摘要:
In a control method and a control system of a gas turbine (2), a pressure atomizing liquid fuel injector (9) is mounted in a combustor (3), and the flow rate of a working fluid for a compressor (1) is reduced in a part load region of the gas turbine (2) to be smaller than a flow rate of the working fluid for the compressor (1), which is set such that performance of the compressor is maximized. Emissions of carbonaceous particulate matters generated in the part load region can be suppressed while ensuring the advantages of the pressure atomizing liquid fuel injector (9).
摘要:
In a control method and a control system of a gas turbine (2), a pressure atomizing liquid fuel injector (9) is mounted in a combustor (3), and the flow rate of a working fluid for a compressor (1) is reduced in a part load region of the gas turbine (2) to be smaller than a flow rate of the working fluid for the compressor (1), which is set such that performance of the compressor is maximized. Emissions of carbonaceous particulate matters generated in the part load region can be suppressed while ensuring the advantages of the pressure atomizing liquid fuel injector (9).