| 摘要 |
The invention relates to a method for controlling the operation of a gas turbine with a compressor (2) compressing intake air (1) and with at least one combustor (8, 9) for the combustion of liquid and/or gaseous fuel (5, 6) in the compressed gas stream (12, 14) and at least one turbine (3, 4) for expanding the combustion air downstream of the combustor (8, 9) for the generation of work, wherein a closed loop control and/or a protection system is used for controlling actuators of the gas turbine, and wherein this closed loop control is at least partly based on the measurement of a combustor wall temperature (28-30). The invention furthermore relates to a gas turbine unit, in particular with flue gas recirculation, for carrying out such a method. |
