Method for operating a gas turbine plant
View Patent ↗A method for operating a gas turbine plant utilizing sequential combustion is provided. The gas turbine plant includes a compressor for compressing inducted combustion air, a first combustion chamber for combustion of a first fuel by utilizing the compressed combustion air, with a first turbine which is connected downstream of the first combustion chamber, and a second combustion chamber for combustion of a second fuel by utilizing the gases which emerge from the first turbine, with a second turbine which is connected downstream of the second combustion chamber. The method provides quick running up with simultaneously low emissions and homogeneous distribution of the turbine inlet temperature is achieved by the second combustion chamber being completely shut down for achieving a low partial load mode of the gas turbine plant.
1. A method for operating a gas turbine plant, comprising,
(a) compressing inducted combustion air using at least one compressor;
(b) combusting a first fuel using the compressed combustion air in a first combustion chamber located downstream of the at least one compressor, the first combustion chamber comprises a plurality of individual burners, which are arranged in the first combustion chamber in a distributed manner;
(c) driving a first turbine located downstream of the first combustion chamber; and,
(d) in a first state:
(d1) combusting a second fuel using gases which emerge from the first turbine in a second combustion chamber located downstream of the first turbine;
(d2) driving a second turbine which is connected downstream of the second combustion chamber; and,
(e) in a second state:
(e1) completely shutting down the second combustion chamber for a time (t 1 );
(e2) operating all of the burners of the first combustion chamber in a lean premix mode during the time (t 1 );
(e3) driving the second turbine which is connected downstream of the second combustion chamber; and
(e4) achieving a low partial load mode of operation of the gas turbine plant.
2. The method as claimed in 1 , further comprising selectively operating the gas turbine plant in either one of the first or second states.
3. The method as claimed in claim 1 , wherein the gas turbine plant in low partial load mode is operated with a relative load (RL) of less than 20%.
4. The method as claimed in claim 3 , wherein the gas turbine plant is part of a combined cycle power plant including a water/steam cycle, a steam turbine, and a heat recovery steam generator which receives a through-flow of exhaust gases of the gas turbine plant, further comprising operating the combined cycle power plant in low partial load mode with a relative load (RL) of less than 25%.
5. The method as claimed in claim 1 , wherein the gas turbine plant is part of a combined cycle power plant including a water/steam cycle, a steam turbine, and a heat recovery steam generator which receives a through-flow of exhaust gases of the gas turbine plant, further comprising operating the combined cycle power plant in low partial load mode with a relative load (RL) of less than 25%.
6. The method as claimed in claim 1 , wherein the gas turbine plant in low partial load mode is operated with a relative load (RL) of less than 20%.
7. The method as claimed in claim 1 , wherein the gas turbine plant is part of a combined cycle power plant including a water/steam cycle, a steam turbine, and a heat recovery steam generator which receives a through-flow of exhaust gases of the gas turbine plant, further comprising operating the combined cycle power plant in low partial load mode with a relative load (RL) of less than 25%.