| CPC F01D 21/02 (2013.01) [F01D 15/08 (2013.01); F01D 15/12 (2013.01); F01D 17/06 (2013.01); F01D 17/105 (2013.01); F01D 19/00 (2013.01); F01D 21/003 (2013.01); F01D 21/006 (2013.01); F04B 17/05 (2013.01); F04B 49/02 (2013.01); F04B 49/065 (2013.01); E21B 43/2607 (2020.05)] | 19 Claims | 

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               1. A gas turbine overspeed protection method, comprising: 
            acquiring a power utilization load of a generator collected by a first sensor, and a rotating speed value, monitored by a second sensor, of a gas turbine; 
                judging whether the power utilization load suddenly decreases or disappears, and in response to determining that the power utilization load suddenly decreases or disappears, controlling, by a controller, an excitation current in an eddy current retarder to provide a braking torque for the generator that simulates the power utilization load; 
                judging whether the rotating speed value exceeds a set speed range, and in response to determining that the rotating speed value exceeds the set speed range, controlling, by the controller, the gas turbine to reduce fuel supply, and opening a discharge valve of a gas compressor to discharge a high-pressure gas to reduce a power output and the rotating speed of the gas turbine; and 
                controlling, by the controller, the braking torque provided by the eddy current retarder to compensate for hysteresis of reducing fuel supply and opening the discharge valve in controlling a rotational speed of the gas turbine. 
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