Steam turbine rotating blade
A rotating blade for a steam turbine includes a root section and an airfoil section contiguous with the root section. The airfoil section is shaped to optimize aerodynamic performance while providing optimized flow distribution and minimal centrifugal and bending stresses. The blade also includes a tip section continuous with the airfoil section, and a cover formed as part of the tip section. The cover defines a radial seal that serves to minimize tip losses. The rotating blade is capable of running at operating speeds between 5626 and 11250 rotations per minute.
1. A rotating blade for a steam turbine comprising:
a root section;
an airfoil section contiguous with the root section, the airfoil section being shaped to optimize aerodynamic performance while providing optimized flow distribution and minimal centrifugal and bending stresses;
a tip section continuous with the airfoil section; and
a cover formed as part of the tip section, the cover defining a radial seal that minimizes tip losses,
wherein an exit annulus area of the rotating blade is 0.461 m 2 .
2. A rotating blade according to claim 1 , wherein an operating speed range of the blade is between 5625 and 11250 rotations per minute.
3. A rotating blade according to claim 2 , comprising a maximum mass flow of 30.9 kg/s.
4. A rotating blade according to claim 1 , wherein an operating speed range of the blade is between 5625 and 11250 rotations per minute.
5. A rotating blade according to claim 1 , wherein the blade is designed for operation as a last stage blade.
6. A rotating blade according to claim 5 , wherein the cover is sized such that at speed, the cover engages an adjacent cover of an adjacent blade.
7. A rotating blade according to claim 6 , wherein the cover is integral with the tip section.
8. A rotating blade according to claim 1 , wherein the cover is integral with the tip section.
9. A rotating blade according to claim 1 , wherein the radial seal comprises at least one tip seal.
10. A rotating blade for a steam turbine comprising:
a root section;
an airfoil section contiguous with the root section, the airfoil section being shaped to optimize aerodynamic performance while providing optimized flow distribution and minimal centrifugal and bending stresses;
a tip section continuous with the airfoil section and having a tip width; and
a cover formed as part of the tip section, the cover defining a radial seal that minimizes tip losses, wherein the cover is wider than the tip width such that at speed, the cover engages an adjacent cover of an adjacent blade, and
wherein an exit annulus area of the blade is 0.461 m 2 , an operating speed range of the blade is between 5625 and 11250 rotations per minute, and a maximum mass flow of the blade is 30.9 kg/s.
11. A rotating blade according to claim 10 , wherein the airfoil section comprises an optimal pitch to width ratio.
12. A rotating blade according to claim 10 , wherein a thickness distribution of the airfoil section is configured to optimize blade speed capabilities and resistance to low cycle fatigue.
13. A rotating blade according to claim 10 , wherein the airfoil section comprises a curvature that lowers pressure losses and shock losses.
14. A rotating blade according to claim 10 , wherein the airfoil section is twisted such that at rest, there is a gap between the cover and a cover of an adjacent blade, and wherein at speed, the airfoil section is configured to untwist such that the cover engages the cover of the adjacent blade.
15. A rotating blade according to claim 10 , wherein the blade is formed of M152 steel.