초록 ▼

The invention provides a method of operating a gas turbine arranged in a power generation system and comprising a source of compressed air, a combustor having a combustion chamber and multiple burners. A gas turbine controller controls the activation and deactivation of the single burners and/or bur

The invention provides a method of operating a gas turbine arranged in a power generation system and comprising a source of compressed air, a combustor having a combustion chamber and multiple burners. A gas turbine controller controls the activation and deactivation of the single burners and/or burner groups according to a switching criterion that is proportional to the difference between a combustion chamber air inlet temperature and a temperature downstream of the combustion chamber. The switching criterion according to the invention fully accounts for large temperature fluctuations of the combustion chamber inlet air, which then result in only relatively small variations in burner equivalence ratio. The invention is particularly suited for application in compressed air energy power generation plants.

대표청구항 ▼

1. Method of operating a gas turbine arranged in a power generation system comprising a source of compressed air, a combustor having a combustion chamber, anda plurality of burners, anda gas turbine controller that activates and deactivates the burners according to a switching criterionwherein the s

1. Method of operating a gas turbine arranged in a power generation system comprising a source of compressed air, a combustor having a combustion chamber, anda plurality of burners, anda gas turbine controller that activates and deactivates the burners according to a switching criterionwherein the switching criterion is proportional to a difference between a temperature of the compressed air upstream of the combustion chamber and the temperature of the combustion chamber exhaust downstream of the combustion chamber.2. Method of operating a gas turbine according to claim 1 wherein the burners are activated and deactivated individually and/or in groups.3. Method of operating a gas turbine according to claim 1 wherein the burners are activated and deactivated in order to vary and limit the heat load of the burners.4. Method of operating a gas turbine according to claim 1 wherein cooling media are admitted to the burners, the combustion chamber, and/or the gas turbine.5. Method of operating a gas turbine according to claim 1 wherein the said switching criterion is the temperature difference between the combustion chamber air inlet temperature immediately before the entry to the combustion chamber and the temperature of the combustion chamber exhaust at any point downstream from the point in the combustion chamber where the chemical combustion reaction is complete.6. Method of operating a gas turbine according to claim 1 wherein the temperature downstream of the combustion chamber is the gas turbine inlet temperature.7. Method of operating a gas turbine according to claim 1 wherein the temperature downstream of the combustion chamber is a virtual temperature TGT TITcalculated for a mixture of combustion chamber exhaust gases and cooling media admitted to the burners, combustion chamber and/or gas turbine.8. Method of operating a gas turbine according to claim 7 wherein said switching criterion is proportional to an equivalence ratio &PHgr;CCof the combustion chamber, which is defined by the ratio of the fuel mass flow rate to the air mass flow rate through the combustion chamber and the fuel's stoichiometric oxidizer to fuel ratio.9. Method of operating a gas turbine according to claim 7 wherein the switching criterion is proportional to the equivalence ratio &PHgr;GTof the gas turbine which is defined by the ratio of the fuel mass flow and the total air mass flow admitted to the gas turbine and the fuel's stoichiometirc oxidizer to fuel ratio.10. Method of operating a gas turbine according to claim 7 wherein the switching criterion is proportional to the equivalence ratio &PHgr;SBof a single burner which is defined by the ratio of the fuel mass flow and the total air mass flow admitted to the single burner and the fuel's stoichiometric oxidizer to fuel ratio.11. Method of operating a gas turbine according to claim 1 wherein the gas turbine is arranged in a compressed air energy storage power generation system.