发明名称 NI-CR-CO ALLOY FOR ADVANCED GAS TURBINE ENGINES
摘要 A wrought age-hardenable nickel-chromium-cobalt based alloy suitable for use in high temperature gas turbine transition ducts possessing a combination of three specific key properties, namely resistance to strain age cracking, good thermal stability , and good creep--rupture strength contains in weight percent 17 to 22 chromium, 8 to 1 5 cobalt, 4.0 to 9.1 molybdenum, up to 7 tungsten, 1.39 to 1.65 aluminum, 1.50 to 2.30 titanium, up to 0.80 niobium, 0.01 to 0.2 carbon, up to 0.01 boron, up to 3 iron, up to 1.5 tantalum and less than 0.02 zirconium, with a balance of nickel and impurities. Certain alloying element s must be present in amounts according to two equations here disclosed.
申请公布号 CA2560147(A1) 申请公布日期 2007.12.13
申请号 CA20062560147 申请日期 2006.09.15
申请人 HAYNES INTERNATIONAL, INC. 发明人 PIKE, LEE M., JR.
分类号 C22C19/05 主分类号 C22C19/05
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