发明名称 INTERNAL CORE PROFILE FOR A TURBINE NOZZLE AIRFOIL
摘要 First stage nozzle airfoils have internal core profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I wherein X, Y and Z values are in inches. The X and Y values are distances which, when connected by smooth continuing arcs, define internal core profile sections at each radial distance Z. The profile sections at each distance Z are joined smoothly to one another to form a complete internal core profile. The X, Y and Z distances may be scalable as a function of the same constant or number to provide a scaled-up or scaled-down internal core profile. The nominal internal core profile given by the X, Y and Z distances lies within an envelope of ±0.030 inches in directions normal to any internal core surface location.
申请公布号 US2005265829(A1) 申请公布日期 2005.12.01
申请号 US20040853240 申请日期 2004.05.26
申请人 GENERAL ELECTRIC COMPANY 发明人 HUMANCHUK DAVID J.;JACKS CURTIS J.;COIGN ROBERT W.
分类号 F01D9/02;B63H1/14;F01D5/14;F01D5/18;F01D9/04;(IPC1-7):B63H1/14 主分类号 F01D9/02
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