Fuel injectors for gas turbine engines

1. A fuel injector for a gas turbine engine, comprising:

a monolithic nozzle body defining therein at least one fuel circuit, the at least one fuel circuit including:

an inlet and an outlet orifice;

a main passage fluidly coupling the inlet and the outlet orifice; and

a branch passage connected to the main passage,

wherein the branch passage diverges from the main passage downstream of the inlet, wherein the branch passage converges with and joins the main passage upstream of the outlet orifice, and wherein the branch passage connects to the main passage downstream of the inlet and upstream of the outlet orifice to form an effective metering flow area that is smaller than a flow area of the outlet orifice.

2. The fuel injector as recited in claim 1 , wherein the branch passage includes an arcuate segment with an axial component oriented toward the nozzle body inlet.

3. The fuel injector as recited in claim 1 , wherein the branch passage rejoins the main passage at an angle opposing a direction of flow through the main passage.

4. The fuel injector as recited in claim 1 , wherein the branch passage diverges from the main passage at a diverging junction, wherein a segment of the main passage upstream and adjacent to the diverging junction is coaxial with a segment of the branch passage downstream and adjacent to the diverging junction.

5. A The fuel injector as recited in claim 4 , wherein flow axes defined by a segment of the main passage downstream and adjacent to the diverging junction and the segment of the diverging passage downstream of the diverging junction intersect one another at an acute angle.

6. The fuel injector as recited in claim 1 , wherein the branch passage rejoins the main passage at a converging junction, wherein a flow axis defined by the branch passage upstream an adjacent to the converging junction intersects a flow axis defined by the main passage upstream and adjacent to the converging junction at an obtuse angle .

7. The fuel injector as recited in claim 6 , wherein the branch passage flow axis has a component that opposes the main passage flow axis through a segment of the main passage adjacent to and upstream of the converging junction.

8. The fuel injector as recited in claim 1 , further including a distribution header fluidly coupling the inlet with the main passage of the fuel circuit.

9. The fuel injector as recited in claim 1 , wherein the main passage fluidly couples the branch passage with both the inlet and outlet orifice of the nozzle body.

10. The fuel injector as recited in claim 1 , wherein the fuel circuit is a first fuel circuit, and further including a second fuel circuit, wherein the second fuel circuit connects the inlet to a second outlet orifice.

11. A fuel injector for a gas turbine engine, comprising:

a prefilmer; and

a monolithic nozzle body disposed within the prefilmer and defining within its interior at least one fuel circuit, the at least one fuel circuits including:

an inlet and an outlet orifice;

a main passage fluidly coupling the inlet and the outlet orifice; and

a branch passage connected to the main passage, wherein the branch passage diverges from the main passage downstream of the inlet,

wherein the branch passage converges with and joins the main passage upstream of the outlet orifice, and wherein the branch passage connects to the main passage downstream of the inlet and upstream of the outlet orifice to form an effective metering flow area that is smaller than a flow area of the outlet orifice.

12. The fuel injector as recited in claim 11 , wherein the main passage fluidly couples a turning segment of the branch passage with both the inlet and outlet orifice of the nozzle body.

13. A fuel injector as recited in claim 11 , wherein the fuel circuit is a first fuel circuit, and further including a second fuel circuit, wherein the second fuel circuit connects the inlet to a second outlet orifice.