Not Applicable
Not Applicable
This invention relates to the field of heat exchangers, and more particularly to a heat exchanger with metal tubes, a plastic main shell extrusion, and plastic manifolds.
In marine applications, a heat exchanger is used to cool the engine. The space available for installation of a heat exchanger is limited, due to engine compartment configurations. Typically, the space is adequate in length fore-and-aft, and in height, but limited in width transversely. Heat exchangers in the prior art are housed in either a circular cylinder or a flat plate box. A circular cylinder of adequate,capacity will not fit into the limited space. The pressure inside the cooling system is about 15 psi. A flat plate of only 12 by 24 inches will develop 4320 lbs of force under 15 psi. A flat-sided box will not withstand the pressure. Other considerations in a marine system are corrosion due to electrolysis, and fouling by marine organisms such as mussels, barnacles, algae, and weeds.
Plastic heat exchangers are known, and have taken a variety of configurations in the past. Some examples of plastic heat exchangers in the art are found in these patents:
Heier, U.S. Pat. No. 6,929,060; shows metal tubes mounted into a plastic manifold. The enclosure is flat-sided.
Stafford, U.S. Pat. No. 4,323,115; discloses a shell and tube heat exchanger with metal tubes set into plastic sheets. The enclosure is cylindrical.
Baker, U.S. Pat. No. 3,363,680; illustrates a shell and tube heat exchanger with plastic tubes. The enclosure is cylindrical.
Humpolik, U.S. Pat. No. 4,576,223; shows metal tubes mounted into a plastic sheet and plastic manifold. The enclosure is flat-sided.
Accordingly, there is a need to provide a heat exchanger that can provide significant capacity within a limited width space.
There is a further need to provide a heat exchanger of the type described and that can withstand at least fifteen pounds per square inch internal pressure.
There is a yet further need to provide a heat exchanger of the type described and that will resist electrolytic corrosion in a salt-water environment.
There is a still further need to provide a heat exchanger of the type described and that will resist the growth of marine organisms.
There is another need to provide a heat exchanger of the type described and that can be manufactured cost-effectively in large quantities of high quality.
In accordance with the present invention, there is provided a plastic heat exchanger 30 is for transferring heat between a primary fluid coolant 32 and a secondary fluid coolant 34. The plastic heat exchanger 30 comprises a shell 36 with a plurality of tanks 42 disposed side-by-side. The first tank is a first distribution tank 44. The last tank is a last distribution tank 46. Intermediate the first and last tanks are heat transfer tanks 48, which are each attached to adjacent tanks 42 along opposite front 50 and rear 52 webs. The shell 36 has a plurality of flow gaps 58, to allow the primary fluid coolant 32 to flow from each tank to the adjacent tank. Each flow gap 58 is disposed between front 50 and rear 52 webs. The tanks 42 each communicate with adjacent tanks 42 through the flow gaps 58. The distribution tanks 44 and 46 are connected to the primary fluid coolant 32.
A plurality of spacers 59 is disposed in each flow gap 58 between a respective front 50 and rear 52 web to maintain the flow gaps 58 in an open condition.
An upper flange 60 is sealingly attached to the shell upper end 38 with an adhesive. The upper flange 60 has a plurality of flange holes 74, each in alignment with one of the tanks 42. Each flange hole 74 has an annular wall 76 adapted to encircle one of the tanks 42 to preclude the shell 36 from expanding outward under internal pressure.
A lower flange 96 is sealingly attached to the shell lower end 38 with an adhesive. The lower flange 96 has a plurality of flange holes 110, each in alignment with one of the tanks. Each flange hole 110 has an annular wall 112 adapted to encircle one of the tanks 42 to preclude the shell 36 from expanding outward.
An upper manifold 134 is disposed adjacent the upper flange 60. The upper manifold 134 has a plurality of chambers 152 disposed side-by-side. Each chamber 152 corresponds to a respective heat transfer tank 48. Each chamber 152 is in communication with the adjacent chamber 152. Each chamber 152 is separated from the adjacent chamber 152 by opposed front 154 and rear 156 channels. The upper manifold 134 is connected to the secondary fluid coolant 34.
A lower manifold 178 is disposed adjacent the lower flange 96. The lower manifold 178 has a plurality of chambers 196 disposed side-by-side. Each chamber 196 corresponds to a respective heat transfer tank 48. Each chamber 196 is in communication with the adjacent chamber 196. Each chamber 196 is separated from the adjacent chamber 196 by opposed front 198 and rear 200 channels. The lower manifold 178 is connected to the secondary fluid coolant 34.
At least one baffle 246 is adapted to be removably received in a pair of the opposed front 154 and rear 156 channels of the upper manifold 134, and in a pair of the opposed front 198 and rear 200 channels of the lower manifold 178. The baffles 246 are used to selectively block communication between the respective adjacent chambers 152 of the upper manifold 134, and between the respective adjacent chambers 196 of the lower manifold 178. A plurality of baffles 246 can be installed in selected channels in the upper 134 and lower 178 manifolds, to direct the flow of secondary fluid coolant 34.
An upper tube header 222 and a lower tube header 226 are provided. A plurality of generally straight and parallel tubes 230 extend between the upper 222 and lower 226 tube headers, and comprise a tube bundle 242. Each tube bundle 242 is removably received within one of the heat transfer tanks 48.
A header sealing means, header O-ring 244 is juxtaposed between each header 222 and 226, and the respective flange. An upper seal plate 248 is disposed against the upper flange 60. The upper seal plate 248 has an upper seal plate hole 262 for each heat transfer tank 48. Each upper seal plate hole 262 is juxtaposed in collinear alignment with one of the upper flange holes 74, defining an upper hole pair 264. Each upper hole pair 264 has at least one upper annular recess 266, forming an upper header O-ring groove 268 to receive the header O-ring 244. A manifold sealing means, upper seal 292 is juxtaposed between the upper manifold 134 and the upper seal plate 248.
A lower seal plate 270 is disposed against the lower flange 96. The lower seal plate 270 has a lower seal plate hole 284 for each heat transfer tank 48. Each lower seal plate hole 284 is juxtaposed in collinear alignment with one of the lower flange holes 74, defining a lower hole pair 286. Each lower hole pair 286 has at least one lower annular recess 288, forming a lower header O-ring groove 290 to receive the header O-ring 244. A lower seal 294 is juxtaposed between the lower manifold 178 and the lower seal plate 270.
The distribution tanks 44 and 46 are connected to the primary fluid coolant 32 by first 298 and second 312 flange connectors. A flange connector O-ring 296 is provided for rotatably sealing the first 298 and second 312 flange connectors to the flanges 60 and 96.
Two flange plugs 330 are provided to selectively block the flow of primary fluid coolant 32 a flange plug O-ring 340 is provided for sealing the flange plugs 330 to the flanges 60 and 96.
The upper 134 and lower 178 manifolds are connected to the secondary fluid coolant 34 by first 346 and second 360 manifold connectors. A manifold connector O-ring 374 is provided for rotatably sealing the first 346 and second 360 manifold connectors to the manifolds 134 and 178.
Two manifold plugs 380 are provided to selectively block the flow of secondary fluid coolant 34. A manifold plug O-ring 390 is provided for sealing the manifold plugs 380 to the manifolds 134 and 178.
The shell 36, manifolds 134 and 178, headers 222 and 226, and the flanges 60 and 96, are constructed of a non-metallic corrosion resistant polymeric material. The tubes 230 are constructed of metal materials having efficient heat transfer properties.
A more complete understanding of the present invention may be obtained from consideration of the following description in conjunction with the drawing, in which:
a is a partial, cross-sectional, elevational, perspective view of the plastic heat exchanger of
b is a partial, cross-sectional, elevational, perspective view of the plastic heat exchanger of
a is a partial, cross-sectional, elevational, detail view of the plastic heat exchanger of
b is a partial, cross-sectional, elevational, detail view of the plastic heat exchanger of
c is a partial, cross-sectional, elevational, detail view of the plastic heat exchanger of
d is a partial, cross-sectional, elevational, detail view of the plastic heat exchanger of
e is a partial, cross-sectional, elevational, detail view of the plastic heat exchanger of
f is a partial, cross-sectional, elevational, detail view of the plastic heat exchanger of
Referring now to the drawing, and especially to
A plurality of spacers 59 is disposed in each flow gap 58 between a respective front 50 and rear 52 web adjacent the web upper 56 and lower 54 ends. Additional spacers 59 can be inserted intermediate the web upper 56 and lower 54 ends, as shown in
An upper flange 60 is sealingly attached to the shell upper end 38 with an adhesive. The upper flange 60 extends between opposite first 62 and second 64 ends, and between opposite front 66 and rear 68 edges. The upper flange 60 has an outer surface 70 facing away from the shell 36 and an inner surface 72 facing toward the shell 36. The upper flange 60 has a plurality of flange holes 74. Each flange hole 74 is in alignment with one of the tanks 42 and extends through the upper flange 60 from the outer surface 70 to the inner surface 72. Each flange hole 74 has an annular wall 76 extending away from the inner surface 72. Each upper flange annular wall 76 is adapted to encircle one of the tanks 42 at the shell upper end 38. This will preclude the shell 36 from expanding outward under internal pressure. The upper flange 60 has an upper flange first receiver 78 adjacent the upper flange first end 62, and an upper flange last receiver 88 adjacent the upper flange second end 64. The upper flange first 78 and last 88 receivers are unitary, or one-piece, with the upper flange. The upper flange first receiver 78 has a central axis, and a boss 80 extending between a proximal end 82 at the flange outer surface 70 and a distal end 84. The upper flange first receiver 78 has a circular bore 86 passing through the boss 80 and is in communication with the first distribution tank 44. The upper flange last receiver 88 has a central axis, and a boss 90 extending between a proximal end 92 at the flange outer surface 70 and a distal end 94. The upper flange last receiver 88 has a circular bore 95 passing through the boss 90 and in is communication with the last distribution tank 46.
A lower flange 96 is sealingly attached to the shell lower end 38 with an adhesive. The lower flange 96 extends between opposite first 98 and second 100 ends, and between opposite front 102 and rear 104 edges. The lower flange 96 has an outer surface 106 facing away from the shell 36 and an inner surface 108 facing toward the shell 36. The lower flange 96 has a plurality of flange holes 110. Each flange hole 110 is in alignment with one of the tanks 42 and extends through the lower flange 96 From the outer surface 106 to the inner surface 108. Each flange hole 110 has an annular wall 112 extending away from the inner surface 108. Each lower flange annular wall 112 is adapted to encircle one of the tanks 42 at the shell lower end 38. This will preclude the shell 36 from expanding outward under internal pressure. The lower flange 96 has a lower flange first receiver 114 adjacent the lower flange first end 98, and a lower flange last receiver 124 adjacent the lower flange second end 100. The lower flange first 114 and last 124 receivers are unitary, or one-piece, with the lower flange 96. The lower flange first receiver 114 has a central axis, and a boss 116 extending between a proximal end 118 at the flange outer surface 106 and a distal end 120. The lower flange first receiver 114 has a circular bore 122 passing through the boss 116 and is in communication with the first distribution tank 44. The lower flange last receiver 124 has a central axis, and a boss 126 extending between a proximal end 128 at the flange outer surface 106 and a distal end 130. The lower flange last receiver 124 has a circular bore 132 passing through the boss 126 and is in communication with the last distribution tank 46.
An upper manifold 134 is disposed adjacent the upper flange 60. The upper manifold 134 has a front wall 136, a rear wall 138, a first end wall 140, and a second end wall 142. The walls extend between inner 144 and outer 146 edges. The upper manifold 134 has an outer plate 148 extending between the front 136 and rear 138 walls and between the first 140 and second 142 end walls along the outer edges 146 of the walls. The upper manifold 134 has a rim 150 extending around the inner edges 144 of the walls. The upper manifold 134 has a plurality of chambers 152 enclosed within the front 136 and rear 138 walls, the first 140 and second 142 end walls, and the outer plate 148. The chambers 152 are disposed side-by-side in an array that corresponds with the tank array. Each chamber 152 corresponds to a respective heat transfer tank 48. Each chamber 152 is in communication with the adjacent chamber 152. Each chamber 152 is separated from the adjacent chamber 152 by opposed front 154 and rear 156 channels. Each front channel 154 extends along the front wall 136 between the inner 144 and outer 146 edges. Each rear channel 156 extends along the rear wall 138 between the inner 144 and outer 146 edges. The upper manifold 134 is connected to the secondary fluid coolant system, so as to convey the secondary fluid coolant 34 between the secondary fluid coolant system and the heat transfer tanks 48. The upper manifold 134 has an upper manifold first receiver 158 adjacent the first end wall 140, and an upper manifold last receiver 168 adjacent the second end wall 142. The upper manifold first 158 and last 168 receivers are unitary, or one-piece, with the upper manifold 134. The upper manifold first receiver 158 has a central axis, and a boss 160 extending between a proximal end 162 at the upper manifold outer plate 148 and a distal end 164. The upper manifold first receiver 158 has a circular bore 166 passing through the boss 160 and in communication with one of the chambers 152, namely the first chamber in the array. The upper manifold last receiver 168 has a central axis, and a boss 170 extending between a proximal end 172 at the upper manifold outer plate 148 and a distal end 174. The upper manifold last receiver 168 has a circular bore 176 passing through the boss 170 and in communication with one of the chambers 152, namely the last chamber in the array.
A lower manifold 178 is disposed adjacent the lower flange 96. The lower manifold 178 has a front wall 180, a rear wall 182, a first end wall 184, and a second end wall 186. The walls extend between inner 188 and outer 190 edges. The lower manifold 178 has an outer plate 192 extending between the front 180 and rear 182 walls and between the first 184 and second 186 end walls along the outer edges 190 of the walls. The lower manifold 178 has a rim 194 extending around the inner edges 188 of the walls. The lower manifold 178 has a plurality of chambers 196 enclosed within the front 180 and rear 182 walls, the first 184 and second 186 end walls, and the outer plate 192. The chambers 196 are disposed side-by-side in an array that corresponds with the tank array. Each chamber 196 corresponds to a respective heat transfer tank 48. Each chamber 196 is in communication with the adjacent chamber 196. Each chamber 196 is separated from the adjacent chamber 196 by opposed front 198 and rear 200 channels. Each front channel 198 extends along the front wall 180 between the inner 188 and outer 190 edges. Each rear channel 200 extends along the rear wall 182 between the inner 188 and outer 190 edges. The lower manifold 178 is connected to the secondary fluid coolant system, so as to convey the secondary fluid coolant 34 between the secondary fluid coolant system and the heat transfer tanks 48. The lower manifold 178 has a lower manifold first receiver 202 adjacent the first end wall 184, and a lower manifold last receiver 212 adjacent the second end wall 186. The lower manifold first 202 and last 212 receivers are unitary, or one-piece, with the lower manifold 178. The lower manifold first receiver 202 has a central axis, and a boss 204 extending between a proximal end 206 at the lower manifold outer plate 192 and a distal end 208. The lower manifold first receiver 202 has a circular bore 210 passing through the boss 204 and in communication with one of the chambers 196, namely the first chamber in the array. The lower manifold last receiver 212 has a central axis, and a boss 214 extending between a proximal end 216 at the lower manifold outer plate 192 and a distal end 218. The lower manifold last receiver 212 has a circular bore 220 passing through the boss 214 and in communication with one of the chambers 196, namely the last chamber in the array.
At least one baffle 246 is adapted to be removably received in a pair of the opposed front 154 and rear 156 channels of the upper manifold 134. At least one baffle 246 is adapted to be removably received in a pair of the opposed front 198 and rear 200 channels of the lower manifold 178. The baffles 246 are used to selectively block communication between the respective adjacent chambers 152 of the upper manifold 134, and between the respective adjacent chambers 196 of the lower manifold 178. A plurality of baffles 246 can be installed in selected channels in the upper 134 and lower 178 manifolds, to direct the flow of secondary fluid coolant 34. The flow paths of the secondary fluid coolant 34 can be selected to control the heat transfer characteristics of the plastic heat exchanger. Some sample flow patterns are shown in
An upper tube header 222 is provided, and has an outer periphery 224. A lower tube header 226 is provided, and has an outer periphery 228. The upper 222 and lower 226 tube headers are spaced apart and generally parallel.
A plurality of generally straight and parallel tubes 230 extend between the upper 222 and lower 226 tube headers. The tubes 230 each have an outer surface 232 and a bore 234. The tubes 230 each have a tube wall 236 extending between the outer surface 232 and the bore 234. The tubes 230 each have upper 238 and lower 240 open ends attached to and penetrating the upper 222 and lower 226 tube headers, respectively.
The plastic heat exchanger 30 has a plurality of tube bundles 242, wherein the upper tube header 222, the lower tube header 226, and the tubes 250, comprise a tube bundle 242. Each tube bundle 242 is removably received within one of the heat transfer tanks 48. The upper tube header 222 of the tube bundle 242 is juxtaposed with the upper flange 60, and the lower tube header 226 is juxtaposed with the lower flange 96.
A header sealing means, header O-ring 244 is juxtaposed between each header 222 and 226, and the respective flange, for sealing the upper 222 and lower 226 tube headers against leakage. Any number of configurations of the O-ring installation is possible. In the preferred embodiment, an upper seal plate 248 is disposed against the upper flange outer surface 70. The upper seal plate 248 extends between opposite first 250 and second 252 ends, and between opposite front 254 and rear 256 edges. The upper seal plate 248 has an outer surface 258 facing away from the shell 36, and an inner surface 260 facing toward the shell 36. The upper seal plate 248 has an upper seal plate hole 262 for each heat transfer tank 48. Each upper seal plate hole 262 extends through the upper seal plate 248 from the outer surface 258 to the inner surface 260. Each upper seal plate hole 262 is juxtaposed in collinear alignment with one of the upper flange holes 74, defining an upper hole pair 264. Each upper hole pair 264 has at least one upper annular recess 266. Each upper hole pair 264 receives one of the upper tube headers 222 inserted into the hole pair 264. The upper tube header outer periphery 224 and the respective hole pair annular recess 266 defines an upper header O-ring groove 268. The header O-ring 244 is received in the upper header O-ring groove 268.
A lower seal plate 270 is disposed against the lower flange outer surface 106. The lower seal plate 270 extends between opposite first 272 and second 274 ends, and between opposite front 276 and rear 278 edges. The lower seal plate 270 has an outer surface 280 facing away from the shell 36, and an inner surface 282 facing toward the shell 36. The lower seal plate 270 has a lower seal plate hole 284 for each heat transfer tank 48. Each lower seal plate hole 284 extends through the lower seal plate 270 from the outer surface 280 to the inner surface 282. Each lower seal plate hole 284 is juxtaposed in collinear alignment with one of the lower flange holes 74, defining a lower hole pair 286. Each lower hole pair 286 has at least one lower annular recess 288. Each lower hole pair 286 receives one of the lower tube headers 226 inserted into the hole pair 286. The lower tube header outer periphery 228 and the respective hole pair annular recess 288 defines a lower header O-ring groove 290. The header O-ring 244 is received in the lower header O-ring groove 290.
A manifold sealing means, upper seal 292 extends around the upper manifold rim and is juxtaposed between the upper manifold rim 150 and the upper flange 60 for sealing the upper manifold 134 against leakage. Specifically, the upper seal is a gasket 292 or an O-ring (not shown). The upper seal 292 is disposed directly against the upper manifold rim 150 and the upper seal plate 248.
A lower seal 294 extends around the lower manifold rim 194 and is juxtaposed between the lower manifold rim 194 and the lower flange 96 for sealing the lower manifold 178 against leakage. Specifically, the lower seal is a gasket 294 or an O-ring (not shown). The lower seal 294 is disposed directly against the lower manifold rim 194 and the lower seal plate 270.
The upper 134 and lower 178 manifolds, and the upper 248 and lower 270 seal plates are secured to the upper and lower flanges by threaded fasteners 271.
The distribution tanks 44 and 46 are connected to the primary fluid coolant system by first 298 and second 312 flange connectors. The first flange connector 298 has a central axis and a body 300 extending between upper 302 and lower 304 ends. The body lower end 304 has a pilot 306. The body upper end 302 has a nozzle 308. The nozzle 308 has an axis at an angle to the connector central axis of between zero and ninety degrees. The first flange connector pilot 306 is removably and rotatably received within any one of the upper and lower flange receiver bores 86, 95, 122, and 132. Typically, the first flange connector 298 will be installed in the upper flange first receiver circular bore 86, as shown in
The second flange connector 312 has a central axis and a body 314 extending between upper 316 and lower 318 ends. The body lower end 318 has a pilot 320. The body upper end 316 has a nozzle 322. The nozzle 322 has an axis at an angle to the connector central axis of between zero and ninety degrees. The second flange connector pilot 320 is removably and rotatably received within any one of the upper and lower flange receiver bores 86, 95, 122, and 132. Typically, the second flange connector 312 will be installed in the lower flange last receiver circular bore 132, as shown in
Flange connector sealing means is provided for rotatably sealing the first 298 and second 312 flange connectors to the flange receivers. This allows connection of the nozzles 308 and 322 to the external conduits in any orientation, as shown in
Retaining means is provided for retaining the flange connector pilot in the receiver bore, while allowing selective rotation of the connector about the connector central axis. Specifically, the retaining means is a flange connector retainer 326 secured by threaded fasteners 328.
Two flange plugs 330 are provided to selectively block the flow of primary fluid coolant 32. Each flange plug 330 has a central axis and a body 332 extending between upper 334 and lower 336 ends. The body lower end 336 has a pilot 338. Each flange plug pilot 338 is adapted to be removably received within one of the upper and lower flange receiver bores 86, 95, 122, and 132.
Flange plug sealing means is provided for sealing the flange plugs 330 to the flange receivers. Specifically, a flange plug O-ring 340 is sealingly juxtaposed between each one of the flange plug pilots 338 and the respective one of the flange receiver bores 86, 95, 122, and 132.
Retaining means is provided for retaining the flange plug pilot in the receiver bore. Specifically, the retaining means is a flange plug retainer 342 secured by threaded fasteners 344.
The upper 134 and lower 178 manifolds are connected to the secondary fluid coolant system by first 346 and second 360 manifold connectors. The first manifold connector 346 has a central axis and a body 348 extending between upper 350 and lower 352 ends. The body lower end 352 has a pilot 354. The body upper end 350 has a nozzle 356. The nozzle 356 has an axis at an angle to the connector central axis of between zero and ninety degrees. The first manifold connector pilot 354 is removably and rotatably received within any one of the upper and lower manifold receiver bores 166, 176, 216, and 220. Typically, the first manifold connector 346 is installed in the upper manifold first receiver bore 166, as shown in
The second manifold connector 360 has a central axis and a body 362 extending between upper 364 and lower 366 ends. The body lower end 366 has a pilot 368. The body upper end 364 has a nozzle 370. The nozzle 370 has an axis at an angle to the connector central axis of between zero and ninety degrees. The second manifold connector pilot 368 is removably and rotatably received within any one of the upper and lower manifold receiver bores 166, 176, 216, and 220. In one embodiment, the second manifold connector 360 is installed in the upper manifold last receiver bore 176, as shown in
Manifold connector sealing means is provided for rotatably sealing the first 346 and second 360 manifold connectors to the manifold receivers. This is to allow connection of the nozzles 356 and 370 to the external conduits in any orientation. Specifically, at least one manifold connector O-ring 374 is sealingly juxtaposed between each one of the manifold connector pilots 354 and 368, and the respective one of the manifold receiver bores 166, 176, 216, and 220.
Retaining means is provided for retaining the manifold connector pilot in the receiver bore, while allowing selective rotation of the connector about the connector central axis. Specifically, the retaining means is a manifold connector retainer 376 secured by threaded fasteners 378.
Two manifold plugs 380 are provided to selectively block the flow of secondary fluid coolant 34. Each manifold plug 380 has a central axis and a body 382 extending between upper 384 and lower 386 ends, the body lower end 386 has a pilot 388. Each manifold plug pilot 388 is adapted to be removably received within one of the upper and lower manifold receiver bores 166, 176, 216, and 220.
Manifold plug sealing means is provided for sealing the manifold plugs 380 to the manifold receivers. Specifically, a manifold plug O-ring 390 is sealingly juxtaposed between each one of the manifold plug pilots 388 and the respective one of the manifold receiver bores 166, 176, 216, and 220.
Retaining means is provided for retaining the manifold plug pilot in the receiver bore. Specifically, the retaining means is a manifold plug retainer 392 secured by threaded fasteners 394.
The shell 36, the manifolds 134 and 178, the headers 222 and 226, and the flanges 60 and 96, are constructed of a non-metallic corrosion resistant polymeric material. The material is selected from the group consisting of thermoset resins and thermoplastic resins.
The tubes 230 are constructed of metal materials having efficient heat transfer properties. The metals are typically selected from the group consisting of copper, bronze, stainless steel, and MonelĀ©. It is to be understood that other metals may be substituted. The headers 222 and 226 can also be metal.
Turning now to
Another embodiment,
Yet another embodiment,
Still another embodiment,
A further embodiment,
A yet further embodiment,
Referring now to
Turning now to
Referring now to
Referring now to
It is to be understood that the above-described combinations of baffles 246 and heat transfer tanks 48 are only a sampling of the preferred embodiments of the invention. Many more combinations are possible, such as five or six or more heat transfer tanks 48, and additional baffles 246. Alternatives to the flange connectors 298 and 312 and the manifold connectors 346 and 360 may be employed. Various sealing means are available and well known. Numerous modifications and alternative embodiments of the invention will be apparent to those skilled in the art in view of the foregoing description. Accordingly, this description is to be construed as illustrative only and is for the purpose of teaching those skilled in the art the best mode of carrying out the invention. Details of the structure may be varied substantially without departing from the spirit of the invention and the exclusive use of all modifications that will come within the scope of the appended claims is reserved.
Part No. Description
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Number | Date | Country | |
---|---|---|---|
20100012296 A1 | Jan 2010 | US |