Nickel-base single-crystal superalloys, method for manufacturing the
same, and gas turbine parts prepared therefrom
    1.
    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。