发明名称 |
Process and system for fabricating gamma tial turbine engine components |
摘要 |
A process for manufacturing a turbine engine component (10) comprises the steps of: casting ingots made of a gamma TiAl material using a double vacuum arc remelting casting technique; subjecting the cast ingots to a hot isostatic pressing to close porosity; forming at least one pancake of the gamma TiAl material by isothermally forging the hot isostatic pressed ingots; sectioning each pancake into a plurality of blanks; heat treating the blanks to produce a desired microstructure and mechanical properties; and machining the blanks into finished turbine engine components (10). A system for performing the process is also disclosed. |
申请公布号 |
EP2423340(A1) |
申请公布日期 |
2012.02.29 |
申请号 |
EP20110179093 |
申请日期 |
2011.08.26 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DAS, GOPAL |
分类号 |
C22C14/00;B21K3/04;B23H7/00;B23P15/02;B26D1/00;B26F3/00;B30B11/00;C22F1/18;F01D5/00 |
主分类号 |
C22C14/00 |
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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