发明名称 Airfoil shape for a compressor
摘要 An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLES 1-11, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.
申请公布号 US9017019(B2) 申请公布日期 2015.04.28
申请号 US201213526863 申请日期 2012.06.19
申请人 General Electric Company 发明人 McKeever Matthew John;Liu Gang;Garg Umesh;Murphy Ryan Wesley;Schurr Edward Charles;Dutka Michael James;Rengarajan Govindarajan;Delvernois Paul Griffin;Chiu Ya-Tien;Beharrysingh Roger Claude;Blohm Marc Edward;Narendran SenthilKumar
分类号 F01D9/02;F04D29/54;F01D5/14 主分类号 F01D9/02
代理机构 代理人 Pemrick James W.;Cusick Ernest G.;Landgraff Frank A.
主权项 1. An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLES 1-11, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.
地址 Schenectady NY US