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
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