EP2816307B1 - Integrierter Verteiler eines Wärmetauschers - Google Patents

Integrierter Verteiler eines Wärmetauschers 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
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EP14166550.5A
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English (en)
French (fr)
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EP2816307A2 (de
EP2816307A3 (de
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/de
Publication of EP2816307A2 publication Critical patent/EP2816307A2/de
Publication of EP2816307A3 publication Critical patent/EP2816307A3/de
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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)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
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  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Claims (14)

  1. Wärmetauscher (10; 210), umfassend:
    eine erste Einlassöffnung (14; 214A);
    eine erste Auslassöffnung (32; 232A), die in Längsrichtung von der ersten Einlassöffnung (14; 214A) beabstandet ist;
    eine Vielzahl von im Wesentlichen parallelen Trennplatten (144; 344); und
    eine Vielzahl von ersten Strömungsräumen (146; 346), die eine Verbindung zwischen der ersten Einlassöffnung (14; 214A) und der ersten Auslassöffnung (32; 232A) bereitstellt; wobei die Vielzahl von ersten Strömungsräumen (146; 346) zwischen angrenzenden der mindestens einigen der Trennplatten (144; 344) definiert ist;
    dadurch gekennzeichnet, dass:
    der Wärmetauscher (10; 210) ferner eine Vielzahl von Dosierplatten (154; 354) umfasst, die über ein stromaufwärts gelegenes Ende von mindestens einem der ersten Strömungsräume (146; 346) angeordnet ist, wobei jede der Vielzahl von Dosierplatten (154; 354) mindestens eine Dosieröffnung (156; 356) beinhaltet, die eine Fluidverbindung zwischen der ersten Einlassöffnung (14; 214A) und dem mindestens einen ersten Strömungsraum (146; 346) bereitstellt; und
    die Trennplatten (144; 344) entlang einer Nichtströmungsachse (129; 239) aufeinandergeschichtet sind.
  2. Wärmetauscher (10; 210) nach Anspruch 1, wobei die Vielzahl von Dosierplatten eine erste Schließleiste (154; 354) umfasst, die entlang einer ersten Kante (166; 366) des mindestens einen ersten Strömungsraums (146; 346) in der Nähe der ersten Einlassöffnung (14; 214A) angebracht ist.
  3. Wärmetauscher (10, 210) nach Anspruch 2, wobei die erste Schließleiste (154; 354) metallurgisch mit den angrenzenden der Trennungsplatten (144; 344) verbunden ist, die den einen der ersten Strömungsräume (146; 346) begrenzen.
  4. Wärmetauscher (10; 210) nach Anspruch 2 oder 3, ferner umfassend eine zweite Schließleiste (168; 368), die quer zu der ersten Schließleiste (154; 354) entlang einer zweiten Kante (170; 370) des ersten Strömungsraums (146; 346) angebracht ist, wobei die zweite Schließleiste (168; 368) frei von jeglichen Dosieröffnungen ist.
  5. Wärmetauscher (10; 210) nach einem der vorhergehenden Ansprüche, wobei eine Querschnittsfläche jeder Dosieröffnung (156; 356) entlang der Nichtströmungsachse (129; 329) und/oder einer Querachse (128; 328) variiert.
  6. Wärmetauscher (10; 210) nach einem der vorhergehenden Ansprüche, wobei eine Querschnittsfläche jeder Dosieröffnung (156; 356) derart konfiguriert ist, einen im Wesentlichen äquivalenten Druckabfall durch jeden der Vielzahl der ersten Strömungsräume (146; 346) zwischen der ersten Einlassöffnung (14; 214A) und der ersten Auslassöffnung (32; 232A) bereitzustellen.
  7. Wärmetauscher (10; 210) nach einem der vorhergehenden Ansprüche, ferner umfassend eine Vielzahl von Fluiddurchlässen (120; 320), die sich entlang einer Längsachse (122; 232) des mindestens einen ersten Strömungsraums (146; 346) erstreckt.
  8. Wärmetauscher (10; 210) nach Anspruch 7, wobei die Vielzahl von ersten Fluiddurchlässen (146; 346) eine erste Vielzahl von Rippen (150; 350) umfasst, die in dem mindestens einen ersten Strömungsraum (146; 346) angeordnet ist.
  9. Wärmetauscher (10; 210) nach Anspruch 7 oder 8, wobei jede der Vielzahl von Dosieröffnungen (156; 356) mindestens eine Dosieröffnung (156; 356) beinhaltet, die in Verbindung mit jeder der ersten Fluiddurchlässe (120; 320) steht.
  10. Wärmetauscher (10; 210) nach einem der Ansprüche 7 bis 9, ferner umfassend eine Einlasskammer (18; 218), die in Fluidverbindung zwischen der ersten Einlassöffnung (14; 214A) und der Vielzahl von Dosieröffnungen (156; 356) angeordnet ist.
  11. Wärmetauscher (10; 210) nach einem der Ansprüche 7 bis 10, ferner umfassend:
    eine zweite Einlassöffnung (214B);
    eine zweite Auslassöffnung (232B); und
    eine Vielzahl von zweiten Strömungsräumen (148; 348), die eine Verbindung zwischen der zweiten Einlassöffnung (214B) und der zweiten Auslassöffnung (232B) bereitstellen, wobei die Vielzahl von zweiten Strömungsräumen (148; 348) zwischen angrenzenden der mindestens einigen der Trennplatten (144; 344) definiert wird.
  12. Wärmetauscher (10; 210) nach Anspruch 11, wobei die Vielzahl von Trennplatten (144; 344) sich abwechselnde der ersten Vielzahl von Strömungsräumen (146; 346) und der zweiten Vielzahl von zweiten Strömungsräumen (148; 348) definiert.
  13. Wärmetauscher (10; 210) nach Anspruch 11 oder 12, ferner umfassend eine zweite Vielzahl von Rippen (162; 362), die in dem mindestens einen zweiten Strömungsraum (148; 348) angeordnet ist, wobei die zweite Vielzahl von Rippen (162; 362) eine Vielzahl von zweiten Fluiddurchlässen (126; 326) definiert, die sich durch den mindestens einen zweiten Strömungsraum (148; 348) erstreckt.
  14. Wärmetauscher (10; 210) nach Anspruch 13,
    wobei sich die Vielzahl von zweiten Fluiddurchlässen (126; 326):
    entlang einer Querachse (128); oder
    entlang einer Längsachse erstreckt.
EP14166550.5A 2013-04-30 2014-04-30 Integrierter Verteiler eines Wärmetauschers Active EP2816307B1 (de)

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US3380517A (en) 1966-09-26 1968-04-30 Trane Co Plate type heat exchangers
GB1216306A (en) 1967-03-31 1970-12-16 Marston Excelsior Limiited Plate-type heat exchangers
GB1288227A (de) 1968-09-11 1972-09-06
NL6918069A (de) * 1969-03-03 1970-09-07
US4249595A (en) 1979-09-07 1981-02-10 The Trane Company Plate type heat exchanger with bar means for flow control and structural support
US4450903A (en) 1982-09-20 1984-05-29 The Trane Company Plate type heat exchanger with transverse hollow slotted bar
FR2547898B1 (fr) 1983-06-24 1985-11-29 Air Liquide Procede et dispositif pour vaporiser un liquide par echange de chaleur avec un deuxieme fluide, et leur application a une installation de distillation d'air
US4844151A (en) * 1986-12-23 1989-07-04 Sundstrand Corporation Heat exchanger apparatus
US5029640A (en) * 1989-05-01 1991-07-09 Sundstrand Corporation Gas-liquid impingement plate type heat exchanger
US20010047862A1 (en) * 1995-04-13 2001-12-06 Anderson Alexander F. Carbon/carbon heat exchanger and manufacturing method
TW552382B (en) * 2001-06-18 2003-09-11 Showa Dendo Kk Evaporator, manufacturing method of the same, header for evaporator and refrigeration system
US20090100854A1 (en) * 2007-10-18 2009-04-23 Ilya Reyzin Evaporatively cooled condenser
PL2737270T3 (pl) * 2011-07-28 2018-10-31 Nestec S.A. Sposoby i urządzenia do podgrzewania lub chłodzenia materiałów lepkich
US9279626B2 (en) * 2012-01-23 2016-03-08 Honeywell International Inc. Plate-fin heat exchanger with a porous blocker bar
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EP3462119B1 (de) 2021-03-31
EP2816307A2 (de) 2014-12-24
US20140318175A1 (en) 2014-10-30
EP2816307A3 (de) 2015-01-14

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