US3161234A - Multipass evaporator - Google Patents

Multipass evaporator Download PDF

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US3161234A
US3161234A US230878A US23087862A US3161234A US 3161234 A US3161234 A US 3161234A US 230878 A US230878 A US 230878A US 23087862 A US23087862 A US 23087862A US 3161234 A US3161234 A US 3161234A
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continuous
continuous fin
fin element
evaporator
elements
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US230878A
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George C Rannenberg
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Raytheon Technologies Corp
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United Aircraft Corp
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    • 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
    • F25B39/022Evaporators with plate-like or laminated elements
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S165/00Heat exchange
    • Y10S165/355Heat exchange having separate flow passage for two distinct fluids
    • Y10S165/399Corrugated heat exchange plate

Definitions

  • an evaporator is that part of a refrigeration system where the refrigerant enters the evaporator as a liquid and is vaporized to produce refrigeration. As the air passes through the evaporator, it comes in indirect heat exchange relation with the refrigerant, gives up its heat thereto and is discharged at a much lower temperature than it was when entering the evaporator.
  • the temperature of the refrigerant decreases as a function of its length of travel in the evaporator until it reaches a particular point intermediate the inlet and outlet of the evaporator. At this point, the liquid refrigerant vaporizes and becomes superheated and hence becomes hotter as it continues its travel. The temperature of the refrigerant increases until it reaches the outlet of the evaporator.
  • Conventional refrigerant evaporators constructed of tubes are often arranged to take advantage of this feature by locating the first refrigerant pass intermediate the refrigerant inlet and refrigerant outlet of the evaporator.
  • the air to be cooled is first placed in indirect heat exchange relation with the fourth pass (Where the temperature of the refrigerant is at its hottest value) and the third pass is placed in indirect heat exchange relation with the air leaving the evaporator.
  • the second pass is sandwiched between the first and third pass.
  • FIG. 1 is an isometric view of a portion of the evaporator showing an arrangement in which internal and external headers are used.
  • FIG. 2 is a cross-sectional view taken along line 22 of FIG. 1, particularly showing the novel location of the refrigerant passes.
  • FIG. 3 is a schematic illustration showing the novel arrangement of external headers, one inside the other.
  • FIG. 4 is a schematic illustration wherein all the headers are internal.
  • FIG. 1 shows a portion 7 of the core of the evaporator generally illustrated by numeral fill and a pair of air passes indicated by the jnumerals i2 and 14 sandwiching the refrigerant core eempereral 16.
  • this section of the core has been exploded to illustrate the inventive concept, but only represents a portion of the entire core. It should be understood that the entire evaporator is built up by alternately stacking similar air and refrigerant core elements to obtain the size necessary to afford optimum refrigeration in any given application.
  • the general construction of the evaporator may take any conventional form, however, the plate-fin type of heat exchanger is often preferred for reasons of low weight and volume.
  • the partial core comprises end plate 16 and dividing walls 18, 26 and 22 extending longitudinally through the evaporator.
  • Generally parallel fin section 24 is sandwiched between end plate 16 and dividing wall 18 for defining an air pass.
  • the generally parallel fin section 24 may be pierced, serrated, rufiled or straight, depending on such matters as economics and the fluids involved.
  • the air is admitted at the top end of the evaporator and is discharged at the bottom in FIG. 1, although any orientation with gravity may be used.
  • another air passage, shown in FIG. 1, is formed from a pair of dividing walls 29 and 22, closure members 32 and 34 and the heat transfer fins 26.
  • the refrigerant passes located between a pair of air passes, comprise a similar plate-fin construction, only extending transversely of the air passes. Since the actual construction of the evaporator may take any well-known form, a description thereof, for the sake of convenience, is omitted.
  • FIG. 2 illustrates the novel arrangement of the refrigerant passes.
  • the refrigerant is admitted into the evaporator through a plurality of tubes, indicated by numeral 34, which lead into header 36.
  • the header directs the flow through the first pass, indicated by Letter A.
  • the first pass is located intermediate the top and bottom closure plates of the refrigerant core.
  • the pass comprises a plurality of fins which extend between the dividing plates 13 and 20.
  • Turning passages 37 defined by fins, are mounted at the far end of the inlet and direct the refrigerant to the second pass B and similarly, turning fins B located between the third pass C and the second pass B direct refrigerant to the third pass.
  • the refrigerant feeds into an external header 41 which conducts the refrigerant in the third pass to the fourth pass D.
  • the refrigerant which at this point has vaporized and become superheated, is discharged into the outlet header 44 and then directed through the discharge conduit 46 to the next stage (not shown) in the refrigeration system.
  • each pass may contain a different number of passages, and preferably, the number of passages in each pass are increased as the liquid is vaporized.
  • the liquid passing through the evaporator remains a liquid until it reaches the end of the third or the beginning of the fourth pass.
  • the hot air entering the evaporator is immediately in indirect heat exchange relation with the superheated refrigerant passing through pass D.
  • the air becomes cooled, it passes in indirect heat exchange relationship with the liquid refrigerant in passes A and B, and finally theair passes over the lowest temperature refrigerant as it reaches pass C. after'which the air.
  • the evaporator has a highheat transfer efiiciency and hence achieves minimum heat exchanger or evaporator size for 'agiven application.
  • FIGS. 3 and 4 are exemplaryshowings of a refrigerant core element embodying the t' present' invention,- but,eni-' ploying diiferent header arrangements; .
  • the letters A, B, 'C and D represent successive passes in therefrigeration core.
  • FIG. 3 shows all the headers mounted externally of the As noted in the drawing, header 50 is inserted in-" ternally of header 52 and wall 54 forms a common wali dividing the two headers. This placing of one header inside the other with flow in opposite directions is a v unique and novel wayof accomplishing the desired core temperature distribution. Header 56 is connectedto the. inlet of the evaporator and header 58"is connected to the V The refrigerant'core element depicted in FIG. 4" is, inmost respects, identical to the core element. shown inFIGSJ 1 and 2, excepttha't internal header 53' connects outlet.
  • this invention is'a novel arrangement of the passes in therefrigerant' core section of an evaporator which, by virtue ofthis arrangement, provides an effective evaporator while permitting'a' reduc-' tion of the overall evaporator size. It will be appreciated that this advantage is particularly important in aircraftapplication, since size and the attendant reduction in weight increase the overall performance of-the aircraft. a
  • the invention is not limited enema versely to said channels'formed from first, second, third and fourth fin elements and being adapted to place fiuid passing straight: through said open-ended channel formed from saidfifth continuous fin element in heat exchange relation to the 'fiuid passing through channels formed from said first, second, thirdand fourth fin elements, so
  • a continuous fin element is in immediate heat exchange relation with the fluid in said first continuous fin element and fluiddischarging frorn said open-ended channel of the fifth continuous finelement is in heat exchange relation with the fluid in said thirdcontinuous fin element.
  • a multichannel, multiplate and fin evaporator comprising at'least onecontinuous fin element,.spaced apart parallel extending'plate ,rnembers. sandwiching the opposite'ends of thefin element for defining therewith a series.
  • I claimf r 1 A multiplate and jfin core section of an evaporator fiuid intended t0 be' cooled, a series of fin elements mounted adjacent one of said parallel, extending plate members, and extending in transverse relationto said one of continuousfin elements for defining four passes for receiving a refrigerant, other spaced apart parallel extending plate' members lying transversely to said spaced apart parallel extending plate members, sandwiching the series of fin elements for defining therewith four. passes, said fourpasses being located one next to the other such "that the fourth passis'adjacent to the inlet of said chancomprising a first continuous fin element, a second con-' tinuous fin element located adjacent.
  • first contin-T' uous fin element a third continuous fin element located adjacent to said second continuous fin element, and a fourth continuous fin element located adjacent to said third continuous fin element, spaced plates sandwiching said first, second, third and fourthcontinuousfin elements for I defining parallel channels, closure plate members extending laterally from said .space'd 'plates separating said ffir-st,
  • a refrigerant core section of an evaporator having side wall plates and top and bottom closure members, continuous fin elements extending between said side wall plates for defining a series of open-ended channels, means separating said continuous fin elements for defining a pair of outwardly mounted passes mounted adjacent the bottom and top closure members and inwardly mounted passes mounted between said outwardly mounted passes, first and second external headers mounted adjacent to one end of said continuous fin elements, a common wall separating said first external headers, said first external header connecting the pair of inwardly mounted passes and the second external header connecting the outwardly mounted passes, a third external header mounted adja cent to an inwardly mounted and an outwardly mounted continuous fin element and disposed on the opposite end from said first and second external headers, means for leading fluid through said channels and defining a How path through one of said inwardly mounted passes through one of the external headers through the other inwardly mounted passes, through another externally mounted header, through an outwardly mounted pass, through another externally mounted header and through an outwardly mounted pass,

Description

1964 G. c. RANNENBERG 3,161,234
MULTIPASS EVAPQRATOR Filed Oct. 16, 1962 2 Sheets-Sheet 2 6 i 5. i w
United States Patent Office 3,ldl,234 Patented Dec. 15, 1964 3,1dl,2 34 MULTEPASS APBQRATQR George C. Rannenherg, Granhy, ilonn, assignor to United Aircraft Qorporation, East Hartford, Quinn, a corporation of Delaware p Filed Set. 16, 1962, Ser. No. 230,818 6 Qlaims. Cl. 165--163) This invention relates to heat exchangers and more particularly to evaporators adapted to be used in a refrigeration system.
As is well known, an evaporator is that part of a refrigeration system where the refrigerant enters the evaporator as a liquid and is vaporized to produce refrigeration. As the air passes through the evaporator, it comes in indirect heat exchange relation with the refrigerant, gives up its heat thereto and is discharged at a much lower temperature than it was when entering the evaporator.
The temperature of the refrigerant decreases as a function of its length of travel in the evaporator until it reaches a particular point intermediate the inlet and outlet of the evaporator. At this point, the liquid refrigerant vaporizes and becomes superheated and hence becomes hotter as it continues its travel. The temperature of the refrigerant increases until it reaches the outlet of the evaporator. Conventional refrigerant evaporators constructed of tubes are often arranged to take advantage of this feature by locating the first refrigerant pass intermediate the refrigerant inlet and refrigerant outlet of the evaporator. In addition, the air to be cooled is first placed in indirect heat exchange relation with the fourth pass (Where the temperature of the refrigerant is at its hottest value) and the third pass is placed in indirect heat exchange relation with the air leaving the evaporator. The second pass is sandwiched between the first and third pass. In this manner, maximum temperature differences for heat transfer between the refrigerant and the hot air intended to be cooled are maintained with resultant maximum utilization of the heat exchanger surface area. By the innovation of this invention, I am able to obtain maximum utilization of heat exchanger surface area with a plate-fin configuration. as was obtainable heretofore only with tube bundle configurations. The plate-fin evaporator made possible by this invention has the advantage of lower weight and volume than that required by previous conventional plate-fin evaporators.
It is the object of this invention to provide in an evaporator, as described, a novel arrangement of the headers of the evaporator, which include locating external headers one within the other with a common wall separating each, combining external headers with internal headers, and locating the headers internally, so as to obtain maximum temperature difference for heat transfer.
Other features and advantages will be apparent from the specification and claims and from the accompanying drawings which illustrate an embodiment of the invention.
FIG. 1 is an isometric view of a portion of the evaporator showing an arrangement in which internal and external headers are used.
FIG. 2 is a cross-sectional view taken along line 22 of FIG. 1, particularly showing the novel location of the refrigerant passes.
FIG. 3 is a schematic illustration showing the novel arrangement of external headers, one inside the other.
FIG. 4 is a schematic illustration wherein all the headers are internal.
Now referring to the drawings, FIG. 1 shows a portion 7 of the core of the evaporator generally illustrated by numeral fill and a pair of air passes indicated by the jnumerals i2 and 14 sandwiching the refrigerant core elerneral 16. As is noted from the drawing, this section of the core has been exploded to illustrate the inventive concept, but only represents a portion of the entire core. It should be understood that the entire evaporator is built up by alternately stacking similar air and refrigerant core elements to obtain the size necessary to afford optimum refrigeration in any given application.
As will be appreciated by one skilled in the art, the general construction of the evaporator may take any conventional form, however, the plate-fin type of heat exchanger is often preferred for reasons of low weight and volume. As noted in FIG. 1, the partial core comprises end plate 16 and dividing walls 18, 26 and 22 extending longitudinally through the evaporator. Generally parallel fin section 24 is sandwiched between end plate 16 and dividing wall 18 for defining an air pass. The generally parallel fin section 24 may be pierced, serrated, rufiled or straight, depending on such matters as economics and the fluids involved. Closure bars 28 and 30, also extending longitudinally, define passage chambers for receiving the fins so that the fins, together with the end plate, dividing wall and closure bars define a passage for the air intended to be cooled. The air is admitted at the top end of the evaporator and is discharged at the bottom in FIG. 1, although any orientation with gravity may be used. Similarly, another air passage, shown in FIG. 1, is formed from a pair of dividing walls 29 and 22, closure members 32 and 34 and the heat transfer fins 26.
The refrigerant passes, located between a pair of air passes, comprise a similar plate-fin construction, only extending transversely of the air passes. Since the actual construction of the evaporator may take any well-known form, a description thereof, for the sake of convenience, is omitted.
Reference is now made to FIG. 2, which illustrates the novel arrangement of the refrigerant passes. As shown in FIG. 2, the refrigerant is admitted into the evaporator through a plurality of tubes, indicated by numeral 34, which lead into header 36. The header directs the flow through the first pass, indicated by Letter A. In accordance with the present invention, the first pass is located intermediate the top and bottom closure plates of the refrigerant core. As indicated above, the pass comprises a plurality of fins which extend between the dividing plates 13 and 20. Turning passages 37, defined by fins, are mounted at the far end of the inlet and direct the refrigerant to the second pass B and similarly, turning fins B located between the third pass C and the second pass B direct refrigerant to the third pass. Finally, the refrigerant feeds into an external header 41 which conducts the refrigerant in the third pass to the fourth pass D. The refrigerant, which at this point has vaporized and become superheated, is discharged into the outlet header 44 and then directed through the discharge conduit 46 to the next stage (not shown) in the refrigeration system.
It will be noted that each pass may contain a different number of passages, and preferably, the number of passages in each pass are increased as the liquid is vaporized. Thus, the liquid passing through the evaporator remains a liquid until it reaches the end of the third or the beginning of the fourth pass. Thus, by virtue of the novel arrangement of the passes, the hot air entering the evaporator is immediately in indirect heat exchange relation with the superheated refrigerant passing through pass D. As the air becomes cooled, it passes in indirect heat exchange relationship with the liquid refrigerant in passes A and B, and finally theair passes over the lowest temperature refrigerant as it reaches pass C. after'which the air.
is completely refrigerated.
From the foregoing, it will be appreciated that the air intended to be cooled when at its hottest temperature,
comes into indirect heat relation with the refrigerant at its hottest temperature.""While, obviously the heat differential between the hot air and the refrigerant at its coolest, temperature would be atitsgreatestvalue, yet from the standpoint of the overall temperatureditferential of all the passes, the temperature difierential obtained by the arrangement shown by'the present invention is higher. Because of this feature,.the evaporator has a highheat transfer efiiciency and hence achieves minimum heat exchanger or evaporator size for 'agiven application.
' FIGS. 3 and 4 are exemplaryshowings of a refrigerant core element embodying the t' present' invention,- but,eni-' ploying diiferent header arrangements; .Various factors,
such as the shape of the volume available for th'e evaporator, materials, and brazing capabilities will determine detailed arrangement selected. Again, for. the sake of convenience, reference to the construction and the details of the core elements are omitted. It will be appreciated, however, that the mechanical details of construction of the core can be of any well-known, plate-fin form. As in FIGS. 1 and 2, the construction of the core elements shown in FIGS. 3 and 4 are of the plate-fin type. Also, it will be appreciated that the location of the passes. are
identical to the location of the passes noted in FIG. 2.
The letters A, B, 'C and D represent successive passes in therefrigeration core.
FIG. 3, shows all the headers mounted externally of the As noted in the drawing, header 50 is inserted in-" ternally of header 52 and wall 54 forms a common wali dividing the two headers. This placing of one header inside the other with flow in opposite directions is a v unique and novel wayof accomplishing the desired core temperature distribution. Header 56 is connectedto the. inlet of the evaporator and header 58"is connected to the V The refrigerant'core element depicted in FIG. 4" is, inmost respects, identical to the core element. shown inFIGSJ 1 and 2, excepttha't internal header 53' connects outlet.
the passages in pass C with 'the passages in pass .D.
What has been shownby this invention is'a novel arrangement of the passes in therefrigerant' core section of an evaporator which, by virtue ofthis arrangement, provides an effective evaporator while permitting'a' reduc-' tion of the overall evaporator size. It will be appreciated that this advantage is particularly important in aircraftapplication, since size and the attendant reduction in weight increase the overall performance of-the aircraft. a
It is to be understood that the invention is not limited enema versely to said channels'formed from first, second, third and fourth fin elements and being adapted to place fiuid passing straight: through said open-ended channel formed from saidfifth continuous fin element in heat exchange relation to the 'fiuid passing through channels formed from said first, second, thirdand fourth fin elements, so
that the fluid enteringsaid open-ended channel of the fifth A continuous fin element is in immediate heat exchange relation with the fluid in said first continuous fin element and fluiddischarging frorn said open-ended channel of the fifth continuous finelement is in heat exchange relation with the fluid in said thirdcontinuous fin element.
2. A multiplate and fin. core'section of anevaporator i having -a--top" and bottomIclosurc member, a'first' continuous fin element mounted adjacent to said top closure member; a second continuous fin element mounted adjacent to said first continuous fin element,;a third con- 3: tinuous fin element mounted adjacent, to said second'fin element, and :a fourth continuous fin element mounted. ad-
jacent to said third continuous fin element, spaced apart parallel members sandwiching the opposite ends of the first, second, third and fourth continuous firr elements and having opposing ends abutting'the top and bottom closure members defining therewith open channels, means inter,- connecting said first, second, third. and fou'rth finelement defining a continuous fiow path for said channels, an inlet header and an outlet header mounted on the evaporator and conducting the flow of refrigerant successively through said second, third, fourth and first continuous fin elements, an adjacent passformed from afoontinuous fin element sandwiched between flat plates defininglaterall'y extending channels'relative to said first, second, thirdand fourth continuous'fin elements for placing fluid in 'heat exchange relationship so that the-fluid attheinlet of the adjacent pass is immediately inlindirect'heat relation to the fluid in the channels defined by the first continuous fin element.--
3. A multichannel, multiplate and fin evaporator comprising at'least onecontinuous fin element,.spaced apart parallel extending'plate ,rnembers. sandwiching the opposite'ends of thefin element for defining therewith a series.
:" 0f separateparallel openended channels. for receiving a to the specific embodiment herein illustrated and 'de scribed, but may be' used in other ways without departing from its spirit as defined by'the following-claims.
I claimf r 1. A multiplate and jfin core section of an evaporator fiuid intended t0 be' cooled, a series of fin elements mounted adjacent one of said parallel, extending plate members, and extending in transverse relationto said one of continuousfin elements for defining four passes for receiving a refrigerant, other spaced apart parallel extending plate' members lying transversely to said spaced apart parallel extending plate members, sandwiching the series of fin elements for defining therewith four. passes, said fourpasses being located one next to the other such "that the fourth passis'adjacent to the inlet of said chancomprising a first continuous fin element, a second con-' tinuous fin element located adjacent. to .said first contin-T' uous fin element, a third continuous fin element located adjacent to said second continuous fin element, and a fourth continuous fin element located adjacent to said third continuous fin element, spaced plates sandwiching said first, second, third and fourthcontinuousfin elements for I defining parallel channels, closure plate members extending laterally from said .space'd 'plates separating said ffir-st,
second, third and fourth continuous fin elements from each other for ,defining'four separate'passes, means for connecting said parallel channels to each other-to'form a continuous flow path fora refrigerant, an inlet header mounted on the evaporator and havingan opening comnels, the third pass is adjacent the outlet of said channels, the first pass is adjacent said fourth pass and said second pass is intermediate-said first pass and said third pass, said passes directing refrigerant successively from the first pass, to the second, pass,.:to thethird pass and then the fourth pass. I V 1 a In a 'refrigerant core section of an evaporator having sidewall platesand top and'bottom closure members,
continuous fin. elements extendingbetween said" side wall plates for defining a series of openended channels, means for separating 'sai'd continuous fin elements for defining a pair of'outwardly mounted passes mounted adjacent the bottom and top closure" membersv and inwardly mounted passesmounted between said outwardly mounted passes,
inunicating with one of'said v fin elements, means for connecting said first, second, third andfourth comm nted elements so that said refrigerant passes "successively through said, second, third,'fourth. and first continuous 1 fin elements, said evaporator also, having a fifth con- V tinuous fin elementdisposed .adjacentfto said first,;second,
third and fourth continuous finelernents, spaced'plates adjacent the edges of saidi-fifth continuous finelement-{j defining therewith open-ended channels extending; trans ,7 5
an internal headerformed at one endofdthe inwardly mountedl fin elements, vand another internal header rnounted on'the oppositeend of one of said inwardly mounted fin elements and one of said externally mounted .2 fin; elements, an enema header communicating with bothof said outwardly mounted fin elements, said internal headers and said external headers forminga successive continuous .fiow path throughsaid gchannels, 1 an inlet Z; er mounted adjacentto cheer said inwardly m'ounted passes and an outlet header mounted adjacent to the last pass in said flow path, an adjacent pass formed from a continuous fin element sandwiched between spaced parallelly mounted plates defining a plurality of channels for passing a fluid in heat exchange relationship with the fiuid in the adjacent series of channels.
5. In a refrigerant core section of an evaporator having side wall plates and top and bottom closure members, continuous fin elements extending between said side wall plates for defining a series of open-ended channels, means separating said continuous fin elements for defining a pair of outwardly mounted passes mounted adjacent the bottom and top closure members and inwardly mounted passes mounted between said outwardly mounted passes, first and second external headers mounted adjacent to one end of said continuous fin elements, a common wall separating said first external headers, said first external header connecting the pair of inwardly mounted passes and the second external header connecting the outwardly mounted passes, a third external header mounted adja cent to an inwardly mounted and an outwardly mounted continuous fin element and disposed on the opposite end from said first and second external headers, means for leading fluid through said channels and defining a How path through one of said inwardly mounted passes through one of the external headers through the other inwardly mounted passes, through another externally mounted header, through an outwardly mounted pass, through another externally mounted header and through an outwardly mounted pass, said evaporator having an air core section comprising of at least one continuous fin element, parallel spaced fiat walls abutting the opposite edges of said fin element defining therewith a plurality of openended channels extending transverse but adjacent to said open-ended channels in the refrigerant core section, the inlet end of said open-ended channel in the air core section disposed adjacent one of said outwardly mounted passes and the outlet end of said open-ended channel in the air core section disposed adjacent the other of said outwardly mounted passes.
6. In a refrigerant core section of an evaporator having side wall plates and top and bottom closure members, continuous fin elements extending between said side wall plates for defining open-ended channels, means separating said continuous fin elements for defining a pair of outwardly mounted passes mounted adjacent the bottom and top closure members and inwardly mounted passes mounted between said outwardly mounted passes, first, second and third internal headers located in the core section, said first internal header mounted at one end of the inwardly mounted passes, said second internal header mounted on the opposite end of the inwardly mounted passes and connecting one of said inwardly mounted passes to an outwardly mounted pass, said third internal header mounted adjacent said first internal header and connecting the outwardly mounted passes with each other, first external header leading to an inlet and connected to an inwardly mounted pass for receiving a refrigerant and a second external header having an outlet for communicating with one of said outwardly mounted passes providing a continuous refrigerant fiow path from said first external header, to one of said inwardly mounted passes, to said first internal inlet header, to said other inwardly mounted passes, to said third internal header to one of said outwardly mounted passes, to said second internal header, to the other of said outwardly mounted passes and to said second external header, said evaporator having an air core section comprising of at least one continuous fin element parallel spaced fiat walls abutting the opposite edges of said fin element defining therewith a plurality of open-ended channels extending transverse but adjacent to said open-ended channels in the refrigerant core section, the inlet end of said open-ended channel in the air core section disposed adjacent one of said outwardly mounted passes and the outlet end of said open-ended channel in the air core section disposed adjacent the other of said outwardly mounted passes.
References Qited by the Examiner UNITED STATES PATENTS 1,139,549 5/15 Lovekin 165163 2,875,986 3/59 Holm l65l65 3,043,110 7/62 Ahern 165-145 CHARLES SUKALO, Primary Examiner.
FREDERICK L. MATTESON, JR., Examiner.

Claims (1)

1. A MULTIPLATE AND FIN CORE SECTION OF AN EVAPORATOR COMPRISING A FIRST CONTINUOUS FIN ELEMENT, A SECOND CONTINUOUS FIN ELEMENT LOCATED ADJACENT TO SAID FIRST CONTINUOUS FIN ELEMENT, A THIRD CONTINUOUS FIN ELEMENT LOCATED ADJACENT TO SAID SECOND CONTINUOUS FIN ELEMENT, AND A FOURTH CONTINUOUS FIN ELEMENT LOCATED ADJACENT TO SAID THIRD CONTINUOUS FIN ELEMENT, SPACED PLATES SANDWICHING SAID FIRST, SECOND, THIRD AND FOURTH CONTINUOUS FIN ELEMENTS FOR DEFINING PARALLEL CHANNELS, CLOSURE PLATE MEMBERS EXTENDING LATERALLY FROM SAID SPACED PLATES SEPARATING SAID FIRST, SECOND, THIRD AND FOURTH CONTINUOUS FIN ELEMENTS FROM EACH OTHER FOR DEFINING FOUR SEPARATE PASSES, MEANS FOR CONNECTING SAID PARALLEL CHANNELS TO EACH OTHER TO FORM A CONTINUOUS FLOW PATH FOR A REFRIGERANT, AN INLET HEADER MOUNTED ON THE EVAPORATOR AND HAVING AN OPENING COMMUNICATING WITH ONE OF SAID FIN ELEMENTS, MEANS FOR CONNECTING SAID FIRST, SECOND, THIRD AND FOURTH CONTINUOUS FIN ELEMENTS SO THAT SAID REFRIGERANT PASSES SUCCESSIVELY THROUGH SAID SECOND, THIRD, FOURTH AND FIRST CONTINUOUS FIN ELEMENTS, SAID EVAPORATOR ALSO HAVING A FIFTH CONTINUOUS FIN ELEMENT DISPOSED ADJACENT TO SAID FIRST, SECOND, THIRD AND FOURTH CONTINUOUS FIN ELEMENTS, SPACED PLATES ADJACENT THE EDGES OF SAID FIFTH CONTINUOUS FIN ELEMENT DEFINING THEREWITH OPEN-ENDED CHANNELS EXTENDING TRANSVERSELY TO SAID CHANNELS FORMED FORM FIRST, SECOND, THIRD AND FOURTH FIN ELEMENTS AND BEING ADAPTED TO PLACE FLUID PASSING STRAIGHT THROUGH SAID OPEN-ENDED CHANNEL FORMED FROM SAID FIFTH CONTINUOUS FIN ELEMENT IN HEAT EXCHANGE RELATION TO THE FLUID PASSING THROUGH CHANNELS FORMED FROM SAID FIRST, SECOND, THIRD AND FOURTH FIN ELEMENTS, SO THAT THE FLUID ENTERING SAID OPEN-ENDED CHANNEL OF THE FIFTH CONTINUOUS FIN ELEMENT IS IN IMMEDIATE HEAT EXCHANGE RELATION WITH THE FLUID IN SAID FIRST CONTINUOUS FIN ELEMENT AND FLUID DISCHARGING FROM SAID OPEN-ENDED CHANNEL OF THE FIFTH CONTINUOUS FIN ELEMENT IS IN HEAT EXCHANGE RELATION WITH THE FLUID IN SAID THIRD CONTINUOUS FIN ELEMENT.
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Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3304730A (en) * 1965-06-09 1967-02-21 Robert B Gorham Device to aid pumping of volatile gases
US3635284A (en) * 1970-05-21 1972-01-18 Earl W Hoch Flash boiler
US4623019A (en) * 1985-09-30 1986-11-18 United Aircraft Products, Inc. Heat exchanger with heat transfer control
US4712612A (en) * 1984-10-12 1987-12-15 Showa Aluminum Kabushiki Kaisha Horizontal stack type evaporator
US4729427A (en) * 1985-10-30 1988-03-08 Ing. Walter Hengst Gmbh & Co. Kg Heat exchanger
US4793407A (en) * 1986-02-22 1988-12-27 Ing. Walter Hengst Gmbh & Co. Kg Heat exchanger for two fluid media
US4829780A (en) * 1988-01-28 1989-05-16 Modine Manufacturing Company Evaporator with improved condensate collection
US4862952A (en) * 1988-05-09 1989-09-05 United Technologies Corporation Frost free heat exchanger
US5214935A (en) * 1990-02-20 1993-06-01 Allied-Signal Inc. Fluid conditioning apparatus and system
US6484798B1 (en) * 2000-10-23 2002-11-26 Carrier Corporation Furnace heat exchanger
US20090090495A1 (en) * 2006-03-10 2009-04-09 Behr Gmbh & Co. Kg Heat Exchanger for a Motor Vehicle
US20090313993A1 (en) * 2008-06-20 2009-12-24 Christian Bausch Vaporizer for a waste heat recovery system
US20100084120A1 (en) * 2008-10-03 2010-04-08 Jian-Min Yin Heat exchanger and method of operating the same
US20110180242A1 (en) * 2010-01-27 2011-07-28 Sumitomo Precision Products Co., Ltd. Stack type heat exchanger
US8196708B2 (en) * 2008-12-23 2012-06-12 Chang Cheng Kung Lubricant circulation system
US20130240186A1 (en) * 2010-11-22 2013-09-19 Michael F. Taras Multiple Tube Bank Flattened Tube Finned Heat Exchanger
US20150308295A1 (en) * 2012-06-26 2015-10-29 Eberspächer Exhaust Technology GmbH & Co. KG Evaporator
US20160214460A1 (en) * 2015-01-22 2016-07-28 Ford Global Technologies. Llc Active seal arrangement for use with vehicle condensers
US20170089643A1 (en) * 2015-09-25 2017-03-30 Westinghouse Electric Company, Llc. Heat Exchanger
US10821509B2 (en) 2016-01-20 2020-11-03 General Electric Company Additive heat exchanger mixing chambers

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US1139549A (en) * 1912-07-15 1915-05-18 Luther D Lovekin Fluid heating and cooling apparatus.
US2875986A (en) * 1957-04-12 1959-03-03 Ferrotherm Company Heat exchanger
US3043110A (en) * 1961-01-26 1962-07-10 Marquardt Corp Apparatus and method of utilizing the conversion of parahydrogen to orthohydrogen to obtain a refrigerating effect

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1139549A (en) * 1912-07-15 1915-05-18 Luther D Lovekin Fluid heating and cooling apparatus.
US2875986A (en) * 1957-04-12 1959-03-03 Ferrotherm Company Heat exchanger
US3043110A (en) * 1961-01-26 1962-07-10 Marquardt Corp Apparatus and method of utilizing the conversion of parahydrogen to orthohydrogen to obtain a refrigerating effect

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3304730A (en) * 1965-06-09 1967-02-21 Robert B Gorham Device to aid pumping of volatile gases
US3635284A (en) * 1970-05-21 1972-01-18 Earl W Hoch Flash boiler
US4712612A (en) * 1984-10-12 1987-12-15 Showa Aluminum Kabushiki Kaisha Horizontal stack type evaporator
US4623019A (en) * 1985-09-30 1986-11-18 United Aircraft Products, Inc. Heat exchanger with heat transfer control
US4729427A (en) * 1985-10-30 1988-03-08 Ing. Walter Hengst Gmbh & Co. Kg Heat exchanger
US4793407A (en) * 1986-02-22 1988-12-27 Ing. Walter Hengst Gmbh & Co. Kg Heat exchanger for two fluid media
US4829780A (en) * 1988-01-28 1989-05-16 Modine Manufacturing Company Evaporator with improved condensate collection
USRE37040E1 (en) 1988-01-28 2001-02-06 Modine Manufacturing Company Evaporator with improved condensate collection
US4862952A (en) * 1988-05-09 1989-09-05 United Technologies Corporation Frost free heat exchanger
US5214935A (en) * 1990-02-20 1993-06-01 Allied-Signal Inc. Fluid conditioning apparatus and system
US6484798B1 (en) * 2000-10-23 2002-11-26 Carrier Corporation Furnace heat exchanger
US8573286B2 (en) * 2006-03-10 2013-11-05 Behr Gmbh & Co. Kg Heat exchanger for a motor vehicle
US20090090495A1 (en) * 2006-03-10 2009-04-09 Behr Gmbh & Co. Kg Heat Exchanger for a Motor Vehicle
US20090313993A1 (en) * 2008-06-20 2009-12-24 Christian Bausch Vaporizer for a waste heat recovery system
US8550153B2 (en) * 2008-10-03 2013-10-08 Modine Manufacturing Company Heat exchanger and method of operating the same
US20100084120A1 (en) * 2008-10-03 2010-04-08 Jian-Min Yin Heat exchanger and method of operating the same
US8196708B2 (en) * 2008-12-23 2012-06-12 Chang Cheng Kung Lubricant circulation system
US20110180242A1 (en) * 2010-01-27 2011-07-28 Sumitomo Precision Products Co., Ltd. Stack type heat exchanger
US20130240186A1 (en) * 2010-11-22 2013-09-19 Michael F. Taras Multiple Tube Bank Flattened Tube Finned Heat Exchanger
US20150308295A1 (en) * 2012-06-26 2015-10-29 Eberspächer Exhaust Technology GmbH & Co. KG Evaporator
US9982570B2 (en) * 2012-06-26 2018-05-29 Eberspächer Exhaust Technology GmbH & Co. KG Stacked plate evaporator
US20160214460A1 (en) * 2015-01-22 2016-07-28 Ford Global Technologies. Llc Active seal arrangement for use with vehicle condensers
US10252611B2 (en) * 2015-01-22 2019-04-09 Ford Global Technologies, Llc Active seal arrangement for use with vehicle condensers
US20170089643A1 (en) * 2015-09-25 2017-03-30 Westinghouse Electric Company, Llc. Heat Exchanger
US10821509B2 (en) 2016-01-20 2020-11-03 General Electric Company Additive heat exchanger mixing chambers

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