发明名称 Ni-based heat resistant alloy, gas turbine component and gas turbine
摘要 A Ni-based heat resistant alloy has a composition of, by mass percent, carbon: 0.001 to 0.1%, chromium: 16 to 22%, aluminum: 0.5 to 1.5%, molybdenum: 0.1 to 2.0%, tungsten: 0.1 to 6.0%, niobium: 3.5 to 5.5%, titanium: 0.8 to 3.0%, iron: 16 to 20%, and the balance being nickel and inevitable impurities. A parameter Ps indicating a segregation tendency is in a range of Ps≧−3.5. The parameter Ps is represented by Formula (1). Ps=1.05×Al content+0.6×Ti content−0.8×Nb content−0.3×Mo content  (1)
申请公布号 US8685316(B2) 申请公布日期 2014.04.01
申请号 US201113286274 申请日期 2011.11.01
申请人 SATO JUN;IMANO SHINYA;DOI HIROYUKI;HITACHI, LTD. 发明人 SATO JUN;IMANO SHINYA;DOI HIROYUKI
分类号 C22C19/05;F01D5/00 主分类号 C22C19/05
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