Interior cooling circuits in turbine blades

Patent metadata

Field	Value
Publication number	US-9765630-B2
Application number	US-201313737023-A
Country	US
Kind code	B2
Filing date	Jan 9, 2013
Priority date	Jan 9, 2013
Publication date	Sep 19, 2017
Grant date	Sep 19, 2017

Abstract

A rotor blade including an airfoil portion and a root portion, and an internal cooling circuit having flow passages in the root portion and the airfoil portion, wherein the internal cooling circuit includes: a first flow passage; and a non-integral plug. The plug may include a plug channel configured to correspond to a desired level of coolant flow through the first cooling passage. The plug may be connected to the rotor blade in a fixed blocking position relative to the first flow passage.

First claim

We claim:

1. A method of manufacturing a blade having an internal cooling circuit, the blade configured for use in a combustion turbine engine, wherein the turbine blade comprises an airfoil portion and a root portion, the method comprising the steps of:
casting the internal cooling circuit using a core that includes an oversized supporting connection configured for enhanced core robustness, wherein the oversized supporting connection forms a first flow passage in the internal cooling circuit and is oversized relative to a desired level of coolant flow through the first flow passage during operation;
forming a plug;
forming a plug channel through the interior of the plug, the plug channel configured to correspond to the desired level of coolant flow through the first flow passage; and
connecting the plug to the blade so that the plug is fixed in a blocking position relative to the first flow passage.

2. The method of manufacturing a blade according to claim 1 , wherein the blade comprises a rotor blade in a turbine section of the combustion turbine engine.

3. The method of manufacturing a blade according to claim 2 , wherein the step of connecting the plug to the blade includes brazing the plug in the blocking position.

4. The method of manufacturing a blade according to claim 2 , wherein the blocking position comprises aligning the plug so coolant flow through the plug channel is allowed while any other coolant flow through the first flow passage is prevented.

5. The method of manufacturing a blade according to claim 2 , wherein the plug and first flow passage are configured so to include a mechanical interference fit therebetween preventing downstream movement of the plug beyond a predetermined point.

6. The method of manufacturing a blade according to claim 5 , wherein the mechanical interference fit includes a seat configured to engage the plug and the predetermined point comprises a narrowed neck section in the first flow passage; and
wherein the blocking position includes the plug residing in an upstream portion of the first flow passage.

7. The method of manufacturing a blade according to claim 6 , wherein the plug comprises a tapering shape, wherein a smaller end of the tapering shape is configured to engage the seat of the mechanical interference fit and a larger end of the tapering shape is configured to engage the neck section.

8. The method of manufacturing a blade according to claim 6 , wherein the plug is spherical in shape.

9. The method of manufacturing a blade according to claim 5 , wherein the forming the plug channel is completed via a machining process after the plug is connected to the blade in the blocking position.

10. The method of manufacturing a blade according to claim 5 , wherein the forming the plug channel is completed before the plug is connected to the blade in the blocking position.

11. The method of manufacturing a blade according to claim 2 , wherein the desired level of coolant flow comprises a minimum level of coolant flow based on blade cooling criteria;
further comprising the steps of:
determining that an actual level of coolant flow through the first flow passage is insufficient; and
widening the plug channel in the first flow passage.

12. The method of manufacturing a blade according to claim 11 , further comprising the steps of:
disconnecting the plug from the blade;
reconnecting the modified plug in the blocking position.

13. The method of manufacturing a blade according to claim 2 , wherein the desired level of coolant flow comprises a minimum level of coolant flow based on blade cooling criteria;
further comprising the steps of:
determining that an actual level of coolant flow through the first flow passage is too large; and
narrowing the plug channel in the first flow passage.

14. The method of manufacturing a blade according to claim 13 , further comprising the steps of:
disconnecting the plug from the blade;
forming a new plug having a reduced plug channel;
reconnecting the new plug in the blocking position.

15. The method of manufacturing a blade according to claim 2 , wherein the plug comprises a first plug;
further comprising the step of replacing the first plug with a second plug, the second plug comprises a modified plug channel compared to the plug channel of the first plug.

16. The method of manufacturing a blade according to claim 2 , wherein the plug comprises a first plug;
further comprising the steps of
forming a second plug;
forming a plug channel through the second plug, the plug channel configured to correspond to a new desired level of coolant flow through the first flow passage;
disconnecting the first plug from the blade; and
connecting the second plug to the blade so the second plug comprises the fixed blocking position relative to the first flow passage.

Assignees

• Gen Electric

Inventors

• Herzlinger Jason Douglas
• Boyer Bradley Taylor
• Bommanakatte Harish
• Giglio Anthony Louis

Classifications

• Y10T29/49341

  with cooling passage · CPC title

• F05D2230/21

  by casting · CPC title

• F01D5/187 Primary

  Convection cooling · CPC title

• F05D2250/232

  conical · CPC title

• Y02T50/676

  Cross-Sectional Technologies · mapped topic