发明名称 |
Frequency tuned turbomachine blade |
摘要 |
<p>A fan blade (10) includes a metal airfoil (14) having first and second opposite sides (16,18) extending radially between a root (20) and tip (22), and axially between a leading edge (24) and a trailing edge (26). The airfoil further includes a plurality of pockets (36) disposed in the first side and separated by corresponding ribs (38). A filler (40) is bonded in the pocket, and is coextensive with the airfoil first side. Radial and diagonal ribs (38a-c) respectively intersect solely each other for selectively increasing torsional and bending stiffness to increase frequency margin between adjacent torsional and bending resonant modes of vibration. <IMAGE></p> |
申请公布号 |
EP0924381(A2) |
申请公布日期 |
1999.06.23 |
申请号 |
EP19980310319 |
申请日期 |
1998.12.16 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
SCHILLING, JAN CHRISTOPHER;STEVENSON, JOSEPH TIMOTHY;CORNELL, JAY L. |
分类号 |
F01D5/14;F01D5/16;F04D29/38;(IPC1-7):F01D5/16 |
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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