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A system and a method to supply a coolant to a turbine bucket of a turbine. The system includes an extraction system configured to extract air from a main compressor airflow, a supply circuit, at least a part of which is disposed at an exterior of the gas turbine, coupled to the extraction system an

A system and a method to supply a coolant to a turbine bucket of a turbine. The system includes an extraction system configured to extract air from a main compressor airflow, a supply circuit, at least a part of which is disposed at an exterior of the gas turbine, coupled to the extraction system and configured to transport the extracted air, as an ingredient of the coolant, from the extraction system to a coolant insertion region, and a cooling system, disposed proximate to the coolant insertion region of the gas turbine and coupled to the supply circuit at a position on-board the gas turbine, the cooling system being configured to supply the turbine bucket with the coolant, including the extracted air.

대표청구항 ▼

1. A system to supply a coolant to a turbine bucket of a gas turbine, the system comprising: an extraction system configured to extract air from a main compressor airflow at a set of extraction points defined axially along the main compressor airflow;a supply circuit partially disposed at an exterio

1. A system to supply a coolant to a turbine bucket of a gas turbine, the system comprising: an extraction system configured to extract air from a main compressor airflow at a set of extraction points defined axially along the main compressor airflow;a supply circuit partially disposed at an exterior of the gas turbine and coupled to the extraction system, the supply circuit being configured to transport a substantial entirety of the extracted air, as an ingredient of the coolant, from the extraction system to the exterior of the gas turbine and then to a coolant insertion region of the gas turbine at a position on-board the gas turbine, which is defined radially inwardly from a radially inward-most portion of a rotation disc driven by the turbine bucket; anda cooling system, disposed proximate to the coolant insertion region and coupled to the supply circuit at the position on-board the gas turbine, the cooling system being configured to supply the turbine bucket with the coolant, including the extracted air, in a radially increasing direction. 2. The system according to claim 1, wherein the air is extracted from the main compressor airflow at the set of extraction points, and wherein the coolant insertion region of the gas turbine is located aft of the set of extraction points. 3. The system according to claim 1, wherein the extraction system comprises an air supplying body coupled to the supply circuit and configured to receive and to store the extracted air. 4. The system according to claim 1, wherein the cooling system comprises a forced vortexing system. 5. The system according to claim 4, wherein the forced vortexing system comprises: an axial tube configured to deliver the coolant, including the extracted air, to the turbine bucket; anda forced vortexing mechanism which captures the flow from the axial tube and configured to increase a coolant flow velocity of the coolant. 6. The system according to claim 1, wherein the cooling system comprises a free vortexing system. 7. The system according to claim 1, wherein the supply circuit comprises a heat exchanger configured to heat and/or to cool the extracted air. 8. The system according to claim 1, wherein the supply circuit comprises a cleaning device configured to clean the extracted air. 9. The system according to claim 1, wherein the supply circuit comprises a measuring device configured to measure a predetermined characteristic of the extracted air. 10. The system according to claim 1, wherein the supply circuit comprises a compressor which is configured to adjust a compression of the extracted air. 11. The system according to claim 1, wherein the cooling system is coupled to the supply circuit via a stationary pipe. 12. The system according to claim 1, wherein the cooling system is coupled to the supply circuit via an air gland with a converging circumferential passage. 13. The system according to claim 1, wherein the cooling system is further configured to re-circulate leaked air. 14. A system to supply a coolant to turbine buckets of a gas turbine, the system comprising: an extraction system configured to extract a set of air supplies from a main compressor airflow at a set of extraction points defined axially along the main compressor airflow;a supply circuit partially disposed at an exterior of the gas turbine, coupled to the extraction system and configured to transport a substantial entirety of each of the supplies of the extracted air, as ingredients of the coolant, from the extraction system to the exterior of the gas turbine and then to a coolant insertion region of the gas turbine at a position on-board the gas turbine, which is defined radially inwardly from radially inward-most portions of rotation discs driven by the turbine buckets; anda cooling system, disposed proximate to the coolant insertion region and coupled to the supply circuit at the position on-board the turbine, the cooling system being configured to supply the turbine buckets with the coolant, including each of the supplies of the extracted air, in a radially increasing direction. 15. The system according to claim 14, wherein the air supplies are extracted from the airflow at the set of extraction points, and wherein the coolant insertion region of the turbine is located aft of the extraction points. 16. The system according to claim 15, wherein increasingly aft positioned turbine buckets are respectively supplied with a portion of the coolant including those supplies of the extracted air that are respectively extracted from increasingly forward positioned extraction points. 17. The system according to claim 14, wherein the supply circuit transports each of the supplies of the extracted air independently from the others. 18. A method of supplying a coolant to a turbine bucket of a gas turbine, the method comprising: extracting air from a main compressor airflow at multiple extraction points defined axially along the main compressor airflow;transporting a substantial entirety of the extracted air, as an ingredient of the coolant, to an exterior of the gas turbine and then to a coolant insertion region of the gas turbine at an on-board position of the gas turbine, which is defined radially inwardly from a radially inward-most portion of a rotation disc driven by the turbine bucket; andsupplying increasingly aft positioned ones of the turbine bucket with the coolant, including the extracted air, in a radially increasing direction. 19. The method according to claim 18, wherein the transporting of the extracted air comprises: exchanging heat with the extracted air;cleaning the extracted air;measuring a predetermined characteristic of the extracted air; andcompressing the extracted air. 20. The method according to claim 18, wherein the extracting of the air comprises extracting the air at the multiple extraction points, and wherein the supplying of the turbine bucket with the coolant comprises supplying multiple turbine buckets with the coolant.