发明名称 DISCRETE LOAD FINS FOR INDIVIDUAL STATOR VANES
摘要 An exemplary embodiment of the invention is directed to a turbine engine having a circumferential casing with a circumferentially extending slot formed in an inner wall. A radially inwardly facing fin-ring is disposed in the slot and has a radially inwardly projecting fin extending axially there across. A radially inwardly extending stator blade has a base and an airfoil. The base is disposed in the casing slot, radially inwardly of the fin-ring. A complementary base slot is disposed in the stator blade base and is configured to receive the fin therein for the transfer of a circumferential force, applied to the stator blade, to the fin-ring.
申请公布号 US2010183436(A1) 申请公布日期 2010.07.22
申请号 US20090356786 申请日期 2009.01.21
申请人 GENERAL ELECTRIC COMPANY 发明人 KASPERSKI DONALD JOSEPH
分类号 F01D25/24 主分类号 F01D25/24
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