发明名称 Turbine bucket angel wing features for forward cavity flow control and related method
摘要 <p>A turbine bucket (66) includes a radially inner mounting portion, a shank (82) radially outward of the mounting portion, a radially outer airfoil (68) and a substantially planar platform (80) radially between the shank (82) and the airfoil (68). At least one axially-extending angel wing seal flange (84) is formed on a leading end of the shank (82) thus forming a circumferentially extending trench cavity (62) along the leading end of the shank (82), radially between an underside of the platform (80) leading edge and the angel wing seal flange (84). A plurality of substantially radially grooves (100) are formed on a radially outer surface of the angel wing seal flange (84) and extend into the shank (82).</p>
申请公布号 EP2586995(A2) 申请公布日期 2013.05.01
申请号 EP20120189646 申请日期 2012.10.23
申请人 GENERAL ELECTRIC COMPANY 发明人 INGRAM, CLINT LUIGIE
分类号 F01D11/00;F01D5/14 主分类号 F01D11/00
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