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 15 cobalt, 4.0 to 9.5 molybdenum, up to 7 tungsten, 1.28 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, and up to 3 iron, with a balance of nickel and impurities. Certain alloying elements must be present in amounts according t o two equations here disclosed.
申请公布号 CA2517056(A1) 申请公布日期 2006.03.03
申请号 CA20052517056 申请日期 2005.08.24
申请人 HAYNES INTERNATIONAL, INC. 发明人 PIKE, JR., LEE M.
分类号 C22C19/05 主分类号 C22C19/05
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