US20180238644A1 - Multi-cross sectional fluid path condenser - Google Patents
Multi-cross sectional fluid path condenser Download PDFInfo
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- US20180238644A1 US20180238644A1 US15/896,008 US201815896008A US2018238644A1 US 20180238644 A1 US20180238644 A1 US 20180238644A1 US 201815896008 A US201815896008 A US 201815896008A US 2018238644 A1 US2018238644 A1 US 2018238644A1
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- Prior art keywords
- refrigerant
- condenser
- sectional area
- section
- heat exchange
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- 239000003507 refrigerant Substances 0.000 claims abstract description 104
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 26
- 239000012080 ambient air Substances 0.000 claims description 3
- 238000000034 method Methods 0.000 claims 4
- 238000005086 pumping Methods 0.000 claims 2
- 230000000670 limiting effect Effects 0.000 abstract description 2
- 239000003570 air Substances 0.000 description 9
- 239000013529 heat transfer fluid Substances 0.000 description 7
- 230000007423 decrease Effects 0.000 description 5
- 230000002829 reductive effect Effects 0.000 description 5
- 239000000110 cooling liquid Substances 0.000 description 4
- 230000007812 deficiency Effects 0.000 description 3
- 238000011144 upstream manufacturing Methods 0.000 description 3
- 230000005494 condensation Effects 0.000 description 2
- 238000009833 condensation Methods 0.000 description 2
- 238000007710 freezing Methods 0.000 description 2
- 230000008014 freezing Effects 0.000 description 2
- 238000005057 refrigeration Methods 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- -1 is not of concern Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
- F28F13/06—Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media
- F28F13/08—Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media by varying the cross-section of the flow channels
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B39/00—Evaporators; Condensers
- F25B39/04—Condensers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28B—STEAM OR VAPOUR CONDENSERS
- F28B7/00—Combinations of two or more condensers, e.g. provision of reserve condenser
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28C—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA COME INTO DIRECT CONTACT WITHOUT CHEMICAL INTERACTION
- F28C1/00—Direct-contact trickle coolers, e.g. cooling towers
- F28C1/14—Direct-contact trickle coolers, e.g. cooling towers comprising also a non-direct contact heat exchange
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D1/00—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
- F28D1/02—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
- F28D1/04—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits
- F28D1/0408—Multi-circuit heat exchangers, e.g. integrating different heat exchange sections in the same unit or heat exchangers for more than two fluids
- F28D1/0417—Multi-circuit heat exchangers, e.g. integrating different heat exchange sections in the same unit or heat exchangers for more than two fluids with particular circuits for the same heat exchange medium, e.g. with the heat exchange medium flowing through sections having different heat exchange capacities or for heating/cooling the heat exchange medium at different temperatures
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D1/00—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
- F28D1/02—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
- F28D1/04—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits
- F28D1/047—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being bent, e.g. in a serpentine or zig-zag
- F28D1/0477—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being bent, e.g. in a serpentine or zig-zag the conduits being bent in a serpentine or zig-zag
- F28D1/0478—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being bent, e.g. in a serpentine or zig-zag the conduits being bent in a serpentine or zig-zag the conduits having a non-circular cross-section
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D1/00—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
- F28D1/02—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
- F28D1/04—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits
- F28D1/053—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D1/00—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
- F28D1/02—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
- F28D1/04—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits
- F28D1/053—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight
- F28D1/0535—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight the conduits having a non-circular cross-section
- F28D1/05366—Assemblies of conduits connected to common headers, e.g. core type radiators
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D3/00—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium flows in a continuous film, or trickles freely, over the conduits
- F28D3/02—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium flows in a continuous film, or trickles freely, over the conduits with tubular conduits
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D3/00—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium flows in a continuous film, or trickles freely, over the conduits
- F28D3/04—Distributing arrangements
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/02—Tubular elements of cross-section which is non-circular
- F28F1/025—Tubular elements of cross-section which is non-circular with variable shape, e.g. with modified tube ends, with different geometrical features
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/24—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely
- F28F1/32—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely the means having portions engaging further tubular elements
- F28F1/325—Fins with openings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F25/00—Component parts of trickle coolers
- F28F25/02—Component parts of trickle coolers for distributing, circulating, and accumulating liquid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
- F28F9/02—Header boxes; End plates
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B2339/00—Details of evaporators; Details of condensers
- F25B2339/04—Details of condensers
- F25B2339/041—Details of condensers of evaporative condensers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
- F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
- F28D2021/0068—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for refrigerant cycles
- F28D2021/007—Condensers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
- F28F9/02—Header boxes; End plates
- F28F2009/0285—Other particular headers or end plates
- F28F2009/029—Other particular headers or end plates with increasing or decreasing cross-section, e.g. having conical shape
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F25/00—Component parts of trickle coolers
- F28F2025/005—Liquid collection; Liquid treatment; Liquid recirculation; Addition of make-up liquid
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B30/00—Energy efficient heating, ventilation or air conditioning [HVAC]
- Y02B30/70—Efficient control or regulation technologies, e.g. for control of refrigerant flow, motor or heating
Definitions
- the present invention relates to refrigeration system air-cooled condensers.
- a typical refrigeration system condenser consists of multiple, serpentine heat transfer fluid paths (or circuits) such that the superheated heat transfer vapor entering each circuit (path) will be condensed completely prior to leaving the heat exchange device.
- FIG. 3 illustrates an example of a prior art condenser tube bundle.
- the condenser consists of approximately 50 serpentine tubes, with one inlet header and one outlet header. Vapor enters the upper header (inlet) and is dispersed into all 50 tubes, all having the same diameter. For the entire fluid flow path, the number of the tubes remains constant, and the cross-sectional area of each tube remains constant. At the bottom of the tube bundle, the condensed refrigerant is collected at the outlet header.
- the overall heat transfer coefficient is primarily controlled by the external heat transfer coefficient and at other times by the internal film heat transfer coefficient.
- the entire volume exists in a gaseous (or vapor) state.
- the initial vapor velocity at each circuit entrance is significant resulting in a high internal pressure drop per incremental fluid circuit length which in turn provides a significant internal film heat transfer coefficient.
- the external heat transfer coefficient governs heat removal in this portion of each circuit. As heat transfer continues between the refrigerant and air along each circuit length and the heat transfer fluid (still in a vapor state) reaches saturation, the vapor begins to condense. As a result, and continuing along each circuit length, the vapor volume and velocity decrease.
- the vapor exit velocity for each circuit is virtually nil—the heat transfer fluid in liquid form exits the condenser.
- the continuous reduction in vapor velocity along each fixed cross sectional area circuit length decreases the internal film heat transfer coefficient.
- the internal film heat transfer coefficient prior to approaching the exit region of each circuit limits the condenser's potential or overall heat transfer capability.
- the present invention ameliorates heat transfer deficiency of the prior art as well as high initial refrigerant pressure drop in the first pass by providing multi-cross sectional fluid paths (circuits) for condensation coupled with segmented headers in lieu of return bends.
- circuits multi-cross sectional fluid paths
- the larger total initial cross sectional area reduces the internal pressure drop and the vapor velocity while maintaining the internal film heat transfer coefficient above the external heat transfer coefficient.
- the total cross sectional area is reduced to maintain a threshold internal film heat transfer coefficient that is equal to or greater than the external heat transfer coefficient.
- This decrease in total cross sectional area may be accomplished by incorporating a multiple pass circuit selection coupled with a greater total cross sectional area for the initial fluid path in comparison to later passes.
- This arrangement lowers the initial heat transfer fluid pressure drop per incremental circuit length with minimal heat transfer sacrifice in the first pass.
- it significantly improves the condenser's heat transfer deficiency by increasing the internal film heat transfer coefficient in the later passes in comparison to the prior art single cross-sectional area circuit devices.
- the multi-cross sectional condenser of the invention provides greater heat rejection at a lower heat transfer fluid pressure drop.
- the multi-cross sectional fluid path condenser of the invention can be implemented using larger tubes in the first pass and smaller tubes in subsequent passes, or by using more tubes in the first pass and fewer tubes in subsequent passes, or by some combination of the two, that is reducing both the number of tubes and the cross-sectional area of the tubes in with each subsequent pass.
- FIG. 1 is a cutaway perspective view of a evaporative refrigerant condenser.
- FIG. 2 shows the principal of operation of an evaporative refrigerant condenser.
- FIG. 3 shows a prior art evaporative refrigerant condenser tube bundle.
- FIG. 4 a is a plan view photograph of a mockup of a multi-cross sectional area tube bundle (also referred to herein as “heat exchange bundle”) according to an embodiment of the invention
- FIG. 4 b is a formal drawing corresponding to the photograph of FIG. 4 a
- FIG. 5 a is a perspective view photograph of the mockup shown in FIG. 5 a.
- FIG. 5 b is a formal drawing corresponding to the photograph of FIG. 5 a
- FIG. 6 a is the plan view photograph of FIG. 2 a , with arrows to show the refrigerant flow path.
- FIG. 6 b is a formal drawing corresponding to the photograph of FIG. 6 a.
- FIG. 7 a is a labeled version of the photograph of FIG. 5 a.
- FIG. 7 b is a formal drawing corresponding to the photograph of FIG. 7 a.
- FIG. 8 is a sketch of an embodiment of the invention having four condenser sections.
- FIG. 9 is a perspective view of an embodiment of the invention having three condenser sections arranged so that the inlet header, outlet header and intermediate headers are all on the same side of the device.
- This invention relates particularly to condenser coil bundles used in refrigerant condensers, and particularly (although not exclusively) in evaporative refrigerant condensers 10 of the type shown in FIGS. 1 and 2 configured to indirectly transfer heat between a superheated refrigerant and ambient air, operative in a wet mode or a dry mode as described below depending on ambient atmospheric conditions, such as temperature, humidity and pressure.
- the apparatus 10 includes a fan 100 for causing air to flow through the apparatus, and as shown schematically in FIG. 1 , sitting atop housing 15 .
- a fan 100 for causing air to flow through the apparatus, and as shown schematically in FIG. 1 , sitting atop housing 15 .
- air is drawn into the plenum 18 of the apparatus via air passages at the bottom of the unit through the open air intake dampers, and enters the evaporative heat transfer section 12 where heat transfer takes place involving the distribution of water from a water distribution assembly 90 driven by a pump 96 .
- the distributor assembly of cooling liquid is turned off
- Prior art refrigerant coil assemblies 20 have a generally parallelepiped overall shape of six sides retained in a frame 21 and has a major/longitudinal axis 23 , where each side is in the form of a rectangle.
- the coil assembly 20 is made of multiple horizontal closely spaced parallel, serpentine tubes connected at their ends to form a number of circuits through which the refrigerant flows.
- Each individual circuit within the coil assembly is a single, continuous length of coil tubing that is subjected to a bending operation which forms the tubing into several U-shaped rows that are in a generally vertical and equally-spaced relationship from each other, such that each circuit has a resultant serpentine shape.
- the coil assembly 20 has an inlet 22 connected to an inlet manifold or header 24 , which fluidly connects to inlet ends of the serpentine tubes of the coil assembly, and an outlet 26 connected to an outlet manifold or header 28 , which fluidly connects to the outlet ends of the serpentine tubes of the coil assembly.
- the assembled coil assembly 20 may be moved and transported as a unitary structure such that it may be dipped, if desired, if its components are made of steel, in a zinc bath to galvanize the entire coil assembly.
- the refrigerant gas discharges from the compressor into the inlet connection of the apparatus. Heat from the refrigerant dissipates through the coil tubes to the water cascading downward over the tubes. Simultaneously, air is drawn in through the air inlet louvers at the base of the condenser and travels upward over the coil opposite the water flow. A small portion of the water evaporates, removing heat from the system. The warm moist air is drawn to the top of the evaporative condenser by the fan and discharged to the atmosphere. The remaining water falls to the sump at the bottom of the condenser where it recirculates through the water distribution system and back down over the coils.
- the invention constitutes a change and improvement over the prior art wherein instead of tube bundles comprising a single cross-sectional area throughout the entire refrigerant flow path through the coil, the indirect heat exchange section has multiple sections, each having different cross-sectional areas, decreasing as the refrigerant travels through the heat exchange section.
- FIGS. 4 a , 5 a , 6 a and 7 a are photographs of a mockup of a multi-cross-sectional area refrigerant condenser according to an embodiment of the invention.
- FIGS. 4 b , 5 b , 6 b and 7 b are formal drawings corresponding to FIGS. 4 a , 5 a , 6 a and 7 a , respectively.
- a first condenser section 103 includes plurality of straight tubes 105 having a first total cross-sectional area. While round tubes are shown in the mock-up, tubes of any shape, size and feature may be used according to the invention.
- any passage capable of permitting refrigerant flow and heat exchange may be adapted for use in connection with the invention in the place of the tubes shown in the Figures, including microchannel plates and other conduit structures.
- the term “tube” will be used, but it should be understood that the words “passage,” or “conduit” may be substituted for the word “tube” in the description herein, whatever the construction, provided that it can convey refrigerant and permit heat exchange between refrigerant inside and air outside.
- total cross-sectional area refers to the sum of the cross-sectional areas of the individual tubes in a condenser section.
- the term “total cross-sectional area” as used herein is not calculated to include the area between tubes in a condenser section.
- the cross-sectional area of each straight tube 105 in first condenser section 103 may be the same as or different from one-another, but the sum of the cross-sectional areas of all straight tubes 105 in first condenser section 103 equals the first total cross-sectional area.
- the tubes in first condenser section 103 are preferably finned.
- Each straight tube 105 in the first condenser section 103 terminates at one end at inlet header or manifold 107 and at terminates at a second end at intermediate header or manifold 109 .
- a second condenser section 111 includes a second plurality of straight tubes 113 having a second total cross-sectional area.
- the cross-sectional area of each straight tube 113 in second condenser section 111 may be the same as or different from one-another, but the sum of the cross-sectional areas of all straight tubes 113 in second condenser section 111 equals the second total cross-sectional area.
- the second total cross-sectional area is less than the first total cross-sectional area.
- each straight tube 113 in the second condenser section may be the same or different from the cross-sectional area of each straight tube 105 in the first condenser section, but the cross-sectional area of each straight tube 113 in the second condenser section is preferably less than cross-sectional area of each straight tube 105 in the first condenser section.
- the number of tubes in the second condenser section may be the same or different from the number of tubes in the first condenser section, but is preferably less.
- the length of the tubes in the second condenser section may optionally be shorter than the length of the tubes in the first condenser section (as shown for example in FIGS. 4 a and 4 b ).
- the tubes in second condenser section 111 are preferably finned.
- the second condenser section receives refrigerant from the first condenser section via intermediate header or manifold 109 .
- each straight tube 113 in the second condenser section terminates at one end at intermediate header or manifold 109 and terminates at a second end at outlet header or manifold (not shown).
- FIG. 8 is a representation of an embodiment of the invention having four condenser sections.
- a second intermediate header or manifold 115 directs refrigerant to a third condenser section 117 , and each of said third 117 , fourth 119 , and fifth or more condenser sections are each constructed of a plurality of straight tubes, and each of said third, fourth, and fifth or more condenser sections each have a total cross-sectional area that is less than a cross-sectional area of an immediately upstream condenser section.
- Each of the straight tubes in said third, fourth, and fifth or more condenser section is connected at one end to an immediately upstream condenser section by an intermediate header or manifold, and at a second end to another intermediate header or manifold 121 (if there is a subsequent condenser section) or to an outlet header or manifold 123 .
- FIG. 9 shows an alternate embodiment of the invention in which the inlet header, outlet header and intermediate headers are all arranged on the same side of the device, and each condenser section contains two sets of straight lengths of tubes connected at an end opposite the header end by U-bends.
- inlet header 201 receives superheated refrigerant vapor and distributes it to first set of straight tubes 203 in a first condenser section 205 .
- the first set of straight tubes 203 are connected at an opposite end to a second set of straight tubes 207 in said first condenser section by U-bends 209 .
- the first and second set of tubes in the first condenser section have the same number of tubes and the tubes have the same diameter.
- U-bends 209 have approximately the same cross-sectional size/diameter as the first and second set of tubes in said first condenser section.
- the side of the second set of tubes in the first condenser section are connected at an end opposite the U-bend end to first intermediate header 211 .
- First intermediate header then delivers the refrigerant to the second condenser section 213 having a second condenser first set of tubes 215 and a second condenser second set of tubes 217 connected at an opposite end from said intermediate header by another set of U-bends 219 .
- the first and second set of tubes in said second condenser section have the same cross-sectional dimensions and are equal in number.
- the U-bends 219 connecting the first and second set of tubes in the second condenser section likewise have approximately the same cross-sectional dimensions as the first and second set of tubes they connect.
- the second condenser section second set of tubes 217 terminate at a second intermediate header 221 .
- the second intermediate header 221 receives refrigerant from the second condenser section set of tubes 217 and direct it to the third condenser section 223 .
- the third condenser section first set of tubes 225 are connected at a first end to the second intermediate header and at an opposite end to yet another set of U-bends (not shown) that are in-turn connected to a first end of third condenser section second set of tubes 227 .
- the third condenser section second set of tubes 227 are connected at the header end to outlet header 229 .
- the tubes of each condenser section are progressively smaller while (according to the embodiment shown in FIG. 9 ) the number of tubes in each condenser section is equal.
- the size of the tubes could be left the same, and the number of tubes could be reduced, so that the total cross-sectional area of each condenser section is smaller than the first section, and is preferably smaller than each upstream section.
- the invention can reduce the inlet vapor velocity more than 50% and thus reduce the refrigerant pressure drop to less than 25% of the original value.
- the entrance vapor velocity, per circuit is sufficient to establish an internal film heat transfer coefficient greater than the external heat transfer coefficient while limiting the internal pressure drop for the heat rejection intended.
- the subsequent decrease in total cross sectional area will occur after the first path or even later in the heat transfer fluid path depending upon operating conditions.
- the number of tubes in the second condenser section may be adjusted to additionally lower vapor velocity which in turn reduces refrigerant pressure drop.
- the second group also exhibits a reduced total cross sectional area then the first group in this illustration and thus maintains vapor velocity prior to entering the last reduction in cross sectional area.
- a third condenser section may have further reduced cross sectional area to re-establish the vapor velocity prior to exiting the condenser. It is most preferred that each condenser section incorporate smaller or same as, cross sectional area paths in comparison to the initial circuits. In doing so, the fluid (vapor) velocity is re-established such that the associated internal film heat transfer coefficient is greater than that leaving the initial total cross sectional area provided coupled with initial circuit quantity.
- Multi-cross sectional interfaces are preferably utilized throughout the condenser as needed via segmented headers (see, e.g., FIGS.
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Abstract
Description
- The present invention relates to refrigeration system air-cooled condensers.
- A typical refrigeration system condenser consists of multiple, serpentine heat transfer fluid paths (or circuits) such that the superheated heat transfer vapor entering each circuit (path) will be condensed completely prior to leaving the heat exchange device.
FIG. 3 illustrates an example of a prior art condenser tube bundle. The condenser consists of approximately 50 serpentine tubes, with one inlet header and one outlet header. Vapor enters the upper header (inlet) and is dispersed into all 50 tubes, all having the same diameter. For the entire fluid flow path, the number of the tubes remains constant, and the cross-sectional area of each tube remains constant. At the bottom of the tube bundle, the condensed refrigerant is collected at the outlet header. - The overall heat transfer coefficient is primarily controlled by the external heat transfer coefficient and at other times by the internal film heat transfer coefficient. At each circuit entrance (or path), the entire volume exists in a gaseous (or vapor) state. The initial vapor velocity at each circuit entrance is significant resulting in a high internal pressure drop per incremental fluid circuit length which in turn provides a significant internal film heat transfer coefficient. The external heat transfer coefficient governs heat removal in this portion of each circuit. As heat transfer continues between the refrigerant and air along each circuit length and the heat transfer fluid (still in a vapor state) reaches saturation, the vapor begins to condense. As a result, and continuing along each circuit length, the vapor volume and velocity decrease. The vapor exit velocity for each circuit is virtually nil—the heat transfer fluid in liquid form exits the condenser. The continuous reduction in vapor velocity along each fixed cross sectional area circuit length decreases the internal film heat transfer coefficient. Moreover, the internal film heat transfer coefficient prior to approaching the exit region of each circuit limits the condenser's potential or overall heat transfer capability.
- Applicant has observed certain deficiencies in the prior art, including that while the volume and velocity of vapor is a maximum at the entrance of the first pass, there is little or no vapor velocity in the last pass. The significant inlet vapor volume produces a high refrigerant pressure drop in the first pass due to the high vapor velocity. This in turn limits the refrigerant mass flow rate per tube (or circuit/path). Conversely, the very low vapor velocity in the last pass adversely affects the internal film heat transfer coefficient and thus reduces the condenser's total heat transfer capability.
- The present invention ameliorates heat transfer deficiency of the prior art as well as high initial refrigerant pressure drop in the first pass by providing multi-cross sectional fluid paths (circuits) for condensation coupled with segmented headers in lieu of return bends. Thus at the entrance of each circuit when the vapor volume is significant, a larger cross-sectional area is provided for each circuit. The larger total initial cross sectional area reduces the internal pressure drop and the vapor velocity while maintaining the internal film heat transfer coefficient above the external heat transfer coefficient. As the vapor volume decreases along each circuit length as a result of condensation, the total cross sectional area is reduced to maintain a threshold internal film heat transfer coefficient that is equal to or greater than the external heat transfer coefficient. This decrease in total cross sectional area may be accomplished by incorporating a multiple pass circuit selection coupled with a greater total cross sectional area for the initial fluid path in comparison to later passes. This arrangement lowers the initial heat transfer fluid pressure drop per incremental circuit length with minimal heat transfer sacrifice in the first pass. Moreover, it significantly improves the condenser's heat transfer deficiency by increasing the internal film heat transfer coefficient in the later passes in comparison to the prior art single cross-sectional area circuit devices. Overall, the multi-cross sectional condenser of the invention provides greater heat rejection at a lower heat transfer fluid pressure drop. The multi-cross sectional fluid path condenser of the invention can be implemented using larger tubes in the first pass and smaller tubes in subsequent passes, or by using more tubes in the first pass and fewer tubes in subsequent passes, or by some combination of the two, that is reducing both the number of tubes and the cross-sectional area of the tubes in with each subsequent pass.
-
FIG. 1 is a cutaway perspective view of a evaporative refrigerant condenser. -
FIG. 2 shows the principal of operation of an evaporative refrigerant condenser. -
FIG. 3 shows a prior art evaporative refrigerant condenser tube bundle. -
FIG. 4a is a plan view photograph of a mockup of a multi-cross sectional area tube bundle (also referred to herein as “heat exchange bundle”) according to an embodiment of the invention; -
FIG. 4b is a formal drawing corresponding to the photograph ofFIG. 4a -
FIG. 5a is a perspective view photograph of the mockup shown inFIG. 5 a. -
FIG. 5b is a formal drawing corresponding to the photograph ofFIG. 5 a -
FIG. 6a is the plan view photograph ofFIG. 2a , with arrows to show the refrigerant flow path. -
FIG. 6b is a formal drawing corresponding to the photograph ofFIG. 6 a. -
FIG. 7a is a labeled version of the photograph ofFIG. 5 a. -
FIG. 7b is a formal drawing corresponding to the photograph ofFIG. 7 a. -
FIG. 8 is a sketch of an embodiment of the invention having four condenser sections. -
FIG. 9 is a perspective view of an embodiment of the invention having three condenser sections arranged so that the inlet header, outlet header and intermediate headers are all on the same side of the device. - This invention relates particularly to condenser coil bundles used in refrigerant condensers, and particularly (although not exclusively) in
evaporative refrigerant condensers 10 of the type shown inFIGS. 1 and 2 configured to indirectly transfer heat between a superheated refrigerant and ambient air, operative in a wet mode or a dry mode as described below depending on ambient atmospheric conditions, such as temperature, humidity and pressure. - The
apparatus 10 includes afan 100 for causing air to flow through the apparatus, and as shown schematically inFIG. 1 , sitting atophousing 15. At normal ambient atmospheric conditions where freezing of the cooling liquid, typically water, is not of concern, air is drawn into theplenum 18 of the apparatus via air passages at the bottom of the unit through the open air intake dampers, and enters the evaporativeheat transfer section 12 where heat transfer takes place involving the distribution of water from awater distribution assembly 90 driven by apump 96. When the ambient temperature and the temperature of the cooling liquid fall to indicate a concern of freezing the cooling liquid, the distributor assembly of cooling liquid is turned off - Prior art
refrigerant coil assemblies 20 have a generally parallelepiped overall shape of six sides retained in aframe 21 and has a major/longitudinal axis 23, where each side is in the form of a rectangle. Thecoil assembly 20 is made of multiple horizontal closely spaced parallel, serpentine tubes connected at their ends to form a number of circuits through which the refrigerant flows. Each individual circuit within the coil assembly is a single, continuous length of coil tubing that is subjected to a bending operation which forms the tubing into several U-shaped rows that are in a generally vertical and equally-spaced relationship from each other, such that each circuit has a resultant serpentine shape. - The
coil assembly 20 has aninlet 22 connected to an inlet manifold orheader 24, which fluidly connects to inlet ends of the serpentine tubes of the coil assembly, and anoutlet 26 connected to an outlet manifold orheader 28, which fluidly connects to the outlet ends of the serpentine tubes of the coil assembly. The assembledcoil assembly 20 may be moved and transported as a unitary structure such that it may be dipped, if desired, if its components are made of steel, in a zinc bath to galvanize the entire coil assembly. - The refrigerant gas discharges from the compressor into the inlet connection of the apparatus. Heat from the refrigerant dissipates through the coil tubes to the water cascading downward over the tubes. Simultaneously, air is drawn in through the air inlet louvers at the base of the condenser and travels upward over the coil opposite the water flow. A small portion of the water evaporates, removing heat from the system. The warm moist air is drawn to the top of the evaporative condenser by the fan and discharged to the atmosphere. The remaining water falls to the sump at the bottom of the condenser where it recirculates through the water distribution system and back down over the coils.
- The invention constitutes a change and improvement over the prior art wherein instead of tube bundles comprising a single cross-sectional area throughout the entire refrigerant flow path through the coil, the indirect heat exchange section has multiple sections, each having different cross-sectional areas, decreasing as the refrigerant travels through the heat exchange section.
-
FIGS. 4a, 5a, 6a and 7a are photographs of a mockup of a multi-cross-sectional area refrigerant condenser according to an embodiment of the invention.FIGS. 4b, 5b, 6b and 7b are formal drawings corresponding toFIGS. 4a, 5a, 6a and 7a , respectively. Afirst condenser section 103 includes plurality ofstraight tubes 105 having a first total cross-sectional area. While round tubes are shown in the mock-up, tubes of any shape, size and feature may be used according to the invention. Indeed, any passage capable of permitting refrigerant flow and heat exchange may be adapted for use in connection with the invention in the place of the tubes shown in the Figures, including microchannel plates and other conduit structures. For the sake of the description of the invention with reference to the mock-ups shown inFIGS. 4a, 5a, 6a and 7a , the term “tube” will be used, but it should be understood that the words “passage,” or “conduit” may be substituted for the word “tube” in the description herein, whatever the construction, provided that it can convey refrigerant and permit heat exchange between refrigerant inside and air outside. - As used herein, the term “total cross-sectional area” refers to the sum of the cross-sectional areas of the individual tubes in a condenser section. The term “total cross-sectional area” as used herein is not calculated to include the area between tubes in a condenser section. The cross-sectional area of each
straight tube 105 infirst condenser section 103 may be the same as or different from one-another, but the sum of the cross-sectional areas of allstraight tubes 105 infirst condenser section 103 equals the first total cross-sectional area. The tubes infirst condenser section 103 are preferably finned. Eachstraight tube 105 in thefirst condenser section 103 terminates at one end at inlet header ormanifold 107 and at terminates at a second end at intermediate header ormanifold 109. - A second condenser section 111 includes a second plurality of
straight tubes 113 having a second total cross-sectional area. The cross-sectional area of eachstraight tube 113 in second condenser section 111 may be the same as or different from one-another, but the sum of the cross-sectional areas of allstraight tubes 113 in second condenser section 111 equals the second total cross-sectional area. The second total cross-sectional area is less than the first total cross-sectional area. The cross-sectional area of eachstraight tube 113 in the second condenser section may be the same or different from the cross-sectional area of eachstraight tube 105 in the first condenser section, but the cross-sectional area of eachstraight tube 113 in the second condenser section is preferably less than cross-sectional area of eachstraight tube 105 in the first condenser section. The number of tubes in the second condenser section may be the same or different from the number of tubes in the first condenser section, but is preferably less. The length of the tubes in the second condenser section may optionally be shorter than the length of the tubes in the first condenser section (as shown for example inFIGS. 4a and 4b ). The tubes in second condenser section 111 are preferably finned. - The second condenser section receives refrigerant from the first condenser section via intermediate header or
manifold 109. As shown, for example inFIGS. 4a and 4b , eachstraight tube 113 in the second condenser section terminates at one end at intermediate header ormanifold 109 and terminates at a second end at outlet header or manifold (not shown). - Alternatively, third, fourth and fifth or more condenser sections may be present.
FIG. 8 is a representation of an embodiment of the invention having four condenser sections. According to these embodiments, a second intermediate header ormanifold 115 directs refrigerant to athird condenser section 117, and each of said third 117, fourth 119, and fifth or more condenser sections are each constructed of a plurality of straight tubes, and each of said third, fourth, and fifth or more condenser sections each have a total cross-sectional area that is less than a cross-sectional area of an immediately upstream condenser section. - Each of the straight tubes in said third, fourth, and fifth or more condenser section is connected at one end to an immediately upstream condenser section by an intermediate header or manifold, and at a second end to another intermediate header or manifold 121 (if there is a subsequent condenser section) or to an outlet header or
manifold 123. -
FIG. 9 shows an alternate embodiment of the invention in which the inlet header, outlet header and intermediate headers are all arranged on the same side of the device, and each condenser section contains two sets of straight lengths of tubes connected at an end opposite the header end by U-bends. Accordingly,inlet header 201 receives superheated refrigerant vapor and distributes it to first set ofstraight tubes 203 in afirst condenser section 205. The first set ofstraight tubes 203 are connected at an opposite end to a second set of straight tubes 207 in said first condenser section byU-bends 209. The first and second set of tubes in the first condenser section have the same number of tubes and the tubes have the same diameter. U-bends 209 have approximately the same cross-sectional size/diameter as the first and second set of tubes in said first condenser section. The side of the second set of tubes in the first condenser section are connected at an end opposite the U-bend end to firstintermediate header 211. First intermediate header then delivers the refrigerant to thesecond condenser section 213 having a second condenser first set oftubes 215 and a second condenser second set oftubes 217 connected at an opposite end from said intermediate header by another set ofU-bends 219. The first and second set of tubes in said second condenser section have the same cross-sectional dimensions and are equal in number. The U-bends 219 connecting the first and second set of tubes in the second condenser section likewise have approximately the same cross-sectional dimensions as the first and second set of tubes they connect. The second condenser section second set oftubes 217 terminate at a secondintermediate header 221. The secondintermediate header 221 receives refrigerant from the second condenser section set oftubes 217 and direct it to thethird condenser section 223. The third condenser section first set of tubes 225 are connected at a first end to the second intermediate header and at an opposite end to yet another set of U-bends (not shown) that are in-turn connected to a first end of third condenser section second set oftubes 227. The third condenser section second set oftubes 227 are connected at the header end tooutlet header 229. The tubes of each condenser section are progressively smaller while (according to the embodiment shown inFIG. 9 ) the number of tubes in each condenser section is equal. However, as with the embodiments described above, the size of the tubes could be left the same, and the number of tubes could be reduced, so that the total cross-sectional area of each condenser section is smaller than the first section, and is preferably smaller than each upstream section. - By increasing the number of circuits (tubes) in the first condenser section and increasing the cross-sectional area of each tube in the first condenser section the invention can reduce the inlet vapor velocity more than 50% and thus reduce the refrigerant pressure drop to less than 25% of the original value. Moreover, the entrance vapor velocity, per circuit, is sufficient to establish an internal film heat transfer coefficient greater than the external heat transfer coefficient while limiting the internal pressure drop for the heat rejection intended. The subsequent decrease in total cross sectional area will occur after the first path or even later in the heat transfer fluid path depending upon operating conditions. The number of tubes in the second condenser section may be adjusted to additionally lower vapor velocity which in turn reduces refrigerant pressure drop. The second group also exhibits a reduced total cross sectional area then the first group in this illustration and thus maintains vapor velocity prior to entering the last reduction in cross sectional area. A third condenser section may have further reduced cross sectional area to re-establish the vapor velocity prior to exiting the condenser. It is most preferred that each condenser section incorporate smaller or same as, cross sectional area paths in comparison to the initial circuits. In doing so, the fluid (vapor) velocity is re-established such that the associated internal film heat transfer coefficient is greater than that leaving the initial total cross sectional area provided coupled with initial circuit quantity. Multi-cross sectional interfaces are preferably utilized throughout the condenser as needed via segmented headers (see, e.g.,
FIGS. 4a, 4b andFIG. 9 ) such that the heat transfer fluid (vapor) velocity can be maintained (on average) leading into the final pass. There are many permutations regarding the path cross sectional area coupled with number of paths per section that can be used with this invention to optimize performance. Iterative calculations can be performed depending upon the operating conditions, refrigerant and heat rejection requirements. There are other advantages with this invention including lower refrigerant inventory as well as better condenser efficiency due to reduced refrigerant pressure drop.
Claims (24)
Priority Applications (10)
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MX2019009613A MX2019009613A (en) | 2017-02-13 | 2018-02-13 | Multi-cross sectional fluid path condenser. |
JP2019543297A JP2020507732A (en) | 2017-02-13 | 2018-02-13 | Multi-section fluid path condenser |
PCT/US2018/018072 WO2018148760A1 (en) | 2017-02-13 | 2018-02-13 | Multi-cross sectional fluid path condenser |
CA3053372A CA3053372A1 (en) | 2017-02-13 | 2018-02-13 | Multi-cross sectional fluid path condenser |
US15/896,008 US20180238644A1 (en) | 2017-02-13 | 2018-02-13 | Multi-cross sectional fluid path condenser |
AU2018217903A AU2018217903A1 (en) | 2017-02-13 | 2018-02-13 | Multi-cross sectional fluid path condenser |
BR112019016728A BR112019016728A2 (en) | 2017-02-13 | 2018-02-13 | multi-cross-section fluid path condenser |
RU2019124960A RU2769608C2 (en) | 2017-02-13 | 2018-02-13 | Condenser with fluid medium flow channel with several cross sections |
KR1020197025772A KR20190118598A (en) | 2017-02-13 | 2018-02-13 | Multi Section Euro Condenser |
ZA2019/05588A ZA201905588B (en) | 2017-02-13 | 2019-08-23 | Multi-cross sectional fluid path condenser |
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US201762458070P | 2017-02-13 | 2017-02-13 | |
US15/896,008 US20180238644A1 (en) | 2017-02-13 | 2018-02-13 | Multi-cross sectional fluid path condenser |
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JP (1) | JP2020507732A (en) |
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CN110822934B (en) * | 2019-11-09 | 2021-01-29 | 南京紫侯弘新型建材有限公司 | Evaporate cauldron steam recycle device that presses |
CN110736359B (en) * | 2019-11-09 | 2021-02-02 | 南京紫侯弘新型建材有限公司 | Evaporate high-efficient recycle device of pressure cauldron steam |
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DE4245046C8 (en) * | 1992-11-18 | 2008-08-21 | Behr Gmbh & Co. Kg | Condenser for an air conditioning system of a vehicle |
RU2045726C1 (en) * | 1993-01-11 | 1995-10-10 | Предприятие "Кубань-ПромАгроСервис" | Condenser |
JP2000257989A (en) * | 1999-03-11 | 2000-09-22 | Nippon Light Metal Co Ltd | Heat exchanger |
DE10065205A1 (en) * | 2000-12-23 | 2002-07-04 | Behr Gmbh & Co | Refrigerant condenser |
JP2004077039A (en) * | 2002-08-20 | 2004-03-11 | Sumitomo Precision Prod Co Ltd | Evaporation type condenser |
BE1015427A3 (en) * | 2003-03-24 | 2005-03-01 | Jaga Nv | Improved radiator. |
KR20090022840A (en) * | 2007-08-31 | 2009-03-04 | 엘지전자 주식회사 | Heat exchanger |
CN101978229B (en) | 2008-10-20 | 2013-03-27 | 株式会社京滨冷暖科技 | Condenser |
US9347764B2 (en) | 2014-04-23 | 2016-05-24 | American Axle & Manufacturing, Inc. | Sensor assembly configured to sense target movement in first direction and insensitive to target movement in second and third directions orthogonal to first direction |
JP6456088B2 (en) * | 2014-09-29 | 2019-01-23 | 三菱重工サーマルシステムズ株式会社 | Radiator and refrigeration cycle device |
-
2018
- 2018-02-13 JP JP2019543297A patent/JP2020507732A/en active Pending
- 2018-02-13 US US15/896,008 patent/US20180238644A1/en not_active Abandoned
- 2018-02-13 RU RU2019124960A patent/RU2769608C2/en active
- 2018-02-13 MX MX2019009613A patent/MX2019009613A/en unknown
- 2018-02-13 CA CA3053372A patent/CA3053372A1/en active Pending
- 2018-02-13 KR KR1020197025772A patent/KR20190118598A/en not_active Application Discontinuation
- 2018-02-13 WO PCT/US2018/018072 patent/WO2018148760A1/en active Application Filing
- 2018-02-13 BR BR112019016728A patent/BR112019016728A2/en not_active Application Discontinuation
- 2018-02-13 AU AU2018217903A patent/AU2018217903A1/en not_active Abandoned
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Patent Citations (4)
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US20020007646A1 (en) * | 2000-06-20 | 2002-01-24 | Showa Denko K.K. | Condenser |
US20020029873A1 (en) * | 2000-09-14 | 2002-03-14 | Hajime Sugito | Cooling device boiling and condensing refrigerant |
US20020039279A1 (en) * | 2000-09-21 | 2002-04-04 | Kenichi Ishikawa | Cooling unit for cooling a heat generating component and electronic apparatus having the cooling unit |
US20020186500A1 (en) * | 2001-06-07 | 2002-12-12 | Patel Chandrakant D. | Disc drive having integral base cooling |
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KR20190118598A (en) | 2019-10-18 |
WO2018148760A1 (en) | 2018-08-16 |
ZA201905588B (en) | 2020-03-25 |
RU2019124960A (en) | 2021-03-16 |
MX2019009613A (en) | 2019-10-14 |
CA3053372A1 (en) | 2018-08-16 |
AU2018217903A1 (en) | 2019-08-29 |
JP2020507732A (en) | 2020-03-12 |
BR112019016728A2 (en) | 2020-04-07 |
RU2769608C2 (en) | 2022-04-04 |
RU2019124960A3 (en) | 2021-06-08 |
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