发明名称 HIGH TEMPERATURE NIOBIUM-BEARING SUPERALLOYS
摘要 Nickel-base superalloys having gamma prime strengthening precipitates in a gamma matrix and little or no tertiary incoherent phases, such as delta, delta variants and eta.
申请公布号 US2015167124(A1) 申请公布日期 2015.06.18
申请号 US201414490103 申请日期 2014.09.18
申请人 Rolls-Royce Corporation 发明人 Helmink Randolph C.;Tin Sammy
分类号 C22C19/05;C22C19/00 主分类号 C22C19/05
代理机构 代理人
主权项 1. A niobium bearing superalloy including about of 2.2 to 4 wt. % aluminum, about 0.01 to 0.05 wt. % boron, about 0.02 to 0.06 wt. % carbon, about 6 to 15 wt. % chromium, about 0 to 20 wt. % cobalt, about 0 to 0.5 wt. % hafnium, about 1 to 3 wt. % molybdenum, about 7.2 to 16 wt. % niobium, about 0 to 0.6 wt. % silicon, about 1 to 5 wt. % tantalum, about 0 to 1.5 wt. % titanium, about 1 to 3 wt. % tungsten, about 0.04 to 0.1 wt. % zirconium and the balance nickel and incidental impurities.
地址 Indianapolis IN US
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