GAS TURBINE COMBUSTOR

摘要

PROBLEM TO BE SOLVED: To provide a gas turbine combustor which suppresses combustive vibrations to a low level while a combustion gas is generated in a combustion chamber. SOLUTION: A gas turbine combustor is provided with a resistor 16 on the upstream side of a swirler 10 surrounding a nozzle 4 for diffuse combustion which is inserted into an air passage 9 for diffuse combustion.