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HOT CORROSION RESISTANT SINGLE CRYSTAL NICKEL-BASED SUPERALLOYS

机译:耐高温单晶镍基高温合金

摘要

from about 14.2 to about 15.5 percent chromium, from about 2.0 to about 4.0 percent cobalt, from about 0.30 to about 0.45 percent molybdenum, from about 4.0 to about 5.0 percent tungston, from about 4.5 to about 5.8 percent tantalum, from about 0.05 to about 0.25 percent columbium, from about 3.2 to about 3.6 percent aluminum, from about 4.0 to about 4.4 percent titanium, from about 0.01 to about 0.06 percent hafnium, and the balance nickel plus incidental impurities, the superalloy having a phasial stability number N^ less than about 2.45. Single crystal articles can be suitably made from the superalloy of this invention. The article can be a component for a gas turbine engine and, more particularly, the component can be a gas turbine blade or gas turbine vane.
机译:铬约14.2%至约15.5%,钴约2.0%至约4.0%,钼约0.30%至约0.45%,钨约4.0%至约5.0%,钽约4.5%至约5.8%,约0.05%至约0.5% 0.25%的,、约3.2%到约3.6%的铝,约4.0%到约4.4%的钛,约0.01%到约0.06%的ha以及余量的镍加上附带的杂质,该超合金的相稳定性数N ^约2.45。单晶制品可以由本发明的高温合金适当地制造。该制品可以是用于燃气涡轮发动机的部件,并且更特别地,该部件可以是燃气涡轮叶片或燃气涡轮叶片。

著录项

  • 公开/公告号IN1995DE01882A

    专利类型

  • 公开/公告日2009-03-13

    原文格式PDF

  • 申请/专利权人

    申请/专利号IN1882/DEL/1995

  • 发明设计人 GARY L ERICTION;

    申请日1995-10-13

  • 分类号C22C9/06;

  • 国家 IN

  • 入库时间 2022-08-21 19:27:38

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