COMBUSTOR WITH A FUEL INJECTOR

A turbine engine (10) having a compressor section (12), a combustion section (14) and a turbine section (16) in serial flow arrangement. The turbine engine (10) further having a combustor (80), provided within the combustion section (14), defining a combustion chamber (86) and having at least one fuel injector (76). The fuel injector (140) having a fuel channel (120), a first set of fuel orifices (122), and a flow restrictor (124) located within the fuel channel (120) and having a second set of fuel orifices (126).