发明名称 Turbine bucket angel wing features for forward cavity flow control and related method
摘要 A turbine bucket includes a radially inner mounting portion, a shank radially outward of the mounting portion, a radially outer airfoil and a substantially planar platform radially between the shank and the airfoil. At least one axially-extending angel wing seal flange is formed on a leading end of the shank thus forming a circumferentially extending trench cavity along the leading end of the shank, radially between an underside of the platform leading edge and the angel wing seal flange. A plurality of substantially radially grooves are formed on a radially outer surface of the angel wing seal flange and extend into the shank.
申请公布号 US8834122(B2) 申请公布日期 2014.09.16
申请号 US201113282121 申请日期 2011.10.26
申请人 General Electric Company 发明人 Ingram Clint Luigie
分类号 F01D11/04;F01D11/00;F01D5/14 主分类号 F01D11/04
代理机构 Nixon & Vanderhye P.C. 代理人 Nixon & Vanderhye P.C.
主权项 1. A turbine bucket comprising: a radially inner mounting portion, a shank radially outward of the mounting portion, a radially outer airfoil and a substantially planar platform radially between the shank and the airfoil; at least one axially-extending angel wing seal flange on a leading end of the shank thus forming a circumferentially extending trench cavity along the leading end of the shank, radially between an underside of the platform leading edge and the angel wing seal flange; and a plurality of grooves formed on a radially outer surface of said angel wing seal flange and extending into said shank, wherein in the grooves extend axially without a curve along their length on the outer surface of the angel wing seal flange.
地址 Schenectady NY US