APPARATUS AND METHOD FOR A BURNER ASSEMBLY
20200191381 ยท 2020-06-18
Assignee
Inventors
- Kenneth Ray George (Parsons, KS, US)
- Michael Joseph Purdon (Coffeyville, KS, US)
- Michael Ryan Martinie (McCune, KS, US)
Cpc classification
F23D2900/00014
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D2209/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/34
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C2900/03005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D2210/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C1/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C2900/06042
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C3/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/36
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23K5/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/70
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C7/008
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D2209/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F23C1/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C3/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C7/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/36
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/64
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A burner assembly having a blower housing, a blower to supply air to the burner assembly, a blast tube having a longitudinal axis, a fuel source to supply fuel to the burner assembly, a center tube that is substantially parallel to the longitudinal axis and conveys air and fuel to a center tube burner end opening, a plurality of premix tubes, each of which is substantially parallel to the longitudinal axis and conveys air and fuel to a premix tube burner end opening, a diffuser that is disposed in the center tube near the center tube burner end opening, a nozzle that is disposed in the center tube substantially perpendicular to the diffuser. The center tube air and fuel mixture is fuel rich and the premix tubes air and fuel mixture is fuel lean. A method for burning the center tube air and fuel mixture and the premix tubes mixtures.
Claims
1. A burner assembly, said burner assembly comprising: (a) a blower housing; (b) a blower, said blower being adapted to supply air to the burner assembly; (c) a blast tube, said blast tube having a longitudinal axis; (d) a fuel source, said fuel source being adapted to supply fuel to the burner assembly; (e) a center tube, said center tube being substantially parallel to the longitudinal axis and being adapted to convey a center tube air and fuel mixture to a center tube burner end opening; (f) a plurality of premix tubes, each of said plurality of premix tubes being substantially parallel to the longitudinal axis and being adapted to convey a premix tube air and fuel mixture to a premix tube burner end opening; (g) a diffuser, said diffuser being disposed in the center tube near the center tube burner end opening; wherein the center tube air and fuel mixture is fuel rich; and wherein the premix tubes air and fuel mixtures are fuel lean.
2. The burner assembly of claim 1 further comprising a blower motor.
3. The burner assembly of claim 1 further comprising a damper.
4. The burner assembly of claim 1 further comprising a mounting flange.
5. The burner assembly of claim 1 further comprising an access cover.
6. The burner assembly of claim 1 further comprising a fuel manifold.
7. The burner assembly of claim 7 wherein the fuel manifold comprises a plurality of orifices.
8. The burner assembly of claim 1 wherein the assembly comprises a scanner.
9. The burner assembly of claim 1 wherein the assembly comprises a pilot.
10. The burner assembly of claim 1 wherein the air comprises ambient air.
11. The burner assembly of claim 1 wherein the fuel comprises gaseous fuel.
12. The burner assembly of claim 1 wherein the fuel comprises liquid fuel.
13. The burner assembly of claim 1 further comprising a nozzle.
14. A burner assembly, said burner assembly comprising: (a) a blower housing, (b) a blower, said blower being adapted to supply ambient air to the blower housing; (c) a blast tube, said blast tube having a longitudinal axis; (d) a gaseous fuel source, said gaseous fuel source being adapted to supply gaseous fuel into the housing; (e) a center tube, said center tube being substantially parallel to the longitudinal axis and being adapted to convey a center tube ambient air and gaseous fuel mixture to a center tube burner end opening; (f) a plurality of premix tubes, each of said plurality of premix tubes being substantially parallel to the longitudinal axis and being adapted to convey a premix tube ambient air and gaseous fuel mixture to a premix tube burner end opening; (g) a diffuser, said diffuser being disposed in the center tube near the center tube burner end opening; wherein the center tube ambient air and gaseous fuel mixture is gaseous fuel rich; and wherein the mixture the plurality of premix tubes ambient air and gaseous fuel mixture is gaseous fuel lean.
15. The burner assembly of claim 14 further comprising a nozzle, said nozzle being disposed in the center tube substantially perpendicular to the diffuser;
16. A method for a burner assembly, said method comprising: (a) providing a burner assembly, said burner assembly comprising: (i) a blower housing; (ii) a blower, said blower being adapted to supply air to the burner assembly; (iii) a blast tube, said blast tube having a longitudinal axis; (iv) a fuel source, said fuel source being adapted to supply fuel to the burner assembly; (v) a center tube, said center tube being substantially parallel to the longitudinal axis and being adapted to convey a center tube air and fuel mixture to a center tube burner end opening; (vi) a plurality of premix tubes, each of said plurality of premix tubes being substantially parallel to the longitudinal axis and being adapted to convey a premix tube air and fuel mixture to a premix tube burner end opening; (vi) a diffuser, said diffuser being disposed in the center tube near the center tube burner end opening; wherein the center tube air and mixture is fuel rich; and wherein the premix tubes air and fuel mixtures are fuel lean; (b) burning the center tube air and fuel mixture and the plurality of premix tubes air and fuel mixtures.
17. The method of claim 16 further comprising mixing the center tube air and fuel mixture in the center tube.
18. The method of claim 16 further comprising mixing the plurality of premix tubes air and fuel mixture in each of the plurality of premix tubes.
19. The method of claim 16 further comprising mixing the center tube air and fuel mixture with the plurality of premix tubes air and fuel mixtures near the plurality of premix tubes burner end opening.
20. The method of claim 16 further comprising attaching a burner flame to the diffuser.
21. The method of claim 16 further comprising conveying the fuel to the center tube and the plurality of premix tubes via a manifold.
22. The method of claim 16 wherein the burner assembly further comprises a nozzle.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0014] The presently preferred embodiments of the invention are illustrated in the accompanying drawings, in which like reference numerals represent like parts throughout, and in which:
[0015]
[0016]
[0017]
DESCRIPTION OF THE PREFERRED EMBODIMENTS OF THE INVENTION
[0018] Referring now to the drawings, the preferred embodiment of the burner assembly in accordance with the present invention is illustrated by
[0019] Still referring to
[0020] Still referring to
[0021] Still referring to
[0022] Still referring to
[0023] Still referring to
[0024] Referring now to
[0025] Referring now to
[0026] The invention also comprises a method for a burner assembly. The preferred method comprises providing a burner assembly as described above in detail. The preferred method also comprises burning the center tube air and fuel mixture and the plurality of premix tubes air and fuel mixtures. In other preferred embodiments of the method of the invention, the method further comprises mixing the center tube air and fuel mixture in the center tube, mixing the plurality of premix tubes air and fuel mixtures in each of the plurality of premix tubes, and mixing the center tube air and fuel mixture with the plurality of premix tubes air and fuel mixtures near the burner end openings. In other preferred embodiments of the method of the invention, the method still further comprises attaching a burner flame to the diffuser and conveying the fuel to the center tube and the plurality of premix tubes via a manifold.
[0027] In operation, several advantages of the preferred embodiments of the burner assembly are achieved. For example, the preferred embodiments of the burner assembly do not produce excessive amounts of the undesirable combination of nitric oxide (NO) and nitrogen dioxide (NO2) (collectively NOx). The preferred embodiments of the burner assembly also do not require either expensive and complex external flue gas recirculation piping and controls or burner geometry using internal flue gas recirculation systems to lower NOx emission levels. The preferred embodiments of the burner assembly further do not require undesirably high amounts of excess oxygen to reduce NOx emission levels. The preferred embodiments of the burner assembly still further do not have undesirably low combustion efficiencies. In addition, the preferred embodiments of the burner assembly do not produce undesirable acoustic coupling. The preferred embodiments of the burner assembly also do not dispose the burner head within the combustion chamber.
[0028] Additionally, in operation, combustion air from the blower is conveyed to the blast tube where it enters into the burner head. Uniform air flow is conveyed to each of the plurality of premix tubes and toward the premix tubes burner end openings. Uniform air flow is also conveyed to the center tube and toward the center tube burner end opening. In addition, gaseous fuel is conveyed to the gas manifold where it exits the manifold through a plurality of orifices. More particularly, gaseous fuel is conveyed to the plurality of premix tubes via a plurality of premix tube orifices, mixed with the combustion air in the premix tubes, and the mixture is conveyed toward the premix tubes burner end openings. A well-mixed lean fuel and air mixture is conveyed in each of the plurality of premix tubes. Simultaneously, gaseous fuel from the manifold enters the center tube via a plurality of center tube orifices and mixes with the combustion air in the center tube. It is also contemplated within the scope of the invention that the gaseous fuel may be conveyed via a center gas gun delivery system in order to more precisely control the fuel to air ratio. The center tube air and fuel mixture is conveyed through the flame stabilizing diffuser to produce a fuel rich stabilized center flame. The well-mixed fuel lean air mixtures exit the plurality of premix tubes burner end openings where the lean fuel mixtures are ignited by the fuel rich stabilized center flame. The well-mixed fuel lean mixture flames produce extremely low NOx levels, and the fuel rich stabilized flame is established on the diffuser.
[0029] More particularly, the high-velocity plurality of premix tubes surrounding the center tube produce very low NOx levels, e.g. less than thirty parts per million (30 ppm) and typically less than ten parts per million (10 ppm), due to operating at a relatively high level of oxygen (O2) (fuel lean). The center tube operates at a relatively low level of oxygen (O2) (fuel rich) or even at a sub-stoichiometric ratio and produces normal NOx levels, e.g. greater than approximately fifty parts per million (50 ppm). When the fuel lean and fuel rich mixtures are slowly combined, the sum of the flue gas results in low NOx levels (e.g., less than 30 ppm) and relatively low excess oxygen (3% or less). Typically, 3% excess oxygen is the desired level to maximize combustion efficiency while still having sufficient excess oxygen to ensure complete combustion.
[0030] In addition, the geometry of the plurality of premix tubes minimizes the risk of flashback, and the combination of the plurality of premix tubes with the standard nozzle mix burner defined in part by center tube minimizes the risk of acoustic coupling which premix burners experience. Further, because the fuel rich standard nozzle mix burner defined in part by the center tube has a very low oxygen level, the temperature of the flame it produces is lower than normal and it produces somewhat lower NOx levels. The fuel lean plurality of premix tubes produce very low NOx levels. Still further, the excess oxygen from the plurality of premix tubes is somewhat delayed in combining with the fuel rich mixture of the center burner and this further reduces NOx levels. The preferred embodiments of the burner assembly of the invention also produce almost no carbon monoxide (CO).
[0031] In testing preferred embodiments of the invention on multiple different-sized burner assemblies, the following results were achieved in one exemplary test: [0032] Rate: 6,900 Mbuth [0033] Excess O2: 2.5% [0034] NOx: 25.2 ppm [0035] CO: 0%
[0036] When the excess O2 level was increased to 3%, the NOx levels were reduced to 24.5 ppm.
[0037] As demonstrated above, the combination of a fuel rich center nozzle mix burner, which provides stability for the entire assembly and an flame in need of oxygen, and the plurality of pre-mix burners surrounding the center nozzle mix burner, which produce extremely low NOx levels and provide the oxygen needed by the center burner, produce low NOx levels with a relatively low amount of excess oxygen.
[0038] Although this description contains many specifics, these should not be construed as limiting the scope of the invention but as merely providing illustrations of some of the presently preferred embodiments thereof, as well as the best mode contemplated by the inventors of carrying out the invention. The invention, as described herein, is susceptible to various modifications and adaptations, and the same are intended to be comprehended within the meaning and range of equivalents of the appended claims.