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
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