EP2816307B1 - Integral heat exchanger distributor - Google Patents

Integral heat exchanger distributor Download PDF

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Publication number
EP2816307B1
EP2816307B1 EP14166550.5A EP14166550A EP2816307B1 EP 2816307 B1 EP2816307 B1 EP 2816307B1 EP 14166550 A EP14166550 A EP 14166550A EP 2816307 B1 EP2816307 B1 EP 2816307B1
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EP
European Patent Office
Prior art keywords
heat exchanger
flow
metering
plates
inlet port
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP14166550.5A
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German (de)
French (fr)
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EP2816307A2 (en
EP2816307A3 (en
Inventor
Michael Zager
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Hamilton Sundstrand Corp
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Hamilton Sundstrand Corp
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Application filed by Hamilton Sundstrand Corp filed Critical Hamilton Sundstrand Corp
Priority to EP18204667.2A priority Critical patent/EP3462119B1/en
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Publication of EP2816307A3 publication Critical patent/EP2816307A3/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D9/00Heat-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
    • F28D9/0062Heat-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B39/00Evaporators; Condensers
    • F25B39/02Evaporators
    • F25B39/028Evaporators having distributing means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F3/00Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • F28F3/02Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations
    • F28F3/025Elements 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02Header boxes; End plates
    • F28F9/026Header boxes; End plates with static flow control means, e.g. with means for uniformly distributing heat exchange media into conduits
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02Header boxes; End plates
    • F28F9/026Header boxes; End plates with static flow control means, e.g. with means for uniformly distributing heat exchange media into conduits
    • F28F9/0282Header boxes; End plates with static flow control means, e.g. with means for uniformly distributing heat exchange media into conduits by varying the geometry of conduit ends, e.g. by using inserts or attachments for modifying the pattern of flow at the conduit inlet or outlet
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0021Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for aircrafts or cosmonautics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0061Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for phase-change applications
    • F28D2021/0064Vaporizers, e.g. evaporators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0068Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for refrigerant cycles
    • F28D2021/0071Evaporators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/008Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for vehicles
    • F28D2021/0085Evaporators

Definitions

  • the described subject matter relates generally to heat exchangers, and more specifically to heat exchangers for use with in various refrigerant systems.
  • the present invention provides a heat exchanger as claimed in claim 1.
  • FIG. 1 depicts crossflow heat exchanger 10 with various portions cut away to illustrate the general location of certain internal features.
  • FIG. 1 also shows first fluid 12, inlet port 14, housing 16, inlet chamber 18, refrigerant passages 20, first/longitudinal axis 22, second incoming fluid 24, air passages 26, second/transverse axis 28, third/no-flow axis 29, outlet chamber 30, and first outlet port 32.
  • Heat exchanger 10 is described with reference to an example evaporator-type heat exchanger for an aircraft.
  • the evaporator can be configured as part of a vapor-cycle air management system (not shown).
  • a vapor-cycle air management system not shown.
  • crossflow heat exchanger 10 shown here is provided for illustrative purposes, and the described subject matter can be readily adapted to other uses.
  • the described subject matter can be adapted to many other heat exchanger configurations in which flow rates of each fluid can be suitably managed.
  • a second non-limiting example embodiment of a counterflow heat exchanger is shown in FIG. 4 .
  • First incoming fluid 12 is received into inlet port 14 formed in housing 16.
  • First incoming fluid 12 can be, for example, a refrigerant having previously been passed through an expansion valve (not shown).
  • Inlet chamber 18 is disposed adjacent to an upstream side of one or more refrigerant passages 20 extending along first or longitudinal axis 22.
  • second incoming fluid 24 e.g., air
  • Air passages 26 can be substantially perpendicular to refrigerant passages 20 and can extend along second or transverse axis 28.
  • parting plates can be stacked along third or no-flow axis 29 to define first and second flow spaces (best shown in FIGS. 2 and 3 ).
  • First flow spaces can provide communication between inlet port 14 and outlet port 32 via refrigerant passages 20, while second flow spaces can provide communication along air passages 26.
  • multiple layers of refrigerant passages 20 and air passages 26 are stacked in alternating first and second flow spaces along third/no-flow axis 29.
  • first incoming fluid 12 is heated and vaporized as it passes through inlet chamber 18, refrigerant passages 20, and outlet chamber 30.
  • First outgoing fluid 36 which in this example is vaporized refrigerant, is then discharged from outlet port 32 spaced longitudinally apart from inlet chamber 14.
  • the heat of vaporization chills adjacent/alternating air passages 26 so that second outgoing fluid 34 has a lower temperature than second incoming fluid 24.
  • first incoming fluid 12 e.g., liquid/vapor phase refrigerant
  • first flow space(s) can be metered before entering refrigerant passages 20 in the first flow space(s).
  • a plurality of metering plates can be disposed across an upstream end of at least one of these first flow spaces.
  • each of the plurality of metering plates can include at least one metering aperture providing fluid communication between the first inlet port and the at least one first flow space.
  • the metering plate(s) can take the form of one or more closure bars or other equivalent structure metallurgically bonded to the internal features of the heat exchanger.
  • FIG. 2 shows a portion of example crossflow heat exchanger 10 taken across line 2-2 of FIG. 1 .
  • FIG. 2 also includes inlet chamber 18, refrigerant passages 20, first/longitudinal axis 22, air passages 26, second/transverse axis 28, third/no-flow axis 29, parting plates 44, first flow spaces 46, second flow spaces 48, first fins 50, upstream refrigerant passage ends 52, first closure bar 54, metering apertures 56, metering plates 60, and second fins 62.
  • a plurality of parting plates 44 are stacked along third/no-flow axis 29 of heat exchanger such that pairs of adjacent parting plates 44 define alternating first flow spaces 46 and second flow spaces 48, therebetween. Portions of first closure bars 56 are cut away to show first flow spaces 46 between parting plates 44, as well as a first plurality of fins 50 disposed in each first flow space 46.
  • First fins 50 form first fluid passages extending along first/longitudinal axis 22. In the evaporator example, the first fluid passages correspond to refrigerant passages 20.
  • Inlet chamber 18 is disposed adjacent to respective upstream ends 52 of each refrigerant passage 20. In the view of FIG. 2 , inlet chamber 18 extends outward from the page.
  • a plurality of first closure bars 54 are disposed along a first edge of first flow space 46 between inlet chamber 18 and upstream refrigerant passage ends 52.
  • One or more metering apertures 56 can be formed (e.g., by machining) through each first closure bar 54, effectively creating a plurality of metering plates 60 disposed in or over an upstream portion of upstream refrigerant passage ends 52.
  • Metering plates 60 either individually or in the form of first closure bar(s) 54, provide fluid communication between inlet chamber 18 and each refrigerant passage 20.
  • First closure bars 54, and/or individual metering plates 60 can be brazed or otherwise metallurgically bonded to adjacent parting plates 44 defining each first flow space 46.
  • First closure bars 54 and/or individual metering plates 60 can be assembled directly to a heat exchanger plate-and-fin subassembly such as the subassembly shown in FIG. 3 .
  • Metering apertures 56 can thus be more closely aligned with each fluid passage (e.g., refrigerant passages 20). It also allows inlet chamber 18 to be an open inlet chamber or header common to multiple refrigerant passages 20.
  • This and other related heat exchanger configurations eliminate the need for a separate distributor tube. In certain embodiments, this reduces the required number of individual fluid headers for each refrigerant passage, potentially reducing weight and manufacturing complexity. Manufacturing variation, tolerance stackup, and assembly errors all increase the occurrence of the misalignment of feedholes formed in the distributor tube relative to individual headers for each refrigerant passage.
  • Metering apertures 56 can be individually configured to control the pressure and resulting flow rate of first incoming fluid 12 (shown in FIG. 1 ) through each refrigerant passage 20.
  • one or more metering apertures 56 are cylindrical or frustoconical.
  • a cross-section of each metering aperture 56 can also be tailored to local or global flow and pressure parameters.
  • each metering aperture 56 can also vary according to its location.
  • the size, shape, and/or cross-sectional area of each aperture can be configured so as to provide a substantially equivalent pressure drop through each of the refrigerant passages 20 between inlet chamber 18 and outlet chamber 30 (shown in FIG. 1 ).
  • the size, shape and/or cross-sectional area of each metering aperture 56 can be made to vary according to its position along at least one of second/transverse axis 28 and third/no-flow axis 29.
  • a plurality of second fluid passages can extend through one or more of the second flow spaces 48.
  • the second fluid passages correspond to air passages 26, extending along second/transverse axis 28 substantially perpendicular to first/longitudinal axis 22 and refrigerant passages 20.
  • a second plurality of fins 62 can be disposed in each second flow space 48 to form first fluid passages extending along first/longitudinal axis 22.
  • the second plurality of fins 62 can be disposed transversely to the first plurality of fins 50.
  • FIG. 3 shows plate-and-fin subassembly 110 for a heat exchanger such as an evaporator.
  • FIG. 3 also includes first fluid passages 120, first/longitudinal axis 122, second fluid passages 126, second/transverse axis 128, third/no-flow axis 129, parting plates 144A, 144B, 144C, first flow space 146, second flow space 148, first fins 150, first closure bar 154, metering apertures 156, metering plates 160, second fins 162, first edges 166A, 166B, second closure bar 168, and second edges 170A, 170B.
  • First parting plate 144A, second parting plate 144B, and third parting plate 144C are generally parallel to one another and spaced apart along third/no-flow axis 129.
  • First plurality of fins 150 are disposed in first flow space 146 between first and second parting plates 144A, 144B, defining a plurality of first fluid passages 120 extending along first/longitudinal axis 122.
  • Second plurality of fins 162 can be disposed in second flow space 148 between second and third parting plates 144B, 144C. In the crossflow configuration, fins 162 can be arranged transversely to fins 150 to define a plurality of second fluid passages 126 extending along second/transverse axis 128.
  • first closure bar 154 is disposed along first edges 166A, 166B of first flow space 146 between first and second parting plates 144A, 144B.
  • First closure bar 154 can include a plurality of metering apertures 156 in communication with first flow space 146 between adjacent ones of fins 150. This forms effective metering plates 160 disposed at one end of each first fluid passage 120.
  • first closure bar 154 and/or individual metering plates 160 are metallurgically bonded to first and second parting plates 144A, 144B.
  • second closure bar 168 can be arranged transversely to first closure bar 154 along second edges 170A, 170B of first flow space 146. Second closure bar 168 can be free of any metering apertures to prevent leakage or intermingling of fluids passing separately through first and second flow spaces 146, 148. A longitudinal axis of second closure bar 168 can thus be arranged parallel to the first plurality of fins 150.
  • FIG. 4 shows an alternative embodiment which includes counterflow heat exchanger 210.
  • Various portions of counterflow heat exchanger 210 are cut away in FIG. 4 to illustrate the general location of certain internal features. Similar to FIG. 1 , which shows an example crossflow heat exchanger 10, counterflow heat exchanger 210 can also be configured as an evaporator-type heat exchanger. However, counterflow heat exchanger 210 is provided for illustrative purposes, and the described subject matter can be readily adapted to other uses.
  • First incoming fluid 212 for example, a liquid/vapor phase refrigerant mixture, can be received into first inlet port 214A formed in housing 216.
  • Inlet chamber 218A is disposed adjacent to an upstream side of one or more first fluid passages 220, with each passage extending along first/longitudinal axis 222.
  • First fluid 212 then enters outlet chamber 230, where it is discharged (as first outgoing fluid 236) from first outlet port 232A longitudinally spaced apart from first inlet port 214A.
  • Second incoming fluid 224 enters via second inlet port 214B, then flows through housing 216 before exiting from second outlet chamber 230B.
  • Second inlet port 214B is also longitudinally spaced apart from second outlet port 232B.
  • second inlet port 214B can be disposed at the same longitudinal end of heat exchanger 210 as first outlet port 232A, while first inlet port 214A can be disposed at the same longitudinal end of heat exchanger 210 as second outlet port 232B.
  • heat exchanger 210 can be further adapted to a coflow relationship in which fluid inlets 214A, 214B are disposed at the same longitudinal end, and are longitudinally spaced apart from outlet ports 232A, 232B.
  • Second fluid 224 flows through heat exchanger 210 via a plurality of longitudinal second fluid passages 226 in heat transfer relationship with the one or more first fluid passages 220.
  • Multiple layers of first fluid passages 220 and second fluid passages 226 can be stacked in an alternating manner between adjacent parting plates along third/no-flow axis 229.
  • passages 226 can be arranged in a serpentine manner through each layer so that second fluid 224 flows back and forth along first axis 222 before exiting via second outlet port 232B. This is best seen in FIG. 5 .
  • FIG. 5 shows plate-and-fin subassembly 310 for a heat exchanger such as counterflow heat exchanger 210 shown in FIG. 4 .
  • First parting plate 344A, second parting plate 344B, and third parting plate 344C are generally parallel to one another and spaced apart along third/no-flow axis 329.
  • First plurality of fins 350 are disposed in first flow space 346 between first and second parting plates 344A, 344B, defining a plurality of first passages 320 extending along first/longitudinal flow axis 322.
  • Second plurality of fins 362 can be disposed in second flow space 348 between second and third parting plates 344B, 344C, defining a plurality of second passages 326 also extending along first/longitudinal flow axis 322. Second fins 362 can thus be arranged parallel to first fins 350.
  • first closure bar 354 is disposed along first edges 366A, 366B of first flow space 346 between first and second parting plates 344A, 344B.
  • First closure bar 354 can include a plurality of metering apertures 356 in communication with first flow space 346 between adjacent ones of first fins 350. This forms effective metering plates 360 disposed at one end of each first fluid passage 320.
  • first closure bar 354 and/or individual metering plates 360 are metallurgically bonded to first and second parting plates 344A, 344B.
  • second closure bar 368 can be arranged transversely to first closure bar 354 along second edges 370A, 370B of first flow space 346. Second closure bar 368 can be free of metering apertures to prevent leakage or intermingling of fluids passing through first and second flow spaces 346, 348.
  • fluid can flow in the same direction along second passages 326.
  • some fins 362 can optionally be recessed from first edges 366B, 366C to allow the fluid in second flow space 348 to change direction.
  • additional closure bars or plates can be disposed along first edges 366B, 366C to enclose the serpentine passages and retain the second fluid within second flow space 348.
  • a further embodiment of any of the foregoing heat exchangers wherein a cross-sectional area of each metering aperture varies along at least one of: the no-flow axis, and a transverse axis.
  • a further embodiment of any of the foregoing heat exchangers wherein a cross-sectional area of each metering aperture is configured so as to provide a substantially equivalent pressure drop through each of the plurality of first flow spaces between the first inlet port and the first outlet port.
  • a further embodiment of any of the foregoing heat exchangers further comprising a plurality of first fluid passages extending along a longitudinal axis of the at least one first flow space.
  • a further embodiment of any of the foregoing heat exchangers wherein the plurality of first fluid passages comprises a first plurality of fins disposed in the at least one first flow space.
  • each of the plurality of metering apertures includes at least one metering aperture in communication with each of the first fluid passages.
  • a further embodiment of any of the foregoing heat exchangers further comprising an inlet chamber disposed in fluid communication between the inlet port and the plurality of metering apertures.
  • a further embodiment of any of the foregoing heat exchangers further comprising a second inlet port; a second outlet port; and a plurality of second flow spaces providing communication between the second inlet port and the second outlet port; the plurality of second flow spaces defined between adjacent ones of at least some of the parting plates.
  • a further embodiment of any of the foregoing heat exchangers further comprising a second plurality of fins disposed in the at least one second flow space, the second plurality of fins defining a plurality of second fluid passages extending through the at least one second flow space.
  • a heat exchanger subassembly comprises a first parting plate, a second parting plate spaced apart from, and substantially parallel to, the first parting plate, a third parting plate spaced apart from, and substantially parallel to, the first and second parting plates.
  • a first flow space is disposed between the first and second parting plates, and a second flow space is disposed between the second and third parting plates.
  • a first closure bar is disposed along a first edge of the first flow space between the first and second parting plates. The first closure bar has a plurality of metering apertures in communication with the first flow space.
  • the heat exchanger subassembly of the preceding paragraph can optionally include, additionally and/or alternatively, any one or more of the following features, configurations and/or additional components:
  • a further embodiment of any of the foregoing heat exchanger subassemblies further comprising a first plurality of fins disposed in the first flow space; and a second plurality of fins disposed in the second flow space.
  • a further embodiment of any of the foregoing heat exchanger subassemblies further comprising a second closure bar arranged transversely to the first closure bar along a second edge of the first flow space, the second closure bar free of metering apertures.
  • An evaporator comprises a plurality of refrigerant passages in heat exchange relationship with a plurality of air passages.
  • a refrigerant inlet header is disposed adjacent to an upstream end of at least one of the plurality of refrigerant passages.
  • a first closure bar is disposed between the refrigerant inlet header and the upstream end of the at least one refrigerant passage.
  • a metering aperture is formed through the first closure bar and is aligned with the at least one refrigerant passage. The metering aperture provides fluid communication between the refrigerant inlet header and the at least one refrigerant passage.
  • the evaporator of the preceding paragraph can optionally include, additionally and/or alternatively, any one or more of the following features, configurations and/or additional components: A further embodiment of the foregoing evaporator, wherein the at least one refrigerant passage extends along a longitudinal axis of the evaporator.
  • a further embodiment of any of the foregoing evaporators further comprising a plurality of parting plates spaced apart along a no-flow axis of the heat exchanger; wherein the plurality of refrigerant passages and the plurality of air passages are stacked in an alternating manner between adjacent ones of the parting plates.
  • thermoelectric relationship includes a crossflow heat exchange relationship

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
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  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Description

    BACKGROUND
  • The described subject matter relates generally to heat exchangers, and more specifically to heat exchangers for use with in various refrigerant systems.
  • The current method of distributing a liquid/vapor mixture to the inlet face of an evaporator-type heat exchanger is through a distributor tube. An attempt is made to position holes of the distributor tube at optimum locations and to line them up with each fin passage of a plate fin heat exchanger. Due to tolerance accumulation and manufacturing variation, however, these holes feeding the liquid/vapor mixture do not readily line up with their respective passages. Thus there is often uneven distribution of the liquid/vapor mixture which reduces efficiency of thermal transfer.
  • A prior art heat exchanger, having the features of the preamble of claim 1, is disclosed in US-2009/0100854 A1 .
  • SUMMARY
  • The present invention provides a heat exchanger as claimed in claim 1.
  • BRIEF DESCRIPTION OF THE DRAWINGS
    • FIG. 1 shows an example evaporator-type heat exchanger.
    • FIG. 2 is a sectional view of the heat exchanger taken through line 2-2 of FIG. 1.
    • FIG. 3 depicts a heat exchanger subassembly suitable for use in the example evaporator-type heat exchanger of FIG. 1.
    • FIG. 4 shows an alternative embodiment of a counterflow heat exchanger.
    • FIG. 5 depicts an alternative heat exchanger subassembly suitable for use in the example counterflow heat exchanger of FIG. 4.
    DETAILED DESCRIPTION
  • FIG. 1 depicts crossflow heat exchanger 10 with various portions cut away to illustrate the general location of certain internal features. FIG. 1 also shows first fluid 12, inlet port 14, housing 16, inlet chamber 18, refrigerant passages 20, first/longitudinal axis 22, second incoming fluid 24, air passages 26, second/transverse axis 28, third/no-flow axis 29, outlet chamber 30, and first outlet port 32.
  • Heat exchanger 10 is described with reference to an example evaporator-type heat exchanger for an aircraft. The evaporator can be configured as part of a vapor-cycle air management system (not shown). However, it will be appreciated that the configuration of crossflow heat exchanger 10 shown here is provided for illustrative purposes, and the described subject matter can be readily adapted to other uses. For example, though shown as a crossflow evaporator-type heat exchanger, the described subject matter can be adapted to many other heat exchanger configurations in which flow rates of each fluid can be suitably managed. A second non-limiting example embodiment of a counterflow heat exchanger is shown in FIG. 4.
  • First incoming fluid 12 is received into inlet port 14 formed in housing 16. First incoming fluid 12 can be, for example, a refrigerant having previously been passed through an expansion valve (not shown). Inlet chamber 18 is disposed adjacent to an upstream side of one or more refrigerant passages 20 extending along first or longitudinal axis 22. In the crossflow heat exchange relationship of FIG. 1, second incoming fluid 24 (e.g., air) flows transversely through a plurality of air passages 26 in heat exchange relationship with the one or more refrigerant passages 20. Air passages 26 can be substantially perpendicular to refrigerant passages 20 and can extend along second or transverse axis 28.
  • In certain embodiments, parting plates can be stacked along third or no-flow axis 29 to define first and second flow spaces (best shown in FIGS. 2 and 3). First flow spaces can provide communication between inlet port 14 and outlet port 32 via refrigerant passages 20, while second flow spaces can provide communication along air passages 26. In certain of these embodiments, multiple layers of refrigerant passages 20 and air passages 26 are stacked in alternating first and second flow spaces along third/no-flow axis 29.
  • In a heat exchange relationship for an evaporator, the mixed liquid/vapor phase of first incoming fluid 12 is heated and vaporized as it passes through inlet chamber 18, refrigerant passages 20, and outlet chamber 30. First outgoing fluid 36, which in this example is vaporized refrigerant, is then discharged from outlet port 32 spaced longitudinally apart from inlet chamber 14. As first incoming fluid 12 passes through refrigerant passages 20, the heat of vaporization chills adjacent/alternating air passages 26 so that second outgoing fluid 34 has a lower temperature than second incoming fluid 24.
  • To optimize heat transfer and fluid flow rates, the flow of first incoming fluid 12 (e.g., liquid/vapor phase refrigerant) can be metered before entering refrigerant passages 20 in the first flow space(s). Thus a plurality of metering plates can be disposed across an upstream end of at least one of these first flow spaces. As will be seen in subsequent figures, each of the plurality of metering plates can include at least one metering aperture providing fluid communication between the first inlet port and the at least one first flow space. In certain embodiments, the metering plate(s) can take the form of one or more closure bars or other equivalent structure metallurgically bonded to the internal features of the heat exchanger.
  • FIG. 2 shows a portion of example crossflow heat exchanger 10 taken across line 2-2 of FIG. 1. FIG. 2 also includes inlet chamber 18, refrigerant passages 20, first/longitudinal axis 22, air passages 26, second/transverse axis 28, third/no-flow axis 29, parting plates 44, first flow spaces 46, second flow spaces 48, first fins 50, upstream refrigerant passage ends 52, first closure bar 54, metering apertures 56, metering plates 60, and second fins 62.
  • A plurality of parting plates 44 are stacked along third/no-flow axis 29 of heat exchanger such that pairs of adjacent parting plates 44 define alternating first flow spaces 46 and second flow spaces 48, therebetween. Portions of first closure bars 56 are cut away to show first flow spaces 46 between parting plates 44, as well as a first plurality of fins 50 disposed in each first flow space 46. First fins 50 form first fluid passages extending along first/longitudinal axis 22. In the evaporator example, the first fluid passages correspond to refrigerant passages 20.
  • Inlet chamber 18 is disposed adjacent to respective upstream ends 52 of each refrigerant passage 20. In the view of FIG. 2, inlet chamber 18 extends outward from the page. A plurality of first closure bars 54 are disposed along a first edge of first flow space 46 between inlet chamber 18 and upstream refrigerant passage ends 52. One or more metering apertures 56 can be formed (e.g., by machining) through each first closure bar 54, effectively creating a plurality of metering plates 60 disposed in or over an upstream portion of upstream refrigerant passage ends 52. Metering plates 60, either individually or in the form of first closure bar(s) 54, provide fluid communication between inlet chamber 18 and each refrigerant passage 20. First closure bars 54, and/or individual metering plates 60 can be brazed or otherwise metallurgically bonded to adjacent parting plates 44 defining each first flow space 46. First closure bars 54 and/or individual metering plates 60 can be assembled directly to a heat exchanger plate-and-fin subassembly such as the subassembly shown in FIG. 3. Metering apertures 56 can thus be more closely aligned with each fluid passage (e.g., refrigerant passages 20). It also allows inlet chamber 18 to be an open inlet chamber or header common to multiple refrigerant passages 20.
  • This and other related heat exchanger configurations eliminate the need for a separate distributor tube. In certain embodiments, this reduces the required number of individual fluid headers for each refrigerant passage, potentially reducing weight and manufacturing complexity. Manufacturing variation, tolerance stackup, and assembly errors all increase the occurrence of the misalignment of feedholes formed in the distributor tube relative to individual headers for each refrigerant passage.
  • Metering apertures 56 can be individually configured to control the pressure and resulting flow rate of first incoming fluid 12 (shown in FIG. 1) through each refrigerant passage 20. In certain embodiments, one or more metering apertures 56 are cylindrical or frustoconical. A cross-section of each metering aperture 56 can also be tailored to local or global flow and pressure parameters.
  • The cross-sectional area of each metering aperture 56 can also vary according to its location. In certain embodiments, the size, shape, and/or cross-sectional area of each aperture can be configured so as to provide a substantially equivalent pressure drop through each of the refrigerant passages 20 between inlet chamber 18 and outlet chamber 30 (shown in FIG. 1). In certain embodiments, the size, shape and/or cross-sectional area of each metering aperture 56 can be made to vary according to its position along at least one of second/transverse axis 28 and third/no-flow axis 29.
  • To further enhance heat transfer relationships, a plurality of second fluid passages can extend through one or more of the second flow spaces 48. In the evaporator example, the second fluid passages correspond to air passages 26, extending along second/transverse axis 28 substantially perpendicular to first/longitudinal axis 22 and refrigerant passages 20. A second plurality of fins 62 can be disposed in each second flow space 48 to form first fluid passages extending along first/longitudinal axis 22. In the crossflow heat exchange relationship, the second plurality of fins 62 can be disposed transversely to the first plurality of fins 50.
  • FIG. 3 shows plate-and-fin subassembly 110 for a heat exchanger such as an evaporator. FIG. 3 also includes first fluid passages 120, first/longitudinal axis 122, second fluid passages 126, second/transverse axis 128, third/no-flow axis 129, parting plates 144A, 144B, 144C, first flow space 146, second flow space 148, first fins 150, first closure bar 154, metering apertures 156, metering plates 160, second fins 162, first edges 166A, 166B, second closure bar 168, and second edges 170A, 170B.
  • First parting plate 144A, second parting plate 144B, and third parting plate 144C are generally parallel to one another and spaced apart along third/no-flow axis 129. First plurality of fins 150 are disposed in first flow space 146 between first and second parting plates 144A, 144B, defining a plurality of first fluid passages 120 extending along first/longitudinal axis 122. Second plurality of fins 162 can be disposed in second flow space 148 between second and third parting plates 144B, 144C. In the crossflow configuration, fins 162 can be arranged transversely to fins 150 to define a plurality of second fluid passages 126 extending along second/transverse axis 128.
  • Similar to FIG. 2, first closure bar 154 is disposed along first edges 166A, 166B of first flow space 146 between first and second parting plates 144A, 144B. First closure bar 154 can include a plurality of metering apertures 156 in communication with first flow space 146 between adjacent ones of fins 150. This forms effective metering plates 160 disposed at one end of each first fluid passage 120. In certain embodiments, first closure bar 154 and/or individual metering plates 160 are metallurgically bonded to first and second parting plates 144A, 144B.
  • In certain embodiments, second closure bar 168 can be arranged transversely to first closure bar 154 along second edges 170A, 170B of first flow space 146. Second closure bar 168 can be free of any metering apertures to prevent leakage or intermingling of fluids passing separately through first and second flow spaces 146, 148. A longitudinal axis of second closure bar 168 can thus be arranged parallel to the first plurality of fins 150.
  • FIG. 4 shows an alternative embodiment which includes counterflow heat exchanger 210. Various portions of counterflow heat exchanger 210 are cut away in FIG. 4 to illustrate the general location of certain internal features. Similar to FIG. 1, which shows an example crossflow heat exchanger 10, counterflow heat exchanger 210 can also be configured as an evaporator-type heat exchanger. However, counterflow heat exchanger 210 is provided for illustrative purposes, and the described subject matter can be readily adapted to other uses.
  • First incoming fluid 212, for example, a liquid/vapor phase refrigerant mixture, can be received into first inlet port 214A formed in housing 216. Inlet chamber 218A is disposed adjacent to an upstream side of one or more first fluid passages 220, with each passage extending along first/longitudinal axis 222. First fluid 212 then enters outlet chamber 230, where it is discharged (as first outgoing fluid 236) from first outlet port 232A longitudinally spaced apart from first inlet port 214A.
  • Second incoming fluid 224, for example, air, enters via second inlet port 214B, then flows through housing 216 before exiting from second outlet chamber 230B. Second inlet port 214B is also longitudinally spaced apart from second outlet port 232B. In a counterflow design, second inlet port 214B can be disposed at the same longitudinal end of heat exchanger 210 as first outlet port 232A, while first inlet port 214A can be disposed at the same longitudinal end of heat exchanger 210 as second outlet port 232B. It will be appreciated that heat exchanger 210 can be further adapted to a coflow relationship in which fluid inlets 214A, 214B are disposed at the same longitudinal end, and are longitudinally spaced apart from outlet ports 232A, 232B.
  • Second fluid 224 flows through heat exchanger 210 via a plurality of longitudinal second fluid passages 226 in heat transfer relationship with the one or more first fluid passages 220. Multiple layers of first fluid passages 220 and second fluid passages 226 can be stacked in an alternating manner between adjacent parting plates along third/no-flow axis 229. In certain embodiments, passages 226 can be arranged in a serpentine manner through each layer so that second fluid 224 flows back and forth along first axis 222 before exiting via second outlet port 232B. This is best seen in FIG. 5.
  • FIG. 5 shows plate-and-fin subassembly 310 for a heat exchanger such as counterflow heat exchanger 210 shown in FIG. 4. First parting plate 344A, second parting plate 344B, and third parting plate 344C are generally parallel to one another and spaced apart along third/no-flow axis 329. First plurality of fins 350 are disposed in first flow space 346 between first and second parting plates 344A, 344B, defining a plurality of first passages 320 extending along first/longitudinal flow axis 322. Second plurality of fins 362 can be disposed in second flow space 348 between second and third parting plates 344B, 344C, defining a plurality of second passages 326 also extending along first/longitudinal flow axis 322. Second fins 362 can thus be arranged parallel to first fins 350.
  • Similar to FIGS. 2 and 3, first closure bar 354 is disposed along first edges 366A, 366B of first flow space 346 between first and second parting plates 344A, 344B. First closure bar 354 can include a plurality of metering apertures 356 in communication with first flow space 346 between adjacent ones of first fins 350. This forms effective metering plates 360 disposed at one end of each first fluid passage 320. In certain embodiments, first closure bar 354 and/or individual metering plates 360 are metallurgically bonded to first and second parting plates 344A, 344B. In certain embodiments, second closure bar 368 can be arranged transversely to first closure bar 354 along second edges 370A, 370B of first flow space 346. Second closure bar 368 can be free of metering apertures to prevent leakage or intermingling of fluids passing through first and second flow spaces 346, 348.
  • In certain embodiments of a counterflow heat exchanger, fluid can flow in the same direction along second passages 326. However, to allow for serpentine flow in second flow space 348, some fins 362 can optionally be recessed from first edges 366B, 366C to allow the fluid in second flow space 348 to change direction. It will be appreciated that, in these embodiments, additional closure bars or plates (not shown for clarity) can be disposed along first edges 366B, 366C to enclose the serpentine passages and retain the second fluid within second flow space 348.
  • While described with reference to an exemplary embodiment(s), it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment(s) disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.
  • A further embodiment of any of the foregoing heat exchangers, wherein a cross-sectional area of each metering aperture varies along at least one of: the no-flow axis, and a transverse axis.
  • A further embodiment of any of the foregoing heat exchangers, wherein a cross-sectional area of each metering aperture is configured so as to provide a substantially equivalent pressure drop through each of the plurality of first flow spaces between the first inlet port and the first outlet port.
  • A further embodiment of any of the foregoing heat exchangers, further comprising a plurality of first fluid passages extending along a longitudinal axis of the at least one first flow space.
  • A further embodiment of any of the foregoing heat exchangers, wherein the plurality of first fluid passages comprises a first plurality of fins disposed in the at least one first flow space.
  • A further embodiment of any of the foregoing heat exchangers, wherein each of the plurality of metering apertures includes at least one metering aperture in communication with each of the first fluid passages.
  • A further embodiment of any of the foregoing heat exchangers, further comprising an inlet chamber disposed in fluid communication between the inlet port and the plurality of metering apertures.
  • A further embodiment of any of the foregoing heat exchangers, further comprising a second inlet port; a second outlet port; and a plurality of second flow spaces providing communication between the second inlet port and the second outlet port; the plurality of second flow spaces defined between adjacent ones of at least some of the parting plates.
  • A further embodiment of any of the foregoing heat exchangers, wherein the plurality of parting plates define alternating ones of the first plurality of flow spaces and the second plurality of second flow spaces.
  • A further embodiment of any of the foregoing heat exchangers, further comprising a second plurality of fins disposed in the at least one second flow space, the second plurality of fins defining a plurality of second fluid passages extending through the at least one second flow space.
  • A further embodiment of any of the foregoing heat exchangers, wherein the plurality of second fluid passages extend along a transverse axis.
  • A further embodiment of any of the foregoing heat exchangers, wherein the plurality of second fluid passages extend along a longitudinal axis.
  • A heat exchanger subassembly comprises a first parting plate, a second parting plate spaced apart from, and substantially parallel to, the first parting plate, a third parting plate spaced apart from, and substantially parallel to, the first and second parting plates. A first flow space is disposed between the first and second parting plates, and a second flow space is disposed between the second and third parting plates. A first closure bar is disposed along a first edge of the first flow space between the first and second parting plates. The first closure bar has a plurality of metering apertures in communication with the first flow space.
  • The heat exchanger subassembly of the preceding paragraph can optionally include, additionally and/or alternatively, any one or more of the following features, configurations and/or additional components:
    A further embodiment of the foregoing heat exchanger subassembly, wherein the first closure bar is metallurgically bonded to the first and second parting plates.
  • A further embodiment of any of the foregoing heat exchanger subassemblies, further comprising a first plurality of fins disposed in the first flow space; and a second plurality of fins disposed in the second flow space.
  • A further embodiment of any of the foregoing heat exchanger subassemblies, wherein the second plurality of fins define a plurality of second flow passages arranged transversely to a plurality of first flow passages defined by the first plurality of fins.
  • A further embodiment of any of the foregoing heat exchanger subassemblies, wherein the second plurality of fins define a plurality of second flow passages arranged parallel to a plurality of first flow passages defined by the first plurality of fins.
  • A further embodiment of any of the foregoing heat exchanger subassemblies, wherein a cross-sectional area of each metering aperture varies along a length of the first closure bar.
  • A further embodiment of any of the foregoing heat exchanger subassemblies, further comprising a second closure bar arranged transversely to the first closure bar along a second edge of the first flow space, the second closure bar free of metering apertures.
  • An evaporator comprises a plurality of refrigerant passages in heat exchange relationship with a plurality of air passages. A refrigerant inlet header is disposed adjacent to an upstream end of at least one of the plurality of refrigerant passages. A first closure bar is disposed between the refrigerant inlet header and the upstream end of the at least one refrigerant passage. A metering aperture is formed through the first closure bar and is aligned with the at least one refrigerant passage. The metering aperture provides fluid communication between the refrigerant inlet header and the at least one refrigerant passage.
  • The evaporator of the preceding paragraph can optionally include, additionally and/or alternatively, any one or more of the following features, configurations and/or additional components:
    A further embodiment of the foregoing evaporator, wherein the at least one refrigerant passage extends along a longitudinal axis of the evaporator.
  • A further embodiment of any of the foregoing evaporators, further comprising a plurality of parting plates spaced apart along a no-flow axis of the heat exchanger; wherein the plurality of refrigerant passages and the plurality of air passages are stacked in an alternating manner between adjacent ones of the parting plates.
  • A further embodiment of any of the foregoing evaporators, wherein a cross-sectional area of each metering aperture varies along a length of the first closure bar.
  • A further embodiment of any of the foregoing evaporators, wherein the heat exchange relationship includes a crossflow heat exchange relationship.
  • A further embodiment of any of the foregoing evaporators, wherein the heat exchange relationship includes a counterflow heat exchange relationship.
  • While described with reference to an exemplary embodiment(s), it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment(s) disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.

Claims (14)

  1. A heat exchanger (10; 210) comprising:
    a first inlet port (14; 214A);
    a first outlet port (32; 232A) longitudinally spaced apart from the first inlet port (14; 214A);
    a plurality of substantially parallel parting plates (144; 344); and
    a plurality of first flow spaces (146; 346) providing communication between the first inlet port (14; 214A) and the first outlet port (32; 232A); the plurality of first flow spaces (146; 346) defined between adjacent ones of at least some of the parting plates (144;344);
    characterised in that:
    the heat exchanger (10;210) further comprises a plurality of metering plates (154; 354) disposed across an upstream end of at least one of the first flow spaces (146; 346), each of the plurality of metering plates (154; 354) including at least one metering aperture (156; 356) providing fluid communication between the first inlet port (14; 214A) and the at least one first flow space (146; 346); and
    the parting plates (144; 344) are stacked along a no-flow axis (129; 239).
  2. The heat exchanger (10; 210) of claim 1, wherein the plurality of metering plates comprises a first closure bar (154; 354) arranged along a first edge (166; 366) of the at least one first flow space (146; 346) proximate to the first inlet port (14; 214A).
  3. The heat exchanger (10; 210) of claim 2, wherein the first closure bar (154; 354) is metallurgically bonded to adjacent ones of the parting plates (144; 344) defining the one of the first flow spaces (146; 346).
  4. The heat exchanger (10; 210) of claim 2 or 3, further comprising a second closure bar (168; 368) arranged transversely to the first closure bar (154; 354) along a second edge (170; 370) of the first flow space (146; 346), the second closure bar (168; 368) being free of any metering apertures.
  5. The heat exchanger (10; 210) of any preceding claim, wherein a cross-sectional area of each metering aperture (156; 356) varies along the no-flow axis (129; 329) and/or a transverse axis (128; 328).
  6. The heat exchanger (10; 210) of any preceding claim, wherein a cross-sectional area of each metering aperture (156; 356) is configured so as to provide a substantially equivalent pressure drop through each of the plurality of first flow spaces (146; 346) between the first inlet port (14; 214A) and the first outlet port (32; 232A).
  7. The heat exchanger (10; 210) of any preceding claim, further comprising a plurality of first fluid passages (120; 320) extending along a longitudinal axis (122; 232) of the at least one first flow space (146; 346).
  8. The heat exchanger (10; 210) of claim 7, wherein the plurality of first fluid passages (146; 346) comprises a first plurality of fins (150; 350) disposed in the at least one first flow space (146; 346).
  9. The heat exchanger (10; 210) of claim 7 or 8, wherein each of the plurality of metering apertures (156; 356) includes at least one metering aperture (156; 356) in communication with each of the first fluid passages (120; 320).
  10. The heat exchanger (10; 210) of any of claims 7 to 9, further comprising an inlet chamber (18; 218) disposed in fluid communication between the first inlet port (14; 214A) and the plurality of metering apertures (156; 356).
  11. The heat exchanger (10; 210) of any of claims 7 to 10, further comprising:
    a second inlet port (214B);
    a second outlet port (232B); and
    a plurality of second flow spaces (148; 348) providing communication between the second inlet port (214B) and the second outlet port (232B), the plurality of second flow spaces (148; 348) being defined between adjacent ones of at least some of the parting plates (144; 344).
  12. The heat exchanger (10; 210) of claim 11, wherein the plurality of parting plates (144; 344) define alternating ones of the first plurality of flow spaces (146; 346) and the second plurality of second flow spaces (148; 348).
  13. The heat exchanger (10; 210) of claim 11 or 12, further comprising a second plurality of fins (162; 362) disposed in the at least one second flow space (148; 348), the second plurality of fins (162; 362) defining a plurality of second fluid passages (126; 326) extending through the at least one second flow space (148; 348).
  14. The heat exchanger (10; 2. 210) of claim 13, wherein the plurality of second fluid passages (126; 326) extend:
    along a transverse axis (128); or
    along a longitudinal axis.
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GB1216306A (en) 1967-03-31 1970-12-16 Marston Excelsior Limiited Plate-type heat exchangers
FR2017807A1 (en) 1968-09-11 1970-05-22 Kobe Steel Ltd
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EP2816307A3 (en) 2015-01-14
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US20140318175A1 (en) 2014-10-30
EP3462119B1 (en) 2021-03-31

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