COMBUSTION CHAMBER FOR A GAS TURBINE FOR THE PRODUCTION OF ENERGY, PARTICULARLY ELECTRICAL ENERGY, COMPRISING ASYMMETRIC DILUTION HOLES IN A FLAME TUBE.

摘要

The present invention relates to a combustion chamber (18) of a gas turbine, in particular of a thermodynamic cycle gas turbine with recuperator, for the production of energy, in particular electrical energy, comprising a housing (112). and a flame tube (122). According to the invention, the flame tube (122) comprises at least one circumferential row of radial dilution orifices (166) and the passage surface of the radial dilution orifices (166) lying above a plane P is greater than the passage surface of the radial dilution holes (166) lying below the plane P, said plane P is the plane which cuts the flame tube (122) lengthwise and which passes through the center of it this.