A gas turbine engine including a turbocooler and configure so that, in one embodiment, cool air from the turbocooler is supplied to the combustor (10) for cooling the combustor (10) and then, after cooling at least a portion of the combustor (10), for mixing with fuel in the fuel injector (30), is described. In one form, the combustor (10) includes a flowpath (42) in flow communication with cool air supplied by the turbocooler. The air flows through the flowpath from an aft portion to an outlet located at the fuel injector (30) The cooling air, after having cooled walls of the combustion chamber (18), mixes with fuel in the fuel injector (30). Mixing the high pressure air form the turbocooler with the fuel in the fuel injector (30) facilitates dispersion of fuel from the fuel injector (30) into the combustion chamber (18), and also aids in increasing the fuel/air energy shear gradients. As a result, the injection velocity is believed to be significantly increased, and NOx emissions are believed to be reduced.