发明名称 Turbine fan blade for a gas turbine engine
摘要 A fan blade (10) includes a metal airfoil (14) having a pocket (34) disposed in a first side (16) thereof, with the pocket including a filler (38) bonded thereto. The pocket includes a plurality of cells (34b) separated by corresponding ribs (36) which are submerged in the filler. <IMAGE>
申请公布号 PL199566(B1) 申请公布日期 2008.10.31
申请号 PL20010346987 申请日期 2001.04.10
申请人 GENERAL ELECTRIC COMPANY 发明人 STEVENSON JOSEPH TIMOTHY;LIN WENDY WEN-LING
分类号 F01D5/12;B64C11/00;F01D5/14;F01D5/16;F04D29/38 主分类号 F01D5/12
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