THERMALLY-CONTROLLED COMPONENT AND THERMAL CONTROL PROCESS
    2.
    发明申请
    THERMALLY-CONTROLLED COMPONENT AND THERMAL CONTROL PROCESS 有权
    热控部件和热控制过程

    公开(公告)号:US20130255248A1

    公开(公告)日:2013-10-03

    申请号:US13690298

    申请日:2012-11-30

    CPC classification number: F03G7/06

    Abstract: A thermally-controlled component and thermal control process are disclosed. The thermally-controlled component includes thermally-responsive features. The thermally-responsive features are configured to modify a flow path to control temperature variation of the thermally-controlled component. The thermally-responsive features deploy from or retract toward a surface of the thermally-controlled component in response to a predetermined temperature change. The thermal control process includes modifying the flow path in the thermally-controlled component to control temperature variation of the thermally-controlled component and/or cooling a region of the thermally-controlled component through the thermally-responsive features deploying from or retracting toward a surface of the thermally-controlled component.

    Abstract translation: 公开了一种热控部件和热控制工艺。 热控制部件包括热响应特征。 热响应特征被配置为修改流路以控制热控部件的温度变化。 响应于预定的温度变化,热响应特征从热控部件的表面展开或缩回。 热控制过程包括修改热控部件中的流动路径以控制热控部件的温度变化和/或通过从表面向或朝向表面展开的热响应特征来冷却热控部件的区域 的热控部件。

    CAST NICKEL-BASE SUPERALLOY INCLUDING IRON
    3.
    发明申请

    公开(公告)号:US20190185973A1

    公开(公告)日:2019-06-20

    申请号:US16283269

    申请日:2019-02-22

    CPC classification number: C22C30/00 C22C19/055 C22C19/056 C22C19/057

    Abstract: A cast nickel-base superalloy that includes iron added substitutionally for nickel. The cast nickel-base superalloy comprises, in weight percent about 1-6% iron, about 7.5-19.1% cobalt, about 7-22.5% chromium, about 1.2-6.2% aluminum, optionally up to about 5% titanium, optionally up to about 6.5% tantalum, optionally up to about 1% Nb, about 2-6% W, optionally up to about 3% Re, optionally up to about 4% Mo, about 0.05-0.18% C, optionally up to about 0.15% Hf, about 0.004-0.015 B, optionally up to about 0.1% Zr, and the balance Ni and incidental impurities. The superalloy is characterized by a γ′ solvus temperature that is within 5% of the γ′ solvus temperature of the superalloy that does not include 1-6% Fe and a mole fraction of γ′ that is within 15% of the mole fraction of the superalloy that does not include 1-6% Fe.

    ARTICLE AND METHOD FOR FORMING ARTICLE
    6.
    发明申请
    ARTICLE AND METHOD FOR FORMING ARTICLE 审中-公开
    文章和形成文章的方法

    公开(公告)号:US20150247220A1

    公开(公告)日:2015-09-03

    申请号:US14193198

    申请日:2014-02-28

    Abstract: An article and a method for forming the article are disclosed. The article includes an equiaxed grain structure and a composition. The composition includes, by weight percent, about 6.0% to about 9.0% aluminum, up to about 0.5% titanium, about 2.5% to about 4.5% tantalum, about 10.0% to about 12.5% chromium, about 5.0% to about 10.0% cobalt, about 0.30% to about 0.80% molybdenum, about 2.0% to about 5.0% tungsten, up to about 1.0% silicon, about 0.35% to about 0.60% hafnium, about 0.005% to about 0.010% boron, about 0.06% to about 0.10% carbon, up to about 0.02% zirconium, up to about 0.1% lanthanum, up to about 0.03% yttrium, and balance nickel and incidental impurities. Rhenium, if present, is a trace element. The method for forming the article includes providing the composition having up to about 0.01% rhenium and forming the article.

    Abstract translation: 公开了一种用于形成物品的制品和方法。 该制品包括等轴晶粒结构和组合物。 该组合物包括按重量百分比计约600%至约9.0%的铝,至多约0.5%的钛,约2.5%至约4.5%的钽,约10.0%至约12.5%的铬,约5.0%至约10.0%的钴 ,约0.30%至约0.80%的钼,约2.0%至约5.0%的钨,至多约1.0%的硅,约0.35%至约0.60%的铪,约0.005%至约0.010%的硼,约0.06%至约0.10% %碳,高达约0.02%的锆,至多约0.1%的镧,至多约0.03%的钇,以及平衡镍和附带的杂质。 铼(如果存在)是微量元素。 形成制品的方法包括提供具有至多约0.01%铼的组合物并形成制品。

    CAST NICKEL-BASE ALLOYS INCLUDING IRON
    7.
    发明申请
    CAST NICKEL-BASE ALLOYS INCLUDING IRON 审中-公开
    CAST镍基合金包括铁

    公开(公告)号:US20140314618A1

    公开(公告)日:2014-10-23

    申请号:US13868481

    申请日:2013-04-23

    CPC classification number: C22C30/00 C22C19/055 C22C19/056 C22C19/057

    Abstract: A cast nickel-base superalloy that includes iron added substitutionally for nickel. The cast nickel base superalloy comprises, in weight percent about 1-6% iron, about 7.5-19.1% cobalt, about 7-22.5% chromium, about 1.2-6.2% aluminum, optionally up to about 5% titanium, optionally up to about 6.5% tantalum, optionally up to about 1% Nb, about 2-6% W, optionally up to about 3% Re, optionally up to about 4% Mo, about 0.05-0.18% C, optionally up to about 0.15% Hf, about 0.004-0.015 B, optionally up to about 0.1% Zr, and the balance Ni and incidental impurities. The superalloy is characterized by a □′ solvus temperature that is within 5% of the □′ solvus temperature of the superalloy that does not include 1-6% Fe and a mole fraction of □′ that is within 15% of the mole fraction of the superalloy that does not include 1-6% Fe.

    Abstract translation: 一种铸镍基超级合金,其中包括替代镍添加的铁。 铸造的镍基超级合金以重量百分比约为1-6%的铁,约7.5-19.1%的钴,约7-22.5%的铬,约1.2-6.2%的铝,任选地最多约5%的钛,任选地直到约 6.5%钽,任选至多约1%Nb,约2-6%W,任选至多约3%Re,任选至多约4%Mo,约0.05-0.18%C,任选至多约0.15%Hf, 约0.004-0.015B,任选至多约0.1%的Zr,余量为Ni和附带的杂质。 超合金的特征在于:“solvus温度在不含1.6%Fe的超合金的”solvus温度的5%以内,“的摩尔分数为”的摩尔分数为15% 超合金不含1-6%Fe。

    ARTICLE AND METHOD FOR FORMING AN ARTICLE
    8.
    发明申请
    ARTICLE AND METHOD FOR FORMING AN ARTICLE 有权
    文章和形成文章的方法

    公开(公告)号:US20150247422A1

    公开(公告)日:2015-09-03

    申请号:US14193576

    申请日:2014-02-28

    Abstract: An article and a method for forming the article are disclosed. The article comprising a composition, wherein the composition comprises, by weight percent, about 13.7% to about 14.3% chromium (Cr), about 9.0% to about 10.0% cobalt (Co), about 3.5% to about 3.9% aluminum (Al), about 3.4% to about 3.8% titanium (Ti), about 4.0% to about 4.4% tungsten (W), about 1.4% to about 1.7% molybdenum (Mo), about 1.55% to about 1.75% niobium (Nb), about 0.08% to about 0.12% carbon (C), about 0.005% to about 0.040% zirconium (Zr), about 0.010% to about 0.014% boron (B), and balance nickel (Ni) and incidental impurities. The composition is substantially free of tantalum (Ta) and includes a microstructure substantially devoid of Eta phase.

    Abstract translation: 公开了一种用于形成物品的制品和方法。 所述制品包含组合物,其中所述组合物包含按重量计约13.7%至约14.3%的铬(Cr),约9.0%至约10.0%的钴(Co),约3.5%至约3.9%的铝(Al) ,约3.4%至约3.8%的钛(Ti),约4.0%至约4.4%的钨(W),约1.4%至约1.7%的钼(Mo),约1.55%至约1.75%的铌(Nb) 约0.08%至约0.12%的碳(C),约0.005%至约0.040%的锆(Zr),约0.010%至约0.014%的硼(B),余量为镍(Ni)和附带的杂质。 组合物基本上不含钽(Ta),并且包括基本上不含Eta相的微结构。

    NICKEL-BASED ALLOY AND TURBINE COMPONENT HAVING NICKEL-BASED ALLOY
    9.
    发明申请
    NICKEL-BASED ALLOY AND TURBINE COMPONENT HAVING NICKEL-BASED ALLOY 审中-公开
    基于镍的合金和具有镍基合金的涡轮机组件

    公开(公告)号:US20140199164A1

    公开(公告)日:2014-07-17

    申请号:US13739109

    申请日:2013-01-11

    CPC classification number: C22C19/057 C22C19/05

    Abstract: A nickel-based alloy and a turbine component are disclosed. The alloy includes, by weight, between about 0.8% and about 1.3% hafnium, between about 5.7% and about 6.4% aluminum, between about 7.0% and about 10.0% cobalt, up to about 0.1% carbon, up to about 8.7% chromium, up to about 0.6% molybdenum, up to about 9.7% tungsten, up to about 0.9% titanium, up to about 0.02% boron, up to about 0.1% manganese, up to about 0.06% silicon, up to about 0.01% phosphorus, up to about 0.004% sulfur, up to about 0.02% zirconium, up to about 1.8% niobium, up to about 0.1% vanadium, up to about 0.1% copper, up to about 0.2% iron, up to about 0.003% magnesium, up to about 0.002% oxygen, up to about 0.002% nitrogen, and a balance nickel. The turbine component is a turbine bucket, a turbine nozzle, or any other suitable turbine component including the alloy.

    Abstract translation: 公开了镍基合金和涡轮部件。 该合金包括约0.8%至约1.3%的铪,约5.7%至约6.4%的铝,约7.0%至约10.0%的钴,至多约0.1%的碳,至多约8.7%的铬 ,至多约0.6%的钼,至多约9.7%的钨,至多约0.9%的钛,至多约0.02%的硼,至多约0.1%的锰,至多约0.06%的硅,至多约0.01%的磷, 高达约0.004%的硫,高达约0.02%的锆,至多约1.8%的铌,至多约0.1%的钒,至多约0.1%的铜,至多约0.2%的铁,至多约0.003%的镁,向上 至约0.002%的氧气,至多约0.002%的氮气和余量的镍。 涡轮机部件是涡轮机桶,涡轮喷嘴或包括合金的任何其它合适的涡轮机部件。

    METALLIC SEAL ASSEMBLY, TURBINE COMPONENT, AND METHOD OF REGULATING AIRFLOW IN TURBO-MACHINERY
    10.
    发明申请
    METALLIC SEAL ASSEMBLY, TURBINE COMPONENT, AND METHOD OF REGULATING AIRFLOW IN TURBO-MACHINERY 有权
    金属密封组件,涡轮机组件及其在涡轮机械中调节气流的方法

    公开(公告)号:US20130259640A1

    公开(公告)日:2013-10-03

    申请号:US13690233

    申请日:2012-11-30

    Abstract: A metallic seal assembly, a turbine component, and a method of regulating flow in turbo-machinery are disclosed. The metallic seal assembly includes a sealing structure having thermally-responsive features. The thermally-responsive features deploy from or retract toward a surface of the sealing structure in response to a predetermined temperature change. The turbine component includes the metallic seal assembly. The method of regulating flow in turbo-machinery includes providing the metallic seal assembly and raising or retracting the thermally-responsive features in response to the predetermined temperature change.

    Abstract translation: 公开了一种金属密封组件,涡轮机部件和调节涡轮机械流量的方法。 金属密封组件包括具有热响应特征的密封结构。 响应于预定的温度变化,热响应特征从密封结构的表面展开或缩回。 涡轮机部件包括金属密封组件。 在涡轮机械中调节流量的方法包括提供金属密封组件,并响应于预定的温度变化升高或缩回热响应特征。

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