Flow deflectors for fuel nozzles

• US 9,388,982 B2
• Filed: 10/26/2011
• Issued: 07/12/2016
• Est. Priority Date: 10/27/2010
• Status: Active Grant

• Current Assignee: General Electric Technology GmbH (GE Aerospace)
• Original Assignee: Alstom Technology Ltd. (Alstom SA)
• Inventors: Donais, Richard E., Hellewell, Todd D., Mills, Wendell H.
• Primary Examiner(s): Rinehart, Kenneth
• Assistant Examiner(s): Lau, Jason
• Application Number:
  US13/281,869
• Publication Number:
  US 20120104055A1
• Time in Patent Office: 1,721 Days
• Field of Search: 110/261, 110/263, 110/104.B, 431/284, 431/169, 431/159, 239500-524
• US Class Current: 1/1
• CPC Class Codes: F23D 1/00 Burners for combustion of pulverulent fuel disposition of burners F23C
• CPC Class Codes: F23D 2201/20 Fuel flow guiding devices
• CPC Class Codes: F23D 2201/30 Wear protection

Abstract

A fuel nozzle assembly including a conduit defining a fuel inlet and a fuel outlet and being operable to convey a fuel stream comprising a solid particulate fuel entrained in a fluid. The conduit has a flow area defined by an interior surface of the conduit. A first flow deflector and a second flow deflector extend inwardly from the interior surface. The first flow deflector and the second flow deflector are positioned to disrupt a velocity profile of the flow stream established upstream of the conduit.

Claims

1. A fuel nozzle assembly comprising:

a conduit defining a fuel inlet and a fuel outlet, operable to convey a fuel stream comprising a solid particulate fuel entrained in a fluid, the conduit having a flow area defined by an interior surface of the conduit, wherein the fuel stream is conveyed to the fuel inlet by an elbow-shaped conduit that results in the fuel stream splitting into at least a first sub-flow fuel stream and a second sub-flow fuel stream diverging from each other concentrated along the interior surface of the conduit;

a first flow deflector extending inwardly from the interior surface of the conduit and longitudinally parallel to a longitudinal axis defining the conduit along the interior surface of the conduit, the first flow deflector having major surface side walls defining the first flow deflector extending longitudinally parallel to the longitudinal axis defining the conduit along the interior surface to disrupt the at least first sub-flow fuel stream to entrain the solid particles back into the fuel stream; and

a second flow deflector extending inwardly from the interior surface of the conduit and longitudinally parallel to the longitudinal axis defining the conduit along the interior surface of the conduit, the second flow deflector having major surface side walls defining the second flow deflector extending longitudinally parallel to the longitudinal axis defining the conduit along the interior surface to disrupt the at least second sub-flow fuel stream to entrain the solid particles back into the fuel stream,

wherein at least one of the first and second flow deflectors each have substantially triangular cross sections along the longitudinal axis defining the conduit, each having the sidewalls joined at terminal ends thereof defining an apex therebetween.

2. The fuel nozzle assembly of claim 1, wherein a portion of opposing portions of the interior surface of the conduit are spaced apart by a first distance and the upstream end of at least one of the first and second deflectors is spaced away from the fuel inlet by a second distance of up to about 10 percent of the first distance.

4. The fuel nozzle assembly of claim 1, wherein the at least one of the first and second flow deflectors define an end face proximate to the fuel inlet, that slopes away from the inside surface toward the fuel outlet.

5. The fuel nozzle assembly of claim 1, wherein at least one of the first and second flow deflectors define an end face, proximate to the fuel outlet, that slopes away from the inside surface toward the fuel inlet.

6. The fuel nozzle assembly of claim 1, wherein a portion of opposing portions of the interior surface are spaced apart by a first distance and at least one of the first and second flow deflectors define an apex which is positioned outwardly from a base of the respective deflector by a second distance equal to about 20 percent to about 25 percent of the first distance.

7. The fuel nozzle assembly of claim 1, wherein the at least one of the first and second flow deflectors include a lip extending from a perimeter of a base of the respective deflector and wherein the lip is operable to secure the respective flow deflector to the interior surface.

8. The fuel nozzle assembly of claim 1, wherein exterior surfaces of at least one of the first and second flow deflectors have an abrasive resistant material disposed thereon.

9. The fuel nozzle assembly of claim 1, wherein the conduit defines a first section coupled to a second section positioned upstream of the first section and the first and second flow deflectors are positioned in the second section.

10. The fuel nozzle assembly of claim 9, wherein the second section extends from an outlet of an elbow and has a substantially cylindrical cross section defining an inside diameter and one end of at least one of the first and second deflectors is spaced away from the outlet of the elbow by a distance of up to about 10 percent of the inside diameter.

11. The fuel nozzle assembly of claim 10, wherein the second section is integral with the elbow.

12. The fuel nozzle assembly of claim 1, wherein the first and second flow deflectors are positioned substantially opposite one another.

13. The fuel nozzle assembly of claim 1, wherein the first and second flow deflectors are positioned substantially symmetrically about a central longitudinal plane defined by the conduit.

14. The fuel nozzle assembly of claim 1, wherein the side walls of the first and second flow deflectors angle downwardly relative to a central longitudinal plane defined by the conduit to prevent accumulation of fuel particles thereon.

15. The fuel nozzle assembly of claim 1, wherein a portion of opposing portions of the interior surface are spaced apart by a first distance and at least one of the first and second flow deflectors have a longitudinal length of about 150% to 160% of the first distance.

16. The fuel nozzle assembly of claim 1, wherein the first flow deflector and second flow deflector are disposed above or below a central longitudinal plane defined by the conduit.

3. A fuel nozzle assembly comprising:

a conduit defining a fuel inlet and a fuel outlet, operable to convey a fuel stream comprising a solid particulate fuel entrained in a fluid, the conduit having a flow area defined by an interior surface of the conduit, wherein the fuel stream is conveyed to the fuel inlet by an elbow-shaped conduit that results in the fuel stream splitting into at least a first sub-flow fuel stream and a second sub-flow fuel stream diverging from each other concentrated along the interior surface of the conduit;

a first flow deflector extending inwardly from the interior surface of the conduit and longitudinally parallel to a longitudinal axis defining the conduit along the interior surface of the conduit, the first flow deflector having major surface side walls defining the first flow deflector extending longitudinally parallel to the longitudinal axis defining the conduit along the interior surface to disrupt the at least first sub-flow fuel stream to entrain the solid particles back into the fuel stream; and

a second flow deflector extending inwardly from the interior surface of the conduit and longitudinally parallel to the longitudinal axis defining the conduit along the interior surface of the conduit, the second flow deflector having major surface side walls defining the second flow deflector extending longitudinally parallel to the longitudinal axis defining the conduit along the interior surface to disrupt the at least second sub-flow fuel stream to entrain the solid particles back into the fuel stream,

wherein at least one of the first and second flow deflectors each have substantially triangular cross sections along the longitudinal axis defining the conduit, each having the sidewalls joined at terminal ends thereof defining an apex therebetween; and

wherein the substantially triangular cross sections each reside in a plane that is substantially orthogonal to the longitudinal axis defining the conduit.

17. The fuel nozzle assembly of claim 3, wherein a portion of opposing portions of the interior surface of the conduit are spaced apart by a first distance and the upstream end of at least one of the first and second deflectors is spaced away from the fuel inlet by a second distance of up to about 10 percent of the first distance.

18. The fuel nozzle assembly of claim 3, wherein the at least one of the first and second flow deflectors define an end face proximate to the fuel inlet, that slopes away from the inside surface toward the fuel outlet.

19. The fuel nozzle assembly of claim 3, wherein at least one of the first and second flow deflectors define an end face, proximate to the fuel outlet, that slopes away from the inside surface toward the fuel inlet.

20. The fuel nozzle assembly of claim 3, wherein a portion of opposing portions of the interior surface are spaced apart by a first distance and at least one of the first and second flow deflectors define an apex which is positioned outwardly from a base of the respective deflector by a second distance equal to about 20 percent to about 25 percent of the first distance.

21. The fuel nozzle assembly of claim 3, wherein the at least one of the first and second flow deflectors include a lip extending from a perimeter of a base of the respective deflector and wherein the lip is operable to secure the respective flow deflector to the interior surface.

22. The fuel nozzle assembly of claim 3, wherein exterior surfaces of at least one of the first and second flow deflectors have an abrasive resistant material disposed thereon.

23. The fuel nozzle assembly of claim 3, wherein the conduit defines a first section coupled to a second section positioned upstream of the first section and the first and second flow deflectors are positioned in the second section.

24. The fuel nozzle assembly of claim 23, wherein the second section extends from an outlet of an elbow and has a substantially cylindrical cross section defining an inside diameter and one end of at least one of the first and second deflectors is spaced away from the outlet of the elbow by a distance of up to about 10 percent of the inside diameter.

25. The fuel nozzle assembly of claim 24, wherein the second section is integral with the elbow.

26. The fuel nozzle assembly of claim 3, wherein the first and second flow deflectors are positioned substantially opposite one another.

27. The fuel nozzle assembly of claim 3, wherein the first and second flow deflectors are positioned substantially symmetrically about a central longitudinal plane defined by the conduit.

28. The fuel nozzle assembly of claim 3, wherein the side walls of the first and second flow deflectors angle downwardly relative to a central longitudinal plane defined by the conduit to prevent accumulation of fuel particles thereon.

29. The fuel nozzle assembly of claim 3, wherein a portion of opposing portions of the interior surface are spaced apart by a first distance and at least one of the first and second flow deflectors have a longitudinal length of about 150% to 160% of the first distance.

30. The fuel nozzle assembly of claim 3, wherein the first flow deflector and second flow deflector are disposed above or below a central longitudinal plane defined by the conduit.