发明名称 |
NICKEL BASED MONOCRYSTALLINE SUPERALLOY, METHOD OF HEAT TREATING SAID ALLOY, AND PARTS MADE THEREFROM |
摘要 |
A NICKEL BASED MONOCRYSTALLINE SUPERALLOY, METHOD OF HEAT TREATING SAID ALLOY, AND PARTS MADE THEREFROM. A monocrystalline superalloy with a nickel based matrix and particularly intended for the manufacture of turbine blades, has the following composition, by weight: Al = 5.4% to 602%; Co = 4% to 7%; Cr = 6% to 9%; Mo = 0% to 2.5%; Ta = 5.5% to 8%; Ti = 0% to 1%; W = 7% to 9%; and Ni = balance to 100%. The invention also provides a method of improving the alloy's resistance to creep, in which the Ni3Al type ?' phase is put completely into solution at a first temperature, and then the ?' phase is precipitated into the ? solid solution at a temperature greater than 1000.degree.C. This treatment considerably increases the alloy's resistance to creep over a wide range of temperatures. |
申请公布号 |
CA1193116(A) |
申请公布日期 |
1985.09.10 |
申请号 |
CA19820400450 |
申请日期 |
1982.04.05 |
申请人 |
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES |
发明人 |
KHAN, TASADDUQ;CARON, PIERRE |
分类号 |
C30B29/52;C22C19/05;C22F1/00;C22F1/10;C30B11/00;C30B29/10;C30B33/00 |
主分类号 |
C30B29/52 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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