A process having three steps utilized individually or in combination to reduce nitrogen oxides, NOx, emissions from gas turbines. One or more injectors disperse very fine fuel droplets to achieve rapid and complete combustion in zone one immediately downstream of the fuel injectors. The second step uses...http://www.google.fr/patents/US7047748?utm_source=gb-gplus-shareBrevet US7047748 - Injection methods to reduce nitrogen oxides emission from gas turbines combustors
Injection methods to reduce nitrogen oxides emission from gas turbines ...