COMBUSTION CHAMBER, IN PARTICULAR FOR A GAS TURBINE, WITH AT LEAST TWO RESONATOR DEVICES

摘要

A combustion chamber according to the invention, in particular for a gas turbine, includes at least one combustion chamber wall (3) through which cooling fluid flows and at least one resonator device (5, 6). The combustion chamber (1) according to the invention is distinguished in that the resonator device (5, 6) is integrated into the combustion chamber wall (3) in such a way that it has the cooling fluid flow passing therethrough.