Low NOx nozzle tip for a pulverized solid fuel furnace

• US 8,701,572 B2
• Filed: 02/26/2009
• Issued: 04/22/2014
• Est. Priority Date: 03/07/2008
• Status: Expired due to Fees

• Current Assignee: General Electric Technology GmbH (GE Aerospace)
• Original Assignee: Alstom Technology Ltd. (Alstom SA)
• Inventors: Donais, Richard E., Hellewell, Todd D., Lewis, Robert D., Richards, Galen H., Towle, David P.
• Primary Examiner(s): Rinehart, Kenneth
• Assistant Examiner(s): Laux, David J
• Application Number:
  US12/393,439
• Publication Number:
  US 20090277364A1
• Time in Patent Office: 1,881 Days
• Field of Search: 110/104.B, 110/260, 110/261, 110/262, 110/263, 110/265, 110/347, 431/8, 431/181, 431/187, 431/186, 431/189
• US Class Current: 110/104.B
• CPC Class Codes: F23C 7/008 Flow control devices F23C7/006 takes precedence
• CPC Class Codes: F23D 1/00 Burners for combustion of pulverulent fuel disposition of burners F23C
• CPC Class Codes: F23D 2201/101 tiltable
• CPC Class Codes: F23D 2201/20 Fuel flow guiding devices

Abstract

A nozzle tip [100] for a pulverized solid fuel pipe nozzle [200] of a pulverized solid fuel-fired furnace includes: a primary air shroud [120] having an inlet [102] and an outlet [104], wherein the inlet [102] receives a fuel flow [230]; and a flow splitter [180] disposed within the primary air shroud [120], wherein the flow splitter disperses particles in the fuel flow [230] to the outlet [104] to provide a fuel flow jet which reduces NOx in the pulverized solid fuel-fired furnace. In alternative embodiments, the flow splitter [180] may be wedge shaped and extend partially or entirely across the outlet [104]. In another alternative embodiment, flow splitter [180] may be moved forward toward the inlet [102] to create a recessed design.

Claims

1. A nozzle tip for a pulverized solid fuel pipe nozzle of a pulverized solid fuel-fired furnace that reduces NOx emissions, the nozzle tip comprising:

a primary air shroud having an inlet and an outlet , wherein the inlet receives a fuel flow;

a first splitter plate having a flow splitter positioned generally in the center of, and separated from the primary air shroud, the flow splitter having a wedge shape with an apex edge and a base, the apex edge positioned closer to the inlet and the base positioned closer to the outlet, the flow splitter extending only partially across the outlet, the flow splitter creating turbulence in the fuel flow that disperses the fuel flow as the fuel flow passes by the flow splitter and out of outlet,

wherein the base extends on opposing sides of the first splitter plate in the center.

2. The nozzle tip of claim 1, further comprising at least one of a shear bar and a bluff point disposed on the first splitter plate.

3. The nozzle tip of claim 1, further comprising an air deflector disposed on the primary air shroud.

4. The nozzle tip of claim 1 wherein the first splitter plate is positioned in a substantially vertical direction.

5. The nozzle tip of claim 1 wherein the first splitter plate is positioned in a substantially horizontal direction.

6. The nozzle tip of claim 1 wherein the flow splitter is positioned between the inlet and the outlet and its base is recessed with respect to the outlet.

7. A nozzle tip for a pulverized solid fuel pipe nozzle of a pulverized solid fuel-fired furnace that reduces NOx emissions, the nozzle tip comprising:

a primary air shroud having an inlet and an outlet, wherein;

the inlet receives solid fuel particles suspended in an airflow stream as a fuel flow,

the outlet generally has a cross-sectional shape with a plurality of lobes each radiating from a central location;

a flow splitter disposed within the primary air shroud substantially at the central location, the flow splitter functioning to deflect solid particles of the fuel flow into each lobe of the output and disperse the particles within the lobes allowing for combustion of the fuel flow with reduced NOx emissions.

8. The nozzle tip of claim 7 further comprising:

a splitter plate [160] disposed within the primary shroud for supporting the flow splitter.

9. A nozzle tip for a pulverized solid fuel pipe nozzle of a pulverized solid fuel-fired furnace that reduces NOx emissions, the nozzle tip comprising:

a primary air shroud having an inlet and an outlet, wherein the inlet receives a fuel flow;

a first splitter plate disposed within the primary air shroud, the first splitter plate and the primary air shroud defining a duct for receiving a first portion of the fuel flow; and

a second splitter plate disposed within the primary air shroud, the second splitter plate and the primary air shroud defining a duct for receiving a second portion of the fuel flow, wherein the first splitter plate, the second splitter plate, and the primary air shroud define a duct for receiving a third portion of the fuel flow disposed intermediate to the first portion and the second portion of the fuel flow, the third portion of the fuel flow comprising a first split flow and a diverging second split flow;

wherein the first split flow and the first portion of the fuel flow combine at the outlet of the primary air shroud to provide a first outlet fuel jet which exits the outlet of the primary air shroud;

wherein the second split flow and the second portion of the fuel flow combine at the outlet of the primary air shroud to provide a second outlet fuel jet;

wherein the first outlet fuel jet and second outlet fuel jet are divergent; and

wherein the first splitter plate and the second splitter plate are divergent outwardly.

10. The nozzle tip of claim 9, wherein

the first outlet fuel jet and the second outlet fuel jet exit the outlet of the primary air shroud separate and discrete from each other, and

the first outlet fuel jet and the second outlet fuel jet remain separate and discrete from each other for a predetermined distance from the outlet of the primary air shroud.

11. The nozzle tip of claim 10, wherein

the predetermined distance is in a range of approximately two (2) diameters of the first outlet fuel jet to approximately eight (8) diameters of the first outlet fuel jet, and

the first outlet fuel jet and the second split flow at least partially combine after traveling the predetermined distance from the outlet of the primary air shroud into the pulverized solid fuel-fired furnace.

12. The nozzle tip of claim 9, further comprising at least one of a shear bar and a bluff point disposed on at least one of the first splitter plate and the second splitter plate.

13. The nozzle tip of claim 9, further comprising a secondary air shroud disposed around the primary air shroud.

14. The nozzle tip of claim 9, wherein the primary air shroud comprises:

at least one side plate;

a top plate; and

a bottom plate, wherein the at least one side plate is connected between the top plate and the bottom plate.

15. The nozzle tip of claim 9, wherein the flow splitter is disposed between the first splitter plate and the second splitter plate.

16. The nozzle tip of claim 9, wherein

the first portion of the fuel flow comprises approximately 30 percent of the fuel flow,

the second portion of the fuel flow comprises approximately 40 percent of the fuel flow, and

the third portion of the fuel flow comprises approximately 30 percent of the fuel flow.

17. The nozzle tip of claim 9, wherein

the first outlet jet and the second outlet jet each comprise approximately 50 percent of the fuel flow.

18. The nozzle tip of claim 9, further including a flow splitter disposed within the primary air shroud, the flow splitter having a pair of diverging surfaces which separates the third portion of the fuel flow into the first split flow and the diverging second split flow.

19. The nozzle tip of claim 9, wherein at least one of the first splitter plate and second splitter plate are curved outwardly.

20. The nozzle tip of claim 9, wherein the primary shroud includes a first wall opposing the first splitter plate and a second wall opposing the second splitter plate, wherein the first wall and the second wall are divergent outwardly.