Gas turbine combustor fed by a plurality of primary combustion chambers

摘要

The system has a plurality of small primary combustion chambers which lead into a larger secondary combustion chamber in order to reduce the amount of nitrous oxides produced during combustion and thus, lower, pollution. The primary combustion chambers are arrayed in a spherical pattern to eliminate the need for individual ignition devices and to provide a better mixing effect and a more uniform temperature distribution within the secondary combustion chamber.