METHOD FOR COMBUSTING HYDROGEN-RICH, GASEOUS FUELS IN A BURNER, AND BURNER FOR PERFORMING SAID METHOD

摘要

A method for the combustion of hydrogen-rich, gaseous fuels in combustion air in a burner of a gas turbine includes injecting the hydrogen-rich, gaseous fuel at least partially isokinetically with respect to the combustion air such that the partially hydrogen-rich, gaseous fuel is injected at least partially in the same direction and at least partially at the same velocity as the combustion air.