Low coke fuel injector for a gas turbine engine

Details Low coke fuel injector for a gas turbine engine Low coke fuel injector for a gas turbine engine

F - Mech Eng,Light,Heat,Weapons

23

R

60/176

F23R 3/32 (2006.01) F23D 11/10 (2006.01) F23R 3/14 (2006.01)

Patent

CA 1306873

LOW COKE FUEL INJECTOR FOR A GAS TURBINE ENGINE ABSTRACT A carbureting device for the combustor of a gas turbine comprises an annular spin chamber which is defined by a generally annular housing having a closed forward end, an exhaust tube which is partially disposed within the spin chamber, and a flange disposed around the exhaust tube. A swirling air entrance is disposed between the annular housing and the flange and a fuel entrance is disposed along the annular housing spaced axially forward of the swirling air entrance. In one embodiment of the invention the exhaust tube is a venturi. In another embodiment a fairing is disposed outside ant aft of the spin chamber and is sized and disposed about and extending at least to the end of the venturi, thereby forming a passageway between the fairing ant the venturi. A second air swirling means is disposed in the passageway formed by the fairing and the venturi.

562393

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