发明名称 Conical tip shroud fillet for a turbine bucket
摘要 A turbine bucket airfoil has a conical fillet about the intersection of the airfoil tip and tip shroud having a nominal profile in accordance with coordinate values of X and Y, offset 1, offset 2 and Rho set forth in Table I. The shape parameters of offset 1, offset 2 and Rho define the configuration of the fillet at the specified X and Y locations about the fillet to provide a fillet configuration accommodating high localized stresses. The fillet shape may be parabolic, elliptical or hyperbolic as a function of the value of the shape parameter ratio of <maths id="MATH-US-00001" num="00001"> <MATH OVERFLOW="SCROLL"> <MFRAC> <MI>D1</MI> <MROW> <MI>D1</MI> <MO>+</MO> <MI>D2</MI> </MROW> </MFRAC> </MATH> </MATHS> at each X, Y location where D1 is a distance between an intermediate point along a chord between edge points determined by offsets O1 and O2 and a shoulder point on the fillet surface and D2 is a distance between the shoulder point and an apex location at the intersection of the airfoil tip and tip shroud.
申请公布号 US7063509(B2) 申请公布日期 2006.06.20
申请号 US20030655623 申请日期 2003.09.05
申请人 GENERAL ELECTRIC COMPANY 发明人 SNOOK DANIEL DAVID;CLEVELAND PETER GAINES
分类号 B63H1/16;F01D5/14 主分类号 B63H1/16
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