发明名称 |
Method for fabricating a thick Ti64 alloy article |
摘要 |
<p>A Ti-6Al-4V-0.20 (Ti64) forged article is fabricated by forging a workpiece to make a forged gas turbine engine component having a thick portion thereof with a section thickness greater than 2-1/4 inches. The forged article is heat treated by solution heat treating at a temperature of from about 50°F to about 75°F below the beta-transus temperature of the alloy, thereafter water quenching the gas turbine engine component to room temperature, and thereafter aging the gas turbine engine component at a temperature of from about 900°F to about 1000°F. The resulting machined gas turbine engine component has a 0.2 percent yield strength of from about 120 ksi to about 140 ksi at its centerline (54), and a 0.2 percent yield strength of from about 160 ksi to about 175 ksi at a location about 1/2 inch below a surface (56) thereof.</p> |
申请公布号 |
EP1538226(A3) |
申请公布日期 |
2006.02.01 |
申请号 |
EP20040256461 |
申请日期 |
2004.10.20 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
WAYTE, PETER;LI, MING CHENG |
分类号 |
C22F1/18;B21K3/04;B44C1/17;C21D9/00;C22C14/00 |
主分类号 |
C22F1/18 |
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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