Method for operating a gas turbine as well as a gas turbine for implementing the method
View Patent ↗In a method for operating a gas turbine ( 11 ) in a combined cycle power plant ( 40 ), air, which is used to burn a syngas that is recovered from coal, is drawn in and compressed by the gas turbine ( 11 ), the compressed air is fed into a combustor ( 18, 19 ) and such that a portion of the compressed air is separated into oxygen and nitrogen. An improved degree of efficiency is achieved by this method by virtue of the fact that a gas turbine ( 11 ) with reheating and two combustors ( 18, 19 ) and two turbines ( 16,17 ) is used. In the first combustor ( 18 ), syngas is burned using the compressed air, and the resultant hot gases are expanded in the first turbine ( 16 ). In the second combustor, syngas is burned using the gases coming from the first turbine ( 16 ) and the resultant gases are expanded in the second turbine ( 17 ) such that the nitrogen that occurs in the separation of the air is led to the gas turbine ( 11 ) to be compressed.
1. A method for the operation of a gas turbine, wherein the gas turbine comprises a first compressor for compressing drawn in air to a first stage of pressure and a second compressor for further compressing air from the first pressure stage to a second, higher pressure stage, the method comprising:
drawing in air and compressing said air with said first and second compressors of the gas turbine;
conducting the compressed air to a combustor;
combusting said compressed air with a syngas in said combustor, said syngas recovered from coal, to generate hot gases;
expanding the hot gases from the combustion in a downstream turbine as said hot gases do work;
separating a portion of the compressed air from the first compressor into oxygen and nitrogen;
using the oxygen in a coal gasifying plant to generate said syngas;
cooling portions of the gas turbine that are exposed to hot gases with a portion of the compressed air;
wherein said gas turbine comprises a reheating gas turbine including a first combustor, a second combustor, a first turbine, and a second turbine;
wherein combusting comprises combusting said syngas in the first combustor with the compressed air;
wherein expanding the hot gases comprises expanding in the first turbine;
combusting syngas in the second combustor with gases from the first turbine;
expanding hot gases from the second combustor in the second turbine; and
conducting the nitrogen from said separating to, and compressing said nitrogen in, said gas turbine.
2. A method according to claim 1 , further comprising:
conducting said nitrogen from said separating to the second compressor.
3. A method according to claim 2 , further comprising:
compressing said nitrogen from said separating in another compressor, to generate pre-compressed nitrogen, before it is conducted to the second compressor.
4. A method according to claim 3 , comprising:
conducting said pre-compressed nitrogen to an inlet of the second compressor.
5. A method according to claim 1 , further comprising:
conducting said nitrogen from said separating back to the first compressor.
6. A method according to claim 5 , wherein conducting the nitrogen comprises conducting from the first compressor to an intermediate stage.
7. A method according to claim 5 , wherein conducting the nitrogen comprises conducting to an inlet of the first compressor.