发明名称 Superalloy for single crystal turbine vanes
摘要 <p>A nickel-base superalloy that is useful for making single crystal castings exhibiting outstanding stress-rupture properties, creep-rupture properties, and an increased tolerance for grain defects contains, in percentages by weight, from about 4.7% to about 4.9% chromium, (Cr), from about 9% to about 10% cobalt (Co), from about 0.6% to about 0.8% molybdenum (Mo), from about 8.4% to about 8.8% tungsten (W), from about 4.3% to about 4.8% tantalum (Ta), from about 0.6% to about 0.8% titanium (Ti), from about 5.6% to about 5.8% aluminum (Al), from about 2.8% to about 3.1% rhenium (Re), from about 1.1% to about 1.5% hafnium (Hf), from about 0.06% to about 0.08% carbon (C), from about 0.012% to about 0.020% boron (B), from about 0.004% to about 0.010% zirconium (Zr), the balance being nickel and incidental impurities. The nickel-base superalloy provides improved casting yield and reduce component cost due to a reduction in rejectable grain defects as compared with conventional directionally solidified casting alloys and conventional single crystal alloys.</p>
申请公布号 EP1382697(A1) 申请公布日期 2004.01.21
申请号 EP20030254456 申请日期 2003.07.11
申请人 CANNON-MUSKEGON CORPORATION 发明人 HARRIS, KENNETH;WAHL, JACQUELINE B.
分类号 F01D5/28;C22C19/05;F02C7/00;(IPC1-7):C22C19/05 主分类号 F01D5/28
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