This application is directed, in general, to heating, ventilation and air conditioning (HVAC) systems and, more specifically, to a gas furnace that comprises a clamshell heat exchanger having reduced plastic strain.
A conventional gas furnace typically employs several heat exchangers, which form a heating zone to warm an air stream passing through the furnace. An 80% furnace is one where approximately 80% of the energy put into the furnace is converted into heat for the purposes of heating the targeted space. These 80% furnaces include “clamshell” or individual panel halves typically formed by stamping mirror images of the combustion chambers into corresponding metal sheets and coupling them together. The air passes through the heating zone from a blower or fan. These 80% furnaces are also characterized by high operating temperatures, which can cause failure within the heating chamber. As a result, hot spots can occur at certain points in the passageway of the clam shell heat exchanger. The high operating temperatures that create these hot spots can create cracking problems, often referred to as “hot cracks” in the clamshell heat exchanger panels. When such cracks appear, their occurrence is considered a failure of the system. To circumvent these problems, some manufacturers have turned to more expensive sheet metal materials, such as Drawing Quality High Temperature (DQHT) sheet metal materials.
One aspect of this disclosure provides a gas furnace, comprising a housing, a heating zone located in the housing and comprising one or more clamshell heating chambers. The one or more clamshell heating chambers comprise opposing halves joined together and the joined opposing halves form a clamshell panel having at least one truncated corner located adjacent a curve in a backend of a chamber path of the one or more clamshell heating chambers. The gas furnace further comprises a blower having an exhaust opening and located adjacent the heating zone and positioned to force air through the heating zone.
Another embodiment provides a heating chamber for a gas furnace that comprises opposing halves joined together. The joined opposing halves form a clamshell panel having at least one truncated corner located adjacent a curve located at a back end of a chamber path of the one or more clamshell heating chambers.
A method of fabricating a gas furnace is also provided. One method embodiment comprises forming opposing halves of a heating chamber, joining the first and second opposing halves to form a clamshell panel, and forming at least one truncated corner located adjacent a curve at a backend of a chamber path of the clamshell panel.
Reference is now made to the following descriptions taken in conjunction with the accompanying drawings, in which:
Described herein are various embodiments of an improved clamshell heating chamber that can be employed in a gas furnace. The present disclosure is based on the discovery that failures typically not only occur in the form of cracks in hot spots (e.g., temperatures of about 1000 degrees), which are known as “hot cracks,” but failure also occurs near relatively cooler spots (e.g. temperatures of about 600 degrees), which are known as “cold cracks” and are the result of high plastic strain within the clamshell panel. The plastic strain is an important variable to the thermal loading, which causes fatigue and cracking failure. The present disclosure recognizes that the plastic strain can be reduced by modifying the existing clamshells by truncating the corner adjacent a cold crack region. Cold crack regions are of particular concern because the hot crack regions can be addressed with baffling or other known solutions that work in view of the higher operating temperatures in that region. However, those techniques do not work well in the cold crack regions due to the relatively lower operating temperatures in those particular regions of the heating chamber.
In one embodiment, at least one of the corners of the clamshell panel is truncated at a specific location near a known cold crack region, which often occurs in a bend or curve in the chamber path located near the back end of the clamshell panel. The cold cracks occur as the result of the deformation, which is caused by thermal expansion, of the female panel (outer panel) imposing a pulling force on the joined male panel (inner panel). However, when the corner of the clamshell panel is truncated by either forming it at an angle of less than 90 degrees or bending the corner in a generally vertical direction along that same angle, the female panel imposes less pulling force on the male panel, and thus reduces the plastic deformation on the male panel. The angle of and distance from the corner near the cold crack region also enhances the benefits associated with the truncation configuration. It has been observed that improved results can be obtained when the truncation is located a distance of 0.0 inches to about 0.50 inches from the line of the cold crack region at the bend or curve of the heating chamber passageway. The angle of the truncation also plays a roll on the plastic stress reduction. The beneficial effects can be obtained from a truncation angle that ranges from about 30 degrees to about 75 degrees. In one specific embodiment, the truncation distance may be about 0.30 inches and at an angle of 60 degrees.
In another embodiment, the corner truncation is effected by bending the corner of the clamshell panel at the desired angle and distance. In such embodiments, about a 30 degree about a 75 degree bend angle near the cold crack area tangent to the curved profile line was found to decrease the plastic strain by imposing pre-compressive stress to act against the thermal tensile stress. In one aspect of this embodiment, at a distance of about 0.30 inches, the angle requirement is about 60 degrees to obtain similar results to that of the previous embodiment.
The heating chambers of 80% gas furnaces have higher surface temperatures at maximum leaving air conditions, which is typically more than 1000° F. At this temperature, a low strength steel (extra deep drawing steel known as EDDS), which is the material of choice for many manufactures, will not survive the required reliability tests. To circumvent these problems, some manufactures turn to more expensive DQHT materials or tolerate a shorter operational life of the furnace. However, given the industry drive to reduce manufacturing costs, it is desirable to use the less costly EDDS material.
To use EDDS material in current 80% gas furnace designs, it is necessary to reduce the cracking attributable to the cold crack effect. Embodiments of the clamshell configuration, as presented herein, have been found to significantly reduce the cold crack effects, even when using less costly EDDS materials.
In general, the various embodiments of the clamshell design, as provided herein, reduces the plastic strain of the clamshell panel, thereby reducing the cold cracking that often occurs in conventional designs. Without being limited by any theory of operation, it is believed that the truncated corner, which may be achieved by stamp cutting the panels of the clamshell to the appropriate angle, trimming a corner of the panel, or by bending a corner to the appropriate angle, achieves a reduction in plastic strain. The strain reduction is achieved by reducing the amount of pulling force of the female portion of the panel exerted on the male portion of the panel in the region of the cold crack area, thereby reducing cracks that occur as the result of higher plastic strain, even where EDDS type materials are used. This advantage allows manufacturers to use the cheaper construction materials without sacrificing operational while at the same time reducing manufacturing costs.
Though the clamshell heating chamber, as presented herein, could be used in any furnace chamber, it provides particular benefits when employed in gas furnaces where 80% of the total amount of fuel used is converted directly into heat. The benefits arise from the fact that these gas furnaces reach high operational temperatures, which cause the heating chambers to prematurely stress and crack at the above-mentioned areas.
A burner assembly 140 contains a thermostatically-controlled solenoid 142, a manifold 144 leading from the valve 142 and across the burner assembly 150, one or more gas orifices (not shown) coupled to the manifold 144 and one or more burners (not shown) corresponding to and located proximate the gas orifices. The illustrated embodiment of the burner assembly 140 has a row of six burners. Alternative embodiments of the burner assembly 140 have more or fewer burners arranged in one or more rows. A flue 146 allows undesired gases (e.g., unburned fuel) to be vented from the burner assembly 140. In an assembled configuration, the burner assembly 140 is located proximate the heat exchanger assembly 120 such that the burners thereof at least approximately align with the inlets 132.
A draft inducer assembly 150 contains a manifold 152, a draft inducing exhaust fan 154 having an inlet coupled to the manifold 152 and a flue 156 coupled to an outlet of the exhaust fan 154. In an assembled configuration, the draft inducer assembly 150 is located proximate the heat exchanger assembly 120, such that the manifold 152 thereof at least approximately aligns with the outlets 134 and the flue 156 at least approximately aligns with the flue 146 of the burner assembly 140.
A blower 160 is suspended from the shelf 110 such that an outlet 162 thereof approximately aligns with the opening 115. An electronic controller 170 is located proximate the blower 160 and, in the illustrated embodiment, controls the blower, the valve 142 and the exhaust fan 154 to cause the furnace to provide heat. A cover 180 may be placed over the front opening 105 of the housing 100.
In the illustrated embodiment, the controller 70 turns on the exhaust fan to initiate a draft in the heat exchangers in the heating zone 130 and purge potentially harmful unburned gases or gaseous combustion products. Then the controller 170 opens the valve 142 to admit gas to the manifold 144 and the one or more gas orifices, whereupon the gas begins to mix with air to form primary combustion air. Then the controller 170 activates an igniter (not shown in
One benefit of the present disclosure is that due to the advantages of the present disclosure, less costly sheet metal materials, such as EDDS metal, can be used in the construction of the heating chamber panel 202 in place of more expensive materials. The presence of the truncated corner 205a provides a reduction in the plastic strain that occurs in cold crack regions, such as those that occur in the curved area 206 of the heating chamber panel 202. The reduction in the plastic strain results in less cold cracks developing in the relatively cooler portions of the heating chamber panel 202. The degree of the angle 209 may vary depending on the embodiment. For example, the angle 209 as taken from a line of an adjacent edge 210 of the heating chamber panel 202 may range from about 30 degrees to about 75 degrees. In one aspect of this embodiment, the angle may be about 60 degrees. At this angle, finite element analysis FEA) showed an improvement wherein the total plastic strain was reduced to about 0.002794, as compared to a total plastic strain of 0.007117 in conventional configurations using an EDDS material.
The distance of the truncation from the curve 206 in the chamber path also affects reduction in the plastic strain. For example, in one embodiment, the distance from an edge 215 of the truncated corner 205a to an edge 220 of the curve 206 may range from about 0.0 inches 0.50 inches. In one aspect of this embodiment, at a distance of about 0.30, the FEA showed an improvement, wherein the total plastic strain was about 0.002794, as compared to conventional total plastic strains of 0.007117 in which EDDS materials were used. In another aspect, the angle is about 60 degrees and the distance from the curve 206 is about 0.30 inches, which resulted in the above-noted improvement. Additionally, an improvement over conventional heating panels using an EDDS material was also indicated at distances of about 0.50 inches (e.g. 0.4375 inches).
One benefit of this embodiment is that due to the advantages of the present disclosure, less costly sheet metal materials, such as EDDS metal, can be used in the construction of the heating chamber panel 302 in place of more expensive materials. The presence of the truncated corner 305a provides a reduction in the plastic strain that occurs in cold crack regions, such as those that occur in the curved area 306 of the heating chamber panel 302. In those embodiments where the angle 309 was 60 degrees and angle 312 ranged from about 10 degrees to about 15, FEA showed an improvement wherein the total plastic strain was reduced to about 0.002794, as compared to a total plastic strain of 0.007117 in conventional configurations using an EDDS material.
The distance from the curve 306 in the chamber path also affects reduction in the plastic strain. For example, in one embodiment, the distance from an edge 315 of the truncated corner 305a to an edge 320 of the curve 306 may range from about 0.0 inches 0.50 inches. In one aspect of this embodiment, at a distance of about 0.30 and an angle 309 of 60 degrees, the FEA showed an improvement, wherein the total plastic strain was about 0.002794, as compared to conventional total plastic strains of 0.007117 in which EDDS materials were used. Additionally, an improvement over conventional heating panels using an EDDS material was also indicated at distances of about 0.50 inches (e.g. 0.4375 inches).
With reference to
In those embodiments, where the truncation is achieved by bending the corner 205, 305, the step of bending includes bending the corner along a line separated from the chamber path 206, 306 by a distance that ranges from about 0.0 inches to about 0.30 inches. Further, an angle of the bending taken from a bottom plane 312 of the first opposing halve ranges from about degrees to about 15 degrees. In one aspect of this embodiment, the distance of the bend line from the chamber path is about 0.30 inches and the angle from the line taken from an adjacent edge is about 60 degrees.
Those skilled in the art to which this application relates will appreciate that other and further additions, deletions, substitutions and modifications may be made to the described embodiments.
This application is a continuation of U.S. patent application Ser. No. 13/715,268, filed on Dec. 14, 2012. U.S. patent application Ser. No. 13/715,268 is incorporated herein by reference.
Number | Name | Date | Kind |
---|---|---|---|
2762612 | Druseikis | Sep 1956 | A |
2796860 | Pinkus et al. | Jun 1957 | A |
2963083 | Speith et al. | Dec 1960 | A |
3073296 | Hollingsworth et al. | Jan 1963 | A |
3140706 | Block et al. | Jul 1964 | A |
3871354 | Jackson et al. | Mar 1975 | A |
3916870 | Beavers | Nov 1975 | A |
4982785 | Tomlinson | Jan 1991 | A |
5060722 | Zdenek et al. | Oct 1991 | A |
5146910 | Grahl | Sep 1992 | A |
5309892 | Lawlor | May 1994 | A |
5347981 | Southern et al. | Sep 1994 | A |
5542470 | Evens | Aug 1996 | A |
5704343 | Ahn et al. | Jan 1998 | A |
5799646 | Zia et al. | Sep 1998 | A |
6257870 | Hugghins et al. | Jul 2001 | B1 |
6938688 | Lengauer, Jr. et al. | Sep 2005 | B2 |
8261733 | Hugghins | Sep 2012 | B2 |
20110174291 | Manohar et al. | Jul 2011 | A1 |
20110174299 | Zimmer | Jul 2011 | A1 |
20120297337 | St. Denis et al. | Nov 2012 | A1 |
20120325445 | Dinulescu | Dec 2012 | A1 |
Number | Date | Country | |
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20190056144 A1 | Feb 2019 | US |
Number | Date | Country | |
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Parent | 13715268 | Dec 2012 | US |
Child | 16167735 | US |