Method of operating a gas turbine with staged and/or sequential combustion
A gas turbine, turbine technology, applied in combustion methods, continuous combustion chambers, gas turbine devices, etc., can solve problems such as minimum fuel flow increase, and achieve the effect of low fuel consumption
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[0072] figure 1 A gas turbine with continuous combustion for carrying out the method according to the invention is schematically shown. It comprises a compressor 1, a first burner 4' comprising a number of burners 9 and a combustion chamber 4, a first turbine 7, a second combustion chamber 15' comprising a number of burners 9' and a combustion chamber 15, and the second turbine 12 . Typically, it comprises a generator 19 at the cold end of the gas turbine, that is to say at the compressor 1, and coupled to the shaft 18 of the gas turbine. The first combustor 4' and the second combustor 15' can be ring frame or barrel frame, while the first turbine 7 is optional.
[0073] The canister architecture includes multiple burners with subsequent canisters arranged in an annular array around the circumference of the turbine shaft, which allows independent combustion operation of the individual canisters 4, 15, and which does not cause detrimental interaction between the individual c...
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