发明名称 |
High stiffness airoil and method of manufacture |
摘要 |
<p>A cast metallic airfoil structure having a high stiffness core positioned therein for increasing the stiffness of the airfoil. In one embodiment, the high stiffness core is preferably formed of gamma titanium aluminde or a titanium metal matrix composite and is metallurgically bonded to the cast metallic airfoil structure. In one form the airfoil structure forms a portion of an integrally bladed rotor, and in a second form the airfoil structure has a dove tail attachment portion. <IMAGE></p> |
申请公布号 |
EP0980962(A2) |
申请公布日期 |
2000.02.23 |
申请号 |
EP19990306441 |
申请日期 |
1999.08.16 |
申请人 |
ALLISON ADVANCED DEVELOPMENT COMPANY;ROLLS-ROYCE CORPORATION |
发明人 |
RESS, ROBERT ANTHONY JR.;KING, BRIAN PAUL;EWING, BRUCE ALLAN |
分类号 |
F01D5/14;F01D5/28;(IPC1-7):F01D5/28 |
主分类号 |
F01D5/14 |
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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