Method for operating a gas turbine
View Patent ↗In method for operating a gas turbine ( 11 ), the compressed air is fed to a combustor ( 18, 19 ) for the combustion of a coal syngas, and the resulting hot gases are expanded in a subsequent turbine ( 16, 17 ). Some of the compressed air is separated into oxygen and nitrogen, and the oxygen is used for producing the syngas. In a first combustor, ( 18 ) syngas is combusted and the resulting hot gases are expanded in a first turbine ( 16 ), and in a second combustor syngas is combusted, using the gases which issue from the first turbine ( 16 ), and the resulting hot gases are expanded in the second turbine ( 17 ). The two combustors ( 18, 19 ) are operated with undiluted syngas, and the first combustor flame temperature (T F ) is lowered compared with the operation with natural gas (T NG ), while the second combustor ( 19 ) is operated in the normal operation (T NG ) for natural gas.
1. A method for operating a gas turbine, in which method air is inducted and compressed by the gas turbine, the compressed air is fed to a combustor for combustion of a syngas which is produced from coal, and the hot gases resulting from combustion are expanded in a subsequent turbine, performing work, wherein some of the compressed air is separated into oxygen and nitrogen, and the oxygen is used in a coal gasification plant for producing the syngas, the method comprising:
providing a reheating gas turbine which comprises first and second combustors and first and second turbines, respectively, wherein said first combustor has a first rated flame temperature for the combustion of natural gas and said second combustor has a second rated flame temperature for the combustion of natural gas;
providing an undiluted syngas produced from coal;
combusting said undiluted syngas in the first combustor with the compressed air to produce first hot gases;
expanding said first hot gases in the first turbine;
combusting undiluted syngas in the second combustor with gases which issue from the first turbine, to produce second hot gases;
expanding said second hot gases in the second turbine;
maintaining the flame temperature in said first combustor 50-150 K below said first rated flame temperature, and maintaining the flame temperature in said second combustor at said second rated temperature.
2. The method as claimed in claim 1 , wherein said undiluted syngas comprises CO-rich syngas, and wherein maintaining the flame temperature in said first combustor comprises maintaining 50-100 K below said first rated flame temperature.
3. The method as claimed in claim 1 , wherein said undiluted syngas comprises H 2 -rich syngas, and wherein maintaining the flame temperature in said first combustor comprises maintaining 100-150 K below said first rated flame temperature.
4. The method as claimed in claim 1 , wherein said gas turbine is in a combined-cycle power plant.