Apparatus and method for reducing carbon monoxide emissions

1. A pilot injector for a gas turbine combustor that reduces the amount of carbon monoxide emissions produced by said combustor, said pilot injector comprising:

A radial swirler;

At least one fuel injector;

A first wall and second wall in spaced relation thereby forming a passageway therebetween, said passageway having an inlet and an outlet;

A means for establishing a recirculation area adjacent said pilot injector wherein said means for establishing a recirculation area is located within said passageway, proximate said outlet; and,

A generally annular extension located proximate said outlet and extending in an axial direction into a combustion liner.

2. The pilot injector of claim 1 wherein said at least one injector comprises a first injector and a second injector.

3. The pilot injector of claim 2 wherein said first injector is located proximate said radial swirler.

4. The pilot injector of claim 2 wherein said second injector injects a fuel into said passageway in a direction that is generally perpendicular to said first injector.

5. The pilot injector of claim 1 wherein said passageway is oriented generally radially proximate said inlet and generally axially proximate said outlet.

6. The pilot injector of claim 1 wherein said means for establishing a recirculation area comprises an annular ring.

7. The pilot injector of claim 6 wherein said annular ring is positioned along said second wall proximate said outlet of said passageway.

8. The pilot injector of claim 1 wherein said means for establishing a recirculation area comprises a plurality of spokes.

9. The pilot injector of claim 8 wherein said plurality of spokes are positioned together in an axial plane along said second wall proximate said outlet of said passageway, and extend from said second wall towards said first wall.

10. The pilot injector of claim 1 wherein said means for establishing a recirculation area comprises an annular ring and a plurality of spokes.

11. The pilot injector of claim 10 wherein said annular ring and plurality of spokes are coplanar and positioned along said second wall proximate said outlet of said passageway, and extend from said second wall towards said first wall.

12. A method of reducing the amount of carbon monoxide emissions produced by a gas turbine combustor at low power settings, said method comprising the steps:

Providing a pilot injector comprising a radial swirler, at least one fuel injector, a first wall and second wall in spaced relation thereby forming a passageway therebetween, said passageway having an inlet and an outlet, a means for establishing a recirculation area adjacent said pilot injector wherein said means for establishing a recirculation area is located within said passageway, proximate said outlet, and a generally annular extension located proximate said outlet and extending in an axial direction into a combustion liner;

Flowing a fuel through said at least one fuel injector to mix with an air supply in said passageway to form a premixture;

Directing said premixture through said passageway and across said means for establishing a recirculation area, such that a low pressure region is created and said premixture circulates in said low pressure region; and,

Burning said premixture along said low pressure region at a higher local reaction temperature, due to the reduced quenching affect by air on the reaction, thereby reducing carbon monoxide emissions.

13. The method of claim 12 wherein said means for establishing a recirculation area comprises an annular ring.

14. The method of claim 13 wherein said annular ring is positioned along said second wall proximate said outlet of said passageway.

15. The method of claim 12 wherein said means for establishing a recirculation area comprises a plurality of spokes.

16. The method of claim 15 wherein said plurality of spokes are positioned together in an axial plane along said second wall proximate said outlet of said passageway, and extend from said second wall towards said first wall.

17. The method of claim 12 wherein said means for establishing a recirculation area comprises an annular ring and a plurality of spokes.

18. The method of claim 17 wherein said annular ring and plurality of spokes are coplanar and positioned along said second wall proximate said outlet of said passageway, and extend from said second wall towards said first wall.