The present invention relates generally to fuel-fired heating apparatus, such as fuel-fired air heating furnaces, and more particularly relates to specially designed fuel/air mixing and combustion sections of such fuel-fired heating apparatus.
In fuel-fired heating appliances such as, for example, furnaces, a known firing method is to flow a fuel/air mixture into a burner box structure in which a suitable ignition device is disposed to combust the fuel/air mixture and thereby create hot combustion gases used to heat air (or another fluid as the case may be) for delivery to a location served by the heating appliance. The hot combustion gases are flowed through a series of heat exchanger tubes, externally across which the fluid to be heated is flowed, and then discharged from the heating appliance into a suitable flue structure. Due to various configurational characteristics of the heating appliance, during firing of the appliance undesirable uneven heating of the combustion product-receiving heat exchanger tubes may occur such that an undesirable non-uniform temperature distribution is present in the overall heat exchanger tube array.
In addition to this potential heat exchange unevenness problem, other problems that may arise in the design of fuel-fired heating appliances include an undesirable noise level generated in the creation of the fuel/air mixture delivered to the burner box, an undesirably low level of mixing of the fuel and air, and an undesirably high level of NOx generated in the fuel/air mixture combustion process.
As can be seen, a need exists for alleviating the above-noted problems associated with conventional fuel-fired heating appliances of various types. It is to this need that the present invention is primarily directed.
A specially designed combustion system 10 of a fuel-fired heating appliance, representatively an air heating furnace 12, is schematically depicted in
Referring to
Venturi structure 38 has perforations 44 formed in its sidewall. Representatively, the perforations 44 are formed only in the inlet end portion 40 of the venturi structure 38, but could be located on additional or other portions of the venturi structure sidewall if desired. As shown in
Turning now to
The previously mentioned heat exchanger tubes 20 form with the fuel/air mixture combustion structure 18 a heat transfer structure portion of the furnace 12 and have, as viewed in
Still referring to
The fuel/air mixture 80 within the secondary mixing housing 54 is then drawn through the perforated diffuser plate 64 into the interior of the burner box housing portion 62 wherein the igniter 68 combusts the fuel/air mixture 80 to form therefrom hot combustion gas 82 that is flowed rightwardly through the heat exchanger tubes 20.
Simultaneously with the flow of hot combustion gas 82 through the heat exchanger tubes 20, a supply air fan portion of the furnace 12 (not shown) flows air 84 to be heated externally across the heat exchanger tubes 20 to receive combustion heat therefrom and create a flow of heated air 84a for delivery to a conditioned space served by the furnace 12. Combustion heat transfer from the heat exchanger tubes 20 to the air 84 causes the tube-entering hot combustion gas 82 to rightwardly exit the heat exchanger tubes 20 as cooled combustion gas 82a that enters the collector box 70 and is expelled therefrom, by the draft inducer fan 72, to a suitable flue structure (not shown).
Compared to conventional fuel/air mixing structures, the venturi-based primary fuel/air mixing structure 14 provides several advantages. For example, due to the cross-flow injection technique utilizing the combustion air 74a swirling through the venturi interior in combination with the radially directed interior fuel jets 78, an improved degree of fuel/air mixing is achieved within the venturi structure 38. This enhanced degree of fuel/air mixing is further increased by the use of the secondary fuel/air mixing structure 16 which serves to further mix the fuel and air by providing further “residence” time for the fuel/air mixture created in the venturi structure 38 before it enters the fuel/air mixture burner box housing 62 for combustion therein.
Additionally, the construction of the primary fuel/air mixing structure 14 substantially reduces the fuel/air mixing noise during both start-up and steady state operation of the furnace 12. In the primary fuel/air mixing structure 14 the perforations 44 in the sidewall of the venturi structure 38 permit the fuel/air mixture traversing it to enter and fill the chamber 50 circumscribing the venturi structure 38. This creates within the chamber 50 a fluid damping volume that absorbs and damps noise-creating fluid pressure oscillations in the venturi interior, thereby desirably lessening the operational sound level of the primary fuel/air mixing structure 14. Moreover, the enhanced mixing of the fuel/air mixture to be combusted desirably reduces the level of NOx emissions created by the furnace 12 during firing thereof.
As may best be seen in
With reference now to
Accordingly, during firing of the furnace 12, the presence of the diffuser plate 64 lessens the flow of hot combustion gas 82 through the central heat exchanger tubes 20b and increases the flow of hot combustion gas 82 through the end heat exchanger tubes 20a, with the perforation pattern in the diffuser plate 64 functioning to substantially alleviate non-uniform temperature distribution across the heat exchanger tube array that might otherwise occur. As can readily be seen, principles of the present invention provide a simple and quite inexpensive solution to the potential problem of non-uniform temperature distribution across the heat exchanger tube array. Additionally, in developing the present invention it has been discovered that the use of the non-uniformly perforated diffuser plate 64 also provides for further mixing of the fuel/air mixture 80 entering the burner box housing 62, thereby providing an additional beneficial reduction in the NOx level of the discharged combustion gas 82a.
While a particular hole pattern in the diffuser plate has been representatively described herein, it will be readily appreciated by those of ordinary skill in this particular art that a variety of alternative hole patterns and sizes may be alternatively be utilized if desired. For example, while a combination of different size perforation has been representatively illustrated and described, the perforations could be of uniform size but with more perforations/area being disposed on the opposite ends of the diffuser plate 64 than in the longitudinally intermediate portion thereof. Further, the hole pattern could be a non-uniformly spaced pattern to suit the particular application. Additionally, if desired, the diffuser plate hole pattern could have a different overall configuration operative to alter in a predetermined, different manner the relative combustion gas flow rates through selected ones of the heat exchanger tubes 20.
While principles of the present invention have been representatively illustrated and described herein as being incorporated in a fuel-fired air heating furnace, a combustion system utilizing such invention principles could also be incorporated to advantage in the combustion systems of a wide variety of other types of fuel-fired heating apparatus using fire tube-type heat exchangers to heat either a gas or a liquid.
The foregoing detailed description is to be clearly understood as being given by way of illustration and example only, the spirit and scope of the present invention being limited solely by the appended claims.
The present application claims the benefit of the filing date of provisional U.S. patent application No. 61/883,031 filed Sep. 26, 2013. The entire disclosure of the provisional application is hereby incorporated herein by this reference.
Number | Name | Date | Kind |
---|---|---|---|
3181646 | Edwards | May 1965 | A |
3701481 | Reichmann et al. | Oct 1972 | A |
3888018 | Gaski, Jr. | Jun 1975 | A |
4762530 | Koziol | Aug 1988 | A |
4773384 | Koziol | Sep 1988 | A |
4805587 | Schweitzer | Feb 1989 | A |
5127824 | Barker | Jul 1992 | A |
5240411 | Abalos | Aug 1993 | A |
5291875 | Koziol | Mar 1994 | A |
5460512 | Lifshits et al. | Oct 1995 | A |
5791137 | Evans et al. | Aug 1998 | A |
6022213 | Harthun | Feb 2000 | A |
20020166553 | Topp | Nov 2002 | A1 |
20040121697 | Kojima | Jun 2004 | A1 |
20040250810 | Schultz | Dec 2004 | A1 |
20050106517 | Okada | May 2005 | A1 |
20110104622 | Sherrow | May 2011 | A1 |
20110220847 | Hendershot | Sep 2011 | A1 |
20130213379 | Schultz | Aug 2013 | A1 |
20140202443 | Sherrow | Jul 2014 | A1 |
Entry |
---|
International Search Report and Written Opinion issued for PCT/US2014/055381 dated Dec. 16, 2014, 13 pgs. |
Number | Date | Country | |
---|---|---|---|
20150086934 A1 | Mar 2015 | US |
Number | Date | Country | |
---|---|---|---|
61883031 | Sep 2013 | US |