Apparatus for cooling a platform of a turbine component
The present subject matter discloses a turbine component including a platform and an airfoil extending radially upward from the platform. A plurality of curved cooling passages may be defined in the platform. Each of the curved cooling passages may have at least one end disposed at an exterior surface of the platform. Additionally, each of the cooling passages may be configured to direct a cooling medium through the platform.
1. A turbine component comprising:
a platform;
an airfoil extending radially upward from said platform, said airfoil including a pressure side and a suction side;
a plurality of concentric curved cooling passages defined in said platform, each of said plurality of cooling passages extending between a first end and a second end, at least one of said first end or said second end being disposed at an exterior surface of said platform, each of said plurality of cooling passages defining a constant radius between said first and second ends; and
wherein each of said plurality of cooling passages is configured to direct a cooling medium through said platform.
2. The turbine component of claim 1 , wherein said turbine component comprises a turbine bucket.
3. The turbine component of claim 1 , wherein each of said plurality of cooling passages is defined in said platform on said pressure side of said airfoil.
4. The turbine component of claim 1 , wherein each of said plurality of cooling passages is turbulated along its length.
5. The turbine component of claim 1 , wherein the cooling medium is supplied to said plurality of cooling passages from an airfoil cooling circuit at least partially disposed in said airfoil.
6. The turbine component of claim 1 , wherein the cooling medium flowing through said plurality of cooling passages is expelled into an airfoil cooling circuit at least partially disposed in said airfoil.
7. The turbine component of claim 1 , wherein the cooling medium flowing through each of said plurality of cooling passages is expelled through a plurality of film cooling holes defined through a top surface of said platform.
8. The turbine component of claim 1 , wherein said first and second ends of each of said plurality of cooling passages are defined through a side face of said platform.
9. The turbine component of claim 8 , further comprising a plug disposed at at least one of said first end or said second end.
10. The turbine component of claim 8 , further comprising a plug disposed at said common end.
11. A turbine component comprising:
a platform;
an airfoil extending radially upward from said platform, said airfoil including a pressure side and a suction side;
a plurality of non-concentric curved cooling passages defined in said platform, each of said plurality of cooling passages being configured to direct a cooling medium through said platform, each of said plurality of cooling passages extending from a common end; and
wherein a common cooling medium inlet supplies the cooling medium to each of said plurality of cooling passages, the common cooling medium inlet being disposed adjacent to the common end.
12. The turbine component of claim 11 , wherein said turbine component comprises a turbine bucket.
13. The turbine component of claim 11 , wherein each of said plurality of cooling passages is defined in said platform on said pressure side of said airfoil.
14. The turbine component of claim 11 , wherein each of said plurality of cooling passages is turbulated along its length.
15. The turbine component of claim 11 , wherein each of said plurality of cooling passages has a curvature that varies along its length.
16. The turbine component of claim 11 , comprising an airfoil cooling circuit at least partially disposed in said airfoil, said airfoil cooling circuit being in flow communication with said common cooling medium inlet.
17. The turbine component of claim 11 , comprising a common cooling medium outlet in flow communication with each of said plurality of cooling passages, said common cooling medium outlet configured to expel the cooling medium from each of said plurality of cooling passages.
18. The turbine component of claim 17 , wherein said common cooling medium outlet is in flow communication with an airfoil cooling circuit at least partially disposed within said airfoil.
19. The turbine component of claim 11 , comprising a plurality of film cooling holes defined through a top surface of said platform, wherein the cooling medium flowing through said plurality of cooling passages is expelled through said plurality of film cooling holes.
20. A turbine component comprising:
a platform;
an airfoil extending radially upward from said platform, said airfoil including a pressure side and a suction side;
a plurality of non-concentric curved cooling passages defined in said platform, each of said plurality of cooling passages being configured to direct a cooling medium through said platform; and
wherein a common cooling medium inlet supplies the cooling medium to each of said plurality of cooling passages,
wherein a common cooling medium outlet is in flow communication with each of said plurality of cooling passages, said common cooling medium outlet configured to expel the cooling medium from each of said plurality of cooling passages.