| 摘要 |
The present invention relates to a gas turbine system comprising a gas turbine engine (101) for generating power, a control unit (102) for controlling the gas turbine engine (101), a data acquisition system (108) comprising a thermodynamic model unit (104) and a test sequence unit (105), a sensor device (103) which is coupled to the gas turbine engine (101) for measuring a performance parameter (115) of the gas turbine engine (101), and a comparative unit (109). The thermodynamic model unit (104) generates computed performance parameter (113) on the basis of a mechanical model (106) of the gas turbine engine (101) and on the basis of a thermodynamic model (107) of the gas turbine engine (101). The test sequence unit (105) generates test sequence data (114) comprising set point operating data and time schedule data with which a test cycle of the gas turbine engine (101) is runnable. The data acquisition system (108) generates test control data (112) on the basis of the test sequence data (114), wherein the data acquisition system (108) is coupled to the control unit (102) for providing the test control data (112) to the control unit (102) such that the gas turbine engine (101) is controllable on the basis of the test control data (112). The comparative unit (109) is coupled to the data acquisition system (108) such that the measured performance parameter (115) measured by the sensor device (103) is comparable with the computed performance parameter (113). |
