Patent Application
20110146594
1. Field of the Invention
The present invention relates generally to apparatus for heating water or the like, and more particularly, to the construction of heat exchange tubes of the type which carry hot combustion gases therethrough for heat exchange with water or the like flowing around the outside of the tube.
2. Description of the Prior Art
Traditionally heat exchangers, particularly condensing fire tube heat exchangers, have utilized a tube bundle made up of a plurality of relatively small diameter cylindrical tubes extending between an inlet tube sheet and an outlet tube sheet. Typically those tubes have been of a diameter in the range of from ½ to ¾ of an inch. This has required the use of a large number of tubes within a tube bundle to achieve the necessary heat exchange between hot combustion gases and the water or other fluid flowing around the tubes. The use of relatively large numbers of relatively small diameter tubes leads to a substantial effort and expense in welding all of the tubes in place within their respective tube sheets.
There is a need for improved designs for the heat exchange tubes for fire tube heat exchangers.
In one embodiment a fire tube heater apparatus includes a shell, a tube bundle received in the shell and having an inlet tube sheet and an outlet tube sheet, and a plurality of heat exchange tubes extending between the inlet and outlet tube sheets. A burner section is communicated with the inlet tube sheet so that hot gas from the combustion chamber of the burner section enters the heat exchange tubes at the inlet tube sheet. Each of the heat exchange tubes includes a circular inlet end and a circular outlet end. The inlet end has an inlet outside diameter. Each tube includes a flattened intermediate portion having a tube width greater than the inlet outside diameter and having a tube thickness transverse to the width and less than the inlet outside diameter. The flattened intermediate portion includes generally parallel first and second opposed walls spanning the width of the intermediate portion. The first and second opposed walls each include at least one longitudinally extending inwardly protruding rib. The at least one rib of the first wall is opposed to and protrudes toward the at least one rib of the second wall to form at least one pair of opposed ribs separated by a gap so that upon application of external pressure to the tube the at least one pair of opposed ribs may move toward and engage each other to limit deformation of the intermediate portion due to such external pressure.
In another embodiment a fire tube boiler apparatus includes a burner section for providing a heat input of at least 1.5 million BTU. The apparatus includes a tube bundle including a plurality of fire tubes for conducting hot burner gases therethrough from the burner section. The plurality of fire tubes includes between 30 and 60 fire tubes, each tube having a heat transfer capacity in the range of from 25,000 BTU to 50,000 BTU.
In another embodiment a heater tube apparatus includes a cylindrical inlet end portion having an outside diameter and a cylindrical outlet end portion. A serpentine intermediate portion is located between the end portions. The intermediate portion has a width greater than the outside diameter of the inlet portion and has a thickness transverse to the width less than the outside diameter of the inlet portion.
Numerous objects, features and advantages of the present invention will be readily apparent to those skilled in the art upon a reading of the following disclosure when taken in conjunction with the accompanying drawings.
Referring now to the drawings, and particularly to
The water heating apparatus 10 illustrated in
The water heating apparatus 10 shown in
The apparatus 10 includes an outer jacket or shell 24. The water inlet 12 and water outlet 14 communicate through the jacket 24 with a water chamber 26 or water side 26 of the heat exchanger. In an upper or primary heat exchanger portion 28, an inner heat exchange wall or inner jacket 30 has a combustion chamber or combustion zone 32 defined therein. The lower end of the combustion chamber 32 is closed by an upper tube sheet 34. A plurality of fire tubes 36 have their upper ends connected to upper tube sheet 34 and their lower ends connected to a lower tube sheet 38. The fire tubes extend through a secondary heat exchanger portion 40 of the heat exchanger apparatus 10. The tube sheets 34 and 38, and tubes 36, comprise a tube bundle 37.
A burner assembly or burner apparatus 42 is located within the combustion chamber 32. The burner assembly 42 burns premixed fuel and air within the combustion chamber 32. The hot gases from the combustion chamber 32 flow down through the fire tubes 36 to an exhaust collector 44 and out an exhaust flue 46. The burner 42 and combustion chamber 32 comprise a burner section 43.
Water from flow loop 16 to be heated flows in the water inlet 12, then around the exterior of the fire tubes 36 and up through a secondary heat exchanger portion 48 of water side 26, and continues up through a primary heat exchanger portion 50 of water side 26, and then out through water outlet 14. It will be appreciated that the interior of the apparatus 10 includes at least one baffle, along with the unique orientation of the tubes as shown for example in
Referring again to
The first blower assembly 52 includes a variable flow blower 56 driven by a variable frequency drive motor. A venturi 58 is provided for mixing combustion air and fuel gas. An air supply duct 60 provides combustion air to the venturi 58. A gas supply line 62 provides fuel gas to the venturi 58. A gas control valve 64 is disposed in supply line 62 for regulating the amount of gas entering the venturi 58. The gas control valve 64 includes an integral shutoff valve. In some embodiments the gas control valve and the venturi may be combined into a single integral unit. The gas control valve is preferably a zero governor modulating gas valve for providing fuel gas to the venturi 58 at a variable gas rate which is proportional to the negative air pressure within the venturi caused by the speed of the blower, hence varying the flow rate entering the venturi 58, in order to maintain a predetermined air to fuel ratio over the flow rate range within which the blower 56 operates. In order to provide the variable input operation of the burner assembly 42, the variable flow blower 56 delivers the premixed combustion air and fuel gas to the burner assembly 42 at a controlled blower flow rate within a first blower flow rate range extending from a first range low end to a first range high end. Thus the first blower assembly 52 has a first turndown ratio at least equal to the first range high end divided by the first range low end.
Similarly, the second blower assembly 54 includes variable speed blower 66, venturi 68, air supply duct 70, gas supply line 72 and gas valve 74. The second blower assembly 54 supplies premixed fuel and air to the burner assembly 42 and has a second flow rate range extending from a second range low end to a second range high end so that the second blower assembly has a second turndown ratio equal to the second range high end divided by the second range low end.
Referring now to
A blower transition manifold 79 is attached to the header wall 78 and connects the outlets of blower assemblies 52 and 54 to the burner assembly 42. Via manifold 79 the first blower 56 is communicated with first plenum 82, and second blower 66 is communicated with second plenum 84.
A duct 91 extends between divider wall 80 and header wall 78 and extends upward into the manifold 79. Duct 91 is welded or otherwise attached to header wall 78 and divider wall 80. The lower end of duct 91 communicates through opening 93 in divider wall 80 with the second zone 84, and defines a passage communicating second blower 66 with second zone 84.
The burner apparatus 42 further includes an upper collar 95 attached to and extending downward from header wall 78. A perforated cylindrical support screen 97 is attached to collar 95 and divider wall 80. A lower support ring 99 is received in the lower end of support screen 97. A flat lower burner screen 101 is attached to and spans across ring 99. The header wall 78, neck 95, duct 91, divider wall 80, support screen 97, support ring 99, and bottom screen 101 are all preferably constructed of metal and welded together to form a structural skeleton of the burner assembly 42.
A foraminous outer sock is received about the cylindrical screen 97 and bottom screen 101 and held in place by a retaining band. First and second foraminous outer wall portions of the sock are located adjacent the first and second interior zones 82 and 84, respectively.
Additional details of construction of the heater apparatus 10 and particularly of the blowers, intake manifold 79 and control system for the heater apparatus 10, are set forth in U.S. patent application Ser. No. 12/252,841 filed Oct. 16, 2008 by Jim C. Smelcer and entitled “Gas Fired Modulating Water Heating Appliance With Dual Combustion Air Mix Blowers”, the details of which are incorporated herein by reference.
The details of construction of the heat exchange tubes 36 are best shown in
The tube 36, as further described below, may be formed from cylindrical round wall tubing stock which is stamped to deform the intermediate portion into the shape as shown. This results in tapered transition portions 206 and 208 which join the inlet and outlet portions 200 and 202, respectively, to the intermediate portion 204. The inlet and outlet portions 200 and 202 have outside diameters 210 and 212, respectively, which may be substantially equal to each other and which may be substantially equal to the outside diameter of the tubing stock from which the heat exchange tube 36 is formed.
The tube has an overall length 214 from its inlet end 216 to its outlet end 218. The serpentine flattened intermediate portion 204 has a length 220. The intermediate portion 204 has an inlet width 222 and an outlet width 224. The width of the intermediate portion 204 may increase from the inlet width 222 to the outlet width 224.
The intermediate portion 204 also has a thickness transverse to its width, which thickness may decrease from its inlet thickness 226 shown in
In general, the intermediate portion 204 can be described as having a width greater than the outside diameter 210 of the cylindrical inlet portion 200 of the tube, and having a thickness transverse to the width less than the outside diameter 210 of the inlet portion of the tube.
The tube 36 may be designed so that the internal cross-sectional area generally shown at 230 in
As is best appreciated in viewing the edgewise view of
In one embodiment the wavelength 234 may be in the range of from about 1.0 to about 2.0 times the greatest width 224 of the intermediate portion 204, and the height 240 may be less than a greatest thickness 226 of the intermediate portion 204.
In another embodiment the height 240 may be in the range of from about 0.05 to about 0.20 times the maximum width 244 of the intermediate section.
In one embodiment the peak to trough height 240 may be substantially the same for all of the undulations.
In an embodiment, the wavelength 234 may be substantially the same for all of the undulations, but it need not be for all embodiments.
The undulating shape having dimensions generally like those just described may be described as a gentle undulating shape having relatively shallow gradual curves or directional changes. This shape provides multiple important functions. One purpose of the undulating shape is to cause gradual gentle directional changes for the hot gases flowing therethrough so as to provide improved heat transfer as compared to that which would be achieved with a straight tube. These shallow curves provide enough flow disruption for good heat exchange, but not so much as to cause excessive pressure drop.
Another purpose of the undulating shape is that it allows the tube to flex when subjected to thermal changes which would otherwise cause the tube to attempt to contract or expand its length. This provides a relatively stress free tube construction which does not impose substantial thermal stresses on the locations where the tubes are welded to the tube sheets. Thus lengthwise stresses imposed upon the tube by thermal changes are accommodated by resilient bending of the undulating shape.
Although the undulating shape is generally describable as a series of shallow curves, the shape may be formed by forming a series of generally straight sections which may for example include a repeating series made up of a longitudinally oriented first section 270, an inclined second section 272, a longitudinally oriented third section 274, and an inclined fourth section 276 inclined in a direction oppositely from that of the second section 272.
In an embodiment the tubes 36 are designed with an overall length 214 of no greater than 50 inches in order to provide an overall height of the apparatus 10 which could be utilized in typical boiler rooms of buildings.
In one embodiment the outside diameters 210 and 212 may be in the range of from about 2.0 to about 3.0 inches, and in another embodiment the outside diameters may be approximately 2.5 inches.
In an embodiment the widths 222 and 224 may be generally in the range of from about 3.0 to about 4.0 inches.
In an embodiment the thicknesses such as 226 and 228 may be in the range of from about 0.25 to about 1.0 inch.
In one embodiment such as shown in
In another embodiment, as illustrated in
As shown in the cross-sectional view of
As is apparent in viewing
The ribs may serve multiple purposes. One purpose is to provide structural reinforcement to the cross-sectional shape of the intermediate portion 204, so that thinner wall tube materials can be used while providing structural strength equivalent to a thicker wall tube without ribs. As will be appreciated by those skilled in the art, many water heater apparatus such as the apparatus 10 are required to pass tests specified in certain design codes such as for example the ASME boiler code, which requires structures such as the heat exchange tube 36 to pass external pressure tests. These pressure tests may require that upon the application of an external proof test pressure of for example 480 psi the structure does not undergo any substantial permanent deformation.
Another purpose of the inwardly protruding ribs is to provide additional flow disruption for improved heat transfer purposes.
In one embodiment, the tube 36 having the longitudinal ribs such as illustrated in
In the embodiment shown in
In one embodiment, each of the heat exchange tubes 36 may have a heat exchange capacity in the range of from about 25,000 BTU to about 50,000 BTU, and more particularly in a range of from about 30,000 BTU to about 40,000 BTU and most particularly having a heat exchange capacity of approximately 35,000 BTU. Such heat exchange capacities may be achieved at a tube inlet temperature of approximately 2200° F., a tube outlet temperature range of approximately 200-225° F., and a water exit temperature range of approximately 210-250° F.
An example of a tube 36 having a heat exchange capacity of approximately 35,000 BTU is as follows. The tube may be formed from 2.5 inch diameter 316L stainless steel tubing having a wall thickness of about 0.065 inch. The tube length 214 may be about 49 inches, and the length 220 of the intermediate portion may be about 42.5 inches. The intermediate portion may have a total of eight undulations having wavelength 234 of about 5.1 inches, and having a height 240 of about 0.39 inch. The thickness 226,228 of the intermediate portion may taper from about 0.551 inch to about 0.405 inch. The inlet end width 222 of the intermediate portion may be about 3.485 inches and the outlet end width 224 may be about 3.568 inches.
When such a tube design has been provided, the same dimension tube may be utilized for heat exchangers of different capacities by providing different numbers of tubes in the tube bundle. For example, utilizing a heat exchanger tube 36 having a heat transfer capability of 35,000 BTU, a water heater 10 having a capacity of 1.5 million BTU may include approximately 43 such tubes. Similarly, a heat exchanger having a capacity of 2.0 million BTU may include approximately 57 such tubes. Similarly, a heat exchanger having a capacity of 2.5 million BTU may include approximately 72 such tubes. Similarly, a heat exchanger having a capacity of 3.0 million BTU may include approximately 86 such tubes. Similarly, a heat exchanger having a capacity of 3.5 million BTU may include approximately 100 such tubes.
For example,
More generally, for a boiler providing a heat capacity of about 1.5 million BTU, the tube bundle may include between 30 and 60 fire tubes, each tube having a heat transfer capacity in a range of from 25,000 BTU to 50,000 BTU.
The tubes 36 may be formed by liquid impact forming. In a first step a dry cylindrical tube is stamped between two forms to achieve about 75% of the required deformation. Then in a second step the partially formed tube is filled with water and connected to a pressure relief valve to limit internal pressure. The water filled partially formed tube is then stamped between two forms a second time to achieve the final deformation.
Several advantages are provided by the heat exchange tube construction disclosed herein as contrasted to the use of cylindrical heat exchange tubes.
One advantage is that the use of relatively large diameter tubes having an outside diameter of their inlet and outlet ends in the range of from 2 to 3 inches requires much less set up time for welding of tubes to tube sheets as compared to an equivalent capacity heat exchanger utilizing cylindrical tubes having outside diameters of from ½ to ¾ inch.
Another advantage is that due to the much larger flow capacity of these larger diameter tubes, there is significantly less pressure drop through the tubes, and thus much smaller blowers are required for the heater. For example the tube 36 may have a pressure drop of approximately two inches of water, whereas a conventional one-half inch diameter cylindrical fire tube may have a pressure drop in the range of 7 to 10 inches of water.
Also, due to the much larger physical size of the inlet ends of the tubes, the high temperature combustion gases entering those tubes can dissipate their heat much more readily through the ratio of increased surface area of the large tubes in contact with the water backed medium for the intended loading, and thus the inlet ends of the tubes operate at considerably lower operating pressures thus aiding the life of the tubes.
Another advantage of the serpentine tube design is that it accommodates the operation of the heater apparatus 10 in a condensing mode where water vapor from the hot combustion gases condenses into liquid form within the tubes 36. As the hot combustion gases flow downward through the tubes 36 the gases become cooler. At some point, perhaps half way down the length 214 of the tube 36, water vapor may begin to condense on the inside of the tubes. This liquid water must be carried downward through the tubes. In a non-serpentine tube such water vapor will tend to flow in a wicking manner in a film downward along the inside walls of the tube thus significantly decreasing the available flow area for the hot gases and thereby increasing the pressure drop through the tube. Also the presence of a water layer on the inside of a non-serpentine tube may decrease heat transfer from the lower portions of the tube. The serpentine shaped tube 36, on the other hand, causes the condensate to be in more of a dripping state rather than a wicking state, so that the hot combustion gases still engage the interior walls of the lower portions of the tube and the drops of condensate tend to be entrained in the downwardly flowing gases rather than clinging to the walls. The undulations provide alternating flow disruptions extending transverse to the tube length, so that downward flow of condensed water within the tubes is disrupted to reduce wicking flow of water on the inside surfaces of the tube walls. This reduces the pressure drop through the tubes and increases the heat transfer from the lower portions of the tubes as compared to tubes without the undulations provided by the serpentine shape.
Thus it is seen that the apparatus of the present invention readily achieve the ends and advantages mentioned as well as those inherent therein. While certain preferred embodiments of the invention have been illustrated and described for purposes of the present disclosure, numerous changes in the arrangement and construction of parts may be made by those skilled in the art, which changes are encompassed within the scope and spirit of the present invention as defined by the appended claims.
