.0重量%,Ti:0.1〜2.0重量%,Re:3.0-4.0重量%以下,Ru:0.2〜4.0重量%,Hf:0.01-0.2重量% 其余为Ni和不可避免的杂质,其制造方法,以及涡轮叶片或涡轮叶片部件。 Ni基超合金在高温环境下具有高蠕变强度和结构稳定性,适用于大型燃气轮机的涡轮叶片或涡轮叶片部件。