发明名称 |
Turbine nozzle airfoil profile |
摘要 |
The present application provides a turbine nozzle including an airfoil shape. The airfoil shape may have a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table 1. 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. The X and Y values 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 may be joined smoothly with one another to form a complete airfoil shape. |
申请公布号 |
US8876485(B2) |
申请公布日期 |
2014.11.04 |
申请号 |
US201113304730 |
申请日期 |
2011.11.28 |
申请人 |
General Electric Company |
发明人 |
Gustafson Ross James;Winn Aaron Gregory |
分类号 |
F01D9/04;F01D5/14 |
主分类号 |
F01D9/04 |
代理机构 |
Sutherland Asbill & Brennan LLP |
代理人 |
Sutherland Asbill & Brennan LLP |
主权项 |
1. A turbine nozzle comprising an airfoil shape, the airfoil shape having a nominal profile 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. |
地址 |
Schenectady NY US |