Optimized aerodynamic airfoil for a turbine blade
View Patent ↗When cold and in the uncoated state, the aerodynamic airfoil is substantially identical to a nominal airfoil determined by the Cartesian coordinates X, Y, Z′ given in Table 1, in which the coordinate Z′ is the ratio D/H where D is the distance from the point in question to a reference plane P 0 , located at the base of the nominal airfoil, and H is the height of this airfoil, measured from said reference plane up to the tip of the blade. The D and H measurements being taken radially with respect to the axis of the turbine whereas the X coordinate is measured in the axial direction of the turbine.
1. An aerodynamic airfoil for a turbine blade, which, when cold and in the uncoated state, is substantially identical to a nominal airfoil determined by the Cartesian coordinates X, Y, Z′ given in Table 1, in which the coordinate Z′ is the ratio D/H where D is the distance from the point in question to a reference plane P 0 , located at the base of the nominal airfoil, and H is the height of this airfoil, measured from said reference plane up to the tip of the blade, the D and H measurements being taken radially with respect to the axis of the turbine whereas the X coordinate is measured in the axial direction of the turbine.
2. The aerodynamic airfoil as claimed in claim 1 , which is defined within an envelope of ±1 mm in a direction normal to the surface of the nominal airfoil.
3. The aerodynamic airfoil as claimed in claim 1 or 2 , wherein the X, Y coordinates of said airfoil lie within the ±5% range with respect to the X, Y coordinates of the nominal airfoil.
4. A turbine blade, which has an aerodynamic airfoil as claimed in claim 1 .
5. A turbine, which includes turbine blades having aerodynamic airfoils as claimed in claim 1 .
6. The turbine as claimed in claim 5 , which includes a ring of fixed guide blades having between 32 and 40 blades, each having an aerodynamic airfoil as claimed in claim 1 .
7. A turbomachine equipped with a turbine that includes blades having aerodynamic airfoils as claimed in claim 1 .