Method for the start-up of a gas turbine
A method is described for the start-up of a gas turbine comprising the phases of effecting a preliminary purging cycle of the discharge duct ( 28 ) of the turbine ( 20 ), establishing a predetermined minimum value (FSR 1 ) for the flow of gaseous fuel entering the combustor ( 14 ) for a period of time which is adequate for effecting a first attempt at ignition and effecting a first attempt at ignition, effecting an intermediate purging cycle of the discharge duct ( 28 ), interrupting the flow of gaseous fuel to the combustor ( 14 ), and progressively increasing the value (FSR n ) of the flow of gaseous fuel entering the combustor ( 14 ), effecting further attempts at ignition until the mixture of air/gaseous fuel has been ignited and the consequent start-up of the turbine ( 20 ), or until a predetermined maximum value (FSR max ) of the flow of gaseous fuel has been reached.
1. A method for the start-up of a gas turbine of the type having at least one compressor, which compresses the air introduced therein through an inlet duct, at least one combustor, in which said compressed air is mixed and combusted with a gaseous fuel, coming from a feeding duct, and at least one turbine, which transforms the energy of the combusted gas coming from said combustor into work energy, the method comprising the following phases:
a) establishing a predetermined minimum value (FSR 1 ) of the fuel flow entering said combustor and effecting a first attempt at ignition, wherein the predetermined minimum value is established by being set at a value that is sufficient to ignite a richest fuel/air mixture among a predetermined group of gaseous fuels; and
b) progressively increasing the value (FSR n ) of the fuel flow entering said combustor and effecting further attempts at ignition until the complete ignition of the air/fuel mixture and consequent start-up of said turbine, or until a predetermined maximum value (FSR max ) of said fuel flow is reached, wherein in said phase b) an intermediate purging cycle of said discharge duct is effected, interrupting the flow of gaseous fuel to said combustor before the increase in said value (FSR n ) of the fuel flow.
2. The method according to claim 1 , wherein before said first phase a) a preliminary purging cycle of the discharge duct of said turbine is effected.
3. The method according to claim 2 , wherein said preliminary purging cycle is effected while said turbine is rotating in particular at the purging rate or at the light off rate.
4. The method according to claim 1 , wherein after phase b), a final purging cycle of said turbine is effected, in the case of ignition failure of the air/fuel mixture when said predetermined maximum value (FSR max ) of the fuel flow has been reached, to be effected after said turbine has been brought to predefined rotation regime and before stopping said turbine to restart with the sequence of ignition phases.
5. The method according to claim 1 , also comprising purging cycles with said turbine in rotation.
6. The method according to claim 1 , wherein said gaseous fuel is selected from a plurality of gaseous fuels having different Wobbe indexes.
7. The method according to claim 6 , wherein said predetermined minimum value (FSR 1 ) of the flow of gaseous fuel entering said combustor is sufficient for igniting the richest air/fuel mixture among those obtainable with said plurality of gaseous fuels having different Wobbe indexes.