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
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