Nickel-based superalloy and gas turbine blade using the same
    1.
    发明授权
    Nickel-based superalloy and gas turbine blade using the same 有权
    镍基超级合金和燃气轮机叶片使用相同

    公开(公告)号:US09103003B2

    公开(公告)日:2015-08-11

    申请号:US12543623

    申请日:2009-08-19

    申请人: Akira Yoshinari

    发明人: Akira Yoshinari

    IPC分类号: C22C19/05 F01D5/28

    摘要: A Ni-based superalloy contains 13.1 to 16.0 percent by mass of Cr, 1.0 to 6.8 percent by mass of Co, 3.0 to 3.4 percent by mass of Al, 4.6 to 5.6 percent by mass of Ti, 2.0 to 4.4 percent by mass of Ta, 3.5 to 4.9 percent by mass of W, 0.1 to 0.9 percent by mass of Mo, 0.3 to 1.4 percent by mass of Nb, 0.05 to 0.20 percent by mass of C, and 0.01 to 0.03 percent by mass of B with the remainder being nickel and inevitable impurities. The superalloy excels in corrosion resistance, oxidation resistance, has high strength, and is used in parts of a gas turbine to be used at high temperature. The resulting gas turbine excels in durability.

    摘要翻译: 作为Ni系的超合金,含有13.1〜16.0质量%的Cr,1.0〜6.8质量%的Co,3.0〜3.4质量%的Al,4.6〜5.6质量%的Ti,2.0〜4.4质量%的Ta ,W:3.5〜4.9质量%,Mo:0.1〜0.9质量%,Nb:0.3〜1.4质量%,C:0.05〜0.20质量%,B:0.01〜0.03质量% 镍和不可避免的杂质。 超耐热合金的耐腐蚀性,抗氧化性优异,强度高,用于高温下使用的燃气轮机的部件。 所得到的燃气轮机的耐久性优异。

    NICKEL-BASED SUPERALLLOY AND GAS TURBINE BLADE USING THE SAME
    2.
    发明申请
    NICKEL-BASED SUPERALLLOY AND GAS TURBINE BLADE USING THE SAME 有权
    基于镍的超级合金和使用相同的气体涡轮叶片

    公开(公告)号:US20100080730A1

    公开(公告)日:2010-04-01

    申请号:US12543623

    申请日:2009-08-19

    申请人: Akira YOSHINARI

    发明人: Akira YOSHINARI

    IPC分类号: C22C19/05

    摘要: A Ni-based superalloy contains 13.1 to 16.0 percent by mass of Cr, 1.0 to 6.8 percent by mass of Co, 3.0 to 3.4 percent by mass of Al, 4.6 to 5.6 percent by mass of Ti, 2.0 to 4.4 percent by mass of Ta, 3.5 to 4.9 percent by mass of W, 0.1 to 0.9 percent by mass of Mo, 0.3 to 1.4 percent by mass of Nb, 0.05 to 0.20 percent by mass of C, and 0.01 to 0.03 percent by mass of B with the remainder being nickel and inevitable impurities. The superalloy excels in corrosion resistance, oxidation resistance, has high strength, and is used in parts of a gas turbine to be used at high temperature. The resulting gas turbine excels in durability.

    摘要翻译: 作为Ni系的超合金,含有13.1〜16.0质量%的Cr,1.0〜6.8质量%的Co,3.0〜3.4质量%的Al,4.6〜5.6质量%的Ti,2.0〜4.4质量%的Ta ,W:3.5〜4.9质量%,Mo:0.1〜0.9质量%,Nb:0.3〜1.4质量%,C:0.05〜0.20质量%,B:0.01〜0.03质量% 镍和不可避免的杂质。 超耐热合金的耐腐蚀性,抗氧化性优异,强度高,用于高温下使用的燃气轮机的部件。 所得到的燃气轮机的耐久性优异。

    Single-crystal Ni-based superalloy with high temperature strength, oxidation resistance and hot corrosion resistance
    3.
    发明申请
    Single-crystal Ni-based superalloy with high temperature strength, oxidation resistance and hot corrosion resistance 失效
    单晶Ni基超耐热合金,耐高温,耐氧化,耐热腐蚀

    公开(公告)号:US20050067062A1

    公开(公告)日:2005-03-31

    申请号:US10914502

    申请日:2004-08-10

    IPC分类号: C22C19/05 C30B29/52

    CPC分类号: C22C19/057

    摘要: An object of this invention is to provide a single-crystal nickel-based superalloy having high creep rupture strength at high temperatures and excel at corrosion resistance and oxidation resistance at high temperatures. Single-crystal nickel-based superalloys with high temperature strength, hot corrosion resistance and oxidation resistance comprising by weight, 3.0 to 7.0% Cr, 9.5 to 15.0% Co, 4.5 to 8.0% W, 3.3 to 6.0% Re, 4.0 to 8.0% Ta, 0.8 to 2.0% Ti, 4.5 to 6.5% Al, 0.01 to 0.2% Hf, less than 0.5% Mo, 0.01% or less C, 0.005% or less B, 0.01% or less Zr, 0.005% or less O, 0.005% or less N, and balance substantially Ni.

    摘要翻译: 本发明的目的是提供一种在高温下具有高蠕变断裂强度的单晶镍基超级合金,并且在高温下具有优异的耐腐蚀性和抗氧化性。 含有重量比为3.0〜7.0%的Cr,9.5〜15.0%的Co,4.5〜8.0%的W,3.3〜6.0%的Re,4.0〜8.0%的高温强度,耐热腐蚀性和耐氧化性的单晶镍基超耐热合金, Ta,0.8〜2.0%Ti,4.5〜6.5%Al,0.01〜0.2%Hf,小于0.5%Mo,0.01%以下C,0.005%以下B,0.01%以下Zr,0.005%以下O, 0.005%以下N,余量基本上为Ni。

    Ni-based alloy, and turbine rotor and stator blade for gas turbine
    4.
    发明授权
    Ni-based alloy, and turbine rotor and stator blade for gas turbine 有权
    镍基合金,以及用于燃气轮机的涡轮转子和定子叶片

    公开(公告)号:US08916092B2

    公开(公告)日:2014-12-23

    申请号:US13489481

    申请日:2012-06-06

    摘要: A Ni-based alloy including chromium, cobalt, aluminum, titanium, tantalum, tungsten, molybdenum, niobium, carbon, and boron, the balance being nickel and incidental impurities, is provided. The alloy has an alloy composition of, on the basis of mass percent, chromium: 13.10% to 16.00%, cobalt: 8.00% to 12.50%, aluminum: 2.30% to 3.50%, titanium: 4.80% to 5.50%, tantalum: 0.40% to less than 1.00%, tungsten: 4.50% to 6.00%, molybdenum: 0.10% to 1.50%, niobium: 0.60% to 1.70%, carbon: 0.01% to 0.20%, boron: 0.005% to 0.02%, and the balance: nickel and incidental impurities.

    摘要翻译: 提供了包括铬,钴,铝,钛,钽,钨,钼,铌,碳和硼的Ni基合金,其余为镍和附带的杂质。 该合金的合金组成为:质量%:13.10%〜16.00%,钴:8.00%〜12.50%,铝:2.30%〜3.50%,钛:4.80%〜5.50%,钽:0.40 %至小于1.00%,钨:4.50%至6.00%,钼:0.10%至1.50%,铌:0.60%至1.70%,碳:0.01%至0.20%,硼:0.005%至0.02%,余量 :镍和杂质。

    Ni-BASED ALLOY, AND TURBINE ROTOR AND STATOR BLADE FOR GAS TURBINE
    5.
    发明申请
    Ni-BASED ALLOY, AND TURBINE ROTOR AND STATOR BLADE FOR GAS TURBINE 有权
    镍基合金,涡轮转子和定子叶片用于气体涡轮机

    公开(公告)号:US20120328429A1

    公开(公告)日:2012-12-27

    申请号:US13489481

    申请日:2012-06-06

    IPC分类号: F01D5/14 F01D9/02 C22C19/05

    摘要: A Ni-based alloy including chromium, cobalt, aluminum, titanium, tantalum, tungsten, molybdenum, niobium, carbon, and boron, the balance being nickel and incidental impurities, is provided. The alloy has an alloy composition of, on the basis of mass percent, chromium: 13.10% to 16.00%, cobalt: 8.00% to 12.50%, aluminum: 2.30% to 3.50%, titanium: 4.80% to 5.50%, tantalum: 0.40% to less than 1.00%, tungsten: 4.50% to 6.00%, molybdenum: 0.10% to 1.50%, niobium: 0.60% to 1.70%, carbon: 0.01% to 0.20%, boron: 0.005% to 0.02%, and the balance: nickel and incidental impurities.

    摘要翻译: 提供了包括铬,钴,铝,钛,钽,钨,钼,铌,碳和硼的Ni基合金,其余为镍和附带的杂质。 该合金的合金组成为:质量%:13.10%〜16.00%,钴:8.00%〜12.50%,铝:2.30%〜3.50%,钛:4.80%〜5.50%,钽:0.40 %至小于1.00%,钨:4.50%至6.00%,钼:0.10%至1.50%,铌:0.60%至1.70%,碳:0.01%至0.20%,硼:0.005%至0.02%,余量 :镍和杂质。

    NI-BASED ALLOY, AND GAS TURBINE ROTOR BLADE AND STATOR BLADE EACH USING SAME
    6.
    发明申请
    NI-BASED ALLOY, AND GAS TURBINE ROTOR BLADE AND STATOR BLADE EACH USING SAME 有权
    基于NI的合金和燃气轮机叶片和使用相同的定子叶片

    公开(公告)号:US20120308393A1

    公开(公告)日:2012-12-06

    申请号:US13579642

    申请日:2011-03-16

    IPC分类号: C22C19/05 F01D5/14

    CPC分类号: C22C19/056 C22F1/10

    摘要: This invention provides an Ni-based alloy, which is particularly used for standard casting and is provided with properties such as strength at high temperatures, corrosion resistivity, and oxidation resistivity in a more balanced manner, compared with existing materials. The Ni-based alloy comprises Cr, Co, Al, Ti, Ta, W, Mo, Nb, C, B, and unavoidable impurities, with the balance consisting of Ni. Composition of the alloy is represented by mass: 13.1% to 15.0% Cr, 1.0% to 15.0% Co, 2.3% to 3.3% Al, 4.55% to 6.0% Ti, 3.05% to 4.0% Ta, 4.35% to 4.9% W, 0.1% to 2.0% Mo, 0.05% to 0.5% Nb, less than 0.05% Zr, 0.05% to 0.2% C, and 0.01% to 0.03% B.

    摘要翻译: 本发明提供了一种Ni基合金,其特别用于标准铸造,并且与现有材料相比,以更均衡的方式提供诸如高温强度,耐腐蚀性和氧化电阻率的性能。 Ni基合金包含Cr,Co,Al,Ti,Ta,W,Mo,Nb,C,B和不可避免的杂质,余量由Ni组成。 合金组成以质量计:13.1%至15.0%的Cr,1.0%至15.0%的Co,2.3%至3.3%的Al,4.55%至6.0%的Ti,3.05%至4.0%的Ta,4.35%至4.9%的W ,0.1〜2.0%的Mo,0.05〜0.5%的Nb,小于0.05%的Zr,0.05〜0.2%的C,和0.01〜0.03%的B.

    Nickel based superalloys with excellent mechanical strength, corrosion resistance and oxidation resistance
    7.
    发明授权
    Nickel based superalloys with excellent mechanical strength, corrosion resistance and oxidation resistance 失效
    镍基超级合金具有优异的机械强度,耐腐蚀性和抗氧化性

    公开(公告)号:US07597843B2

    公开(公告)日:2009-10-06

    申请号:US11212644

    申请日:2005-08-29

    IPC分类号: C22C19/05

    摘要: Nickel based superalloys with excellent mechanical strength, corrosion resistance and oxidation resistance, which consist essentially of chromium in an amount of 3 to 7% by weight, cobalt in an amount of 3 to 15% by weight, tungsten in an amount of 4.5 to 8% by weight, rhenium in an amount of 3.3 to 6% by weight, tantalum in an amount of 4 to 8% by weight, titanium in an amount of 0.8 to 2% by weight, aluminum in an amount of 4.5 to 6.5% by weight, ruthenium in an amount of 0.1 to 6%, hafnium in an amount of 0.01 to 0.2% by weight, molybdenum in an amount of less than 0.5% by weight, carbon in an amount 0.06% by weight or less, boron in an amount of 0.01% by weight or less, zirconium in an amount of 0.01% by weight or less, oxygen in an amount of 0.005% by weight or less, nitrogen in an amount of 0.005% by weight or less and inevitable impurities and the balance being nickel.

    摘要翻译: 镍基超级合金具有优异的机械强度,耐腐蚀性和抗氧化性,其基本上由3〜7重量%的铬组成,3〜15重量%的钴,4.5〜8的钨 重量%的铼,3.3〜6重量%的铼,4〜8重量%的钽,0.8〜2重量%的钛,4.5〜6.5重量%的铝 重量的钌,0.1〜6%的钌,0.01〜0.2重量%的铪,少于0.5重量%的钼,0.06重量%以下的碳, 0.01重量%以下的锆,0.01重量%以下的锆,0.005重量%以下的氧,0.005重量%以下的氮和不可避免的杂质,余量 是镍。

    NI-BASED SINGLE CRYSTAL ALLOY
    8.
    发明申请
    NI-BASED SINGLE CRYSTAL ALLOY 审中-公开
    基于NI的单晶合金

    公开(公告)号:US20090214379A1

    公开(公告)日:2009-08-27

    申请号:US12389633

    申请日:2009-02-20

    IPC分类号: C22C19/05

    摘要: Disclosed is a single crystal alloy consisting essentially of, by weight, 0.06-0.09% carbon, 0.016-0.035% B, 0.2-0.4% Hf, 0-0.02% Zr, 6.5-8.5% Cr, 0.4-1.0% Mo, 5.5-9.5% W, 1.2-3.1% Re, 8-10% Ta, 0.3-1.0% Nb, 0-0.4% Ti, 4.7-5.4% Al, 0.5-5.0% Co, 0.1-5% Fe, and the balance of Ni and unavoidable impurities. The alloy is free from solidification cracks during casting a large-sized blade of gas turbines, has grain boundary strength sufficient for assuring the reliability during operation, and further has excellent oxidation resistance to a high combustion gas temperature while having excellent high-temperature strength comparable to that of a conventional single crystal alloy.

    摘要翻译: 公开了基本上由0.06-0.09%的碳,0.016-0.035%的B,0.2-0.4%的Hf,0-0.02%的Zr,6.5-8.5%的Cr,0.4-1.0%的Mo,5.5 -9.5%W,1.2-3.1%Re,8-10%Ta,0.3-1.0%Nb,0-0.4%Ti,4.7-5.4%Al,0.5-5.0%Co,0.1-5%Fe,余量 的Ni和不可避免的杂质。 该合金在铸造大型燃气轮机叶片期间没有固化裂纹,具有足够的晶界强度以确保运行时的可靠性,并且还具有优异的耐高温燃烧气体温度的抗氧化性,同时具有优异的高温强度可比性 与传统的单晶合金相比。