发明名称 |
Trapped insert turbine airfoil |
摘要 |
A gas turbine engine airfoil (10) is manufactured by forming an internal retention seat in two complementary airfoil parts (26, 28). An insert is fabricated for retention in the seat. The two parts (26, 28) are assembled with the insert disposed in the seat therebetween. The parts are then bonded together to trap the insert therein to collectively define the airfoil (10), The insert and seat may be precisely fabricated for improving the efficiency of the airfoil. <IMAGE> |
申请公布号 |
EP0990771(A1) |
申请公布日期 |
2000.04.05 |
申请号 |
EP19990307225 |
申请日期 |
1999.09.13 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
ACQUAVIVA, PAUL JOSEPH;LIOTTA, GARY CHARLES;FLECK, JAMES NORWOOD |
分类号 |
B23P15/04;F01D5/18;F02C7/00 |
主分类号 |
B23P15/04 |
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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