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 to two equations here disclosed.
申请公布号 MXPA05009401(A) 申请公布日期 2006.03.07
申请号 MX2005PA09401 申请日期 2005.09.02
申请人 HAYNES INTERNATIONAL, INC. 发明人 LEE M. PIKE, JR.
分类号 C22C19/05;(IPC1-7):C22C19/05 主分类号 C22C19/05
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