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An injector for a multipoint combustor system includes an inner air swirler which defines an interior flow passage and a plurality of swirler inlet ports in an upstream portion thereof. The inlet ports are configured and adapted to impart swirl on flow in the interior flow passage. An outer air cap

An injector for a multipoint combustor system includes an inner air swirler which defines an interior flow passage and a plurality of swirler inlet ports in an upstream portion thereof. The inlet ports are configured and adapted to impart swirl on flow in the interior flow passage. An outer air cap is mounted outboard of the inner swirler. A fuel passage is defined between the inner air swirler and the outer air cap, and includes a discharge outlet between downstream portions of the inner air swirler and the outer air cap for issuing fuel for combustion. The outer air cap defines an outer air circuit configured for substantially unswirled injection of compressor discharge air outboard of the interior flow passage.

대표청구항 ▼

1. An airblast injector for a multipoint combustor system comprising: an inner air swirler defining an interior flow passage and a plurality of swirler inlet ports in an upstream portion thereof configured and adapted for fluid communication of compressor discharge air through the swirler inlet port

1. An airblast injector for a multipoint combustor system comprising: an inner air swirler defining an interior flow passage and a plurality of swirler inlet ports in an upstream portion thereof configured and adapted for fluid communication of compressor discharge air through the swirler inlet ports into the interior flow passage such that swirl is imparted on flow in the interior flow passage; andan outer air cap mounted radially outboard of the inner swirler relative to a longitudinal axis defined by the inner air swirler and the outer air cap, with a fuel passage defined between the inner air swirler and the outer air cap, the fuel passage including a discharge outlet between downstream portions of the inner air swirler and the outer air cap for issuing fuel for combustion, and wherein the outer air cap defines an outer air circuit configured for substantially swirl-free injection of compressor discharge air outboard of the interior flow passage, wherein the outer air circuit is oriented to converge toward the longitudinal axis. 2. An airblast injector as recited in claim 1, wherein the outer air cap includes a plurality of cylindrical bores therethrough radially outboard of the fuel, wherein the cylindrical bores define the outer air circuit. 3. An airblast injector as recited in claim 2, wherein the cylindrical bores are oriented to converge toward the longitudinal axis defined by the inner air swirler and outer air cap. 4. An airblast injector as recited in claim 1, wherein the inner air swirler and outer air circuit are configured and adapted to pass about 30-60% of the total airflow of the injector through the inner air swirler. 5. An airblast injector as recited in claim 1, wherein the outer air cap includes a plurality of slotted outer air flow channels radially outboard of the fuel passage, wherein the slotted outer air flow channels define the outer air circuit. 6. An airblast injector as recited in claim 5, wherein the slotted airflow channels converge downstream towards the longitudinal axis defined by the inner air swirler and outer air cap. 7. An airblast injector as recited in claim 5, wherein the inner air swirler and outer air circuit are configured and adapted to pass about 30-60% of the total airflow of the injector through the inner air swirler. 8. An airblast injector as recited in claim 1, wherein the fuel passage includes a multi-start threaded passage defined between the inner air swirler and the outer air cap for even fuel distribution at low pressures. 9. An airblast injector as recited in claim 1, wherein the inner air swirler includes an upstream dome with a plurality of cylindrical swirl bores defined therethrough for passage of compressor discharge air into the inner air swirler. 10. An airblast injector as recited in claim 9, wherein the cylindrical bores of the inner air swirler are radially offset and converge downstream relative to the longitudinal axis defined by the inner air swirler and outer air cap. 11. An airblast injector for a multipoint combustor system comprising: an inner air swirler defining an interior flow passage and a plurality of swirler inlet ports in an upstream portion thereof configured and adapted for fluid communication of compressor discharge air through the swirler inlet ports into the interior flow passage such that swirl is imparted on flow in the interior flow passage; andan outer air cap mounted radially outboard of the inner swirler relative to a longitudinal axis defined by the inner air swirler and the outer air cap, with a fuel passage defined between the inner air swirler and the outer air cap, the fuel passage including a discharge outlet between downstream portions of the inner air swirler and the outer air cap for issuing fuel for combustion, wherein the outer air cap includes a plurality of cylindrical bores therethrough radially outboard of the fuel passage, wherein the cylindrical bores define an outer air circuit and are all oriented to converge toward the longitudinal axis defined by the inner air swirler and the outer air cap for substantially swirl-free injection of compressor discharge air outboard of the interior flow passage. 12. An airblast injector as recited in claim 11, wherein the inner air swirler and outer air circuit are configured and adapted to pass about 30-60% of the total airflow of the injector through the inner air swirler. 13. An airblast injector as recited in claim 11, wherein the inner air swirler includes an upstream dome with a plurality of cylindrical swirl bores defined therethrough for passage of compressor discharge air into the inner air swirler. 14. An airblast injector as recited in claim 13, wherein the cylindrical bores of the inner air swirler are radially offset and converge downstream relative to the longitudinal axis defined by the inner air swirler and outer air cap. 15. An airblast injector for a multipoint combustor system comprising: an inner air swirler defining an interior flow passage and a plurality of swirler inlet ports in an upstream portion thereof configured and adapted for fluid communication of compressor discharge air through the swirler inlet ports into the interior flow passage such that swirl is imparted on flow in the interior flow passage; andan outer air cap mounted radially outboard of the inner swirler relative to a longitudinal axis defined by the inner air swirler and the outer air cap, with a fuel passage defined between the inner air swirler and the outer air cap, the fuel passage including a discharge outlet between downstream portions of the inner air swirler and outer air cap for issuing fuel for combustion, wherein the outer air cap includes at least one slotted outer air flow channel radially outboard of the fuel passage configured and adapted for substantially swirl-free injection of compressor discharge air outboard of the interior flow passage, wherein the at least one slotted outer air flow channel defines an outer air circuit, and wherein the at least one slotted airflow channel converges downstream toward the longitudinal axis defined by the inner air swirler and the outer air cap. 16. An airblast injector as recited in claim 15, wherein the inner air swirler and outer air circuit are configured and adapted to pass about 30-60% of the total airflow of the injector through the inner air swirler. 17. An airblast injector as recited in claim 15, wherein the fuel passage includes a multi-start threaded passage defined between the inner air swirler and the outer air cap for even fuel distribution at low pressures. 18. An airblast injector as recited in claim 15, wherein the inner air swirler includes an upstream dome with a plurality of cylindrical swirl bores defined therethrough for passage of compressor discharge air into the inner air swirler. 19. An airblast injector as recited in claim 18, wherein the cylindrical bores of the inner air swirler are radially offset and converge downstream relative to the longitudinal axis defined by the inner air swirler and outer air cap.