发明名称 Material for gas turbine disk
摘要 A material for a gas turbine disk comprises 0.05 to 0.15 wt % of carbon, 0.10 wt % or less of silicon, 0.40 wt % or less of manganese, 9.0 to 12.0 wt % of chromium, 1.0 to 3.5 wt % of nickel, 0.50 to 0.90 wt % of molybdenum, 1.0 to 2.0 wt % of tungsten, 0.10 to 0.30 wt % of vanadium, 0.01 to 0.10 wt % of niobium, 0.01 to 0.05 wt % of nitrogen, and a remainder comprising iron and unavoidable impurities, wherein the contents of nickel, molybdenum and tungsten satisfy a relationship -1.5 wt %</=Mo+W/2-Ni</=0.7 wt %. Accordingly, unlike conventional gas turbine disk materials such as a heat resisting steel of 12Cr-type which can be used in an operation at about 400 DEG C., but has reduced toughness and high-temperature creep characteristics in an operation at about 500 DEG C., this material is allowed to have a satisfactory toughness and excellent high-temperature creep characteristics and can be suitably used at high temperatures.
申请公布号 US6106766(A) 申请公布日期 2000.08.22
申请号 US19990236636 申请日期 1999.01.26
申请人 KABUSHIKI KAISHA KOBE SEIKO SHO;MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 KAWAI, HISATAKA;KADOYA, YOSHIKUNI;TAKAHASHI, KOJI;MAGOSHI, RYOTARO;YASUMOTO, YASUHIKO;TSUCHIYAMA, TOMOHIRO
分类号 C22C38/00;C22C38/44;C22C38/46;C22C38/48;C22C38/54;F01D5/28;(IPC1-7):C22C38/44 主分类号 C22C38/00
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