| 摘要 |
A simulator for automatic simulation of the real processes of starting, operating and stopping of the gas turbine in conjunction with the actuating elements (9,9') but without rotating the shafts of the turbines (16, 16'), without supplying fuel and initiating the ignition is operationally connected with outputs (18,33,34) of the automatic control system (7), where generated are starting signals for the starting motor (5) of the gas turbine, control signals for the ignition unit (4) and a test signal confirming the reception by the automatic control system (7), of the signal indicating the detection of the flame in combustion chambers (2). The device is also connected to those inputs (25,25', 36, 37, 38, 43, 44, 44') of the automatic control system (7), which are coupled with a behind-the-compressor air pressure transducer (12), rotational speed transducers (15, 15') of the shafts of the turbines (16, 16'), position transducers (8,8') of the actuating elements (9,9') of the fuel control unit (1), exhaust gas temperature transducers (13), detectors (14) of the flame in the combustion chambers (2), and a position transducer (10) of the actuator (11), of the guide assembly (3). <IMAGE> |
