Fuel nozzle for gas turbine engine

F - Mech Eng,Light,Heat,Weapons – 23 – D

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F23D 11/00 (2006.01) F23D 11/38 (2006.01)

Patent

CA 1170843

Fuel Nozzle For Gas Turbine Engine Abstract A fuel nozzle designed to reduce pollutant emissions and minimize the buildup of coke in the secondary fuel passage of a dual orifice fuel nozzle for the combustor of a gas turbine engine sizes the orifices and passages of the air and fuel so as to increase the pressure in the secondary passage during its inoperative mode and when the primary fuel passage is in the operative mode and having the air and fuel issuing from both the primary and secondary orifices swirl in the same direction.

390190

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