| 摘要 |
PROBLEM TO BE SOLVED: To provide a gas turbine combustor capable of sufficiently coping with the rise of a combustion gas temperature of a gas turbine inlet, the lowering of NOx concentration, and diversification of fuel, and surely suppressing the combustion vibration. SOLUTION: This gas turbine combustor comprises combustor boiler drums 1a, 1b... producing a combustion gas by adding high-pressure air to the fuel, and a plurality of resonators 3a, 3b..., 4a, 4b... mounted on the combustor boiler drums 1a, 1b..., and suppressing the combustion vibration generated from the combustion gas. COPYRIGHT: (C)2005,JPO&NCIPI
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