Combustion chamber with premixing burner and jet propellent exhaust gas recirculation

A combustion chamber for a gas turbine, having a plenum and a dome defining a dome space for guiding compressed combustion air, air flow proceeding from the plenum to the dome space, and comprising:

• a front plate bounding the combustion space at a front end of the combustion chamber and separating the combustion space from said dome space, the combustion space and dome space being surrounded by an enclosed plenum;
• at least one premixing burner mounted with an outlet end at the front plate, the burner including two conical section bodies mounted to define a conical interior, the bodies being mutually positioned to form longitudinal inlet openings for a tangentially directed flow of combustion air into the interior, the inlet openings communicating with the dome space to receive combustion air, and fuel injectors positioned at longitudinal edges of the bodies and directed to inject fuel into the longitudinal inlet openings, wherein fuel and combustion air is mixed and burned in the interior before passing through the outlet end;
• and,
• at least one jet injector connected to an orifice on the front plate, the jet injector having a central nozzle directed to deliver high temperature gas from the combustion space to the dome space to preheat the combustion air, the nozzle including an outlet diffuser, and the jet injector having an annular space surrounding the central nozzle and connected to the plenum for supplying combustion air as a propellant to the annular space.