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 |