Method for automatic positioning of gas turbine rotors
A technology for gas turbines and rotors, applied in position/direction control, engine components, machines/engines, etc., can solve problems such as expensive, unable to provide rotor speed variable speed control, and inaccurate
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[0026] The invention relates to a method for positioning a rotor 2 of a gas turbine 1 in an accurate and automatic manner by means of:
[0027] - a feedback loop comprising a key phaser 40 and an incremental counter 50;
[0028] - frequency converter 60;
[0029] - rotor turning actuator 10;
[0030] - HMI (Human Machine Interface) 30, and
[0031] - a control unit 20 .
[0032] Feedback loop (key phaser 40 and incremental counter 50)
[0033] A key phaser 40 combined with an incremental counter 50 is used as feedback for the control unit 20 .
[0034] The phaser 40 generally comprises a sensor which, through cogs placed on the cam for the phaser 70 , receives a digital pulse for each revolution of the rotor 2 which is used to give information on the placement of the rotor 2 . Incremental counter 50 also typically includes sensors that give digital pulses for each cog of incremental cam 80 . Information from the phase keyer 40 combined with information from the increment...
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