NICKEL-BASED ALLOY AND TURBINE COMPONENT HAVING NICKEL-BASED ALLOY
    1.
    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。

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