Control and tuning of gas turbine combustion
AssigneeGeneral Electric Company
InventorsStephen William Piche, Fred Francis Pickard, Robert Nicholas Petro, Yan Liu, Nurali Virani
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AssigneeGeneral Electric Company
InventorsStephen William Piche, Fred Francis Pickard, Robert Nicholas Petro, Yan Liu, Nurali Virani
Estimating the term…
A system that includes: a gas turbine having a combustion system; a control system operably connected to the gas turbine for controlling an operation thereof; and a combustion auto-tuner, which is communicatively linked to the control system, that includes an optimization system having an empirical model of the combustion system and an optimizer; sensors configured to measure the inputs and outputs of the combustion system; a hardware processor; and machine-readable storage medium on which is stored instructions that cause the hardware processor to execute a tuning process for tuning the operation of the combustion system. The tuning process includes the steps of: receiving current measurements from the sensors for the inputs and outputs; given the current measurements received from the sensors, using the optimization system to calculate an optimized control solution for the combustion system; and communicating the optimized control solution to the control system.
A system comprising:
A method for tuning an operation of a combustion system of a gas turbine, wherein a control system of the gas turbine includes an optimization system that comprises:
Dependencies are inferred from the claim text.