Cooling passage exit opening cross-sectional area reduction for turbine system component
A turbine system component includes a body having an exterior surface, and a cooling passage defined in the body. The cooling passage has a first cross-sectional area in the body. The component also includes a hollow member defining a first exit opening at the exterior surface of the body and coupled in the cooling passage. The hollow member, at the first exit opening, has a second cross-sectional area that is less than the first cross-sectional area, creating an exit opening with a smaller dimension than the original cooling passage. The hollow member is made of a material having a melt temperature higher than an operating temperature of the turbine system. The hollow member(s) reduces the cooling capabilities of the cooling passage. A cooling profile of the component can be generated to identify those cooling passages having excess cooling so they can have their exit openings reduced in cross-sectional area.
1. A method, comprising:
coupling a hollow member into at least one first cooling passage in an exterior surface of a body of a component of a turbine system, the at least one first cooling passage defined in the body and having a first constant cross-sectional area in at least a portion of the at least one first cooling passage in which the hollow member is coupled, wherein a first portion of the hollow member extends outwardly beyond the exterior surface of the body; and
removing the first portion of the hollow member extending beyond the exterior surface of the body, the hollow member defining a first exit opening in fluid communication with the at least one first cooling passage at the exterior surface of the body,
wherein the hollow member at the first exit opening has a second cross-sectional area that is less than the first cross-sectional area, the hollow member has an inner end that is opposite the first exit opening, and a wall thickness of the hollow member increases from the inner end to the first exit opening such that internal cross-sectional area of the hollow member decreases gradually from the inner end to the first exit opening.
2. The method of claim 1 , wherein the coupling of the hollow member includes:
inserting the hollow member into the at least one first cooling passage; and
performing a joining process to couple the hollow member in the at least one first cooling passage.
3. The method of claim 2 , further comprising cleaning the cooling passage prior to inserting the hollow member.
4. The method of claim 1 , wherein the body includes at least one second cooling passage in the exterior surface of the body of the component, the at least one second cooling passage defined in the body having the first cross-sectional area at the exterior surface of the body.
5. The method of claim 4 , further comprising, prior to coupling the hollow member:
identifying the at least one first cooling passage from a plurality of cooling passages including the at least one first cooling passage and the at least one second cooling passage, based on a cooling profile of the component indicating any cooling passages having excess cooling capacity.
6. The method of claim 1 , wherein the hollow member extends inwardly of the exterior surface no less than a hydraulic diameter of the at least one first cooling passage.
7. The method of claim 1 , wherein the first cross-sectional area is 2 to 3 times larger than the second cross-sectional area.
8. A method, comprising:
coupling a hollow member into at least one first cooling passage in an exterior surface of a body of a component of a turbine system, the at least one first cooling passage identified from a plurality of cooling passages defined in the body of the component as having excess cooling capacity, wherein the at least one first cooling passage has a first constant cross-sectional area in at least a portion of the at least one first cooling passage in which the hollow member is coupled; and
the hollow member defining a first exit opening in fluid communication with the at least one first cooling passage at the exterior surface of the body,
wherein the hollow member at the first exit opening has a second cross-sectional area that is less than the first cross-sectional area, the hollow member has an inner end that is opposite the first exit opening, and a wall thickness of the hollow member increases from the inner end to the first exit opening such that internal cross-sectional area of the hollow member decreases gradually from the inner end to the first exit opening.
9. The method of claim 8 , further comprising identifying the at least one first cooling passage from the plurality of cooling passages defined in the body of the component based on the cooling profile of the component.
10. The method of claim 8 , wherein the coupling the hollow member includes:
inserting the hollow member into the at least one first cooling passage; and
performing a joining process to couple the hollow member in the at least one first cooling passage.
11. The method of claim 10 , further comprising cleaning the at least one first cooling passage prior to inserting the hollow member.
12. The method of claim 8 , wherein the plurality of cooling passages in the body includes at least one second cooling passage having a second exit opening in the exterior surface of the body of the component, the at least one second cooling passage defined in the body has the first cross-sectional area at the second exit opening in the exterior surface of the body.
13. The method of claim 8 , further comprising, prior to coupling the hollow member, identifying the at least one first cooling passage from the plurality of cooling passages based on a cooling profile of the component indicating any cooling passages having excess cooling capacity.
14. The method of claim 8 , wherein the hollow member extends inwardly of the exterior surface.
15. The method of claim 8 , wherein the first cross-sectional area is 2 to 3 times larger than the second cross-sectional area.
16. The method of claim 8 , wherein the body includes a nickel or cobalt-based superalloy, and the hollow member includes a nickel-chromium-based superalloy, a cobalt-based superalloy, or a stainless steel.
17. A method, comprising:
creating a cooling profile of a turbine system component based on at least one parameter of the turbine system component, the turbine system component including a plurality of cooling passages defined in an exterior surface of a body of the turbine system component;
identifying at least one first cooling passage of a plurality of cooling passages in a component for a turbine system that has excess cooling capacity based on at least on the cooling profile of the component, the at least one first cooling passage having a first constant cross-sectional area in at least a portion of the at least one first cooling passage in which the hollow member is coupled; and
coupling a hollow member into the at least one first cooling passage, the hollow member defining a first exit opening in fluid communication with the at least one first cooling passage at the exterior surface of the body, wherein the first exit opening has a second cross-sectional area that is less than the first cross-sectional area, the hollow member has an inner end that is opposite the first exit opening, and a wall thickness of the hollow member increases from the inner end to the first exit opening such that internal cross-sectional area of the hollow member decreases gradually from the inner end to the first exit opening, thereby reducing a flow of coolant through the first exit opening of the at least one first cooling passage.
18. The method of claim 17 , wherein the coupling of the hollow member includes:
inserting the hollow member into the at least one first cooling passage; and
performing a joining process to couple the hollow member in the at least one first cooling passage.
19. The method of claim 17 , further comprising determining the second cross-sectional area based at least in part on the excess cooling capacity of the at least one cooling passage.
20. The method of claim 19 , wherein the body includes at least one second cooling passage in the exterior surface of the body of the component, the at least one second cooling passage defined in the body having the first cross-sectional area at the exterior surface of the body.