Steam turbine rotating blade for a low pressure section of a steam turbine engine
A steam turbine rotating blade for a low pressure section of a steam turbine engine is disclosed. The steam turbine rotating blade includes an airfoil portion. A root section is attached to one end of the airfoil portion. A dovetail section projects from the root section, wherein the dovetail section includes a skewed axial entry dovetail. A tip section is attached to the airfoil portion at an end opposite from the root section. A cover is integrally formed as part of the tip section. A part span shroud is attached at an intermediate section of the airfoil portion between the ends thereof. The blade includes an exit annulus area of about 47.7 ft 2 (4.43 m 2 ) or greater.
1. A steam turbine rotating blade, comprising:
an airfoil portion;
a root section attached to one end of the airfoil portion;
a dovetail section projecting from the root section, wherein the dovetail section comprises a skewed axial entry dovetail, wherein the skewed axial entry dovetail comprises about a 19 degree skew angle;
a tip section attached to the airfoil portion at an end opposite from the root section;
a cover integrally formed as part of the tip section;
a part span shroud attached at an intermediate section of the airfoil portion between the ends thereof; and
wherein the blade comprises an exit annulus area of about 47.7 ft 2 (4.43 m 2 ) or more.
2. The steam turbine rotating blade according to claim 1 , wherein the skewed axial entry dovetail comprises a three hook design having six contact surfaces configured to engage with a turbine rotor wheel.
3. The steam turbine rotating blade according to claim 1 , wherein the blade has an operating speed that ranges from about 1500 revolutions per minute to about 3600 revolutions per minute.
4. The steam turbine rotating blade according to claim 1 , wherein the airfoil portion comprises a length of about 26.8 inches (68.1 centimeters) or greater.
5. The steam turbine rotating blade according to claim 1 , wherein the blade operates as a latter stage blade of a low pressure section of a steam turbine.
6. The steam turbine rotating blade according to claim 1 , wherein the blade comprises a 12% chrome stainless steel material.
7. The steam turbine rotating blade according to claim 1 , further comprising a first fillet radius located at a first transition area where the dovetail section projects from the root section.
8. The steam turbine rotating blade according to claim 1 , wherein the part span shroud is triangular in shape and projects outwardly from the airfoil portion at a pressure side of the airfoil portion and a suction side of the airfoil portion.
9. The steam turbine rotating blade according to claim 1 , wherein the cover comprises a flat section that extends away from a leading edge of the airfoil portion at a predetermined distance therefrom to a trailing edge of the airfoil portion, the cover having a width that narrows substantially from an end located at the predetermined distance away from the leading edge to a location that is in a substantially central location with respect to the trailing edge and leading edge, the width of the cover increasing from the central location to the trailing edge, wherein the width of the cover at the end located at the predetermined distance away from the leading edge and the width of the cover at the trailing edge are substantially similar.
10. The steam turbine rotating blade according to claim 9 , further comprising a seal tooth that projects upward from the cover, wherein the seal tooth extends from the end located at the predetermined distance away from the leading edge through the substantially central location to the trailing edge.
11. The steam turbine rotating blade according to claim 9 , wherein the cover extends over a suction side of the airfoil portion at the end located at the predetermined distance away from the leading edge to about the central location, the cover extending over a pressure side of the airfoil portion from the central location to the trailing edge.
12. A low pressure turbine section of a steam turbine, comprising:
a plurality of latter stage steam turbine blades arranged about a turbine rotor wheel, wherein each of the plurality of latter stage steam turbine blades comprises:
an airfoil portion having a length of about 26.8 inches (68.1 centimeters) or greater;
a root section attached to one end of the airfoil portion;
a dovetail section projecting from the root section, wherein the dovetail section comprises a skewed axial entry dovetail, wherein the skewed axial entry dovetail comprises about a 19 degree skew angle;
a tip section attached to the airfoil at an end opposite from the root section;
a cover integrally formed as part of the tip section;
a part span shroud attached at an intermediate section of the airfoil portion between the ends thereof; and
wherein the plurality of latter stage steam turbine blades comprises an exit annulus area of about 47.7 ft 2 (4.43 m 2 ) or greater.
13. The low pressure turbine section according to claim 12 , wherein the plurality of latter stage steam turbine blades operate at a speed that ranges from about 1500 revolutions per minute to about 3600 revolutions per minute.
14. The low pressure turbine section according to claim 12 , wherein the skewed axial entry dovetail comprises a three hook design having six contact surfaces configured to engage with the turbine rotor wheel.
15. The low pressure turbine section according to claim 12 , wherein the covers of the plurality of latter stage steam turbine blades are assembled with a nominal gap with adjacent covers.
16. The low pressure turbine section according to claim 12 , wherein the covers of the plurality of latter stage steam turbine blades form a single continuously coupled structure.
17. The low pressure turbine section according to claim 12 , wherein the part span shrouds for each of the plurality of latter stage steam turbine blades are configured to have a gap therebetween, wherein the gap is closed as the plurality of latter stage steam turbine blades reaches a predetermined operational speed.
18. The low pressure turbine section according to claim 12 , wherein the cover comprises a flat section that extends away from a leading edge of the airfoil portion at a predetermined distance therefrom to a trailing edge of the airfoil portion, the cover having a width that narrows substantially from an end located at the predetermined distance away from the leading edge to a location that is in a substantially central location with respect to the trailing edge and leading edge, the width of the cover increasing from the central location to the trailing edge, wherein the width of the cover at the end located at the predetermined distance away from the leading edge and the width of the cover at the trailing edge are substantially similar, and wherein the cover extends over a suction side of the airfoil portion at the end located at the predetermined distance away from the leading edge to about the central location, the cover extending over a pressure side of the airfoil portion from the central location to the trailing edge.
19. The low pressure turbine section according to claim 18 , further comprising a seal tooth that projects upward from the cover, wherein the seal tooth extends from the end located at the predetermined distance away from the leading edge through the substantially central location to the trailing edge.