Fuel injectors with torch ignitors

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

a fuel nozzle configured to issue a spray of fuel from a fuel outlet in a downstream direction along an injection axis, the fuel nozzle defining a main flow passage therethrough;

an injection fuel line extending radially inward, relative to the injection axis, to an annular wall of the fuel nozzle and in fluid communication with the fuel nozzle to supply fuel to the fuel nozzle, wherein a centerline axis of the annular wall of the fuel nozzle is the injection axis; and

a torch ignitor including a combustion chamber, the torch ignitor configured to combust fuel to produce a flame, the torch ignitor further including a flame outlet opening into the main flow passage of the fuel nozzle for issuing the flame into the main flow passage, wherein the injection fuel line and the torch ignitor define a feed arm extending along a flame axis that is angled more than zero degrees and less than one-hundred-eighty degrees relative to the injection axis.

2. The fuel injector as recited in claim 1 , wherein the flame outlet meets the main flow passage at a position that is upstream of the fuel outlet with respect to the downstream direction along the injection axis.

3. The fuel injector as recited in claim 1 , wherein the main flow passage defines a main outlet for flame from the torch ignitor, wherein the fuel outlet is an annular opening.

4. The fuel injector as recited in claim 1 , wherein the torch ignitor includes:

a torch wall defining the combustion chamber therein, wherein the combustion chamber is connected to issue flame through the flame outlet, the flame outlet extending through the torch wall and into the main flow passage of the fuel nozzle; and

a torch fuel injector mounted to the torch wall to issue fuel into the combustion chamber; and

at least one ignitor mounted to the torch wall, positioned to ignite fuel issued from the fuel injector.

5. The fuel injector as recited in claim 4 , wherein the combustion chamber is connected to the flame outlet by a flame tube, wherein the flame tube and the flame outlet are oriented tangentially relative to the injection axis to swirl flame from the combustion chamber around the main flow passage of the fuel nozzle.

6. The fuel injector as recited in claim 1 , wherein the fuel nozzle includes an inner air swirler of the main flow passage, the inner air swirler defining a plurality of passages configured to impart swirl on a flow of air flowing therethrough.

7. The fuel injector as recited in claim 6 , wherein the plurality of passages of the inner air swirler are upstream of the flame outlet with respect to the downstream direction along the injection axis.

8. The fuel injector as recited in claim 6 , wherein the fuel nozzle includes an inner heat shield outboard of the inner air swirler, with an insulation gap defined between the inner heat shield and the inner air swirler, wherein an intermediate air swirler is defined between the inner air swirler and the inner heat shield.

9. The fuel injector as recited in claim 8 , wherein the fuel nozzle includes a fuel distributor outboard of the inner heat shield.

10. A fuel injector comprising:

a fuel nozzle configured to issue a spray of fuel from a fuel outlet in a downstream direction along an injection axis, the fuel nozzle defining a main flow passage therethrough;

an injection fuel line in fluid communication with the fuel nozzle to supply fuel to the fuel nozzle; and

a torch ignitor with a flame outlet opening into the main flow passage of the fuel nozzle for issuing flame into the main flow passage, wherein the fuel nozzle includes a fuel distributor and a prefilmer outboard of the fuel distributor, wherein the prefilmer includes a prefilming surface, wherein the fuel outlet is defined between the fuel distributor and the prefilming surface,

wherein the fuel nozzle includes an outer heat shield outboard of the prefilmer, with an insulation gap defined between the prefilmer and the outer heat shield, and

wherein the injection fuel line passes through the outer heat shield, the insulation gap, and the prefilmer into a fuel circuit defined between the fuel distributor and the prefilmer.

11. The fuel injector as recited in claim 10 , wherein the outer heat shield defines an outer air passage outboard of the outer heat shield.

12. The fuel injector as recited in claim 11 , wherein the torch ignitor passes through an inner heat shield and an inner air swirler.

13. A system comprising:

an engine case;

a combustor within the engine case; and

a plurality of fuel injectors extending from outside the engine case to the combustor to issue fuel and air into the combustor for combustion, wherein each of the fuel injectors in the plurality of fuel injectors includes:

a fuel nozzle connected to the combustor to issue a spray of fuel from a fuel outlet in a downstream direction along an injection axis, the fuel nozzle defining a main flow passage therethrough;

an injection fuel line extending radially inward, relative to the injection axis, to an annular wall of the fuel nozzle and in fluid communication with the fuel nozzle to supply fuel to the fuel nozzle, wherein a centerline axis of the annular wall of the fuel nozzle is the injection axis; and

a torch ignitor including a combustion chamber, the torch ignitor configured to combust fuel to produce a flame, the torch ignitor further including a flame outlet opening into the main flow passage of the fuel nozzle for issuing the flame into the main flow passage, wherein the injection fuel line and the torch ignitor define a feed arm extending along a flame axis that is angled relative to the injection axis.