发明名称 SINGLE CRYSTAL NICKEL-BASED SUPERALLOY HAVING A LOW SPECIFIC GRAVITY, AND BLADE OF A TURBO MACHINE MADE FROM THIS SUPERALLOY
摘要 A low density nickel based superalloy having good creep characteristics when hot, and intended in particular for making turbomachine parts by monocrystalline solidification, wherein the composition of the alloy in percentages by weight is as follows: -Co: 5% to 7% Cr: 5% to 10% Mo: 0.5% to 2.5% -W: 3% to 5% Al: 6% to 7.5% Ti: 1.5% to 2.25% -Nb: 0% to 0.5% Ta: 2% to 4% V: 0.3% to 0.6% -Ni: balance to- 100%. - Parts, e.g. turbomachine blades, made from the alloy.
申请公布号 EP0143694(B1) 申请公布日期 1987.07.22
申请号 EP19840402323 申请日期 1984.11.14
申请人 OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES (O.N.E.R.A.) 发明人 KHAN, TASADDUQ;CARON, PIERRE;RAFFESTIN, JEAN-LOUIS
分类号 C22C19/05;C22F1/00;C22F1/10;C30B11/00;C30B29/52;F01D5/28 主分类号 C22C19/05
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