发明名称 Turbine nozzle airfoil profile
摘要 A turbine nozzle is provided including a nozzle airfoil having an airfoil shape, the nozzle airfoil having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table 1 wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances in inches by multiplying the Cartesian coordinate values of X, Y and Z by a height of the airfoil in inches, and wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z, the airfoil profile sections at Z distances being joined smoothly with one another to form a complete airfoil shape.
申请公布号 US8814526(B2) 申请公布日期 2014.08.26
申请号 US201113304732 申请日期 2011.11.28
申请人 General Electric Company 发明人 Stein Alexander;Morgan Victor John;Brunt Thomas James;Gergely George Andrew
分类号 F01D5/14 主分类号 F01D5/14
代理机构 代理人 Pemrick James W.;Cusick Ernest G.;Landgraff Frank A.
主权项 1. A turbine nozzle including a nozzle airfoil having an airfoil shape, the nozzle airfoil having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table 1 wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a height of the nozzle airfoil, and wherein X and Y are distances which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z, the airfoil profile sections at Z distances being joined smoothly with one another to form a complete airfoil shape.
地址 Schenectady NY US
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