Method for operation of a burner in particular a burner for a gas turbine and device for carrying out said method
A technology of burner and fuel characteristics, applied in gas turbine installations, combustion methods, combustion air/fuel supply, etc., can solve problems such as increased nitrogen oxide emissions
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[0034] The gas turbine system shown in FIG. 1 has a gas turbine 1 with a compressor 3 , a combustion chamber 9 and a turbine 17 downstream of the combustion chamber 9 . Compressor 3 and turbine 17 are optionally coupled via a common rotor shaft 5 . A generator 19 is connected downstream of the turbine 17 and is coupled to the turbine 17 , for example via a generator shaft 25 . The combustion chamber 9 comprises a combustion zone 11 and a burner 13 protruding into the combustion zone 11 for burning a liquid or gaseous fuel 15 . When the gas turbine 1 is working, the air 7 is sucked into the compressor 3, where the air is compressed. The compressed air 7 is fed to the burner 13 as combustion air and mixed with fuel 15 . The fuel-air mixture thus formed is combusted in the combustion zone 11 , producing very hot combustion gases. The high-temperature combustion gas is delivered to the turbine 17, where it expands to perform work, thereby driving the rotor shaft 5 on the compre...
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