Patent ID: 8726672

Claim:
A cooling system for a gas turbine comprising: a first duct configured to feed a compressed working fluid from a first tapping of the compressed working fluid from a compressor to a first cavity for cooling of an expansion turbine; a second duct configured to feed the compressed working fluid from a second tapping of the compressed working fluid of the compressor to a second cavity for cooling of an expansion turbine, wherein the second duct is at a higher pressure than the first duct, and wherein the second tapping is downstream from the first tapping; a fluid dynamic system comprising an ejector directly coupled to the first duct, the ejector configured to prevent the working fluid from returning to the compressor; wherein the fluid-dynamic system is configured to selectively combine the working fluid from the first tapping to the working fluid of the second tapping to selectively increase the flow of the working fluid of the first tapping during partial load operation conditions to keep the temperature at least in the first cavity within acceptable limits for the protection of the materials of the gas turbine therearound; and a control system electronically connected to the fluid-dynamic system configured to selectively feed a part of the working fluid from the second tapping into the first duct during partial load operation conditions, based on the monitoring of operating parameters, to keep the temperature of the first cavity within the acceptable limits for the protection of the materials of the gas turbine engine therearound.