Turbine bucket with notched squealer tip

1. A turbine bucket comprising:

an airfoil including a pressure side and a suction side extending between a leading edge and a trailing edge, the airfoil further including a tip, the tip comprising:

a tip floor; and

a tip wall extending outwardly from the tip floor, the tip wall including an offset portion that is recessed relative to at least one of the pressure side or the suction side such that a tip shelf is defined at the offset portion, the offset portion of the tip wall defining an outer surface,

wherein a plurality of notches are defined by the outer surface of the offset portion of the tip wall, each of the plurality of notches being defined between opposed notch edges of the outer surface and extending radially between the tip shelf and a top surface of the tip wall,

wherein a plurality of cooling holes are defined in the tip shelf, a first cooling hole of the plurality of cooling holes being aligned with a first notch of the plurality of notches, the first cooling hole defining an outlet at the tip shelf for directing a cooling medium from an internal cooling circuit of the airfoil to an exterior of the airfoil,

wherein the first cooling hole extends lengthwise between the internal cooling circuit and the tip shelf such that the first cooling hole is angled towards the outer surface of the offset portion of the tip wall.

2. The turbine bucket of claim 1 , wherein the offset portion of the tip wall is disposed on the pressure side of the airfoil.

3. The turbine bucket of claim 1 , wherein each of the plurality of notches extends at an angle along the outer surface of the offset portion of the tip wall between the tip floor and the top surface of the tip wall.

4. The turbine bucket of claim 3 , wherein the angle ranges from 1 degree to 30 degrees.

5. The turbine bucket of claim 3 , wherein the outer surface of the offset portion of the tip wall and the first cooling hole are angled in the same direction.

6. The turbine bucket of claim 1 , wherein at least one cooling hole of the plurality of cooling holes is defined in the tip shelf so as to be positioned between two notches of the plurality of notches.

7. The turbine bucket of claim 1 , wherein the outlet of the first cooling hole defines a dimensional parameter that is smaller than an area defined between the opposed notch edges of the first notch.

8. The turbine bucket of claim 7 , wherein the outlet of the first cooling hole is spaced apart from the first notch along the tip shelf such that portions of the tip shelf extend outwardly from the outlet around an entire perimeter of the outlet.

9. The turbine bucket of claim 7 , wherein the dimensional parameter corresponds to a cross-sectional area of the outlet at the tip shelf.

10. The turbine bucket of claim 7 , wherein the outlet of the first cooling hole is positioned entirely within the area defined between the opposed notch edges of the first notch.

11. The turbine bucket of claim 10 , wherein the area is defined between the opposed notch edges at a radial location at which the first notch intersects the top surface of the tip wall.

12. The turbine bucket of claim 7 , wherein the outlet of the first cooling hole is positioned entirely outside the area defined between the opposed notch edges of the first notch.

13. A squealer tip for an airfoil, the squealer tip comprising:

a tip floor; and

a tip wall extending outwardly from the tip floor, the tip wall including an offset portion that is recessed relative to at least one of the pressure side or the suction side such that a tip shelf is defined at the offset portion, the offset portion of the tip wall defining an outer surface,

wherein a plurality of notches are defined by the outer surface of the offset portion of the tip wall, each of the plurality of notches being defined between opposed notch edges of the outer surface and extending radially between the tip shelf and a top surface of the tip wall,

wherein a plurality of cooling holes are defined in the tip shelf, a first cooling hole of the plurality of cooling holes being aligned with a first notch of the plurality of notches, the first cooling hole defining an outlet at the tip shelf for directing a cooling medium from an internal cooling circuit of the airfoil to an exterior of the airfoil,

wherein the first cooling hole extends lengthwise between the internal cooling circuit and the tip shelf such that the first cooling hole is angled towards the outer surface of the offset portion of the tip wall.

14. The squealer tip of claim 13 , wherein each of the plurality of notches extends at an angle along the outer surface of the offset portion of the tip wall between the tip floor and the top surface of the tip wall.

15. The squealer tip of claim 14 , wherein the angle ranges from 1 degree to 30 degrees.

16. The squealer tip of claim 14 , wherein the outer surface of the outer portion of the tip wall and the first cooling hole are angled in the same direction.

17. The squealer tip of claim 13 , wherein the outlet of the first cooling hole defines a dimensional parameter that is smaller than an area defined between the opposed notch edges of the first notch.

18. The squealer tip of claim 17 , wherein the outlet of the first cooling hole is spaced apart from the first notch along the tip shelf such that portions of the tip shelf extend outwardly from the outlet around an entire perimeter of the outlet.

19. The squealer tip of claim 13 , wherein the outlet of the first cooling hole is positioned entirely within or entirely outside the area defined between the opposed notch edges of the first notch.

20. The squealer tip of claim 19 , wherein the outlet of the first cooling hole is positioned entirely within the area defined between the opposed notch edges of the first notch, the area being defined between the opposed notch edges at a radial location at which the first notch intersects the top surface of the tip wall.