Bucket assembly treating apparatus and method for treating bucket assembly

Patent metadata

Field	Value
Publication number	US-9447691-B2
Application number	US-201113214583-A
Country	US
Kind code	B2
Filing date	Aug 22, 2011
Priority date	Aug 22, 2011
Publication date	Sep 20, 2016
Grant date	Sep 20, 2016

Abstract

A bucket assembly and a method for treating a bucket assembly are disclosed. The bucket assembly includes a platform, the platform defining a platform cooling circuit, and an airfoil extending generally radially outward from the platform, the airfoil defining an airfoil cooling circuit. The bucket assembly additionally includes a lower body portion extending generally radially inward from the platform, the lower body portion defining a root and a cooling passage extending from the root, the cooling passage in fluid communication with the airfoil cooling circuit. The bucket assembly further includes a transfer passage defined between and in fluid communication with the airfoil cooling circuit and the platform cooling circuit such that a cooling medium may flow from the airfoil cooling circuit through the transfer passage to the platform cooling circuit.

First claim

What is claimed is:

1. A bucket assembly comprising:
a platform, the platform defining a platform cooling circuit;
an airfoil extending generally radially outward from the platform, the airfoil defining an airfoil cooling circuit;
a lower body portion extending generally radially inward from the platform, the lower body portion defining a root and a cooling passage extending from the root, the cooling passage in fluid communication with the airfoil cooling circuit; and
a transfer passage defined between and in fluid communication with the airfoil cooling circuit and the platform cooling circuit such that a cooling medium may flow from the airfoil cooling circuit through the transfer passage to the platform cooling circuit,
wherein the airfoil cooling circuit terminates at the transfer passage such that cooling medium flowing from a terminal end of the airfoil cooling circuit flows only into the transfer passage, and
wherein the transfer passage couples to the platform cooling circuit between an upstream end of the platform cooling circuit and a downstream end of the platform cooling circuit at a location spaced apart from the upstream end of the platform cooling circuit and the downstream end of the platform cooling circuit.

2. The bucket assembly of claim 1 , further comprising a plurality of transfer passages.

3. The bucket assembly of claim 1 , wherein the airfoil defines a plurality of airfoil cooling circuits and the lower body portion defines a plurality of cooling passages, each of the cooling passages in fluid communication with one of the airfoil cooling circuits, and wherein the transfer passage is defined between and in fluid communication with one of the plurality of airfoil cooling circuits and the platform cooling circuit.

4. The bucket assembly of claim 3 , wherein the plurality of airfoil cooling circuits comprises a leading edge cooling circuit, a middle cooling circuit, and a trailing edge cooling circuit, and wherein the transfer passage is defined between and in fluid communication with the middle cooling circuit and the platform cooling circuit.

5. The bucket assembly of claim 3 , wherein at least one of the plurality of airfoil cooling circuits comprises a plurality of passages, each of the plurality of passages in fluid communication with another of the plurality of passages, and wherein the transfer passage is defined between and in fluid communication with one of the plurality of passages and the platform cooling circuit.

6. The bucket assembly of claim 5 , wherein the plurality of passages includes at least one upflow passage and at least one downflow passage, and wherein the transfer passage is defined between and in fluid communication with the at least one downflow passage and the platform cooling circuit.

7. The bucket assembly of claim 1 , the platform further defining an exhaust passage, the exhaust passage configured to exhaust cooling medium from the platform cooling circuit adjacent the platform.

8. The bucket assembly of claim 1 , wherein the lower body portion includes a shank and a dovetail, the dovetail defining the root.

9. A turbine system comprising:
a compressor;
a turbine coupled to the compressor;
a plurality of bucket assemblies disposed in at least one of the compressor or the turbine, at least one of the bucket assemblies comprising:
a platform, the platform defining a platform cooling circuit;
an airfoil extending generally radially outward from the platform, the airfoil defining an airfoil cooling circuit;
a lower body portion extending generally radially inward from the platform, the lower body portion defining a root and a cooling passage extending from the root, the cooling passage in fluid communication with the airfoil cooling circuit; and
a transfer passage defined between and in fluid communication with the airfoil cooling circuit and the platform cooling circuit such that a cooling medium may flow from the airfoil cooling circuit through the transfer passage to the platform cooling circuit,
wherein the airfoil cooling circuit terminates at the transfer passage such that cooling medium flowing from a terminal end of the airfoil cooling circuit flows only into the transfer passage, and
wherein the transfer passage couples to the platform cooling circuit between an upstream end of the platform cooling circuit and a downstream end of the platform cooling circuit at a location spaced apart from the upstream end of the platform cooling circuit and the downstream end of the platform cooling circuit.

10. The turbine system of claim 9 , further comprising a plurality of transfer passages.

11. The turbine system of claim 9 , wherein the airfoil defines a plurality of airfoil cooling circuits and the lower body portion defines a plurality of cooling passages, each of the cooling passages in fluid communication with one of the airfoil cooling circuits, and wherein the transfer passage is defined between and in fluid communication with one of the plurality of airfoil cooling circuits and the platform cooling circuit.

12. The turbine system of claim 11 , wherein the plurality of airfoil cooling circuits comprises a leading edge cooling circuit, a middle cooling circuit, and a trailing edge cooling circuit, and wherein the transfer passage is defined between and in fluid communication with the middle cooling circuit and the platform cooling circuit.

13. The turbine system of claim 11 , wherein at least one of the plurality of airfoil cooling circuits comprises a plurality of passages, each of the plurality of passages in fluid communication with another of the plurality of passages, and wherein the transfer passage is defined between and in fluid communication with one of the plurality of passages and the platform cooling circuit.

14. The turbine system of claim 13 , wherein the plurality of passages includes at least one upflow passage and at least one downflow passage, and wherein the transfer passage is defined between and in fluid communication with the at least one downflow passage and the platform cooling circuit.

15. The turbine system of claim 9 , the platform further defining an exhaust passage, the exhaust passage configured to exhaust cooling medium from the platform cooling circuit adjacent the platform.

16. The turbine system of claim 9 , wherein the lower body portion includes a shank and a dovetail, the dovetail defining the root.

17. The turbine system of claim 9 , wherein each of the plurality of bucket assemblies comprises a platform, an airfoil, a lower body portion, and a transfer passage.

18. The turbine system of claim 9 , wherein the plurality of bucket assemblies are disposed in the turbine.

19. A method for treating a bucket assembly, the method comprising:
flowing a cooling medium into an airfoil cooling circuit from a cooling passage, the airfoil cooling circuit defined in an airfoil that extends generally radially outward from a platform, the cooling passage defined in a root that extends generally radially inward from the platform;
flowing the cooling medium through the airfoil cooling circuit; and,
exhausting the cooling medium from the airfoil cooling circuit into a platform cooling circuit through a transfer passage, the platform cooling circuit defined in the platform,
wherein the airfoil cooling circuit terminates at the transfer passage such that cooling medium flowing from a terminal end of the airfoil cooling circuit flows only into the transfer passage, and
wherein the transfer passage couples to the platform cooling circuit between an upstream

Assignees

• Smith Aaron Ezekiel
• Itzel Gary Michael
• Ellis Scott Edmond
• Gen Electric

Inventors

• Smith Aaron Ezekiel
• Itzel Gary Michael
• Ellis Scott Edmond

Classifications

• F01D5/186

  Film cooling (F01D5/187 takes precedence) · CPC title

• F01D5/187 Primary

  Convection cooling · CPC title

• F05D2240/81

  Cooled platforms · CPC title