Non-symmetrical low NOx burner apparatus and method

Abstract

A burner apparatus for a furnace system and a method of burner operation wherein a non-symmetrical positioning of one combustion fuel discharge tip or a grouping of fuel discharge tips within the burner wall produces side-by-side lean and fuel rich combustion stage zones and also produces internal flue gas recirculation.

Claims

1. A burner apparatus comprising: a burner wall having a forward end, wherein said burner wall surrounds an air flow passageway which extends through said burner wall, said air flow passageway has a forward discharge opening at said forward end of said burner wall, and said burner wall has a longitudinal axis which extends through said air flow passageway and said burner apparatus having within said air flow passageway surrounded by said burner wall only one combustion fuel discharge tip assembly, said combustion fuel discharge tip assembly within said air flow passageway comprising a single combustion fuel discharge tip having a forward end and a flame stabilizing structure located at, forwardly of, or rearwardly of said forward end of said combustion fuel discharge tip, wherein said combustion fuel discharge tip is located laterally outward with respect to said longitudinal axis of said burner wall at a position which is between said longitudinal axis and said burner wall.

2. The burner apparatus of claim 1 wherein said forward end of said combustion fuel discharge tip is located within a range of from not more than 50 mm reawardly to not more than 50 mm forwardly of said forward discharge opening of said air flow passageway.

3. The burner apparatus of claim 1 wherein said flame stabilizing structure contacts or is within 50 mm of said burner wall.

4. The burner apparatus of claim 1 wherein said combustion fuel discharge tip is a gas fuel discharge tip.

5. The burner apparatus of claim 1 wherein said combustion fuel discharge tip is a round flame discharge tip.

6. The burner apparatus of claim 1 wherein said flame stabilizing structure is a stabilization cone.

7. The burner apparatus of claim 6 wherein at least 75% of a diameter of said stabilization cone is located in a first lateral half of said air flow passageway between said longitudinal axis of said burner wall and a first interior side of said burner wall and not more than 25% of said diameter of said stabilization cone is located in a second lateral half of said air flow passageway between said longitudinal axis of said burner wall and a second interior side of said burner wall opposite said first interior side of said burner wall.

8. The burner apparatus of claim 7 wherein said stabilization cone has a forward edge which contacts or is within 50 mm of said first interior side of said burner wall.

9. The burner apparatus of claim 1 wherein said combustion fuel discharge tip assembly further comprises a fuel riser which extends longitudinally through said air flow passageway to said combustion fuel discharge tip.

10. The burner apparatus of claim 1 wherein said burner wall is a refractory tile wall structure.

11. A burner apparatus comprising: a burner wall having a forward end, wherein said burner wall surrounds a flow passageway which extends through said burner wall for flow of an oxygen-containing gas, said flow passageway has a forward discharge opening at said forward end of said burner wall, and said burner wall has a longitudinal axis which extends through said flow passageway; said burner apparatus having within said flow passageway surrounded by said burner wall only one combustion fuel discharge tip, said combustion fuel discharge tip being located in said flow passageway at a laterally outward position with respect to said longitudinal axis of said burner wall which is between said longitudinal axis of said burner wall and a first interior side of said burner wall; a lean combustion zone projecting forwardly from said forward discharge opening of said flow passageway wherein combustion occurs in an excess oxygen to fuel ratio, said lean combustion zone being located adjacent to a second interior side of said burner wall opposite said first interior side of said burner wall; and a fuel rich combustion zone projecting forwardly from said forward discharge opening of said flow passageway wherein combustion occurs in an excess fuel to oxygen ratio, said fuel rich combustion zone being located adjacent to said first interior side of said burner wall.

12. The burner apparatus of claim 11 wherein said combustion fuel discharge tip has a forward end which is located within a range of from 50 mm rearwardly to 50 mm forwardly of said forward discharge opening of said flow passageway.

13. The burner apparatus of claim 11 further comprising a flue gas recirculation region projecting forwardly from said forward discharge opening of said flow passageway wherein combustion occurs with recirculated inert products of combustion being present, said flue gas recirculation region being located adjacent to said first interior side of said burner wall.

14. The burner apparatus of claim 11 wherein said combustion fuel discharge tip is a gas fuel discharge tip.

15. The burner apparatus of claim 11 wherein said combustion fuel discharge tip is a round flame discharge tip.

16. The burner apparatus of claim 11 further comprising a flame stabilizing structure located within a range of from 50 mm rearwardly to 50 mm forwardly of said forward end of said combustion fuel discharge tip.

17. The burner apparatus of claim 16 wherein said flame stabilizing structure is a stabilization cone.

18. The burner apparatus of claim 17 wherein at least 75% of a diameter of said stabilization cone is located in a first lateral half of said flow passageway between said longitudinal axis of said burner wall and said first interior side of said burner wall and not more than 25% of said diameter of said stabilization cone is located in a second lateral half of said flow passageway between said longitudinal axis and said second interior side of said burner wall.

19. The burner apparatus of claim 17 wherein said stabilization cone has a forward edge which contacts or is within 50 mm of said first interior side of said burner wall.

20. The burner apparatus of claim 11 wherein said burner wall is a refractory tile wall structure.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a partially cutaway elevational side view of an embodiment 10 of the inventive non-symmetrical burner apparatus.

(2) FIG. 2 is a discharge end view of the inventive non-symmetrical burner apparatus 10.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

(3) An embodiment 10 of the inventive burner apparatus is illustrated in FIGS. 1 and 2. The inventive burner 10 is a non-symmetrical burner apparatus which preferably comprises: a housing 12 having an outlet end 14; a burner wall 16 which is positioned at the outlet end 14 of the housing 12 and has a longitudinal axis 18 which extends therethrough; an air flow passageway 22 which extends through and is surrounded by the burner wall 16 and has a forward discharge opening 24 at the forward end 20 of the burner wall 16; a single combustion fuel discharge tip assembly 26 which extends through a discharge section 28 of the housing 12 and into the air flow passageway 22 of the burner wall 16; and a pilot burner assembly 30 which also extends through the discharge section 28 of the housing 12 and into the air flow passageway 22 of the burner wall 16.

(4) The housing 12 comprises: an inlet section 32 upstream of the discharge section 28 for receiving combustion air or other oxygen containing gas via an inlet opening 34; a muffler 36 provided at the inlet opening 34; and an adjustable damper 40 which is provided in the inlet section 32 and includes an exterior adjustment handle 42.

(5) Combustion air (or an alternative oxygen-containing gas) is received through the inlet opening 34 of the housing 12 and flows through the housing 12 to the inlet end 35 of the burner wall 16. The air (or other oxygen-containing gas) then flows through the flow passageway 22 of the burner wall 16 and exits the forward discharge opening 24 of the passageway 22. The quantity of combustion air entering housing 12 can be regulated using the inlet damper 40. The damper is preferably mounted using a bearing assembly 44 for smooth, precise operation. Combustion air can be provided to housing 12 by forced circulation, natural draft, a combination thereof, or in any other manner employed in the art. In the case of forced air circulation, the muffler 36 will preferably be removed to allow a forced air connection.

(6) The burner wall 16 is preferably constructed of a high temperature refractory burner tile material. However, it will be understood that the burner wall 16 could alternatively be formed of or provided by the furnace floor, a metal band, a refractory band, or any other material or structure which is capable of (a) providing an acceptable combustion air flow orifice (i.e., passageway) into the fired heating system and (b) withstanding high temperature operating conditions.

(7) The forward (discharge) end 20 of burner wall 16 is in communication with the interior of the boiler, fired heater, furnace or other fired heating system enclosure in which combustion takes place. As a result of the combustion process which takes place in the enclosure of the fired heating system, the enclosure will also contain combustion product gases (i.e., flue gas) 72. The inventive burner 10 can be installed, for example, through a floor or wall 46 of the fired heating system enclosure, which will typically be formed of metal. An insulating material will also typically be secured to the interior surface of the floor or wall 46 outside of the burner wall 16.

(8) The burner wall 16 and the air flow passageway 22 extending therethrough will preferably have round (circular) cross-sectional shapes. However, it will be understood that the cross-sectional shapes of the burner wall 16 and the air flow passageway 22 can alternatively be square, rectangular, oval, or generally any other shape desired.

(9) The pilot burner assembly 30 will preferably be located within the combustion air passageway 22 of the burner wall 16 for initiating combustion at the outer (forward) end 48 of the combustion fuel discharge tip assembly 26. As will be understood by those skilled in the art, the inventive burner apparatus 10 can also include one or more auxiliary pilots or, rather than using one or more pilot burners, combustion in the apparatus 2 can be initiated using, for example, a temporary ignition device suitable for achieving reliable ignition.

(10) The combustion fuel discharge tip assembly 26 preferably comprises: a combustion fuel riser or other conduit 58 which extends through the discharge section 28 of the housing 12 and into the air flow passageway 22 of the burner wall 22; a combustion fuel discharge tip 60 on the outer (forward) end of the fuel riser 58; and a flame stabilizing structure 62 which is preferably positioned at or proximate to the outer (forward) end 48 of the combustion fuel discharge tip 60. More preferably, the forward most edge, surface, or other forward most portion 86 of the flame stabilizing structure 62 will be positioned within a range of from 50 mm forwardly to 50 mm rearwardly of the outer (forward) end 48 of the combustion fuel discharge tip 60 and will most preferably be positioned within a range of from 25 mm forwardly to 25 mm rearwardly of the outer end 48.

(11) As used herein and in the claims, the terms combustion fuel discharge tip assembly and combustion fuel discharge tip refer to the fuel delivery and discharge assemblies and structures used in the burner for delivering and discharging the fuel which is combusted by the burner for process heat transfer in the fired heating system. Consequently, the terms combustion fuel discharge tip assembly and combustion fuel discharge tip do not refer to and do not include pilot burner assemblies and tips, such as, for example, the pilot burner assembly 30 used in the inventive burner apparatus 10. In other words, as used herein, combustion fuel discharge tip assemblies and combustion fuel discharge tips refer to assemblies and structures for delivering non-pilot combustion fuel.

(12) The inventive burner apparatus 10 as shown in FIGS. 1 and 2 is referred to herein as a non-symmetrical burner because the single combustion fuel discharge tip 60 used in the burner apparatus 10 is not centrally located within the burner wall 16 in alignment with the longitudinal axis 18. Rather, the discharge tip 60 is positioned laterally outward within the air flow passageway 22 with respect to the longitudinal axis 18 such that the discharge tip 60 is positioned closer to one interior side 64 of the burner wall 16 than it is the interior side 66 of the burner wall 16 which is directly opposite the interior side 64.

(13) This inventive non-symmetrical positioning of the single combustion fuel discharge tip 60 in the air flow passage 22 produces a staged air operation in the inventive burner 10 wherein the ejection of the combustion fuel from the combustion fuel discharge tip 60 simultaneously creates (a) a forwardly projecting fuel rich combustion zone 68 which is adjacent to the lateral interior side 64 of the burner wall 16 and (b) a forwardly projecting lean combustion zone 70 which is adjacent to the lateral interior side 66 of said burner wall 16 opposite the lateral interior side 64. In other words, the fuel rich combustion zone 68 and the lean combustion zone 70 project forwardly from opposite lateral sides of the forward discharge opening 24 of the burner wall 10.

(14) In the fuel rich combustion zone or stage 68 of the inventive burner 10, combustion occurs in an excess fuel to air ratio. In the lean combustion zone or stage 70, on the other hand, combustion occurs in an excess air to fuel ratio.

(15) By way of further explanation, since the fuel discharge tip 60 and the flame stabilizer 62 are located next to or closer to one side (i.e., the lateral interior side 64) of the burner wall 16, a first portion of the fuel ejected from the fuel discharge tip 60 is caused to flow adjacent to the combustion air stream 65 traveling through the air flow passage 22 while a second portion of the ejected fuel is caused to flow adjacent to the products of combustion 72 outside of the burner wall 16. Consequently, a much larger proportion of the total combustion air stream 65 mixes with the first portion of the ejected fuel, thus forming the lean combustion zone or stage 70. Since more combustion air than fuel gas is present in the lean combustion zone 70, the peak flame temperature in the lean combustion zone 70 is reduced, resulting in lower thermal NO emissions.

(16) The second portion of the fuel, on the other hand, is burned in the fuel rich zone or stage 68 where much less combustion air is available. In addition, because the portion of the fuel combusted in the fuel rich combustion zone 68 is ejected adjacent to, and therefore mixes with, the inert products of combustion 72 outside of the burner wall 16, the inert products of combustion also condition this portion of the fuel to thereby further lower the flame temperature in the fuel rich zone 68 and produce lower thermal NO emissions. This Internal Flue Gas Recirculation (IFGR) in the fuel rich combustion zone 68 is also enhanced significantly by the forward discharge momentum of the combustion air stream 65 which assists in pulling the exterior inert products of combustion 72 into the ejected fuel.

(17) In the inventive non-symmetrical burner 10, IFGR can be produced in the entire fuel rich combustion zone 68 or can occur in a smaller or different flue gas recirculation region 75 which projects forwardly from the forward discharge opening 24 of the air flow passageway 22. In other words, the flue gas recirculation region 75 can be either (a) the entire fuel rich combustion zone 68, (b) an outer portion of the fuel rich combustion zone 68 or (c) a separate region which is adjacent to the fuel rich combustion zone 68.

(18) Although the inventive burner apparatus 10 illustrated in FIGS. 1 and 2 includes only a single combustion fuel discharge tip assembly 26 and a single combustion fuel discharge tip 60, it will be understood that alternative embodiments of the inventive non-symmetrical burner which have side-by-side fuel rich and lean combustion zones and which also provide IFGR in or adjacent to the fuel rich zone can be produced using two or more discharge tip assemblies and discharge tips.

(19) By way of example, in accordance with the method of the present invention, an inventive non-symmetrical burner can be provided and operated by discharging, either from a single discharge tip or from a collection of two or more discharge tips, significantly more fuel (preferably all or substantially all of the fuel) from one lateral half 82 (or more preferably a smaller portion of the lateral half 82) of the forward opening 24 of the burner wall 16 versus the opposing other half 84 of the forward opening 24, thereby creating side-by-side lean and fuel rich combustion zones. When using multiple fuel discharge tips and assemblies, such a flow pattern can produced, for example, by grouping the multiple discharge tip assemblies and discharge tips within the burner wall 16 at locations which are closer to one lateral interior side 64 of the burner wall 16 than to the opposite lateral interior side 66 of the burner wall 16.

(20) The use of multiple fuel discharge tips will also allow multiple gas or liquid fuels to be burned simultaneously in the same burner. In this scenario, each fuel stream can, for example, be dedicated to a single tip located against or proximate to one burner wall to allow the inventive NO.sub.x reduction method to be utilized for each fuel stream individually.

(21) In the inventive burner 10, the fuel discharge tip 60 is located laterally outward with respect to the longitudinal axis 18 of the burner wall 16 at a position which is between the longitudinal axis 18 and the interior side 64 of the burner wall 16. The fuel discharge tip 60 (or the grouping of discharge tips if more than one tip is used) will preferably be located laterally outward with respect to the longitudinal axis 18 at a position which is at least one quarter (more preferably at least one third) of the radial distance 76 from the longitudinal axis 18 to the lateral interior side 64 burner wall 16. Still more preferably, the fuel discharge tip 60 will be located laterally outward with respect to the longitudinal axis 18 of the burner wall 16 at a position which is at least 40% of the radial distance 76 from the longitudinal axis 18 to the lateral interior side 64 burner wall 16.

(22) The fuel discharge tip 60 of the inventive burner 10 can be a gas fuel ejection tip or a liquid fuel ejection tip, but will preferably be a gas ejection tip. The fuel gas used in the inventive burner and method can be natural gas, refinery gas, or generally any other type of gas fuel or gas fuel blend employed in process heaters, boilers, or other gas-fired heating systems. Examples of types of fuel ejection tips preferred for use in the inventive burner 10 include, but are not limited to, round flame tips and flat flame tips. The fuel discharge tip 60 used in the inventive burner 10 will preferably be a round flame tip.

(23) The forward end 48 of the fuel discharge tip 60 will preferably be located at or proximate to the forward discharge opening 24 of the air flow passageway 22. The forward end 48 of the fuel ejection tip 60 will preferably be located within a range of from not more than 50 mm rearwardly to not more than 50 mm forwardly of the discharge opening 24 and will more preferably be located within a range of from 25 mm rearwardly to 25 mm forwardly of the discharge opening 24.

(24) Examples of types of flame stabilizing structures suitable for use used in the discharge tip assembly 26 of the inventive burner 10 include, but are not limited to, stabilization cones, swirlers, air diffusers, spin vanes, regeneration tiles, or any bluff body, including an extension of the burner tile, for providing a region of mixing and stable flame.

(25) The flame stabilizing structure 62 used in the inventive burner 10 will preferably be a stabilization cone as illustrated in FIGS. 1 and 2. The stabilization cone or other structure 62 is preferably, but not limited to be, positioned in the air flow passageway 22 of the burner wall 16 such that at least 75% (more preferably at least 90%) of the diameter or width 80 of the stabilization cone or other structure 62 is located in the lateral half 82 of the air flow passageway 22 adjacent to the lateral interior side 64 of the burner wall 16 and not more than 25% (more preferably not more than 10%) of the diameter or width 80 of the stabilization cone or other structure 62 is located in the opposite lateral half 84 of the air flow passageway 22 adjacent to the opposite lateral interior side 66 of the burner wall 16. More preferably, the entire stabilization cone or other structure 62 is located in the lateral half 82 of the air flow passageway 22 adjacent to the lateral interior side 64 of the burner wall 16.

(26) In addition, the stabilization cone 62 has a forward edge 86 which preferably either contacts or is proximate to the lateral interior side 64 of the burner wall 16. The forward edge 86 of the stabilization cone is preferably within at least 50 mm (more preferably within at least 25 mm) of the lateral interior side 64 of the burner wall 16.

(27) Also, it will be understood that further reduction in NO.sub.x emissions can be achieved in the inventive burner and method by optionally including the use of (a) external flue gas recirculation, (b) steam and/or inert injection into the combustion air stream, (c) steam and/or inert injection into the combustion fuel stream, (d) flameless combustion, and/or (e) an additional staged air region outside the burner wall.

(28) As yet another option, it will be understood that additional reduction in NO.sub.x emissions can be achieved in the inventive burner by also including the use of staged fuel gas tips or a gas annulus located on the exterior of the burner wall 16.

(29) Thus, the present invention is well adapted to carry out the objectives and attain the ends and advantages mentioned above as well as those inherent therein. While presently preferred embodiments and steps have been described for purposes of this disclosure, the invention is not limited in its application to the details of the preferred embodiments and steps. Numerous changes and modifications will be apparent to those of ordinary skill in the art. Such changes and modifications are encompassed within this invention as defined by the claims. In addition, unless expressly stated, the phraseology and terminology employed herein is for the purpose of description and not of limitation.