Patent ID: 6817183
Filing Date: 2004-11-16
Classification: F23D

Abstract:
A fuel injector for a gas turbine burner comprising:an injector head having an outlet; a first tube for flowing fuel; a central duct screw threaded at one end to said head and butt welded at an opposite end to said first tube, said duct having an axially extending passageway in communication with said first tube and said head for flowing fuel to said outlet; an external tube about said first tube forming a first annular passage for flowing air under pressure; a tubular covering element about said duct and said head and connected at one end to said external tube forming an second passage in communication with said first annular passage for flowing air from said external tube past said head; said covering element extending axially beyond said head at an opposite end thereof terminating in an inwardly tapered opening convergent in a downstream direction from said outlet for flowing air outwardly from said injector and mixing with fuel flowing from said outlet; a plurality of blades carried by said duct projecting into said second annular passage for imparting a swirl to the air passing along said second annular passage.