Gas turbine assembly with fluidic injector

摘要

The injector has an annular combustion chamber operated with self-ignition of a fuel-oxidizer mixture. A gas path (44) is used for supplying oxidant stream (43) to the combustion chamber, and a fuel line (14) is used for supplying fuel to the combustion chamber. An inlet nozzle allows the fuel to enter into an interaction space, and an outlet nozzle allows the fuel to exit from the interaction space. A return line from an inlet area of the outlet nozzle leads back to an outlet of the inlet nozzle.