| 摘要 |
PROBLEM TO BE SOLVED: To provide a method for operating a gas turbine comprising an annular combustion chamber and/or a number of cans disposed around a rotor, each can having a single combustion area or performing a sequential combustion, which enables operation with an incremented power and reduced CO emissions.SOLUTION: The gas turbine comprises at least one compressor, and a primary combustor connected downstream of the compressor. Hot gases of the primary combustor are admitted at least to an intermediate turbine or directly or indirectly to a secondary combustor. Hot gases of the secondary combustor are admitted to a further turbine or directly or indirectly to an energy recovery. At least one combustor liner has air passages, and at least one of the air passages is formed as a damper neck. The damper neck is connected to a damper volume, which is part of a connecting duct extending between a compressor air plenum and the combustor. |
