US20140060789A1 - Heat exchanger and method of operating the same - Google Patents
Heat exchanger and method of operating the same Download PDFInfo
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- US20140060789A1 US20140060789A1 US14/048,446 US201314048446A US2014060789A1 US 20140060789 A1 US20140060789 A1 US 20140060789A1 US 201314048446 A US201314048446 A US 201314048446A US 2014060789 A1 US2014060789 A1 US 2014060789A1
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- slots
- fluid
- heat exchanger
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- plate
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Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated elements
- F28F3/02—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations
- F28F3/025—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being corrugated, plate-like elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated elements
- F28F3/08—Elements constructed for building-up into stacks, e.g. capable of being taken apart for cleaning
- F28F3/086—Elements constructed for building-up into stacks, e.g. capable of being taken apart for cleaning having one or more openings therein forming tubular heat-exchange passages
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K23/00—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
- F01K23/02—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled
- F01K23/06—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle
- F01K23/065—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle the combustion taking place in an internal combustion piston engine, e.g. a diesel engine
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K23/00—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
- F01K23/02—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled
- F01K23/06—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle
- F01K23/10—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle with exhaust fluid of one cycle heating the fluid in another cycle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K25/00—Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for
- F01K25/08—Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for using special vapours
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F22—STEAM GENERATION
- F22B—METHODS OF STEAM GENERATION; STEAM BOILERS
- F22B1/00—Methods of steam generation characterised by form of heating method
- F22B1/02—Methods of steam generation characterised by form of heating method by exploitation of the heat content of hot heat carriers
- F22B1/18—Methods of steam generation characterised by form of heating method by exploitation of the heat content of hot heat carriers the heat carrier being a hot gas, e.g. waste gas such as exhaust gas of internal-combustion engines
- F22B1/1807—Methods of steam generation characterised by form of heating method by exploitation of the heat content of hot heat carriers the heat carrier being a hot gas, e.g. waste gas such as exhaust gas of internal-combustion engines using the exhaust gases of combustion engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F22—STEAM GENERATION
- F22B—METHODS OF STEAM GENERATION; STEAM BOILERS
- F22B29/00—Steam boilers of forced-flow type
- F22B29/06—Steam boilers of forced-flow type of once-through type, i.e. built-up from tubes receiving water at one end and delivering superheated steam at the other end of the tubes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
- F28D21/0001—Recuperative heat exchangers
- F28D21/0003—Recuperative heat exchangers the heat being recuperated from exhaust gases
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D9/0031—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other
- F28D9/0043—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other the plates having openings therein for circulation of at least one heat-exchange medium from one conduit to another
- F28D9/005—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other the plates having openings therein for circulation of at least one heat-exchange medium from one conduit to another the plates having openings therein for both heat-exchange media
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D9/0062—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by spaced plates with inserted elements
- F28D9/0068—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by spaced plates with inserted elements with means for changing flow direction of one heat exchange medium, e.g. using deflecting zones
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D9/0062—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by spaced plates with inserted elements
- F28D9/0075—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by spaced plates with inserted elements the plates having openings therein for circulation of the heat-exchange medium from one conduit to another
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated elements
- F28F3/02—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations
- F28F3/04—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being integral with the element
- F28F3/042—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being integral with the element in the form of local deformations of the element
- F28F3/046—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being integral with the element in the form of local deformations of the element the deformations being linear, e.g. corrugations
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
- F28F9/02—Header boxes; End plates
- F28F9/026—Header boxes; End plates with static flow control means, e.g. with means for uniformly distributing heat exchange media into conduits
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
- F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
- F28D2021/0061—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for phase-change applications
- F28D2021/0064—Vaporizers, e.g. evaporators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
- F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
- F28D2021/0068—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for refrigerant cycles
- F28D2021/0071—Evaporators
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/30—Technologies for a more efficient combustion or heat usage
Definitions
- the present invention relates to heat exchangers, and more particularly to evaporative heat exchangers having a number of stacked plates at least partially defining two separate and substantially adjacent fluid flow paths
- a counter-flow orientation may be desirable when the hot fluid is to be cooled to as low a temperature as possible, or when the evaporating fluid is to be superheated to as high a temperature as possible.
- a concurrent flow orientation may be desirable when the hot fluid and the evaporating fluid are to exit the heat exchanger at one common temperature. Examples of such applications include, but are not limited to, air-conditioning and refrigeration chillers, Rankine cycle evaporators, and water and/or fuel vaporizers for fuel processing and fuel cell applications.
- a disadvantage of using a tube and fin evaporator construction in such applications is the difficulties that it poses in arranging the hot and cold fluid flows in a circuiting arrangement other than cross-flow.
- a stacked plate evaporative heat exchanger for the transfer of heat from a first fluid to a second fluid to vaporize the second fluid includes a plurality of separate parallel flow passages to direct the first fluid through the heat exchanger, and a plurality of parallel arranged fluid flow plates for the second fluid interleaved with the parallel flow passages for the first fluid.
- the fluid flow plates have a first and second set of flow channels extending from a first end of the fluid flow plate to a second end of the fluid flow plate to define a first flow pass for the second fluid.
- the fluid flow plates further have a third set of flow channels to define a second flow pass for the second fluid parallel to the first pass.
- a first collection manifold is located at the second end to receive at least a portion of the second fluid flow from the first pass and transfer it to the second pass.
- a second collection manifold is located between the first and second ends and intersects the second set of flow channels and at least some of the third set of flow channels, but not the first set of flow channels, to receive at least a portion of the second fluid from the first pass and transfer it to the second pass.
- the fluid flow plate is constructed by corrugating a thin sheet of material.
- the second collection manifold may be defined by slots passing through the corrugations of the fluid flow plate.
- the plurality of separate parallel flow passages are arranged to direct the first fluid through the heat exchanger in a direction approximately perpendicular to the first and second flow passes for the second fluid. In some embodiments the plurality of separate parallel flow passages are arranged to direct the first fluid in two or more sequential passes through the heat exchanger.
- the pressure resistance and heat transfer performance of the heat exchanger may be improved by having a uniformly narrow channel width for the flow channels of the fluid flow plates.
- the second collection manifold can consist of one or more slots extending through the fluid flow plate.
- the one or more slots can each have a slot width that is approximately equal to the channel width.
- the fluid flow plates include a fourth set of flow channels to additionally define the second flow pass, and a fifth set of flow channels to define a third pass downstream of the first and second passes
- a third collection manifold is located at the first end of the fluid flow plate to receive at least a portion of the second fluid from the second pass and transfer it to the third pass.
- a fourth collection manifold is located between the first and second ends and intersects the fourth set of flow channels and at least some of the fifth set of flow channels, but not the third set of flow channels, to receive at least a portion of the second fluid from the second pass and transfer it to the third pass.
- the fluid flow plates include additional flow passes downstream of the third pass.
- the plurality of separate parallel flow passages are at least partially defined by a plurality of stamped plates.
- Each of the stamped plates can include a recessed area to receive one of the fluid flow plates.
- the present invention provides an evaporative heat exchanger operable to at least partially vaporize fluid.
- the heat exchanger can include a number of parallel flow passages extending through the heat exchanger, together the flow passages define a first fluid flow path, and a number of substantially parallel stacked plates interleaved with the parallel flow passages.
- Each plate can have a first end and a second end spaced apart from the first end and at least partially define a first set of flow channels extending from the first end to the second end and a second set of flow channels extending from the first end to the second end parallel to the first set of flow channels.
- the first and second sets of flow channels together can comprise a first flow pass of a second fluid flow path.
- Each plate can also include a third set of flow channels extending from the first end to the second end and comprising a second flow pass of the second fluid flow path substantially parallel to the first flow pass of the second fluid flow path, a first collection manifold adjacent to the second end and connecting the first and second passes, and a second collection manifold between the first end and the second end, the second collection manifold intersecting the second set of flow channels and at least some of the third set of flow channels.
- The can plate separate the first set of flow channels from the second collection manifold.
- the present invention provides an evaporative heat exchanger that is operable to at least partially vaporize fluid.
- the heat exchanger includes first and second stacked plates that define a first fluid flow path between the first and second stacked plates.
- the first and second stacked plates each have a first end and a second end, and the first stacked plate defines a plane.
- Third and fourth stacked plates define a second fluid flow path between the third and fourth stacked plates.
- the third stacked plate is positioned adjacent the second stacked plate.
- a fluid flow plate is positioned between the first and second stacked plates.
- the fluid flow plate has flow channels extending in a first direction between the first end and the second end. The first direction is substantially parallel to the plane.
- At least one of the first and second stacked plates and the fluid flow plate includes slots that form a portion of the first fluid flow path so that fluid flowing along the first fluid flow path flows along at least one of the flow channels in the first direction and then flows in a second direction into at least one of the slots.
- the second direction is non-parallel to the plane.
- the fluid then flows in a third direction toward an adjacent one of the flow channels.
- the third direction is substantially parallel to the plane.
- the fluid then flows in a fourth direction into the adjacent one of the flow channels.
- the fourth direction is substantially non-parallel to the plane.
- the fluid flows in a fifth direction along the adjacent one of the flow channels.
- the fifth direction is substantially parallel to the plane.
- the present invention provides an evaporative heat exchanger that is operable to at least partially vaporize fluid.
- the heat exchanger includes first and second stacked plates that define a first fluid flow path between the first and second stacked plates.
- the first and second stacked plates each have a first end and a second end, and the first stacked plate defines a plane.
- Third and fourth stacked plates define a second fluid flow path between the third and fourth stacked plates.
- the third stacked plate is positioned adjacent the second stacked plate.
- a fluid flow plate is positioned between the first and second stacked plates.
- the fluid flow plate has flow channels that extend in a first direction between the first end and the second end. The first direction is substantially parallel to the plane.
- At least one of the first and second stacked plates includes slots that form a portion of the first fluid flow path so that fluid flowing along the first fluid flow path flows along at least one of the flow channels in the first direction, then flows along at least one of the slots, then flows into an adjacent one of the flow channels and then along the adjacent flow channel in a second direction, substantially parallel to the first direction.
- FIG. 1 is an isometric view of a heat exchanger according to some embodiments of the present invention.
- FIG. 2 is a partially exploded isometric view of the heat exchanger of FIG. 1 .
- FIG. 3 is an isometric view of certain portions of the heat exchanger of FIGS. 1 and 2 .
- FIG. 4 is similar to FIG. 3 but with certain details removed to more clearly show fluid flow paths.
- FIGS. 5 a - c are diagrammatic illustrations of possible fluid flow paths through a heat exchanger according to embodiments of the present invention.
- FIG. 6 is an isometric view of a heat exchanger according to another embodiment of the present invention.
- FIG. 7 is an isometric view of certain portions of the heat exchanger of FIG. 6 .
- FIG. 8 is an isometric view of a heat exchanger according to another embodiment of the present invention.
- FIG. 9 is an isometric view of certain portions of the heat exchanger of FIG. 8 .
- FIG. 10 is an exploded view of FIG. 9 .
- FIG. 11 is a cross-sectional view taken along line 11 - 11 of FIG. 8 .
- FIG. 12 is a close-up view of a portion of FIG. 11 .
- FIGS. 13-16 illustrate alternative embodiments of stacked plate assemblies of heat exchangers according to some embodiments of the present invention.
- FIG. 17 illustrates an alternative embodiment of a plate for use in any of the heat exchangers described here.
- FIGS. 1 and 2 illustrate a heat exchanger 1 according to some embodiments of the present invention.
- the heat exchanger 1 is adapted to receive a first fluid flow 2 and a second fluid flow 3 and to place them in heat exchange relation with one another so as to transfer heat from one of the fluid flows to the other of the fluid flows.
- the heat exchanger 1 is especially well suited for use when the fluid flow 2 is a hot gas flow and the fluid flow 3 is a liquid or partially liquid flow having a boiling point or bubble point temperature that is lower than the entering temperature of the fluid flow 2 , so that heat can be transferred from the first fluid flow 2 to the second fluid flow 3 in order to substantially vaporize the second fluid flow 3 .
- the heat that is so transferred may be sufficient to fully vaporize the second fluid flow 3 , whereas in other applications the heat may be sufficient to vaporize only a portion of the first fluid flow 3 . Furthermore, in some applications, the heat that is transferred from the first fluid flow 2 to the second fluid flow 3 may exceed the amount of latent heat required to fully vaporize the second fluid flow 3 , so that the second fluid flow 3 exits the heat exchanger 1 as a superheated vapor.
- the heat exchanger 1 shown in FIGS. 1 and 2 may be especially useful as an evaporator in a Rankine cycle waste heat recovery system for an internal combustion engine.
- the first fluid flow 2 can be a flow of exhaust gas from the internal combustion engine
- the second fluid flow 3 can be a Rankine cycle working fluid such as water, ammonia, ethanol, methanol, R245fa or similar refrigerants, or a combination thereof.
- the utility of the heat exchanger 1 is not limited to such applications, however, and no limitations to the use of a heat exchanger according to the present invention are implied unless expressly recited in the claims.
- the heat exchanger 1 includes a plurality of parallel arranged stamped shells 5 , each of which is adapted to house a fluid flow plate 4 for the second fluid flow 3 .
- the heat exchanger 1 further includes a plurality of convoluted fin structures 6 for the first fluid flow 2 interleaved with the stamped shells 5 , and a plurality of stamped shells 7 located between the convoluted fin structures 6 and the fluid flow plates 4 in order to maintain separation between the first and second fluid flows 2 and 3 traveling through the heat exchanger 1 .
- stamped shells 5 , 7 can be formed in manners other than stamping.
- the shells 5 , 7 can be positioned along or form less than the entire first and second fluid flows 2 , 3 .
- the stamped plates 5 and 7 are adapted to form sealed edges along the length of the heat exchanger 1 .
- the heat exchanger 1 further includes a top plate 8 and a bottom plate 9 , as well as header plates 10 to define an inlet and outlet for the first fluid flow 2 .
- the components of the heat exchanger 1 may be joined to one another by brazing, soldering, welding, or other methods known in the art.
- the stamped shells 5 include a fluid inlet port 11 to receive the second fluid flow 3 and a fluid outlet port 12 through which the second fluid flow 3 can exit the heat exchanger 1 . Between the inlet port 11 and the outlet port 12 the second fluid flow 3 is routed through multiple flow passes defined by the stamped shell 5 and the fluid flow plate 4 , with the flow passes extending between parallel ends 40 , 41 of the fluid flow plate 4 .
- a fluid flow would encounter eight passes as it travels from inlet port 11 to outlet port 12 .
- the eight passes are depicted using dashed lines in FIG. 4 , with arrows indicating the direction of flow through each pass. It should be recognized that the desirable number of passes would vary with the application, and that heat exchangers having fewer than or more than eight passes are possible.
- the fluid flow plate 4 is a corrugated thin metal sheet.
- Each of the eight fluid passes 14 - 21 comprise a plurality of flow channels 13 defined by corrugations of the fluid flow plate 4 .
- the crests of the corrugations may be rounded as shown, or they may be some other shape such as, for example, flat or peaked.
- the crests of the corrugations can be bonded to the adjacent surfaces of the stamped plates 5 and 7 in order to define the flow channels 13 .
- the crest of the corrugations can engage correspondingly shaped recesses or protrusions on the adjacent surfaces of the stamped plates 5 and 7 to seal the flow channels 13 .
- Adjacent ones of the channels 13 are generally non-communicative with each other, except in the manifold regions to be described later on.
- the inlet port 11 is directly connected to the channels 13 comprising the fluid pass 14 at the end 40 , so that a portion of the second fluid flow 3 can enter the space between the stamped shell 5 and an adjacent stamped shell 7 or top plate 8 and can flow through the fluid pass 14 .
- the fluid can transfer to the pass 15 by way of the collection manifold 22 located at the end 41 , and additionally by way of the collection manifold 23 located between the ends 40 and 41 .
- the collection manifold 23 does not intersect some of the channels 13 comprising the pass 14 , so that any fluid traveling through these channels is forced to travel the entire length of the channels and through the manifold 20 .
- the collection manifold 23 as shown does not intersect some of the channels 13 comprising the pass 15 , and any fluid traveling through those channels must come from the collection manifold 22 .
- the fluid can transfer to the pass 16 by way of the collection manifold 24 located at the end 40 , and additionally by way of the collection manifold 25 located between the ends 40 and 41 .
- the collection manifold 25 as shown does not intersect some of the channels comprising the pass 15 and does not intersect some of the channels comprising the pass 16 .
- the number of channels comprising any one pass need not be equal to the number of channels comprising any other pass.
- the reduced number of channels in the upstream passes can aid in achieving a uniform distribution of flow among the channels when the flow is all or mostly liquid and consequently has a relatively high density. As the flow moves downstream and the vapor quality increases, the mean density of the flow decreases and a greater number of channels can be used in order to accommodate the increased volumetric flow rate without compromising flow distribution.
- the collection manifold 25 consists of three approximately parallel slots 25 a, 25 b and 25 c extending through the fluid flow plate 4 .
- the collection manifold can consist of more or fewer slots, so that the flow area in the collection manifold can be adjusted.
- a smaller slot width will provide greater structural support to resist deformation of the shells 5 , 7 when the second fluid flow 3 is at a substantially higher pressure than the first fluid flow 2 , as is frequently the case in evaporative systems. It should be understood by those having skill in the art that the proper slot width and number of slots may vary depending on the application.
- the fluid flows through the pass 16 , then by way of the manifolds 26 and 27 through the pass 17 , then by way of the manifolds 28 and 29 through the pass 18 , then by way of the manifolds 30 and 31 through the pass 19 , then by way of the manifolds 32 and 33 through the pass 20 , then by way of the manifolds 34 and 35 through the pass 21 , after which the fluid exits the heat exchanger 1 through outlet port 12 .
- the manifolds 24 , 28 and 32 at the end 40 are separated from each other by protrusions 36 that extend from the wall of the recess in the plate 5 that houses the fluid flow plate 4 .
- These protrusions extend approximately to the end 40 of the fluid flow plate 4 in order to provide a highly tortuous flow path for the fluid to flow directly from one of the manifolds 24 , 28 and 32 to an adjacent one of the manifolds 24 , 28 and 32 without passing through two of the flow passes in the plate 4 .
- Similar protrusions 36 prevent or substantially inhibit bypass flow from the inlet port 11 to the manifold 24 , and between the manifolds 22 , 26 , 30 and 34 located at the end 41 .
- the bypass prevention may be improved by providing notches in the fluid flow plate 4 to receive portions of the protrusions 36 therein in order to provide an even more tortuous flow path.
- the protrusions 36 may be joined to one or more of the corrugations comprising the channels 13 of the fluid flow plate 4 to completely block such bypass flow. In some such embodiments, the joining can be accomplished by creating a brazed joint.
- the protrusions 36 can block off one end of one or more of the channels 13 located between adjacent passes in the fluid flow plate 4 in order to direct substantially all of the fluid flow through the passes.
- the flow blocking protrusions 36 may alternatively extend from the fluid flow plate 4 to engage the wall of the plate 5 .
- the flow manifolds 26 , 28 , 30 , 32 and 34 also can be seen to include a flow area constriction region defined by features 37 that extend partially into the manifolds from the wall of the plate 5 , the purpose of which will be described later.
- FIG. 5 a illustrates a portion of the fluid flow path for the second fluid flow 3 as it passes through a heat exchanger 1 according to some embodiments of the present invention.
- the arrows represent the overall flow direction of the fluid in the various depicted sections of the fluid flow path.
- the portion of the fluid flow path shown in FIG. 5 a includes a pass A and a pass B located adjacent to and immediately downstream from the pass A, each of the passes A, B comprising a plurality of parallel flow channels such as the channels 13 of the embodiment of FIG. 3 .
- the passes A and B may be any two adjacent passes along the fluid flow path. For example, they could represent any adjacent pair of the passes 14 - 21 in the embodiment of FIGS. 3 and 4 .
- the passes A and B extend from an end 38 of the fluid flow plate 4 to an end 39 of the fluid flow plate 4 . Additional (not shown) flow passes may be located upstream and/or downstream of the passes A and B.
- the ends 38 and 39 can correspond to the ends 40 and 41 , respectively, in the embodiment of FIGS. 3 and 4 if the pass A corresponds to one of the even-numbered passes 14 , 16 , 18 or 20 .
- the ends 38 and 39 can correspond to the ends 41 and 40 , respectively, in the embodiment of FIGS. 3 and 4 if the pass A corresponds to one of the odd-numbered passes 15 , 17 or 19 .
- the passes A and B are fluidly connected to one another by way of manifolds C and D, where manifold C is located at the end 39 and manifold D is located between the ends 38 and 39 .
- the pass A comprises a set of channels Al that directly connect to the manifold C, and another set of channels A 2 that directly connect to both manifolds C and D.
- the channels comprising the pass B are each connected to at least one of the manifolds C and D. As shown in FIG. 5 a , in some embodiments, some of the channels comprising the pass B are connected to the manifold C but are not connected to the manifold D, while the other of the channels comprising the pass B are connected to both manifolds C and D. In other embodiments, such as the one shown in FIG. 5 b , some of the channels comprising the pass B are connected to the manifold D but are not connected to the manifold C. In still other embodiments, all of the channels comprising the pass B may be connected to both manifolds C and D.
- a heat exchanger including a flow plate 4 according to the embodiment of FIG. 5 a When a heat exchanger including a flow plate 4 according to the embodiment of FIG. 5 a is operated as an evaporative heat exchanger, with the evaporating fluid flowing as a two-phase fluid through pass A, the liquid and vapor phases of the portion of the fluid in the set of channels A 2 will tend to separate from one another when the fluid encounters the manifold D. Due to its lower density, the vapor phase will experience a much greater pressure drop than the liquid phase will in passing from the manifold D back into the channel region between manifolds D and C. As a result, the vapor phase portion of the fluid traveling in the channels of section A 2 will tend to flow in greater proportion through the manifold D. The liquid phase portion, in contrast, is more likely to continue straight through into the manifold C.
- FIG. 5 a in some embodiments, it is preferable to include a local constriction of the manifold C, such as by the presence of the partial flow blocking feature 37 . Including such a local constriction can prevent the entirety of the flow in manifold C from flowing all the way to the end of that manifold and into only the last few channels of the pass B. When the fluid reaches the local constriction, a substantial portion of the fluid will be directed into the manifold D, from where it can then be distributed into the channels of pass B that are directly connected to manifold D.
- the manifold C does not extend to all of the channels of pass B, and all of the fluid in the manifold C is directed into the manifold D, from where it can then be distributed to the channels of pass B.
- an additional flow pass E immediately adjacent to pass B is shown.
- the passes B and E are fluidly connected to one another by a manifold F located at the end 38 of the flow plate 4 , and by a manifold G located between the ends 38 and 39 .
- One set B 1 of the channels of pass B are connected only to the manifold F, while a separate set B 2 of the channels are connected to both manifolds F and G, so that the manifolds F and G can provide similar benefits as was described with reference to the manifolds C and D. It should be readily apparent that this pattern can be repeated as necessary in order to provide the desirable number of flow passes for a particular application.
- FIG. 6 illustrates another embodiment of a heat exchanger 101 of the present invention.
- a hot fluid flow 102 and an evaporating fluid flow 103 are directed into and out of the heat exchanger 101 through ports in the top plate 108 of the heat exchanger 101 .
- Such an embodiment can operate as a liquid chiller in a refrigeration or climate control system, wherein the hot fluid flow 102 is a liquid that is chilled by evaporation of a refrigerant flow 103 .
- the fluid flow plate 104 can include openings 111 , 112 corresponding to the port locations for the fluid flow 103 .
- the flow 103 is distributed by way of the openings 111 to the plurality of layers 105 containing the flow plates 104 .
- the fluid flow 103 is directed though multiple passes of the parallel arranged flow channels 113 , as indicated by the arrows in FIG. 7 .
- the flow 113 is distributed into the first pass by way of the manifolds 115 and 116 . From the first pass, the flow 113 is distributed into the second pass by way of the manifolds 117 and 118 , which serve the purpose of the manifolds C and D of FIGS. 5 a - c . Specifically, it can be seen that some of the channels 113 belonging to the first pass are connected to the manifold 117 but not to the manifold 118 , whereas others of the channels are connected to both manifolds 117 and 118 .
- Some of the flow channels 113 may be blocked by a ring 115 surrounding a port 110 through which the flow 102 is collected from the plurality of flow layers 107 interleaved with the flow layers 105 .
- a portion 118 a of the manifold 118 is located so as to intersect those channels and allow for the fluid passing through those channels to bypass around the ring 115 .
- the flow 103 is directed into the second pass from the manifolds 117 and 118 , and is directed from the second pass into the third pass through the manifolds 119 and 120 .
- the fluid is directed from the third pass to the fourth pass through the manifolds 121 and 122 , and from the fourth pass to the fifth pass through the manifolds 123 and 124 .
- the manifolds 125 and 126 redirect the fluid from the fifth pass into the port 112 , through which the fluid 103 is removed from the heat exchanger 101 .
- some of the channels in the fifth flow pass are blocked by a ring 114 surrounding the inlet distribution port 106 for the fluid 102 .
- a portion 124 c of the manifold 124 is located such that a portion of the fluid 103 can be directed into those channels despite the flow blockage due to the ring 114 .
- the manifolds 117 , 119 , 121 and 123 have local constrictions caused by protrusions or extensions 128 protruding from the fluid flow plate 104 into the manifold areas. These extensions 128 serve a similar function as the previously described protrusions 37 .
- the manifolds 117 , 121 and 125 are separated from one another by protrusions 136 extending from the wall of the plate 105 , said protrusions being received into notches 127 in the fluid flow plate 104 .
- the manifolds 115 , 119 and 123 are similarly separated from one another.
- FIGS. 8-12 illustrate another embodiment of a heat exchanger 201 of the present invention.
- the illustrated embodiment of FIGS. 8-12 incorporates many of the features described and illustrated with respect to the embodiments of FIGS. 1-7 .
- the discussion of the embodiments of FIGS. 8-12 will primarily focus on the features that are not disclosed in the description or figures of the embodiments of FIGS. 1-7 .
- the heat exchanger 201 includes a hot fluid flow 202 and an evaporating fluid flow 203 .
- the hot fluid flow 202 is shown flowing generally from left to right, but can flow generally right to left in other embodiments.
- the evaporating fluid flow 203 flows generally from right to left, but can flow generally left to right in other embodiments.
- the illustrated heat exchanger 201 is a counter flow heat exchanger. However, in other embodiments, the heat exchanger 201 can have one or more portions of the heat exchanger arranged as parallel flow, cross flow, counter-cross flow or other type of heat exchanging flow relationship.
- the illustrated heat exchanger 201 includes a plurality of stacked plate assemblies.
- One of the stacked plate assemblies is shown in FIGS. 9 and 10 .
- Each of the stacked plate assemblies includes a fluid flow plate 204 , first and second stamped shells 205 a, 205 b, a convoluted fin 206 and first and second stamped shells 207 a, 207 b.
- the plurality of stacked plate assemblies are positioned between a top plate 208 and a bottom plate 209 (shown in FIG. 11 ).
- the hot fluid flow 202 flows into the heat exchanger 201 at a first collection region 210 a and exits the heat exchanger 201 at a second collection region 210 b.
- the hot fluid flow 202 flows from the first collection region 210 a between the first and second stamped shells 207 a, 207 b and along convolutions defined by the convoluted fin 206 prior to flowing into the second collection region 210 b.
- the evaporating fluid flow 203 flows into the heat exchanger 201 at a fluid inlet 211 and flows out of the heat exchanger 201 at a fluid outlet 212 .
- the evaporating fluid flow 203 travels along a circuitous flow path between the fluid inlet 211 and the fluid outlet 212 .
- the circuitous flow path extends between first and second parallel ends 240 , 241 of the heat exchanger 201 .
- the circuitous flow path includes a plurality of fluid passes 214 , 215 , 216 , 217 , 218 and 219 (see stamped shell 205 a of FIG. 10 ).
- the circuitous flow path is defined by a plurality of flow channels 213 formed in the fin 204 and a plurality of slots formed in the stamped shells 205 a, 205 b.
- the plurality of slots include a plurality of groups of substantially parallel slots.
- the first and second stamped shells 205 a, 205 b have corresponding slots.
- the first and second stamped shells 205 a, 205 b can have offset slots or differing numbers and/or configurations of slots.
- a first group of the plurality of slots includes slots 225 a, 225 b, 225 c and 225 d which are positioned adjacent to the fluid inlet port 211 and adjacent the first parallel end 240 .
- a second group of the plurality of slots includes slots 227 a, 227 b and 227 c spaced from the fluid inlet port 211 and positioned adjacent the second parallel end 241 .
- a coordinate axis is included on FIG. 9 for clarity.
- the evaporating fluid flow 203 in the fluid pass 214 travels along the flow channels 213 of the fluid flow plate 204 (along the Y axis) between the first group of slots 225 a - 225 d and the second group of slots 227 a - 227 c.
- the first group of slots 225 a - 225 d allows the fluid to move between adjacent flow channels 213 in the fluid flow plate 204 . Specifically, the fluid can flow along the Z axis into the slots 225 a - 225 d, then along the X axis in the slots 225 a - 225 d, then finally along the Z axis into one or more of the adjacent flow channels 213 .
- the first group of slots 225 a - 225 d and the fluid pass 214 are relatively narrow (when measured along the X axis) when compared to the second group of slots 227 a - 227 c and the fluid pass 215 .
- Each of the slots in the first group of slots 225 a - 225 d is spaced apart a greater distance (when measured along the Y axis) than each of the slots in the second group of slots 227 a - 227 c.
- the second group of slots 227 a - 227 c functions as a turn-around so that the fluid flow reverses direction and flows back toward the parallel end 240 along the fluid pass 215 .
- the fluid flows in the Y direction along some of the flow channels 213 from the first parallel end 240 toward the second parallel end 241 , then into any of the slots 227 a - 227 c which allows the fluid to flow along the X direction into adjacent flow channels 213 .
- the fluid can flow in the Y direction along the fluid pass 215 from the second parallel end 241 toward the first parallel end 240 .
- the second group of slots 227 a - 227 c and the fluid pass 215 are wider (when measured along the X axis) than the first group of slots 225 a - 225 d and the fluid pass 214 , the second group of slots 227 a - 227 c is in fluid connection with a greater number of flow channels 213 than the first group of slots 225 a - 225 d.
- the flow channels 213 that are fluidly connected to the first group of slots 225 a - 225 d form fluid pass 214 and permit fluid to flow from the first parallel end 240 to the second parallel end.
- the flow channels 213 that are fluidly connected to the second group of slots 227 a - 227 c but are fluidly separated from the first group of slots 225 a - 225 d form fluid pass 215 and permit fluid to flow from the second parallel end 241 to the first parallel end 240 .
- the fluid After the fluid is allowed to turn around in the second group of slots 227 a - 227 c, the fluid flows along the Y axis in the fluid pass 215 toward a third group of slots 229 a, 229 b, 229 c, 229 d and 229 e positioned adjacent the first parallel end 240 and the first group of slots 225 a - 225 d. Similar to the discussion above, the third group of slots 229 a - 229 e allows the fluid to move between adjacent flow channels 213 in the fluid flow plate 204 .
- the fluid can flow along the Z axis into the slots 229 a - 229 e, then along the X axis in the slots 229 a - 229 e, then finally along the Z axis into one or more of the adjacent flow channels 213 .
- the slots 227 a - 227 c of the second group are narrower (when measured along the X axis) and fewer in number than the slots 229 a - 229 e of the third group.
- the third group of slots 229 a - 229 e are wider (when measured along the X axis) than the second group of slots 227 a - 227 c, the third group of slots 229 a - 229 e is in fluid connection with a greater number of flow channels 213 than the second group of slots 227 a - 227 c.
- the flow channels 213 that are fluidly connected to the third group of slots 229 a - 229 e but are fluidly separated from the second group of slots 227 a - 227 c form fluid pass 216 and permit fluid to flow from the first parallel end 240 to the second parallel end 241 . Therefore, the fluid is allowed to turn around in the third group of slots 229 a - 229 e and move from fluid pass 215 to fluid pass 216 .
- the fluid flows along the flow channels 213 of the fluid pass 216 from the first parallel end 240 toward a fourth group of slots 231 a, 231 b, 231 c, 231 d, 231 e, 231 f and 231 g adjacent the second parallel end 241 .
- the fourth group of slots 231 a - 231 g like the second and third groups of slots 227 a - 227 c and 229 a - 229 e discussed above, functions as a turn-around for fluid flowing along the flow channels 213 .
- fluid that flows along the fluid pass 216 toward the fourth group of slots 231 a - 231 g can flow along the Z axis into the slots 231 a - 231 g, then along the X axis in the slots 231 a - 231 g, then finally along the Z axis into one or more of the adjacent flow channels 213 .
- the slots 229 a - 229 e of the third group are narrower (when measured along the X axis) and fewer in number than the slots 231 a - 231 g of the fourth group.
- the fourth group of slots 231 a - 231 g are wider (when measured along the X axis) than the third group of slots 229 a - 229 e, the fourth group of slots 231 a - 231 g is in fluid connection with a greater number of flow channels 213 than the third group of slots 229 a - 229 e.
- the flow channels 213 that are fluidly connected to the fourth group of slots 231 a - 231 g but are fluidly separated from the third group of slots 229 a - 229 e form fluid pass 217 and permit fluid to flow from the second parallel end 241 to the first parallel end 240 .
- the fourth group of slots 231 a - 231 g permits the fluid to turn around and move from the fluid pass 216 to the fluid pass 217 .
- Fluid pass 217 is wider (when measured along the X axis) than fluid pass 216 .
- the fluid flows along the flow channels 213 of the fluid pass 217 from the second parallel end 241 toward a fifth group of slots 233 a, 233 b, 233 c, 233 d, 233 e, 233 f, 233 g, 233 h and 233 i adjacent the first parallel end 240 .
- the fifth group of slots 233 a - 233 i like the second, third and fourth groups of slots 227 a - 227 c, 229 a - 229 e and 231 a - 231 g discussed above, functions as a turn-around for fluid flowing along the flow channels 213 .
- fluid that flows along the fluid pass 217 toward the fifth group of slots 233 a - 233 i can flow along the Z axis into the slots 233 a - 233 i, then along the X axis in the slots 233 a - 233 i, then finally along the Z axis into one or more of the adjacent flow channels 213 .
- the slots 233 a - 233 i of the fifth group are wider (when measured along the X axis) and greater in number than the slots 231 a - 231 g of the fourth group.
- the fifth group of slots 233 a - 233 i are wider (when measured along the X axis) than the fourth group of slots 231 a - 231 g, the fifth group of slots 233 a - 233 i is in fluid connection with a greater number of flow channels 213 than the fourth group of slots 231 a - 231 g.
- the flow channels 213 that are fluidly connected to the fifth group of slots 233 a - 233 i but are fluidly separated from the fourth group of slots 231 a - 231 g form fluid pass 218 and permit fluid to flow from the first parallel end 240 to the second parallel end 241 .
- the fifth group of slots 233 a - 233 i permits the fluid to turn around and move from the fluid pass 217 to the fluid pass 218 .
- the fluid flows along the flow channels 213 of the fluid pass 218 from the first parallel end 240 toward a sixth group of slots 235 a, 235 b, 235 c, 235 d, 235 e, 235 f, 235 g, 235 h, 235 i, 235 j and 235 k adjacent the second parallel end 241 .
- the sixth group of slots 235 a - 235 k functions as a turn-around for fluid flowing along the flow channels 213 .
- fluid that flows along the fluid pass 218 toward the sixth group of slots 235 a - 235 k can flow along the Z axis into the slots 235 a - 235 k, then along the X axis in the slots 235 a - 235 k, then finally along the Z axis into one or more of the adjacent flow channels 213 .
- the slots 235 a - 235 k of the sixth group are wider (when measured along the X axis) and greater in number than the slots 233 a - 233 i of the fifth group. Because the sixth group of slots 235 a - 235 k are wider (when measured along the X axis) than the fifth group of slots 233 a - 233 i, the sixth group of slots 235 a - 235 k is in fluid connection with a greater number of flow channels 213 than the fifth group of slots 233 a - 233 i.
- the sixth group of slots 235 a - 235 k permits the fluid to turn around and move from the fluid pass 218 to the fluid pass 219 .
- Fluid pass 219 is wider (when measured along the X axis) than fluid pass 218 .
- first and second stamped shells 207 a and 207 b are substantially mirror images and define a first collection opening 245 a that forms a portion of the first collection region 210 a and a second collection opening 245 b that forms a portion of the second collection region 210 b.
- first and second collection openings 245 a, 245 b are substantially triangular.
- the first and/or section collection openings 245 a, 245 b can have differing shapes and configurations.
- the illustrated first and second stamped shells 205 a and 205 b are substantially mirror images and define first collection openings 247 a, 247 b that form a portion of the first collecting region 210 a and second collection openings 249 a, 249 b that form a portion of the second collecting region 210 b.
- the first and second collection openings 247 a, 247 b, 249 a, 249 b are substantially triangular.
- the first and/or section collection openings 247 a, 247 b , 249 a, 249 b can have differing shapes and configurations.
- the first and second collection openings 247 a, 247 b, 249 a, 249 b each have dimples 251 a , 251 b, 253 a, 253 b that provide points at which the first and second stamped plates 205 a , 205 b can be connected (for example, by brazing).
- dimples 251 a , 251 b, 253 a, 253 b that provide points at which the first and second stamped plates 205 a , 205 b can be connected (for example, by brazing).
- other arrangements of dimples or other shapes can be utilized to connect the first and second stamped plates 205 a, 205 b adjacent the first and second collection openings 247 a, 247 b , 249 a, 249 b.
- FIG. 12 is a close up of the portion of FIG. 11 surrounded by the circle 12 .
- the fluid flow plates 204 are omitted from FIG. 12 for clarity.
- each of the stacked plate assemblies has a substantially identical configuration and has corresponding positions and quantities of slots.
- each of the first, second, third, fourth, fifth and sixth groups of slots 225 a - 225 d , 227 a - 227 c, 229 a - 229 e, 231 a - 231 g, 233 a - 233 i and 235 a - 235 k are present in each of the first and second stamped shells 205 a, 205 b.
- one or more of the stacked plate assemblies can have a different configuration and/or different locations and quantities of slots than the remaining stacked plate assemblies.
- the illustrated stacked plate assembly includes a fluid flow plate 304 positioned between first and second stamped shells 305 a, 305 b.
- the embodiment of FIG. 13 further includes a third stamped shell 305 c positioned adjacent the first stamped shell 305 a and a fourth stamped shell 305 d positioned adjacent the second stamped shell 305 b.
- the fluid flow plate 304 and the first, second, third and fourth stamped shells 305 a, 305 b, 305 c and 305 d are sandwiched between first and second stamped shells 307 a, 307 b.
- first and second stamped shells 307 a, 307 b are illustrated at opposite ends of the fluid flow plate 304
- the first and second stamped shells 307 a, 307 b are positioned in pairs adjacent both the third stamped shell 305 c and the fourth stamped shell 305 d.
- the assemblies formed by the fluid flow plate 304 and the stamped shells 305 a, 305 b, 305 c and 305 d are interleaved with the pairs of stamped shells 307 a, 307 b.
- a convoluted fin can be provided between the first stamped shell 307 a and the second stamped shell 307 b.
- the first, second, third and fourth stamped shells 305 a, 305 b, 305 c, 305 d each include a plurality of groups of slots.
- the slots are substantially identical in each of the first, second, third and fourth stamped shells 305 a, 305 b, 305 c, 305 d.
- the slots illustrated in FIG. 13 substantially correspond to the slots in the first and second stamped shells 205 a, 205 b shown in FIGS. 8-12 and described in detail above.
- the groups of slots form substantially rectangular shapes.
- the slots in one or more of the stamped shells can differ in quantity and/or location across the respective stamped shell.
- the illustrated stacked plate assembly includes a fluid flow plate 404 positioned between first and second stamped shells 405 a, 405 b, as well as a third stamped shell 405 c positioned adjacent the first stamped shell 405 a and a fourth stamped shell 405 d positioned adjacent the second stamped shell 405 b.
- the fluid flow plate 404 and the first, second, third and fourth stamped shells 405 a, 405 b, 405 c and 405 d are sandwiched between first and second stamped shells 407 a, 407 b.
- the first, second, third and fourth stamped shells 405 a, 405 b, 405 c and 405 d have identical slots.
- many of the slots in each group of slots have different widths. Specifically, many of the slots positioned adjacent outer edges of the first, second, third and fourth stamped shells 405 a, 405 b, 405 c and 405 d are wider than the slots positioned inward from the outer edges.
- many of the groups of slots form a substantially trapezoidal shape.
- one or more of the groups can include slots that form substantially trapezoidal shapes whereas one or more of the groups can include other, non-trapezoidal shapes and configurations.
- the illustrated stacked plate assembly includes a fluid flow plate 504 positioned between first and second stamped shells 505 a, 505 b, as well as a third stamped shell 505 c positioned adjacent the first stamped shell 505 a and a fourth stamped shell 505 d positioned adjacent the second stamped shell 505 b.
- the fluid flow plate 504 and the first, second, third and fourth stamped shells 505 a, 505 b, 505 c and 505 d are sandwiched between first and second stamped shells 507 a, 507 b.
- the first, second, third and fourth stamped shells 505 a, 505 b, 505 c and 505 d have identical slots.
- the groups of slots each form a substantially parallelogram shape. Specifically, the slots adjacent an outer edge of the stamped shells 505 a, 505 b, 505 c and 505 d are positioned closer to a second parallel end 541 than the slots spaced from the outer edge.
- the slots in each group of slots have a substantially uniform length.
- at least one of the groups of slots can have the slots adjacent the outer edge positioned closer to a first parallel end 540 than the slots spaced from the outer edge.
- the illustrated stacked plate assembly includes a fluid flow plate 604 positioned between first and second stamped shells 605 a, 605 b, as well as a third stamped shell 605 c positioned adjacent the first stamped shell 605 a and a fourth stamped shell 605 d positioned adjacent the second stamped shell 605 b.
- the fluid flow plate 604 and the first, second, third and fourth stamped shells 605 a, 605 b, 605 c and 605 d are sandwiched between first and second stamped shells 607 a, 607 b.
- the first and second stamped shells 605 a and 605 b have identical slots.
- the third and fourth stamped shells 605 c and 605 d do not have any slots.
- the groups of slots each form a substantially rectangular shape.
- FIG. 17 illustrates a stamped shell 705 that can be utilized with any of the heat exchangers described and illustrated herein.
- the illustrated stamped shell 705 includes first, second, third, fourth, fifth and sixth fluid passes 714 , 715 , 716 , 717 , 718 and 719 that extend between first and second parallel ends 740 , 741 .
- the illustrated stamped shell 705 also includes a first group of slots 725 , a second group of slots 727 , a third group of slots 729 , a fourth group of slots 731 , a fifth group of slots 733 and a sixth group of slots 735 .
- the third, fourth, fifth and sixth groups of slots 729 , 731 , 733 and 735 substantially correspond to the slots described above and illustrated in FIGS. 8-12 .
- each of the slots of the first group of slots 725 form a bypass between the first flow pass 714 and the second flow pass 715 .
- the first group of slots 725 include a first portion that extends across at least a portion of the first flow pass 714 and a second portion that extends across at least a portion of the second flow pass 715 .
- the first portion of the first group of slots 725 is narrower than the second portion when measured in the direction extending between first and second parallel ends 740 , 741 .
- first group of slots 725 extend at a non-parallel angle with respect to the other groups of slots 727 , 729 , 731 , 733 and 735 .
- first portion of the first group of slots 725 extend at a non-parallel angle with respect to the second portion of the first group of slots.
- each of the slots of the second group of slots 727 is thinner in the direction extending between the first and second parallel ends 240 , 241 .
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Abstract
An evaporative heat exchanger includes first and second stacked plates forming a first fluid flow path between a first end and a second end. The first stacked plate defines a plane. Third and fourth stacked plates define a second fluid flow path. A fluid flow plate is positioned between the first and second stacked plates, and has a plurality of flow channels extending substantially parallel to the plane between the first end and the second end. At least one of the first and second stacked plates defines slots that form a portion of the first fluid flow path so that fluid flowing along the first fluid flow path flows along the flow channels in the first direction, then flows along at least one of the slots, then flows into adjacent flow channels and then along the adjacent flow channels in a second direction parallel to the first direction.
Description
- The present application is a continuation-in-part of U.S. application Ser. No. 12/572,310, filed Oct. 2, 2009 which claims priority to U.S. Provisional Patent Application Ser. No. 61/102,458, filed Oct. 3, 2008, the entire contents of both of which are hereby incorporated by reference.
- The present invention relates to heat exchangers, and more particularly to evaporative heat exchangers having a number of stacked plates at least partially defining two separate and substantially adjacent fluid flow paths
- Attempts to use stacked plate style heat exchangers in applications where one of the fluids experiences a change of phase from a liquid to a vapor have been problematic. In such applications the fluid that is evaporating exists, over at least a portion of its flow path through the heat exchanger, as a two-phase fluid having both vapor and liquid fractions. The vapor fraction tends to separate from the liquid fraction due to the substantial differences in densities between the phases, making it difficult to achieve a uniform distribution of the fluid over the multiple parallel passages. This maldistribution effect can be especially pronounced when the flow path through the heat exchanger is circuitous, requiring the fluid to make multiple changes in flow direction. When the distribution is not uniform, the performance of the heat exchanger tends to suffer. Separation of the phases of the evaporating fluid can result in liquid flooding of certain regions, with slugs of the liquid forced through the heat exchanger at a non-constant rate. For this reason, evaporative heat exchangers have often been of a construction wherein the evaporating fluid does not require redistribution along its flow path.
- In certain evaporative heat exchanger applications, it may be especially beneficial to arrange the flow passages so that the hot fluid and the evaporating fluid pass through the heat exchanger in a counter-flow or in a concurrent flow orientation to one another. A counter-flow orientation may be desirable when the hot fluid is to be cooled to as low a temperature as possible, or when the evaporating fluid is to be superheated to as high a temperature as possible. A concurrent flow orientation may be desirable when the hot fluid and the evaporating fluid are to exit the heat exchanger at one common temperature. Examples of such applications include, but are not limited to, air-conditioning and refrigeration chillers, Rankine cycle evaporators, and water and/or fuel vaporizers for fuel processing and fuel cell applications. A disadvantage of using a tube and fin evaporator construction in such applications is the difficulties that it poses in arranging the hot and cold fluid flows in a circuiting arrangement other than cross-flow.
- According to one embodiment of the invention, a stacked plate evaporative heat exchanger for the transfer of heat from a first fluid to a second fluid to vaporize the second fluid includes a plurality of separate parallel flow passages to direct the first fluid through the heat exchanger, and a plurality of parallel arranged fluid flow plates for the second fluid interleaved with the parallel flow passages for the first fluid. The fluid flow plates have a first and second set of flow channels extending from a first end of the fluid flow plate to a second end of the fluid flow plate to define a first flow pass for the second fluid. The fluid flow plates further have a third set of flow channels to define a second flow pass for the second fluid parallel to the first pass. A first collection manifold is located at the second end to receive at least a portion of the second fluid flow from the first pass and transfer it to the second pass. A second collection manifold is located between the first and second ends and intersects the second set of flow channels and at least some of the third set of flow channels, but not the first set of flow channels, to receive at least a portion of the second fluid from the first pass and transfer it to the second pass.
- In some embodiments, the fluid flow plate is constructed by corrugating a thin sheet of material. The second collection manifold may be defined by slots passing through the corrugations of the fluid flow plate.
- In some embodiments, the plurality of separate parallel flow passages are arranged to direct the first fluid through the heat exchanger in a direction approximately perpendicular to the first and second flow passes for the second fluid. In some embodiments the plurality of separate parallel flow passages are arranged to direct the first fluid in two or more sequential passes through the heat exchanger.
- In some embodiments, the pressure resistance and heat transfer performance of the heat exchanger may be improved by having a uniformly narrow channel width for the flow channels of the fluid flow plates. In some embodiments the second collection manifold can consist of one or more slots extending through the fluid flow plate. In some embodiments the one or more slots can each have a slot width that is approximately equal to the channel width.
- In some embodiments, the fluid flow plates include a fourth set of flow channels to additionally define the second flow pass, and a fifth set of flow channels to define a third pass downstream of the first and second passes A third collection manifold is located at the first end of the fluid flow plate to receive at least a portion of the second fluid from the second pass and transfer it to the third pass. A fourth collection manifold is located between the first and second ends and intersects the fourth set of flow channels and at least some of the fifth set of flow channels, but not the third set of flow channels, to receive at least a portion of the second fluid from the second pass and transfer it to the third pass. In some such embodiments the fluid flow plates include additional flow passes downstream of the third pass.
- In some embodiments, the plurality of separate parallel flow passages are at least partially defined by a plurality of stamped plates. Each of the stamped plates can include a recessed area to receive one of the fluid flow plates.
- In some embodiments, the present invention provides an evaporative heat exchanger operable to at least partially vaporize fluid. The heat exchanger can include a number of parallel flow passages extending through the heat exchanger, together the flow passages define a first fluid flow path, and a number of substantially parallel stacked plates interleaved with the parallel flow passages. Each plate can have a first end and a second end spaced apart from the first end and at least partially define a first set of flow channels extending from the first end to the second end and a second set of flow channels extending from the first end to the second end parallel to the first set of flow channels. The first and second sets of flow channels together can comprise a first flow pass of a second fluid flow path. Each plate can also include a third set of flow channels extending from the first end to the second end and comprising a second flow pass of the second fluid flow path substantially parallel to the first flow pass of the second fluid flow path, a first collection manifold adjacent to the second end and connecting the first and second passes, and a second collection manifold between the first end and the second end, the second collection manifold intersecting the second set of flow channels and at least some of the third set of flow channels. The can plate separate the first set of flow channels from the second collection manifold.
- In some embodiments, the present invention provides an evaporative heat exchanger that is operable to at least partially vaporize fluid. The heat exchanger includes first and second stacked plates that define a first fluid flow path between the first and second stacked plates. The first and second stacked plates each have a first end and a second end, and the first stacked plate defines a plane. Third and fourth stacked plates define a second fluid flow path between the third and fourth stacked plates. The third stacked plate is positioned adjacent the second stacked plate. A fluid flow plate is positioned between the first and second stacked plates. The fluid flow plate has flow channels extending in a first direction between the first end and the second end. The first direction is substantially parallel to the plane. At least one of the first and second stacked plates and the fluid flow plate includes slots that form a portion of the first fluid flow path so that fluid flowing along the first fluid flow path flows along at least one of the flow channels in the first direction and then flows in a second direction into at least one of the slots. The second direction is non-parallel to the plane. The fluid then flows in a third direction toward an adjacent one of the flow channels. The third direction is substantially parallel to the plane. The fluid then flows in a fourth direction into the adjacent one of the flow channels. The fourth direction is substantially non-parallel to the plane. Finally, the fluid flows in a fifth direction along the adjacent one of the flow channels. The fifth direction is substantially parallel to the plane.
- In some embodiments, the present invention provides an evaporative heat exchanger that is operable to at least partially vaporize fluid. The heat exchanger includes first and second stacked plates that define a first fluid flow path between the first and second stacked plates. The first and second stacked plates each have a first end and a second end, and the first stacked plate defines a plane. Third and fourth stacked plates define a second fluid flow path between the third and fourth stacked plates. The third stacked plate is positioned adjacent the second stacked plate. A fluid flow plate is positioned between the first and second stacked plates. The fluid flow plate has flow channels that extend in a first direction between the first end and the second end. The first direction is substantially parallel to the plane. At least one of the first and second stacked plates includes slots that form a portion of the first fluid flow path so that fluid flowing along the first fluid flow path flows along at least one of the flow channels in the first direction, then flows along at least one of the slots, then flows into an adjacent one of the flow channels and then along the adjacent flow channel in a second direction, substantially parallel to the first direction.
- Other aspects of the invention will become apparent by consideration of the detailed description and accompanying drawings.
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FIG. 1 is an isometric view of a heat exchanger according to some embodiments of the present invention. -
FIG. 2 is a partially exploded isometric view of the heat exchanger ofFIG. 1 . -
FIG. 3 is an isometric view of certain portions of the heat exchanger ofFIGS. 1 and 2 . -
FIG. 4 is similar toFIG. 3 but with certain details removed to more clearly show fluid flow paths. -
FIGS. 5 a-c are diagrammatic illustrations of possible fluid flow paths through a heat exchanger according to embodiments of the present invention. -
FIG. 6 is an isometric view of a heat exchanger according to another embodiment of the present invention. -
FIG. 7 is an isometric view of certain portions of the heat exchanger ofFIG. 6 . -
FIG. 8 is an isometric view of a heat exchanger according to another embodiment of the present invention. -
FIG. 9 is an isometric view of certain portions of the heat exchanger ofFIG. 8 . -
FIG. 10 is an exploded view ofFIG. 9 . -
FIG. 11 is a cross-sectional view taken along line 11-11 ofFIG. 8 . -
FIG. 12 is a close-up view of a portion ofFIG. 11 . -
FIGS. 13-16 illustrate alternative embodiments of stacked plate assemblies of heat exchangers according to some embodiments of the present invention. -
FIG. 17 illustrates an alternative embodiment of a plate for use in any of the heat exchangers described here. - Before any embodiments of the invention are explained in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangement of components set forth in the following description or illustrated in the following drawings. The invention is capable of other embodiments and of being practiced or of being carried out in various ways. Also, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting. The use of “including,” “comprising,” or “having” and variations thereof herein is meant to encompass the items listed thereafter and equivalents thereof as well as additional items. Unless specified or limited otherwise, the terms “mounted,” “connected,” “supported,” and “coupled” and variations thereof are used broadly and encompass both direct and indirect mountings, connections, supports, and couplings. Further, “connected” and “coupled” are not restricted to physical or mechanical connections or couplings.
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FIGS. 1 and 2 illustrate aheat exchanger 1 according to some embodiments of the present invention. Theheat exchanger 1 is adapted to receive a first fluid flow 2 and asecond fluid flow 3 and to place them in heat exchange relation with one another so as to transfer heat from one of the fluid flows to the other of the fluid flows. Theheat exchanger 1 is especially well suited for use when the fluid flow 2 is a hot gas flow and thefluid flow 3 is a liquid or partially liquid flow having a boiling point or bubble point temperature that is lower than the entering temperature of the fluid flow 2, so that heat can be transferred from the first fluid flow 2 to thesecond fluid flow 3 in order to substantially vaporize thesecond fluid flow 3. - In some such applications, the heat that is so transferred may be sufficient to fully vaporize the
second fluid flow 3, whereas in other applications the heat may be sufficient to vaporize only a portion of thefirst fluid flow 3. Furthermore, in some applications, the heat that is transferred from the first fluid flow 2 to thesecond fluid flow 3 may exceed the amount of latent heat required to fully vaporize thesecond fluid flow 3, so that thesecond fluid flow 3 exits theheat exchanger 1 as a superheated vapor. - The
heat exchanger 1 shown inFIGS. 1 and 2 may be especially useful as an evaporator in a Rankine cycle waste heat recovery system for an internal combustion engine. In such a system, the first fluid flow 2 can be a flow of exhaust gas from the internal combustion engine, and thesecond fluid flow 3 can be a Rankine cycle working fluid such as water, ammonia, ethanol, methanol, R245fa or similar refrigerants, or a combination thereof. The utility of theheat exchanger 1 is not limited to such applications, however, and no limitations to the use of a heat exchanger according to the present invention are implied unless expressly recited in the claims. - As best seen in
FIG. 2 , theheat exchanger 1 includes a plurality of parallel arranged stamped shells 5, each of which is adapted to house afluid flow plate 4 for thesecond fluid flow 3. Theheat exchanger 1 further includes a plurality of convoluted fin structures 6 for the first fluid flow 2 interleaved with the stamped shells 5, and a plurality of stampedshells 7 located between the convoluted fin structures 6 and thefluid flow plates 4 in order to maintain separation between the first and second fluid flows 2 and 3 traveling through theheat exchanger 1. While reference is made herein to stampedshells 5, 7, in some embodiments, theshells 5, 7 can be formed in manners other than stamping. Alternatively or in addition, theshells 5, 7 can be positioned along or form less than the entire first and second fluid flows 2, 3. - In the illustrated embodiment of
FIGS. 1 and 2 , the stampedplates 5 and 7 are adapted to form sealed edges along the length of theheat exchanger 1. Theheat exchanger 1 further includes a top plate 8 and a bottom plate 9, as well as header plates 10 to define an inlet and outlet for the first fluid flow 2. The components of theheat exchanger 1 may be joined to one another by brazing, soldering, welding, or other methods known in the art. - Features of the
fluid flow plates 4 and stamped shells 5 will now be further described with reference toFIGS. 3 and 4 . The stamped shells 5 include afluid inlet port 11 to receive thesecond fluid flow 3 and afluid outlet port 12 through which thesecond fluid flow 3 can exit theheat exchanger 1. Between theinlet port 11 and theoutlet port 12 thesecond fluid flow 3 is routed through multiple flow passes defined by the stamped shell 5 and thefluid flow plate 4, with the flow passes extending between parallel ends 40, 41 of thefluid flow plate 4. In the exemplary embodiment shown inFIGS. 3 and 4 , a fluid flow would encounter eight passes as it travels frominlet port 11 tooutlet port 12. The eight passes are depicted using dashed lines inFIG. 4 , with arrows indicating the direction of flow through each pass. It should be recognized that the desirable number of passes would vary with the application, and that heat exchangers having fewer than or more than eight passes are possible. - In the depicted embodiment, the
fluid flow plate 4 is a corrugated thin metal sheet. Each of the eight fluid passes 14-21 comprise a plurality offlow channels 13 defined by corrugations of thefluid flow plate 4. The crests of the corrugations may be rounded as shown, or they may be some other shape such as, for example, flat or peaked. During fabrication of theheat exchanger 1, the crests of the corrugations can be bonded to the adjacent surfaces of the stampedplates 5 and 7 in order to define theflow channels 13. Alternatively or in addition, the crest of the corrugations can engage correspondingly shaped recesses or protrusions on the adjacent surfaces of the stampedplates 5 and 7 to seal theflow channels 13. Adjacent ones of thechannels 13 are generally non-communicative with each other, except in the manifold regions to be described later on. - The
inlet port 11 is directly connected to thechannels 13 comprising thefluid pass 14 at theend 40, so that a portion of thesecond fluid flow 3 can enter the space between the stamped shell 5 and an adjacent stampedshell 7 or top plate 8 and can flow through thefluid pass 14. After traveling through thepass 14, the fluid can transfer to thepass 15 by way of thecollection manifold 22 located at theend 41, and additionally by way of thecollection manifold 23 located between the 40 and 41. It should be observed that theends collection manifold 23 does not intersect some of thechannels 13 comprising thepass 14, so that any fluid traveling through these channels is forced to travel the entire length of the channels and through the manifold 20. Additionally, thecollection manifold 23 as shown does not intersect some of thechannels 13 comprising thepass 15, and any fluid traveling through those channels must come from thecollection manifold 22. - After flowing through the
pass 15, the fluid can transfer to thepass 16 by way of thecollection manifold 24 located at theend 40, and additionally by way of the collection manifold 25 located between the 40 and 41. Again, the collection manifold 25 as shown does not intersect some of the channels comprising theends pass 15 and does not intersect some of the channels comprising thepass 16. - As can be inferred from inspection of
FIGS. 3 and 4 , the number of channels comprising any one pass need not be equal to the number of channels comprising any other pass. In fact, it may be preferable in some embodiments for the number of channels per pass to increase from the first pass to the second pass and so forth, as is the case for the embodiment ofFIGS. 3 and 4 . The reduced number of channels in the upstream passes can aid in achieving a uniform distribution of flow among the channels when the flow is all or mostly liquid and consequently has a relatively high density. As the flow moves downstream and the vapor quality increases, the mean density of the flow decreases and a greater number of channels can be used in order to accommodate the increased volumetric flow rate without compromising flow distribution. - In the illustrated embodiment, the collection manifold 25 consists of three approximately
25 a, 25 b and 25 c extending through theparallel slots fluid flow plate 4. In different embodiments, the collection manifold can consist of more or fewer slots, so that the flow area in the collection manifold can be adjusted. Some advantages can be found, however, in having multiple slots to comprise the manifold rather than one larger slot. A smaller slot width will result in a smaller hydraulic diameter than a larger slot width, and this will reduce the negative impact on heat transfer performance caused by removal of the corrugations in the slot area. Additionally, a smaller slot width will provide greater structural support to resist deformation of theshells 5, 7 when thesecond fluid flow 3 is at a substantially higher pressure than the first fluid flow 2, as is frequently the case in evaporative systems. It should be understood by those having skill in the art that the proper slot width and number of slots may vary depending on the application. - In a manner similar to that described above, the fluid flows through the
pass 16, then by way of themanifolds 26 and 27 through thepass 17, then by way of the 28 and 29 through themanifolds pass 18, then by way of themanifolds 30 and 31 through thepass 19, then by way of themanifolds 32 and 33 through thepass 20, then by way of themanifolds 34 and 35 through thepass 21, after which the fluid exits theheat exchanger 1 throughoutlet port 12. - The
24, 28 and 32 at themanifolds end 40 are separated from each other byprotrusions 36 that extend from the wall of the recess in the plate 5 that houses thefluid flow plate 4. These protrusions extend approximately to theend 40 of thefluid flow plate 4 in order to provide a highly tortuous flow path for the fluid to flow directly from one of the 24, 28 and 32 to an adjacent one of themanifolds 24, 28 and 32 without passing through two of the flow passes in themanifolds plate 4.Similar protrusions 36 prevent or substantially inhibit bypass flow from theinlet port 11 to the manifold 24, and between the 22, 26, 30 and 34 located at themanifolds end 41. - In some embodiments, the bypass prevention may be improved by providing notches in the
fluid flow plate 4 to receive portions of theprotrusions 36 therein in order to provide an even more tortuous flow path. In some embodiments theprotrusions 36 may be joined to one or more of the corrugations comprising thechannels 13 of thefluid flow plate 4 to completely block such bypass flow. In some such embodiments, the joining can be accomplished by creating a brazed joint. In such embodiments, theprotrusions 36 can block off one end of one or more of thechannels 13 located between adjacent passes in thefluid flow plate 4 in order to direct substantially all of the fluid flow through the passes. In some embodiments, theflow blocking protrusions 36 may alternatively extend from thefluid flow plate 4 to engage the wall of the plate 5. - The flow manifolds 26, 28, 30, 32 and 34 also can be seen to include a flow area constriction region defined by
features 37 that extend partially into the manifolds from the wall of the plate 5, the purpose of which will be described later. - Turning now to
FIGS. 5 a-c, some of the aspects of the present invention will be described.FIG. 5 a illustrates a portion of the fluid flow path for thesecond fluid flow 3 as it passes through aheat exchanger 1 according to some embodiments of the present invention. The arrows represent the overall flow direction of the fluid in the various depicted sections of the fluid flow path. - The portion of the fluid flow path shown in
FIG. 5 a includes a pass A and a pass B located adjacent to and immediately downstream from the pass A, each of the passes A, B comprising a plurality of parallel flow channels such as thechannels 13 of the embodiment ofFIG. 3 . The passes A and B may be any two adjacent passes along the fluid flow path. For example, they could represent any adjacent pair of the passes 14-21 in the embodiment ofFIGS. 3 and 4 . - The passes A and B extend from an
end 38 of thefluid flow plate 4 to anend 39 of thefluid flow plate 4. Additional (not shown) flow passes may be located upstream and/or downstream of the passes A and B. The ends 38 and 39 can correspond to the 40 and 41, respectively, in the embodiment ofends FIGS. 3 and 4 if the pass A corresponds to one of the even-numbered 14, 16, 18 or 20. Likewise, the ends 38 and 39 can correspond to thepasses 41 and 40, respectively, in the embodiment ofends FIGS. 3 and 4 if the pass A corresponds to one of the odd-numbered 15, 17 or 19.passes - The passes A and B are fluidly connected to one another by way of manifolds C and D, where manifold C is located at the
end 39 and manifold D is located between the 38 and 39. The pass A comprises a set of channels Al that directly connect to the manifold C, and another set of channels A2 that directly connect to both manifolds C and D.ends - The channels comprising the pass B are each connected to at least one of the manifolds C and D. As shown in
FIG. 5 a, in some embodiments, some of the channels comprising the pass B are connected to the manifold C but are not connected to the manifold D, while the other of the channels comprising the pass B are connected to both manifolds C and D. In other embodiments, such as the one shown inFIG. 5 b, some of the channels comprising the pass B are connected to the manifold D but are not connected to the manifold C. In still other embodiments, all of the channels comprising the pass B may be connected to both manifolds C and D. - When a heat exchanger including a
flow plate 4 according to the embodiment ofFIG. 5 a is operated as an evaporative heat exchanger, with the evaporating fluid flowing as a two-phase fluid through pass A, the liquid and vapor phases of the portion of the fluid in the set of channels A2 will tend to separate from one another when the fluid encounters the manifold D. Due to its lower density, the vapor phase will experience a much greater pressure drop than the liquid phase will in passing from the manifold D back into the channel region between manifolds D and C. As a result, the vapor phase portion of the fluid traveling in the channels of section A2 will tend to flow in greater proportion through the manifold D. The liquid phase portion, in contrast, is more likely to continue straight through into the manifold C. - As a result of having the set of channels Al only connect to the manifold C, the entirety of the fluid traveling in the set of channels A1 will be directed into manifold C. This can prevent the accumulation of liquid in manifold C, as any vapor present in the set of channels A1 will “push” the liquid through into the pass B. In the embodiment of
-
FIG. 5 a, in some embodiments, it is preferable to include a local constriction of the manifold C, such as by the presence of the partialflow blocking feature 37. Including such a local constriction can prevent the entirety of the flow in manifold C from flowing all the way to the end of that manifold and into only the last few channels of the pass B. When the fluid reaches the local constriction, a substantial portion of the fluid will be directed into the manifold D, from where it can then be distributed into the channels of pass B that are directly connected to manifold D. - In the alternative embodiment of
FIG. 5 b, the manifold C does not extend to all of the channels of pass B, and all of the fluid in the manifold C is directed into the manifold D, from where it can then be distributed to the channels of pass B. - In the embodiment of
FIG. 5 c, an additional flow pass E immediately adjacent to pass B is shown. The passes B and E are fluidly connected to one another by a manifold F located at theend 38 of theflow plate 4, and by a manifold G located between the 38 and 39. One set B1 of the channels of pass B are connected only to the manifold F, while a separate set B2 of the channels are connected to both manifolds F and G, so that the manifolds F and G can provide similar benefits as was described with reference to the manifolds C and D. It should be readily apparent that this pattern can be repeated as necessary in order to provide the desirable number of flow passes for a particular application.ends -
FIG. 6 illustrates another embodiment of a heat exchanger 101 of the present invention. Ahot fluid flow 102 and an evaporatingfluid flow 103 are directed into and out of the heat exchanger 101 through ports in thetop plate 108 of the heat exchanger 101. Such an embodiment can operate as a liquid chiller in a refrigeration or climate control system, wherein thehot fluid flow 102 is a liquid that is chilled by evaporation of arefrigerant flow 103. As seen inFIG. 7 , in such an application, thefluid flow plate 104 can include 111, 112 corresponding to the port locations for theopenings fluid flow 103. Theflow 103 is distributed by way of theopenings 111 to the plurality oflayers 105 containing theflow plates 104. Within thefluid flow plate 104, thefluid flow 103 is directed though multiple passes of the parallel arrangedflow channels 113, as indicated by the arrows inFIG. 7 . - The
flow 113 is distributed into the first pass by way of the 115 and 116. From the first pass, themanifolds flow 113 is distributed into the second pass by way of themanifolds 117 and 118, which serve the purpose of the manifolds C and D ofFIGS. 5 a-c. Specifically, it can be seen that some of thechannels 113 belonging to the first pass are connected to the manifold 117 but not to the manifold 118, whereas others of the channels are connected to bothmanifolds 117 and 118. - Some of the
flow channels 113 may be blocked by aring 115 surrounding aport 110 through which theflow 102 is collected from the plurality of flow layers 107 interleaved with the flow layers 105. Aportion 118 a of the manifold 118 is located so as to intersect those channels and allow for the fluid passing through those channels to bypass around thering 115. - The
flow 103 is directed into the second pass from themanifolds 117 and 118, and is directed from the second pass into the third pass through themanifolds 119 and 120. The fluid is directed from the third pass to the fourth pass through themanifolds 121 and 122, and from the fourth pass to the fifth pass through themanifolds 123 and 124. Themanifolds 125 and 126 redirect the fluid from the fifth pass into theport 112, through which thefluid 103 is removed from the heat exchanger 101. - Similar to the first pass, some of the channels in the fifth flow pass are blocked by a ring 114 surrounding the
inlet distribution port 106 for thefluid 102. Aportion 124 c of the manifold 124 is located such that a portion of the fluid 103 can be directed into those channels despite the flow blockage due to the ring 114. - The
117, 119, 121 and 123 have local constrictions caused by protrusions ormanifolds extensions 128 protruding from thefluid flow plate 104 into the manifold areas. Theseextensions 128 serve a similar function as the previously describedprotrusions 37. - The
117, 121 and 125 are separated from one another bymanifolds protrusions 136 extending from the wall of theplate 105, said protrusions being received intonotches 127 in thefluid flow plate 104. The 115, 119 and 123 are similarly separated from one another.manifolds -
FIGS. 8-12 illustrate another embodiment of aheat exchanger 201 of the present invention. The illustrated embodiment ofFIGS. 8-12 incorporates many of the features described and illustrated with respect to the embodiments ofFIGS. 1-7 . The discussion of the embodiments ofFIGS. 8-12 will primarily focus on the features that are not disclosed in the description or figures of the embodiments ofFIGS. 1-7 . As shown inFIGS. 8-12 , theheat exchanger 201 includes ahot fluid flow 202 and an evaporatingfluid flow 203. Thehot fluid flow 202 is shown flowing generally from left to right, but can flow generally right to left in other embodiments. The evaporatingfluid flow 203 flows generally from right to left, but can flow generally left to right in other embodiments. The illustratedheat exchanger 201 is a counter flow heat exchanger. However, in other embodiments, theheat exchanger 201 can have one or more portions of the heat exchanger arranged as parallel flow, cross flow, counter-cross flow or other type of heat exchanging flow relationship. - The illustrated
heat exchanger 201 includes a plurality of stacked plate assemblies. One of the stacked plate assemblies is shown inFIGS. 9 and 10 . Each of the stacked plate assemblies includes afluid flow plate 204, first and second stamped 205 a, 205 b, ashells convoluted fin 206 and first and second stampedshells 207 a, 207 b. The plurality of stacked plate assemblies are positioned between atop plate 208 and a bottom plate 209 (shown inFIG. 11 ). - The
hot fluid flow 202 flows into theheat exchanger 201 at a first collection region 210 a and exits theheat exchanger 201 at asecond collection region 210 b. Thehot fluid flow 202 flows from the first collection region 210 a between the first and second stampedshells 207 a, 207 b and along convolutions defined by theconvoluted fin 206 prior to flowing into thesecond collection region 210 b. - The evaporating
fluid flow 203 flows into theheat exchanger 201 at a fluid inlet 211 and flows out of theheat exchanger 201 at afluid outlet 212. The evaporatingfluid flow 203 travels along a circuitous flow path between the fluid inlet 211 and thefluid outlet 212. The circuitous flow path extends between first and second parallel ends 240, 241 of theheat exchanger 201. The circuitous flow path includes a plurality of fluid passes 214, 215, 216, 217, 218 and 219 (see stampedshell 205 a ofFIG. 10 ). The circuitous flow path is defined by a plurality offlow channels 213 formed in thefin 204 and a plurality of slots formed in the stamped 205 a, 205 b. The plurality of slots include a plurality of groups of substantially parallel slots. In the illustrated embodiment, the first and second stampedshells 205 a, 205 b have corresponding slots. However, in other embodiments, the first and second stampedshells 205 a, 205 b can have offset slots or differing numbers and/or configurations of slots.shells - A first group of the plurality of slots includes slots 225 a, 225 b, 225 c and 225 d which are positioned adjacent to the fluid inlet port 211 and adjacent the first
parallel end 240. A second group of the plurality of slots includes slots 227 a, 227 b and 227 c spaced from the fluid inlet port 211 and positioned adjacent the secondparallel end 241. A coordinate axis is included onFIG. 9 for clarity. The evaporatingfluid flow 203 in thefluid pass 214 travels along theflow channels 213 of the fluid flow plate 204 (along the Y axis) between the first group of slots 225 a-225 d and the second group of slots 227 a-227 c. The first group of slots 225 a-225 d allows the fluid to move betweenadjacent flow channels 213 in thefluid flow plate 204. Specifically, the fluid can flow along the Z axis into the slots 225 a-225 d, then along the X axis in the slots 225 a-225 d, then finally along the Z axis into one or more of theadjacent flow channels 213. The first group of slots 225 a-225 d and thefluid pass 214 are relatively narrow (when measured along the X axis) when compared to the second group of slots 227 a-227 c and thefluid pass 215. Each of the slots in the first group of slots 225 a-225 d is spaced apart a greater distance (when measured along the Y axis) than each of the slots in the second group of slots 227 a-227 c. - The second group of slots 227 a-227 c functions as a turn-around so that the fluid flow reverses direction and flows back toward the
parallel end 240 along thefluid pass 215. Specifically, the fluid flows in the Y direction along some of theflow channels 213 from the firstparallel end 240 toward the secondparallel end 241, then into any of the slots 227 a-227 c which allows the fluid to flow along the X direction intoadjacent flow channels 213. When the fluid is in theadjacent flow channels 213, the fluid can flow in the Y direction along thefluid pass 215 from the secondparallel end 241 toward the firstparallel end 240. Because the second group of slots 227 a-227 c and thefluid pass 215 are wider (when measured along the X axis) than the first group of slots 225 a-225 d and thefluid pass 214, the second group of slots 227 a-227 c is in fluid connection with a greater number offlow channels 213 than the first group of slots 225 a-225 d. Theflow channels 213 that are fluidly connected to the first group of slots 225 a-225 d formfluid pass 214 and permit fluid to flow from the firstparallel end 240 to the second parallel end. Theflow channels 213 that are fluidly connected to the second group of slots 227 a-227 c but are fluidly separated from the first group of slots 225 a-225 d formfluid pass 215 and permit fluid to flow from the secondparallel end 241 to the firstparallel end 240. - After the fluid is allowed to turn around in the second group of slots 227 a-227 c, the fluid flows along the Y axis in the
fluid pass 215 toward a third group of 229 a, 229 b, 229 c, 229 d and 229 e positioned adjacent the firstslots parallel end 240 and the first group of slots 225 a-225 d. Similar to the discussion above, the third group of slots 229 a-229 e allows the fluid to move betweenadjacent flow channels 213 in thefluid flow plate 204. Specifically, the fluid can flow along the Z axis into the slots 229 a-229 e, then along the X axis in the slots 229 a-229 e, then finally along the Z axis into one or more of theadjacent flow channels 213. The slots 227 a-227 c of the second group are narrower (when measured along the X axis) and fewer in number than the slots 229 a-229 e of the third group. Because the third group of slots 229 a-229 e are wider (when measured along the X axis) than the second group of slots 227 a-227 c, the third group of slots 229 a-229 e is in fluid connection with a greater number offlow channels 213 than the second group of slots 227 a-227 c. Theflow channels 213 that are fluidly connected to the third group of slots 229 a-229 e but are fluidly separated from the second group of slots 227 a-227 c formfluid pass 216 and permit fluid to flow from the firstparallel end 240 to the secondparallel end 241. Therefore, the fluid is allowed to turn around in the third group of slots 229 a-229 e and move fromfluid pass 215 tofluid pass 216. - After the fluid turns around in the third group of slots 229 a-229 e, the fluid flows along the
flow channels 213 of thefluid pass 216 from the firstparallel end 240 toward a fourth group of 231 a, 231 b, 231 c, 231 d, 231 e, 231 f and 231 g adjacent the secondslots parallel end 241. The fourth group ofslots 231 a-231 g, like the second and third groups of slots 227 a-227 c and 229 a-229 e discussed above, functions as a turn-around for fluid flowing along theflow channels 213. Specifically, fluid that flows along thefluid pass 216 toward the fourth group ofslots 231 a-231 g can flow along the Z axis into theslots 231 a-231 g, then along the X axis in theslots 231 a-231 g, then finally along the Z axis into one or more of theadjacent flow channels 213. The slots 229 a-229 e of the third group are narrower (when measured along the X axis) and fewer in number than theslots 231 a-231 g of the fourth group. Because the fourth group ofslots 231 a-231 g are wider (when measured along the X axis) than the third group of slots 229 a-229 e, the fourth group ofslots 231 a-231 g is in fluid connection with a greater number offlow channels 213 than the third group of slots 229 a-229 e. Theflow channels 213 that are fluidly connected to the fourth group ofslots 231 a-231 g but are fluidly separated from the third group of slots 229 a-229 e formfluid pass 217 and permit fluid to flow from the secondparallel end 241 to the firstparallel end 240. Thus, the fourth group ofslots 231 a-231 g permits the fluid to turn around and move from thefluid pass 216 to thefluid pass 217.Fluid pass 217 is wider (when measured along the X axis) thanfluid pass 216. - After the fluid turns around in the fourth group of
slots 231 a-231 g, the fluid flows along theflow channels 213 of thefluid pass 217 from the secondparallel end 241 toward a fifth group of 233 a, 233 b, 233 c, 233 d, 233 e, 233 f, 233 g, 233 h and 233 i adjacent the firstslots parallel end 240. The fifth group of slots 233 a-233 i, like the second, third and fourth groups of slots 227 a-227 c, 229 a-229 e and 231 a-231 g discussed above, functions as a turn-around for fluid flowing along theflow channels 213. Specifically, fluid that flows along thefluid pass 217 toward the fifth group of slots 233 a-233 i can flow along the Z axis into the slots 233 a-233 i, then along the X axis in the slots 233 a-233 i, then finally along the Z axis into one or more of theadjacent flow channels 213. The slots 233 a-233 i of the fifth group are wider (when measured along the X axis) and greater in number than theslots 231 a-231 g of the fourth group. Because the fifth group of slots 233 a-233 i are wider (when measured along the X axis) than the fourth group ofslots 231 a-231 g, the fifth group of slots 233 a-233 i is in fluid connection with a greater number offlow channels 213 than the fourth group ofslots 231 a-231 g. Theflow channels 213 that are fluidly connected to the fifth group of slots 233 a-233 i but are fluidly separated from the fourth group ofslots 231 a-231 gform fluid pass 218 and permit fluid to flow from the firstparallel end 240 to the secondparallel end 241. Thus, the fifth group of slots 233 a-233 i permits the fluid to turn around and move from thefluid pass 217 to thefluid pass 218. - After the fluid turns around in the fifth group of slots 233 a-233 i, the fluid flows along the
flow channels 213 of thefluid pass 218 from the firstparallel end 240 toward a sixth group of 235 a, 235 b, 235 c, 235 d, 235 e, 235 f, 235 g, 235 h, 235 i, 235 j and 235 k adjacent the secondslots parallel end 241. The sixth group ofslots 235 a-235 k, like the second, third, fourth and fifth groups of slots 227 a-227 c, 229 a-229 e, 231 a-231 g and 233 a-233 i discussed above, functions as a turn-around for fluid flowing along theflow channels 213. Specifically, fluid that flows along thefluid pass 218 toward the sixth group ofslots 235 a-235 k can flow along the Z axis into theslots 235 a-235 k, then along the X axis in theslots 235 a-235 k, then finally along the Z axis into one or more of theadjacent flow channels 213. Theslots 235 a-235 k of the sixth group are wider (when measured along the X axis) and greater in number than the slots 233 a-233 i of the fifth group. Because the sixth group ofslots 235 a-235 k are wider (when measured along the X axis) than the fifth group of slots 233 a-233 i, the sixth group ofslots 235 a-235 k is in fluid connection with a greater number offlow channels 213 than the fifth group of slots 233 a-233 i. Theflow channels 213 that are fluidly connected to the sixth group ofslots 235 a-235 k but are fluidly separated from the fifth group of slots 233 a-233 i formfluid pass 219 and permit fluid to flow from the secondparallel end 241 to the firstparallel end 240. Thus, the sixth group ofslots 235 a-235 k permits the fluid to turn around and move from thefluid pass 218 to thefluid pass 219.Fluid pass 219 is wider (when measured along the X axis) thanfluid pass 218. - With continued reference to
FIG. 10 , the illustrated first and second stampedshells 207 a and 207 b are substantially mirror images and define a first collection opening 245 a that forms a portion of the first collection region 210 a and a second collection opening 245 b that forms a portion of thesecond collection region 210 b. In the illustrated embodiment, the first andsecond collection openings 245 a, 245 b are substantially triangular. However, in other embodiments, the first and/orsection collection openings 245 a, 245 b can have differing shapes and configurations. - The illustrated first and second stamped
205 a and 205 b are substantially mirror images and define first collection openings 247 a, 247 b that form a portion of the first collecting region 210 a and second collection openings 249 a, 249 b that form a portion of theshells second collecting region 210 b. In the illustrated embodiment, the first and second collection openings 247 a, 247 b, 249 a, 249 b are substantially triangular. However, in other embodiments, the first and/or section collection openings 247 a, 247 b, 249 a, 249 b can have differing shapes and configurations. In the illustrated embodiment, the first and second collection openings 247 a, 247 b, 249 a, 249 b each have 251 a, 251 b, 253 a, 253 b that provide points at which the first and second stampeddimples 205 a, 205 b can be connected (for example, by brazing). In other embodiments, other arrangements of dimples or other shapes can be utilized to connect the first and second stampedplates 205 a, 205 b adjacent the first and second collection openings 247 a, 247 b, 249 a, 249 b.plates - Turning now to
FIGS. 11 and 12 , the plurality of stacked plate assemblies are shown in cross-section.FIG. 12 is a close up of the portion ofFIG. 11 surrounded by thecircle 12. Thefluid flow plates 204 are omitted fromFIG. 12 for clarity. In the illustrated embodiment, each of the stacked plate assemblies has a substantially identical configuration and has corresponding positions and quantities of slots. While only 231 e, 231 f and 231 g are illustrated in each of the first and second stampedslots 205 a, 205 b, each of the first, second, third, fourth, fifth and sixth groups of slots 225 a-225 d, 227 a-227 c, 229 a-229 e, 231 a-231 g, 233 a-233 i and 235 a-235 k are present in each of the first and second stampedshells 205 a, 205 b. However, in non-illustrated configurations, one or more of the stacked plate assemblies can have a different configuration and/or different locations and quantities of slots than the remaining stacked plate assemblies.shells - Turning now to
FIG. 13 , a portion of an alternate embodiment of a stacked plate assembly is illustrated. Similar to the embodiment ofFIGS. 8-12 , the illustrated stacked plate assembly includes afluid flow plate 304 positioned between first and second stampedshells 305 a, 305 b. The embodiment ofFIG. 13 further includes a third stamped shell 305 c positioned adjacent the first stampedshell 305 a and a fourth stamped shell 305 d positioned adjacent the second stamped shell 305 b. Thefluid flow plate 304 and the first, second, third and fourth stampedshells 305 a, 305 b, 305 c and 305 d are sandwiched between first and second stampedshells 307 a, 307 b. While the first and second stampedshells 307 a, 307 b are illustrated at opposite ends of thefluid flow plate 304, the first and second stampedshells 307 a, 307 b are positioned in pairs adjacent both the third stamped shell 305 c and the fourth stamped shell 305 d. Similar to the embodiments described above, the assemblies formed by thefluid flow plate 304 and the stampedshells 305 a, 305 b, 305 c and 305 d are interleaved with the pairs of stampedshells 307 a, 307 b. Although not illustrated, a convoluted fin can be provided between the first stampedshell 307 a and the second stamped shell 307 b. - The first, second, third and fourth stamped
shells 305 a, 305 b, 305 c, 305 d each include a plurality of groups of slots. The slots are substantially identical in each of the first, second, third and fourth stampedshells 305 a, 305 b, 305 c, 305 d. The slots illustrated inFIG. 13 substantially correspond to the slots in the first and second stamped 205 a, 205 b shown inshells FIGS. 8-12 and described in detail above. Specifically, the groups of slots form substantially rectangular shapes. In other, non-illustrated embodiments, the slots in one or more of the stamped shells can differ in quantity and/or location across the respective stamped shell. - Turning now to
FIG. 14 , a portion of an alternate embodiment of a stacked plate assembly is illustrated. Similar to the embodiment ofFIG. 13 , the illustrated stacked plate assembly includes afluid flow plate 404 positioned between first and second stamped shells 405 a, 405 b, as well as a third stamped shell 405 c positioned adjacent the first stamped shell 405 a and a fourth stamped shell 405 d positioned adjacent the second stamped shell 405 b. Thefluid flow plate 404 and the first, second, third and fourth stamped shells 405 a, 405 b, 405 c and 405 d are sandwiched between first and second stamped shells 407 a, 407 b. Like the embodiments ofFIGS. 1-13 , the first, second, third and fourth stamped shells 405 a, 405 b, 405 c and 405 d have identical slots. In contrast to the embodiments ofFIGS. 1-13 , many of the slots in each group of slots have different widths. Specifically, many of the slots positioned adjacent outer edges of the first, second, third and fourth stamped shells 405 a, 405 b, 405 c and 405 d are wider than the slots positioned inward from the outer edges. In the illustrated embodiments, many of the groups of slots form a substantially trapezoidal shape. In other embodiments, one or more of the groups can include slots that form substantially trapezoidal shapes whereas one or more of the groups can include other, non-trapezoidal shapes and configurations. - Turning now to
FIG. 15 , a portion of an alternate embodiment of a stacked plate assembly is illustrated. Similar to the embodiments ofFIGS. 13 and 14 , the illustrated stacked plate assembly includes a fluid flow plate 504 positioned between first and second stampedshells 505 a, 505 b, as well as a third stampedshell 505 c positioned adjacent the first stampedshell 505 a and a fourth stampedshell 505 d positioned adjacent the second stamped shell 505 b. The fluid flow plate 504 and the first, second, third and fourth stamped 505 a, 505 b, 505 c and 505 d are sandwiched between first and second stampedshells shells 507 a, 507 b. Like the embodiments ofFIGS. 1-14 , the first, second, third and fourth stamped 505 a, 505 b, 505 c and 505 d have identical slots. In contrast to the embodiments ofshells FIGS. 1-14 , the groups of slots each form a substantially parallelogram shape. Specifically, the slots adjacent an outer edge of the stamped 505 a, 505 b, 505 c and 505 d are positioned closer to a secondshells parallel end 541 than the slots spaced from the outer edge. However, the slots in each group of slots have a substantially uniform length. In other embodiments, at least one of the groups of slots can have the slots adjacent the outer edge positioned closer to a firstparallel end 540 than the slots spaced from the outer edge. - Turning now to
FIG. 16 , a portion of an alternate embodiment of a stacked plate assembly is illustrated. Similar to the embodiments ofFIGS. 13-15 , the illustrated stacked plate assembly includes afluid flow plate 604 positioned between first and second stampedshells 605 a, 605 b, as well as a third stamped shell 605 c positioned adjacent the first stampedshell 605 a and a fourth stampedshell 605 d positioned adjacent the second stamped shell 605 b. Thefluid flow plate 604 and the first, second, third and fourth stamped 605 a, 605 b, 605 c and 605 d are sandwiched between first and second stampedshells shells 607 a, 607 b. Like the embodiments ofFIGS. 1-15 , the first and second stampedshells 605 a and 605 b have identical slots. However, the third and fourth stampedshells 605 c and 605 d do not have any slots. Similar to the embodiments ofFIGS. 1-13 , the groups of slots each form a substantially rectangular shape. -
FIG. 17 illustrates a stampedshell 705 that can be utilized with any of the heat exchangers described and illustrated herein. Like the stamped 205 a and 205 b, the illustrated stampedshells shell 705 includes first, second, third, fourth, fifth and sixth fluid passes 714, 715, 716, 717, 718 and 719 that extend between first and second parallel ends 740, 741. The illustrated stampedshell 705 also includes a first group of slots 725, a second group ofslots 727, a third group ofslots 729, a fourth group ofslots 731, a fifth group ofslots 733 and a sixth group ofslots 735. The third, fourth, fifth and sixth groups of 729, 731, 733 and 735 substantially correspond to the slots described above and illustrated inslots FIGS. 8-12 . In contrast to the slots of the embodiment ofFIGS. 8-12 , each of the slots of the first group of slots 725 form a bypass between thefirst flow pass 714 and the second flow pass 715. Specifically, the first group of slots 725 include a first portion that extends across at least a portion of thefirst flow pass 714 and a second portion that extends across at least a portion of the second flow pass 715. The first portion of the first group of slots 725 is narrower than the second portion when measured in the direction extending between first and second parallel ends 740, 741. Additionally, the first group of slots 725 extend at a non-parallel angle with respect to the other groups of 727, 729, 731, 733 and 735. In particular, the first portion of the first group of slots 725 extend at a non-parallel angle with respect to the second portion of the first group of slots. Further in contrast to the embodiment ofslots FIGS. 8-12 , each of the slots of the second group ofslots 727 is thinner in the direction extending between the first and second parallel ends 240, 241. - Other configurations of plates and slots can be utilized with the heat exchangers of the present invention and the illustrated embodiments are given by way of example only.
- Various alternatives to the certain features and elements of the present invention are described with reference to specific embodiments of the present invention. With the exception of features, elements, and manners of operation that are mutually exclusive of or are inconsistent with each embodiment described above, it should be noted that the alternative features, elements, and manners of operation described with reference to one particular embodiment are applicable to the other embodiments.
- The embodiments described above and illustrated in the figures are presented by way of example only and are not intended as a limitation upon the concepts and principles of the present invention. As such, it will be appreciated by one having ordinary skill in the art that various changes in the elements and their configuration and arrangement are possible without departing from the spirit and scope of the present invention.
Claims (20)
1. An evaporative heat exchanger operable to at least partially vaporize fluid, the heat exchanger comprising:
first and second stacked plates defining a first fluid flow path between the first and second stacked plates, the first and second stacked plates each having a first end and a second end, and the first stacked plate defines a plane;
third and fourth stacked plates defining a second fluid flow path between the third and fourth stacked plates, wherein the third stacked plate is positioned adjacent the second stacked plate; and
a fluid flow plate positioned between the first and second stacked plates, the fluid flow plate having a plurality of flow channels extending in a first direction between the first end and the second end, wherein the first direction is substantially parallel to the plane;
wherein at least one of the first and second stacked plates and the fluid flow plate defines a plurality of slots, wherein the plurality of slots form a portion of the first fluid flow path such that fluid flowing along the first fluid flow path flows along at least one of the flow channels in the first direction and then flows in a second direction into at least one of the plurality of slots, wherein the second direction is non-parallel to the plane, and then flows in a third direction toward an adjacent one of the flow channels, wherein the third direction is substantially parallel to the plane, and then in a fourth direction into the adjacent one of the flow channels, wherein the fourth direction is substantially non-parallel to the plane, and then in a fifth direction along the adjacent one of the flow channels, wherein the fifth direction is substantially parallel to the plane.
2. The heat exchanger of claim 1 , wherein at least one of the slots is an elongate slot extending along the third direction.
3. The heat exchanger of claim 1 , wherein the second direction is substantially perpendicular to the plane.
4. The heat exchanger of claim 1 , wherein the first direction is substantially perpendicular to the third direction.
5. The heat exchanger of claim 1 , wherein the first direction is substantially parallel to the fifth direction.
6. The heat exchanger of claim 1 , wherein at least one of the plurality of slots is formed in the first plate.
7. The heat exchanger of claim 1 , wherein at least one of the plurality of slots is formed in the second plate.
8. The heat exchanger of claim 1 , wherein the plurality of slots include at least one slot formed in the first plate and at least one slot formed in the second plate.
9. The heat exchanger of claim 1 , wherein the plurality of slots includes a first group of slots and a second group of slots, wherein the first group of slots is formed in the first plate and wherein the second group of slots is formed in the second plate.
10. The heat exchanger of claim 1 , wherein the fluid flow plate has convolutions that form adjacent the peaks and valleys, and wherein the plurality of flow channels are defined by peaks and valleys.
11. The heat exchanger of claim 1 , wherein the plurality of slots include at least one group of elongate slots each extending in the third direction, substantially perpendicular to the first direction.
12. The heat exchanger of claim 1 , further comprising a convoluted fin positioned between the third and fourth plates.
13. An evaporative heat exchanger operable to at least partially vaporize fluid, the heat exchanger comprising:
first and second stacked plates defining a first fluid flow path between the first and second stacked plates, the first and second stacked plates each having a first end and a second end, and the first stacked plate defines a plane;
third and fourth stacked plates defining a second fluid flow path between the third and fourth stacked plates, wherein the third stacked plate is positioned adjacent the second stacked plate; and
a fluid flow plate positioned between the first and second stacked plates, the fluid flow plate having a plurality of flow channels extending in a first direction between the first end and the second end, wherein the first direction is substantially parallel to the plane;
wherein at least one of the first and second stacked plates defines a plurality of slots, wherein the plurality of slots form a portion of the first fluid flow path such that fluid flowing along the first fluid flow path flows along at least one of the flow channels in the first direction, then flows along at least one of the plurality of slots, then flows into an adjacent one of the flow channels and then along the adjacent flow channel in a second direction, substantially parallel to the first direction.
14. The heat exchanger of claim 13 , wherein the plurality of slots are elongate and extend in a third direction, wherein the third direction is non-parallel to the plane.
15. The heat exchanger of claim 14 , wherein the third direction is substantially perpendicular to the first direction.
16. The heat exchanger of claim 13 , wherein at least one of the plurality of slots is an elongate slot.
17. The heat exchanger of claim 13 , wherein the plurality of slots includes a first plurality of slots formed in the first plate and a second plurality of slots formed in the second plate.
18. The heat exchanger of claim 17 , wherein each the first plurality of slots are substantially aligned with a corresponding one of the second plurality of slots in a direction substantially perpendicular to the plane.
19. The heat exchanger of claim 13 , wherein the fluid flow plate has convolutions that form adjacent peaks and valleys, and wherein the plurality of flow channels are defined by the peaks and valleys.
20. The heat exchanger of claim 13 , further comprising a convoluted fin positioned between the third and fourth plates.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US14/048,446 US20140060789A1 (en) | 2008-10-03 | 2013-10-08 | Heat exchanger and method of operating the same |
| DE201410014670 DE102014014670A1 (en) | 2013-10-08 | 2014-10-02 | Heat exchanger, in particular evaporation heat exchanger |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10245808P | 2008-10-03 | 2008-10-03 | |
| US12/572,310 US8550153B2 (en) | 2008-10-03 | 2009-10-02 | Heat exchanger and method of operating the same |
| US14/048,446 US20140060789A1 (en) | 2008-10-03 | 2013-10-08 | Heat exchanger and method of operating the same |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US12/572,310 Continuation-In-Part US8550153B2 (en) | 2008-10-03 | 2009-10-02 | Heat exchanger and method of operating the same |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20140060789A1 true US20140060789A1 (en) | 2014-03-06 |
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ID=50185807
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US14/048,446 Abandoned US20140060789A1 (en) | 2008-10-03 | 2013-10-08 | Heat exchanger and method of operating the same |
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| Country | Link |
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| US (1) | US20140060789A1 (en) |
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