发明名称 BLADE DOVETAIL BOTTOM
摘要 A blade has an airfoil extending radially outwardly of a dovetail. The dovetail has edges that will be at circumferential sides of the blade when the blade is mounted within a rotor. A bottom surface of the dovetail will be radially inward when the rotor blade is mounted in a rotor, and is formed such that a circumferentially central portion of the bottom surface is radially thicker than are circumferential edges. A fan and a gas turbine engine are also described.
申请公布号 WO2014014539(A3) 申请公布日期 2014.03.27
申请号 WO2013US38573 申请日期 2013.04.29
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 WHITEHURST, SEAN A.;MCKAVENEY, CHRISTOPHER S.;MCCOMB, PATRICK JAMES
分类号 F01D5/30;F02C7/00 主分类号 F01D5/30
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