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An air blast fuel injector for a gas turbine engine includes an elongate feed arm having an inlet fitting for receiving fuel and for distributing the fuel to first and second fuel delivery conduits extending through the feed arm. A nozzle body is operatively connected to the feed arm. The nozzle bod

An air blast fuel injector for a gas turbine engine includes an elongate feed arm having an inlet fitting for receiving fuel and for distributing the fuel to first and second fuel delivery conduits extending through the feed arm. A nozzle body is operatively connected to the feed arm. The nozzle body includes an on-axis inner air circuit and fuel circuitry radially outboard of the inner air circuit for delivering fuel to a fuel swirler outboard of the inner air circuit. The fuel circuitry includes a first fuel circuit configured and adapted to deliver fuel to the fuel swirler from the first fuel conduit of the feed arm and a second fuel circuit configured and adapted to deliver fuel to the fuel swirler from the second fuel conduit of the feed arm.

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1. An air blast fuel injector for a gas turbine engine comprising: a) an elongate feed arm having an inlet fitting for receiving fuel and for distributing the fuel to first and second fuel delivery conduits extending through the feed arm; andb) a nozzle body operatively connected to the feed arm, th

1. An air blast fuel injector for a gas turbine engine comprising: a) an elongate feed arm having an inlet fitting for receiving fuel and for distributing the fuel to first and second fuel delivery conduits extending through the feed arm; andb) a nozzle body operatively connected to the feed arm, the nozzle body including an on-axis inner air circuit and fuel circuitry radially outboard of the inner air circuit for delivering fuel to a fuel swirler outboard of the inner air circuit, the fuel circuitry including a first fuel circuit configured and adapted to deliver fuel to the fuel swirler from the first fuel conduit of the feed arm and a second fuel circuit configured and adapted to deliver fuel to the fuel swirler from the second fuel conduit of the feed arm. 2. An air blast fuel injector as recited in claim 1, further comprising a check valve in fluid communication with the second fuel conduit of the feed arm, the check valve being configured and adapted to allow fuel to flow in the second fuel conduit when fuel pressure at the inlet fitting of the injector exceeds a predetermined threshold pressure. 3. An air blast fuel injector as recited in claim 1, wherein at least part of the second fuel conduit is coaxial with the first fuel conduit. 4. An air blast fuel injector as recited in claim 1, wherein the first fuel circuit of the nozzle body includes a plurality of first fuel passages, and wherein the second fuel circuit of the nozzle body includes a plurality of second fuel passages, wherein the first and second fuel passages are defined on a radially outward surface of the fuel swirler. 5. An air blast fuel injector as recited in claim 4, further comprising a fuel prefilmer outboard of the fuel swirler, the prefilmer including first and second openings therethrough for supplying fuel from the first and second conduits of the feed arm into the first and second fuel passages of the nozzle body, respectively. 6. An air blast fuel injector as recited in claim 5, wherein each of the first fuel passages includes a first fuel inlet in fluid communication with a first opening through the prefilmer, and wherein each of the first fuel passages includes a fuel outlet in fluid communication with a fuel outlet of the nozzle body. 7. An air blast fuel injector as recited in claim 6, wherein each of the second fuel passages extends between the outlet of the nozzle body and a common fuel inlet in fluid communication with a second opening through the prefilmer. 8. An air blast fuel injector as recited in claim 7, wherein one of the second fuel passages extends between each circumferentially adjacent pair of first fuel passages. 9. An air blast fuel injector as recited in claim 4, wherein each of the first and second fuel passages is in fluid communication with a fuel outlet of the nozzle body through a metering slot that is angled with respect to a central axis of the nozzle body, wherein each metering slot is configured and adapted to impart swirl to a stream of fuel flowing therethrough in a first swirl direction. 10. An airblast fuel injector as recited in claim 9, wherein each metering slot is angled between about 30° and about 60° with respect to the central axis. 11. An airblast fuel injector as recited in claim 10, wherein each metering slot is angled about 45° with respect to the central axis. 12. An airblast fuel injector as recited in claim 9, further comprising an inner air swirler within the inner air circuit, wherein the inner air swirler is configured and adapted to impart swirl on a flow of air therethrough in a second swirl direction that is counter-rotational with the first swirl direction of the metering slots of the first and second fuel passages. 13. An airblast fuel injector as recited in claim 9, further comprising an inner air swirler within the inner air circuit, wherein the inner air swirler is configured and adapted to impart swirl on a flow of air therethrough in a second swirl direction that is co-rotational with the first swirl direction of the metering slots of the first and second fuel passages. 14. An air blast fuel nozzle for a gas turbine engine comprising: a) a nozzle body defining an on-axis inner air circuit;b) a fuel swirler radially outboard of the inner air circuit;c) a prefilmer radially outboard of the fuel swirler; andd) first and second fuel circuits defined between the fuel swirler and prefilmer, the first and second fuel circuits being configured and adapted to conduct fuel from first and second fuel sources, respectively, to a common prefilming chamber defined between the fuel swirler and the prefilmer. 15. An air blast fuel nozzle as recited in claim 14, wherein the first fuel circuit includes a plurality of first fuel passages, wherein the second fuel circuit includes a plurality of second fuel passages, and wherein the first and second fuel passages are defined on a radially outward surface of the fuel swirler. 16. An air blast fuel nozzle as recited in claim 15, wherein the prefilmer includes primary and secondary openings therethrough for supplying fuel to the first and second fuel passages, respectively. 17. An air blast fuel nozzle as recited in claim 16, wherein each of the first fuel passages includes a primary fuel inlet in fluid communication with a primary opening through the prefilmer and a primary fuel outlet in fluid communication with the prefilming chamber. 18. An air blast fuel nozzle as recited in claim 15, wherein the second fuel passages extend between the prefilming chamber and a common secondary fuel inlet in fluid communication with a secondary opening of the prefilmer. 19. An air blast fuel nozzle as recited in claim 15, wherein the each of the first fuel passages is in fluid communication with the prefilming chamber through a fluid metering slot that is dimensioned to perform fuel pressure atomization on fuel flowing therethrough. 20. A method of supplying fuel to a gas turbine engine during startup, the method comprising: a) providing a fuel injector including: i) an elongate feed arm having an inlet fitting for receiving fuel and for distributing the fuel to first and second fuel delivery conduits extending through the feed arm; andii) a nozzle body operatively connected to the feed arm, the nozzle body including an on-axis inner air circuit and fuel circuitry radially outboard of the inner air circuit for delivering fuel to a fuel swirler outboard of the inner air circuit, the fuel circuitry including a first fuel circuit configured and adapted to deliver fuel to the fuel swirler from the first fuel conduit of the feed arm, and a second fuel circuit configured and adapted to deliver fuel to the fuel swirler from the second fuel conduit of the feed arm;b) supplying fuel through the first fuel conduit of the feed arm and through the first fuel circuit in the fuel nozzle body to provide a limited flow of fuel for combustion responsive to compressor pressure below a predetermined threshold; andc) supplying fuel through the second fuel conduit in the feed arm and through the second fuel circuit in the fuel nozzle body to provide a flow of fuel for combustion responsive to compressor pressure above the predetermined threshold.