Patent ID: 8904747

Claim:
A system comprising: a compressor including: an inlet bellmouth adjacent to a set of inlet guide vanes (IGVs), wherein the inlet bellmouth has an inner diameter of approximately 70 inches to approximately 95 inches; and an outlet fluidly connected to the inlet bellmouth; a first conduit coupled to the outlet of the compressor, the first conduit including a control valve, the first conduit for diverting a first portion of compressed air from the outlet of the compressor to the inlet bellmouth adjacent the set of IGVs; a gas turbine coupled to the compressor, wherein the gas turbine is configured to receive a second portion of compressed air distinct from the first portion from the outlet of the compressor; a bypass conduit fluidly connected with the first conduit upstream of the control valve, the bypass conduit including a shut-off valve, wherein the bypass conduit is configured to supply the second portion of the compressed air from the outlet of the compressor to a stage of the gas turbine downstream of an inlet of the gas turbine; and a control system operably connected to the control valve and the shut-off valve, the control system configured to monitor parameters of at least one of the gas turbine or the compressor and provide instructions to the control valve for providing the first portion of the compressed air from the outlet to the inlet and the shut-off valve for providing the second portion of the compressed air from the outlet of the compressor to the stage of the gas turbine, wherein the control system determines an amount of compressed air provided in the first portion to the inlet bellmouth based upon a position of the control valve, an angle position of the IGVs and a measured pressure ratio in the compressor.