US20090159248A1 - Heat exchanger, heat exchanger tube and methods of making and using same - Google Patents

Heat exchanger, heat exchanger tube and methods of making and using same Download PDF

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Publication number
US20090159248A1
US20090159248A1 US12/316,715 US31671508A US2009159248A1 US 20090159248 A1 US20090159248 A1 US 20090159248A1 US 31671508 A US31671508 A US 31671508A US 2009159248 A1 US2009159248 A1 US 2009159248A1
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United States
Prior art keywords
tube
heat exchanger
twisted
inner tube
reinforcing sleeve
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Abandoned
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US12/316,715
Inventor
Timothy E. Mimitz, SR.
Sunil Raina
Fred C. Scheideman
Floyd J. Lewis, JR.
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Turbotec Products Inc
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Turbotec Products Inc
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Priority to US12/316,715 priority Critical patent/US20090159248A1/en
Assigned to TURBOTEC PRODUCTS, INC. reassignment TURBOTEC PRODUCTS, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: MIMITZ, SR., TIMOTHY E., RAINA, SUNIL, LEWIS, JR., FLOYD J., SCHEIDEMAN, FRED C.
Publication of US20090159248A1 publication Critical patent/US20090159248A1/en
Abandoned legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/10Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/12Tubular 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
    • F28F1/34Tubular 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 obliquely
    • F28F1/36Tubular 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 obliquely the means being helically wound fins or wire spirals
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C37/00Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape
    • B21C37/06Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape of tubes or metal hoses; Combined procedures for making tubes, e.g. for making multi-wall tubes
    • B21C37/15Making tubes of special shape; Making tube fittings
    • B21C37/20Making helical or similar guides in or on tubes without removing material, e.g. by drawing same over mandrels, by pushing same through dies ; Making tubes with angled walls, ribbed tubes and tubes with decorated walls
    • B21C37/207Making helical or similar guides in or on tubes without removing material, e.g. by drawing same over mandrels, by pushing same through dies ; Making tubes with angled walls, ribbed tubes and tubes with decorated walls with helical guides
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D7/00Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/02Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being helically coiled
    • F28D7/022Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being helically coiled the conduits of two or more media in heat-exchange relationship being helically coiled, the coils having a cylindrical configuration
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D7/00Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/10Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged one within the other, e.g. concentrically
    • F28D7/106Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged one within the other, e.g. concentrically consisting of two coaxial conduits or modules of two coaxial conduits
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/02Tubular elements of cross-section which is non-circular
    • F28F1/06Tubular elements of cross-section which is non-circular crimped or corrugated in cross-section
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/08Tubular elements crimped or corrugated in longitudinal section
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F21/00Constructions of heat-exchange apparatus characterised by the selection of particular materials
    • F28F21/08Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
    • F28F21/081Heat exchange elements made from metals or metal alloys
    • F28F21/086Heat exchange elements made from metals or metal alloys from titanium or titanium alloys
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2210/00Heat exchange conduits
    • F28F2210/06Heat exchange conduits having walls comprising obliquely extending corrugations, e.g. in the form of threads
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4935Heat exchanger or boiler making

Definitions

  • Tube-in-tube heat exchangers are used in a variety of applications for transferring heat from one fluid to another. Particular configurations of tube-in-tube heat exchangers are described in U.S. Pat. Nos. 5,004,047 and 6,012,514.
  • tube-in-tube heat exchangers used for swimming pool heat pumps had CuNi inner tubes enclosed in a copper or steel jacket. Later, titanium alloys were used to form the inner tubes in order to provide improved chlorine resistance, and the outer shells were made of polyvinyl chloride.
  • swimming pool heat pumps are available that have heat exchangers formed from an inner tube of twisted titanium in a plastic polyvinyl chloride jacket.
  • the heat exchangers are suitable for use with R-22 refrigerant.
  • the twisted titanium tube is connected to a copper tube transition with a lock ring connector.
  • One embodiment is a heat exchanger tube comprising a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion, the transition portion including a reinforcing sleeve.
  • Another embodiment is a heat exchanger comprising an outer tube and an inner tube defining an annular opening therebetween, the inner tube including a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion including a reinforcing sleeve formed thereon, the inner tube being configured to withstand a hydrostatic test pressure of at least 2600 psig for at least 2 minutes without mechanical failure.
  • Yet another embodiment is a heat exchanger comprising an outer tube and an inner tube defining an annular opening therebetween, the inner tube including a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion including a reinforcing sleeve formed thereon, the inner tube being configured to pass a fatigue test of 250,000 cycles between 118 psig and 418 psig at a rate of 0.5 cycles/second without mechanical failure.
  • Another embodiment is a method of making a heat exchanger tube comprising forming a inner tube comprising a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion, and forming a reinforcing sleeve over the transition portion.
  • Yet another embodiment is a heat exchanger comprising an inner tube comprising a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion including reinforcing sleeve, and an outer tube or shell surrounding the inner tube.
  • a further embodiment is a method of extending the useful life of a heat exchanger tube comprising a first portion connected to a twisted portion, the method comprising forming a reinforcing sleeve over the connection between the first portion and the twisted portion.
  • Yet another embodiment is a method of forming a heat exchanger tube capable of use at test pressures up to at least 2600 psig, comprising forming a heat exchanger tube comprising a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion, and forming a reinforcing sleeve over the transition portion.
  • Another embodiment is a method of forming a heat exchanger tube capable of use at operating pressures up to at least 500 psig, comprising forming a heat exchanger tube comprising a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion, and forming a reinforcing sleeve over the transition portion.
  • a further embodiment is a method of protecting a twisted heat exchanger tube from fluid impingement on its outer surface, comprising forming a reinforcing sleeve over the upstream part of the twisted portion of the tube.
  • FIG. 1 is a side view of a sleeved tube segment in accordance with certain embodiments.
  • FIG. 2 is a side view of a tube segment with the outer layers cut away to show the transition portion beneath the sleeve.
  • FIG. 3 is a section view of the sleeved tube segment of FIG. 1 .
  • FIG. 4 is a perspective view of a heat exchanger tube containing the sleeved tube segment of FIG. 1 .
  • FIG. 5 is a side view of a segment of the heat exchanger tube with the outer layer cut away to show the sleeved tube segment.
  • a new and improved heat exchanger tube has been developed that enables environmentally favorable and efficient refrigerants to be used in corrosive environments, including in the presence of chlorinated swimming pool water.
  • the new heat exchanger tube can be used at pressures up to 500 psig or more, or 600 psig or more, and is particularly useful when the pressure difference on opposite sides of the tube wall is 300 psig or more.
  • the tube can be used with R-410A refrigerant, which has a zero Ozone Depleting Potential, as well as other refrigerants requiring high pressures.
  • the new tube can be fabricated in a variety of sizes and shapes. Typically, the twisted tube is coiled and is enclosed a hard coil-shaped tube made of plastic or another suitable material. The coils can have various diameters, and various numbers of turns per linear meter.
  • a “twisted portion” of a tube is a portion that has improved heat transfer resulting from increased surface area per unit length of the tube by twisting the tube.
  • a twisted portion of tube material has one or more visible flutes on one or both of its inner and outer surfaces.
  • a “smooth portion” and a “straight portion” of a tube are non-twisted portions of a tube.
  • mechanical failure refers to a fracture or rupture of the tube.
  • a side view of a tube is shown and is generally designated as 10 .
  • the tube 10 includes a first portion 12 (which usually but not necessarily is a non-twisted or straight portion), a twisted portion 14 and a transition portion 18 between the straight portion 12 and the twisted portion 14 .
  • a reinforcing sleeve 16 is mounted over the transition portion 18 .
  • the reinforcing sleeve 16 usually is formed from straight tube material, however other configurations of tube material can be used.
  • the twisted portion 14 of the tube 10 includes a spiraling flute 17 and a corresponding valley 19 , both of which spiral along the length of the twisted portion 14 of the tube 10 .
  • Tube configurations having multiple flutes and valleys also can be used.
  • the first portion 12 and twisted portion 14 usually comprise titanium and often are made from a titanium alloy.
  • the sleeve 16 typically is formed from titanium or a titanium alloy.
  • the sleeve prevents mechanical failure of the twisted portion 14 of the tube material at and near the connection with the first portion 12 of the tube material when the heat exchanger is operated at a 500 or 520 psig (or higher) working pressure.
  • the sleeve also prevents mechanical failure of the twisted portion 14 of the tube material at and near the connection with the first portion 12 of the tube material when the tube 10 is tested at a test pressure of, e.g. 2500-3000 psig for 2-6 minutes.
  • the sleeve typically has an outer diameter in the range of about 0.75 inch to 1.25 inch, and a length of about 5-7 inches. It is noted that tubing with larger and smaller dimensions can be used, and that sleeves of longer and shorter lengths can be used.
  • the flutes typically have a peak-to-valley height of about 0.145′′ to 0.150′′ and a length of approximately 0.375′′ per rotation.
  • the twisted portion of the tube often has an average wall thickness in the range of 0.018′′ to 0.025′′.
  • the thinness of the tube wall provides for effective heat transfer between the fluids on opposite sides of the tube wall.
  • the ratio of the length to the outer diameter of the sleeve typically, but not necessarily, is in the range of 6-8, and often is in the range of 6.5 to 7.0.
  • FIG. 2 shows the portion of a tube 10 ′ that is connected to other tubing.
  • the first portion 12 ′ is connected to a second tube 21 which typically is formed from a different material, such as copper.
  • the second tube 21 and a connector 23 typically are positioned beside (not within) an outer heat exchanger tube (not shown).
  • the connector 23 typically comprises brass or another suitable material and connects the first portion 12 ′ to the second tube 21 .
  • the sleeve 16 ′ is cut away to show further details of the transition portion 18 ′.
  • a first section 13 of the transition portion 18 ′ is straight and a second section 15 is twisted.
  • the first and second sections 13 and 15 typically are part of a continuous piece of tube material.
  • about one quarter of the length of the tube material covered by the sleeve 16 ′ is straight tube, and about three quarters of the length of tube material covered by the sleeve 16 ′ is twisted tube.
  • Inner wall 25 of sleeve 16 ′ is adjacent to the flute 17 ′.
  • the inner wall 25 of sleeve 16 ′ is also configured to fit closely around the outer wall 24 of first portion 12 ′.
  • the sleeve will be slightly tapered to accommodate these dimensions.
  • FIG. 3 shows a cross-sectional view of the tube 10 of FIG. 1 taken along line 3 - 3 of FIG. 1 .
  • the flute 17 on the outer surface of the twisted portion 14 of the second section 15 forms a complementary channel 27 inside the twisted portion 14 of the tube 10 .
  • the valley 19 on the outer surface of the twisted portion forms a corresponding, inwardly projecting portion 29 inside the twisted portion 14 of the tube 10 . This configuration promotes mixing on both sides of the twisted tube wall.
  • FIGS. 4 and 5 show a tube-in-tube heat exchanger 100 .
  • the heat exchanger 100 has a helically coiled outer tube 102 which contains an inner tube 110 , which preferably but not necessarily is coaxial with the outer tube 102 , forming an annular opening 104 therebetween configured for flow of a heat transfer fluid therethrough.
  • a sleeve 116 is positioned over the transition between a first portion 112 and a twisted portion 114 of the tube 110 .
  • the twisted portion 114 has a flute 117 and a valley 119 .
  • the inner tube 110 generally has the configuration of the tube shown in FIG. 1 .
  • the heat exchanger 100 has a water inlet 132 , a water outlet (not shown), a refrigerant inlet section with a refrigerant inlet (not shown), and a refrigerant outlet section 140 with a refrigerant outlet 142 .
  • the outer tube 102 can be made of a material that is resistant to corrosion by the fluid that flows in the annular opening 104 .
  • a hard plastic material such as polyvinyl chloride can be used.
  • the reinforcing sleeve provides for use of the tube in a tube-in-tube heat exchanger in which the pressure difference between the inside and the outside of the tube is at least 300 psi. or at least 450 psi, or at least 550 psi.
  • a refrigerant such as R-410A
  • the pressure on the inside of the inner tube typically reaches a maximum of 600 psig and the pressure on the outside of the inner tube typically is in the range of 25 to 100.
  • Example 1-6 and 9 Seven different sets of tubes having a straight portion and a twisted portion (Samples 1-6 and 9) were tested using fatigue test UL 1995 to determine their suitability for use in a heat exchanger operating with R-410A refrigerant. Two sets of tube material that only contained smooth tubing also were tested (Samples 7-8).
  • the twisted tubes were formed from a titanium alloy and had the following general dimensions: 7 ⁇ 8 inch outer diameter, 0.020 wall thickness along the straight portion, and 0.020 average wall thickness along the twisted portion.
  • the fluted portion had an outer diameter of about 0.810-0.850, a height of about 0.145 from flute to valley as measured on the outer wall, and approximately 33 turns per linear foot.
  • the titanium alloy used in making the tube material has an ultimate tensile strength of approximately 65 ksi, a yield strength of approximately 50 ksi and a nominal composition typical of type 2 titanium.
  • the smooth tubes had the same composition as the twisted tube and the same dimensions as the smooth portion of the twisted tubes.
  • the tubes were cycled between 118 psig and 418 psig for 250,000 cycles. Hydraulic oil was used as the test fluid. The outer surface of the tube was maintained at atmospheric pressure. To pass the test, no failure can occur.
  • the hydraulic system was controlled by a servo valve to pressurize the test articles.
  • the system included a hydraulic pump, interconnecting piping, on/off valves, servo valve, filters, accumulator and PLC electronic controls.
  • UL 1995 requires that the high and low pressure in any cycle be maintained for at least 0.10 seconds. Tests were run at around 0.5 cycles/sec or 2 sec/cycle.
  • Example 10-14 Five different types of tubes having a straight portion and a twisted portion (Samples 10-14) were tested using a hydrostatic strength test to determine their suitability for use in a heat exchanger operating with R-410A refrigerant.
  • the twisted tubes were formed from a titanium alloy and had the following general dimensions: 7 ⁇ 8 inch outer diameter, 0.020′′ wall thickness along the straight portion, and 0.020′′ average wall thickness along the twisted portion.
  • the fluted portion had an outer diameter of about 0.810-0.850′′, a height of about 0.134′′ from flute to valley as measured on the outer wall, and approximately 33 turns per lineal foot.
  • the titanium alloy used in making the tube material has an ultimate tensile strength of approximately 65 ksi, a yield strength of approximately 50 ksi and a nominal composition typical of type 2 titanium.
  • a tube is required to withstand 5 times the desired working pressure for a minimum of 2 minutes.
  • the test is run at 2600 psi, and for a desired working pressure or 600 psi the test is run at 3000 psi. Pressure outside the tube was atmospheric. Water was used as the fluid in the high pressure test.
  • Reinforcing sleeves made of type 2 titanium alloy having an inner diameter of about 7 ⁇ 8 inch and a length of 6 inches were placed (swaged) around the transition point from smooth tubing to twisted tubing of several samples of the same type of tube material of the same dimensions as was used in Example 2.
  • the tubes with the reinforcing sleeves were subjected to the hydrostatic strength test described above in Example 2 using water as the high pressure test fluid.
  • the inside of the twisted tube was brought to a pressure of 2,600 psig, and this pressure was maintained for 2 minutes. Subsequently, the pressure was increased to 2,700 psig for 2 additional minutes, and the pressure was then increased to 3,000 psig for 2 more minutes.
  • the outer surface of the tube was at atmospheric pressure. The twisted tube was then examined for failures.
  • Example 16 The same type of tube samples as were used in Example 3, Sample 16, were subjected to a fatigue test in accordance with UL1995, described above in Example 1, using hydraulic oil as the test fluid. The set of samples passed two full rounds of testing without any failures. The results are shown in Table 1 as Sample 17 (Example TR-2007 041).
  • twisted tubes can be used in conjunction with refrigerants that replace HCFCs.
  • refrigerants that can be used with the embodiments described herein are provided below on Table 2.

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

Abstract

A heat exchanger tube is disclosed herein comprising a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion. The transition portion includes a reinforcing sleeve. A heat exchanger formed from the tube and a method of forming a heat exchanger tube also are disclosed. The tube is useful in making a heat exchanger configured to operate at high pressures without mechanical failure.

Description

    RELATED APPLICATIONS
  • This application claims priority from U.S. Provisional Patent Application No. 61/008,807 filed Dec. 21, 2007.
  • BACKGROUND
  • Tube-in-tube heat exchangers are used in a variety of applications for transferring heat from one fluid to another. Particular configurations of tube-in-tube heat exchangers are described in U.S. Pat. Nos. 5,004,047 and 6,012,514.
  • Traditionally, tube-in-tube heat exchangers used for swimming pool heat pumps had CuNi inner tubes enclosed in a copper or steel jacket. Later, titanium alloys were used to form the inner tubes in order to provide improved chlorine resistance, and the outer shells were made of polyvinyl chloride.
  • Currently, swimming pool heat pumps are available that have heat exchangers formed from an inner tube of twisted titanium in a plastic polyvinyl chloride jacket. The heat exchangers are suitable for use with R-22 refrigerant. The twisted titanium tube is connected to a copper tube transition with a lock ring connector.
  • It would be useful to further improve the efficiency of heat exchangers used in corrosive environments, including but not limited to swimming pool heat exchangers.
  • SUMMARY
  • One embodiment is a heat exchanger tube comprising a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion, the transition portion including a reinforcing sleeve.
  • Another embodiment is a heat exchanger comprising an outer tube and an inner tube defining an annular opening therebetween, the inner tube including a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion including a reinforcing sleeve formed thereon, the inner tube being configured to withstand a hydrostatic test pressure of at least 2600 psig for at least 2 minutes without mechanical failure.
  • Yet another embodiment is a heat exchanger comprising an outer tube and an inner tube defining an annular opening therebetween, the inner tube including a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion including a reinforcing sleeve formed thereon, the inner tube being configured to pass a fatigue test of 250,000 cycles between 118 psig and 418 psig at a rate of 0.5 cycles/second without mechanical failure.
  • Another embodiment is a method of making a heat exchanger tube comprising forming a inner tube comprising a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion, and forming a reinforcing sleeve over the transition portion.
  • Yet another embodiment is a heat exchanger comprising an inner tube comprising a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion including reinforcing sleeve, and an outer tube or shell surrounding the inner tube.
  • A further embodiment is a method of extending the useful life of a heat exchanger tube comprising a first portion connected to a twisted portion, the method comprising forming a reinforcing sleeve over the connection between the first portion and the twisted portion.
  • Yet another embodiment is a method of forming a heat exchanger tube capable of use at test pressures up to at least 2600 psig, comprising forming a heat exchanger tube comprising a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion, and forming a reinforcing sleeve over the transition portion.
  • Another embodiment is a method of forming a heat exchanger tube capable of use at operating pressures up to at least 500 psig, comprising forming a heat exchanger tube comprising a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion, and forming a reinforcing sleeve over the transition portion.
  • A further embodiment is a method of protecting a twisted heat exchanger tube from fluid impingement on its outer surface, comprising forming a reinforcing sleeve over the upstream part of the twisted portion of the tube.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a side view of a sleeved tube segment in accordance with certain embodiments.
  • FIG. 2 is a side view of a tube segment with the outer layers cut away to show the transition portion beneath the sleeve.
  • FIG. 3 is a section view of the sleeved tube segment of FIG. 1.
  • FIG. 4 is a perspective view of a heat exchanger tube containing the sleeved tube segment of FIG. 1.
  • FIG. 5 is a side view of a segment of the heat exchanger tube with the outer layer cut away to show the sleeved tube segment.
  • DETAILED DESCRIPTION
  • A new and improved heat exchanger tube has been developed that enables environmentally favorable and efficient refrigerants to be used in corrosive environments, including in the presence of chlorinated swimming pool water. The new heat exchanger tube can be used at pressures up to 500 psig or more, or 600 psig or more, and is particularly useful when the pressure difference on opposite sides of the tube wall is 300 psig or more. The tube can be used with R-410A refrigerant, which has a zero Ozone Depleting Potential, as well as other refrigerants requiring high pressures. The new tube can be fabricated in a variety of sizes and shapes. Typically, the twisted tube is coiled and is enclosed a hard coil-shaped tube made of plastic or another suitable material. The coils can have various diameters, and various numbers of turns per linear meter.
  • Definitions
  • As used herein, a “twisted portion” of a tube is a portion that has improved heat transfer resulting from increased surface area per unit length of the tube by twisting the tube. A twisted portion of tube material has one or more visible flutes on one or both of its inner and outer surfaces. As used herein, a “smooth portion” and a “straight portion” of a tube are non-twisted portions of a tube. As used herein, “mechanical failure” refers to a fracture or rupture of the tube.
  • Referring first to FIG. 1, a side view of a tube is shown and is generally designated as 10. The tube 10 includes a first portion 12 (which usually but not necessarily is a non-twisted or straight portion), a twisted portion 14 and a transition portion 18 between the straight portion 12 and the twisted portion 14. A reinforcing sleeve 16 is mounted over the transition portion 18. The reinforcing sleeve 16 usually is formed from straight tube material, however other configurations of tube material can be used.
  • The twisted portion 14 of the tube 10 includes a spiraling flute 17 and a corresponding valley 19, both of which spiral along the length of the twisted portion 14 of the tube 10. Tube configurations having multiple flutes and valleys also can be used.
  • The first portion 12 and twisted portion 14 usually comprise titanium and often are made from a titanium alloy. The sleeve 16 typically is formed from titanium or a titanium alloy. The sleeve prevents mechanical failure of the twisted portion 14 of the tube material at and near the connection with the first portion 12 of the tube material when the heat exchanger is operated at a 500 or 520 psig (or higher) working pressure. The sleeve also prevents mechanical failure of the twisted portion 14 of the tube material at and near the connection with the first portion 12 of the tube material when the tube 10 is tested at a test pressure of, e.g. 2500-3000 psig for 2-6 minutes.
  • For a swimming pool or spa heat exchanger, the sleeve typically has an outer diameter in the range of about 0.75 inch to 1.25 inch, and a length of about 5-7 inches. It is noted that tubing with larger and smaller dimensions can be used, and that sleeves of longer and shorter lengths can be used. The flutes typically have a peak-to-valley height of about 0.145″ to 0.150″ and a length of approximately 0.375″ per rotation. The twisted portion of the tube often has an average wall thickness in the range of 0.018″ to 0.025″. The thinness of the tube wall provides for effective heat transfer between the fluids on opposite sides of the tube wall. The ratio of the length to the outer diameter of the sleeve typically, but not necessarily, is in the range of 6-8, and often is in the range of 6.5 to 7.0.
  • FIG. 2 shows the portion of a tube 10′ that is connected to other tubing. In this embodiment, the first portion 12′ is connected to a second tube 21 which typically is formed from a different material, such as copper. The second tube 21 and a connector 23 typically are positioned beside (not within) an outer heat exchanger tube (not shown). The connector 23 typically comprises brass or another suitable material and connects the first portion 12′ to the second tube 21.
  • In FIG. 2, the sleeve 16′ is cut away to show further details of the transition portion 18′. In the particular embodiment shown in FIG. 2, a first section 13 of the transition portion 18′ is straight and a second section 15 is twisted. The first and second sections 13 and 15 typically are part of a continuous piece of tube material. In the embodiment shown in FIG. 2, about one quarter of the length of the tube material covered by the sleeve 16′ is straight tube, and about three quarters of the length of tube material covered by the sleeve 16′ is twisted tube. Inner wall 25 of sleeve 16′ is adjacent to the flute 17′. The inner wall 25 of sleeve 16′ is also configured to fit closely around the outer wall 24 of first portion 12′. In embodiments in which the twisted portion 14′ of the tube 10′ has a larger outer diameter than the first portion 12′, the sleeve will be slightly tapered to accommodate these dimensions.
  • FIG. 3 shows a cross-sectional view of the tube 10 of FIG. 1 taken along line 3-3 of FIG. 1. The flute 17 on the outer surface of the twisted portion 14 of the second section 15 forms a complementary channel 27 inside the twisted portion 14 of the tube 10. The valley 19 on the outer surface of the twisted portion forms a corresponding, inwardly projecting portion 29 inside the twisted portion 14 of the tube 10. This configuration promotes mixing on both sides of the twisted tube wall.
  • FIGS. 4 and 5 show a tube-in-tube heat exchanger 100. The heat exchanger 100 has a helically coiled outer tube 102 which contains an inner tube 110, which preferably but not necessarily is coaxial with the outer tube 102, forming an annular opening 104 therebetween configured for flow of a heat transfer fluid therethrough. A sleeve 116 is positioned over the transition between a first portion 112 and a twisted portion 114 of the tube 110. The twisted portion 114 has a flute 117 and a valley 119. The inner tube 110 generally has the configuration of the tube shown in FIG. 1. The heat exchanger 100 has a water inlet 132, a water outlet (not shown), a refrigerant inlet section with a refrigerant inlet (not shown), and a refrigerant outlet section 140 with a refrigerant outlet 142.
  • The outer tube 102 can be made of a material that is resistant to corrosion by the fluid that flows in the annular opening 104. When the fluid is chlorinated water, a hard plastic material such as polyvinyl chloride can be used. The reinforcing sleeve provides for use of the tube in a tube-in-tube heat exchanger in which the pressure difference between the inside and the outside of the tube is at least 300 psi. or at least 450 psi, or at least 550 psi. When a refrigerant such as R-410A is used, the pressure on the inside of the inner tube typically reaches a maximum of 600 psig and the pressure on the outside of the inner tube typically is in the range of 25 to 100.
  • Various tests were conducted during the process of forming the new heat exchanger tubing. Test procedures and results are shown in Examples 1-3. The examples are included to illustrate features of the invention but are not intended to be limiting.
  • EXAMPLE 1 Fatigue Testing
  • Seven different sets of tubes having a straight portion and a twisted portion (Samples 1-6 and 9) were tested using fatigue test UL 1995 to determine their suitability for use in a heat exchanger operating with R-410A refrigerant. Two sets of tube material that only contained smooth tubing also were tested (Samples 7-8). The twisted tubes were formed from a titanium alloy and had the following general dimensions: ⅞ inch outer diameter, 0.020 wall thickness along the straight portion, and 0.020 average wall thickness along the twisted portion. The fluted portion had an outer diameter of about 0.810-0.850, a height of about 0.145 from flute to valley as measured on the outer wall, and approximately 33 turns per linear foot. According to the literature, the titanium alloy used in making the tube material has an ultimate tensile strength of approximately 65 ksi, a yield strength of approximately 50 ksi and a nominal composition typical of type 2 titanium. The smooth tubes had the same composition as the twisted tube and the same dimensions as the smooth portion of the twisted tubes.
  • In the fatigue test (as per UL 1995), the tubes were cycled between 118 psig and 418 psig for 250,000 cycles. Hydraulic oil was used as the test fluid. The outer surface of the tube was maintained at atmospheric pressure. To pass the test, no failure can occur. The hydraulic system was controlled by a servo valve to pressurize the test articles. The system included a hydraulic pump, interconnecting piping, on/off valves, servo valve, filters, accumulator and PLC electronic controls. UL 1995 requires that the high and low pressure in any cycle be maintained for at least 0.10 seconds. Tests were run at around 0.5 cycles/sec or 2 sec/cycle.
  • As is shown on Table 1 below, none of the twisted tube Samples 1-6 and 9 passed the fatigue test. Both of the smooth tube Samples 7-8 passed the test, showing that the non-twisted material is acceptable for use at the pressures required for R-410A refrigerant.
  • EXAMPLE 2 Hydrostatic Strength Testing
  • Five different types of tubes having a straight portion and a twisted portion (Samples 10-14) were tested using a hydrostatic strength test to determine their suitability for use in a heat exchanger operating with R-410A refrigerant. The twisted tubes were formed from a titanium alloy and had the following general dimensions: ⅞ inch outer diameter, 0.020″ wall thickness along the straight portion, and 0.020″ average wall thickness along the twisted portion. The fluted portion had an outer diameter of about 0.810-0.850″, a height of about 0.134″ from flute to valley as measured on the outer wall, and approximately 33 turns per lineal foot. According to the literature, the titanium alloy used in making the tube material has an ultimate tensile strength of approximately 65 ksi, a yield strength of approximately 50 ksi and a nominal composition typical of type 2 titanium.
  • To pass the hydrostatic strength test, a tube is required to withstand 5 times the desired working pressure for a minimum of 2 minutes. Thus, for a desired working pressure of 520 psi the test is run at 2600 psi, and for a desired working pressure or 600 psi the test is run at 3000 psi. Pressure outside the tube was atmospheric. Water was used as the fluid in the high pressure test.
  • As is shown on Table 1 below, none of Samples 10-14 passed the hydrostatic strength test at 2600 psig, thus showing the difficulty in using twisted tube material in high pressure environments.
  • TABLE I
    Required Acceptance Samples Test
    Task Procedure/Method Task Description Criteria Location Tested Result
    1 Fatigue Test-UL 1995 Turbotec Laboratory 250K cycles Turbotec 3 Fail
    R410A TR2004-134 without failure Inc.
    2 Fatigue Test-UL 1995 Turbotec Laboratory 250K cycles Turbotec 3 Fail
    R410A TR2004-135 without failure Inc.
    3 Fatigue Test-UL 1995 Turbotec Laboratory 250K cycles Turbotec 3 Fail
    R410A TR2006-091 without failure Inc.
    4 Fatigue Test-UL 1995 Turbotec Laboratory 250K cycles Turbotec 3 Fail
    R410A TR2006-101 without failure Inc.
    5 Fatigue Test-UL 1995 Turbotec Laboratory 250K cycles Turbotec 3 Fail
    R410A TR2006-127 without failure Inc.
    6 Fatigue Test-UL 1995 Turbotec Laboratory 250K cycles Turbotec 3 Fail
    R410A TR2006-142 without failure Inc.
    7 Fatigue Test-UL 1995 Turbotec Laboratory 250K cycles Turbotec 3 Pass
    R410A TR2006-177 without failure Inc.
    8 Fatigue Test-UL 1995 Turbotec Laboratory 250K cycles Turbotec 3 Pass
    R410A TR2006-178 without failure Inc.
    9 Fatigue Test-UL 1995 Turbotec Laboratory 250K cycles Turbotec 3 Fail
    R410A TR2006-192 without failure Inc.
    10 Hydostatic Pressure Turbotec Laboratory 2600 psig Turbotec 2 Fail
    Tube Side R410A TR2006-197 Inc.
    11 Hydostatic Pressure Turbotec Laboratory 2600 psig Turbotec 2 Fail
    Tube Side R410A TR2006-206 Inc.
    12 Hydostatic Pressure Turbotec Laboratory 2600 psig Turbotec 2 Fail
    Tube Side R410A TR2006-214 Inc.
    13 Hydostatic Pressure Turbotec Laboratory 2600 psig Turbotec 2 Fail
    Tube Side R410A TR2006-220 Inc.
    14 Hydostatic Pressure Turbotec Laboratory 2600 psig Turbotec 2 Fail
    Tube Side R410A TR2007-007 Inc.
    15 Hydostatic Pressure Turbotec Laboratory 3000 psig Turbotec 2 Fail
    Tube Side R410A TR2007-024 Inc.
    16 Hydostatic Pressure Turbotec Laboratory 3000 psig Turbotec 2 Pass
    Tube Side R410A TR2007-039 Inc.
    17 Fatigue Test-UL 1995 R Turbotec Laboratory 250K cycles Turbotec In 3 Pass
    TF2007-041 without failure
  • EXAMPLE 3 Twisted Tube with Reinforcing Sleeve
  • Reinforcing sleeves made of type 2 titanium alloy having an inner diameter of about ⅞ inch and a length of 6 inches were placed (swaged) around the transition point from smooth tubing to twisted tubing of several samples of the same type of tube material of the same dimensions as was used in Example 2. The tubes with the reinforcing sleeves were subjected to the hydrostatic strength test described above in Example 2 using water as the high pressure test fluid. The inside of the twisted tube was brought to a pressure of 2,600 psig, and this pressure was maintained for 2 minutes. Subsequently, the pressure was increased to 2,700 psig for 2 additional minutes, and the pressure was then increased to 3,000 psig for 2 more minutes. The outer surface of the tube was at atmospheric pressure. The twisted tube was then examined for failures.
  • For Sample set 15 (TR 2007-024) which included the reinforcing sleeve, no failures were detected at 2600 psig but failure occurred at 3000 psig. For tube sample TR 2007-039, which included both a reinforcing sleeve and a tight fit reducer bushing positioned around the plain end, no failure occurred even at 3000 psig.
  • EXAMPLE 4
  • The same type of tube samples as were used in Example 3, Sample 16, were subjected to a fatigue test in accordance with UL1995, described above in Example 1, using hydraulic oil as the test fluid. The set of samples passed two full rounds of testing without any failures. The results are shown in Table 1 as Sample 17 (Example TR-2007 041).
  • An important advantage of the embodiments disclosed herein is that the twisted tubes can be used in conjunction with refrigerants that replace HCFCs. Nonlimiting examples of refrigerants that can be used with the embodiments described herein are provided below on Table 2.
  • TABLE 2
    Refrigerants
    Refrigerant
    Substitute (Name Used in Trade Being Retrofit/
    the Federal Register) Name Replaced New
    HFC-134a 22 N
    THR-03 22 N
    ISCEON 59, NU-22, R- Isceon 59, 22 R, N
    417A NU-22
    R-410A, R-410B AZ-20, 22 N
    Suva 9100,
    Puron
    R-407C Suva 9000, 22 R, N
    Klea 66
    R-507, R-507A AZ-50 22 R, N
    NU-22 NU-22 22 R, N
    Ammonia Absorption 22 N
    Evaporative/Desiccant all HCFCs N
    Cooling
    R-404A HP62 22 R, N
    R-125/134a/600a 22 R, N
    (28.1/70.0/1.9)
    RS-44 RS-44 22 R, N
    R-421A Choice 22 R, N
    R421A
    R-422D ISCEON 22 R, N
    MO29
    R-424A RS-44 22 R, N
    R-125/290/134a/600a ICOR AT- 22 R, N
    (55.0/1.0/42.5/1.5) 22
    R-422C ICOR 22 R, N
    XLT1
    R-422B ICOR 22 R, N
    XAC1
    KDD5 KDD5 22 R, N
    RS-45 (ASHRAE RS-45 22 R, N
    proposed designation: R-
    434A)
    R-125/290/134a/600a ICOR AT- 22 R, N
    (55.0/1.0/42.5/1.5) 22
    R-422B XAC1, 22 R, N
    NU-22B
    R-422C XLT1 22, 402A, R, N
    402B, 408A
    Key:
    R = Retrofit Uses,
    N = New Uses
  • It will be appreciated that features disclosed above and other features and functions, or alternatives thereof, may be desirably combined into many other different systems or applications. Furthermore, currently unforeseen or unanticipated alternatives, modifications, variations or improvements therein may be subsequently made by those skilled in the art which are also intended to be encompassed by the following claims.

Claims (21)

1. A heat exchanger tube comprising a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion, the transition portion including a reinforcing sleeve.
2. The heat exchanger tube of claim 1, wherein the reinforcing sleeve is positioned over the transition portion.
3. The heat exchanger tube of claim 2, wherein the first portion comprises straight tube material.
4. The heat exchanger tube of claim 1, wherein the first portion, twisted portion and transition portion comprise titanium.
5. The heat exchanger of claim 4, wherein the reinforcing sleeve comprises titanium.
6. A heat exchanger comprising an outer tube and an inner tube defining an annular opening therebetween, the inner tube including a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion including a reinforcing sleeve formed thereon, the inner tube being configured to withstand a hydrostatic test pressure of at least 2600 psig for at least 2 minutes without mechanical failure.
7. The heat exchanger of claim 6, wherein the heat exchanger is configured to receive a first fluid in the inner tube and second fluid in the annular portion, and the reinforcing sleeve enables to heat exchanger to operate with a pressure difference of at least 300 psi between the first and second fluids.
8. The heat exchanger of claim 6, wherein the inner tube is configured to withstand a hydrostatic test pressure of at least 3000 psig for at least 2 minutes without mechanical failure.
9. The heat exchanger of claim 6, wherein the outer tube is coiled.
10. The heat exchanger of claim 6, wherein the heat exchanger contains a refrigerant fluid in the inner tube and a second fluid in the annular space between the inner tube and outer tube.
11. The heat exchanger of claim 10, wherein the refrigerant is at least one of R410A, R-410b, R-417a, R-134a and R-407a.
12. The heat exchanger of claim 10, wherein the second fluid comprises water.
13. The heat exchanger of claim 10, wherein the second fluid comprises chlorinated water.
14. A heat pump comprising the heat exchanger of claim 6.
15. A heat exchanger comprising an outer tube and an inner tube defining an annular opening therebetween, the inner tube including a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion including a reinforcing sleeve formed thereon, the inner tube being configured to pass a fatigue test of 250,000 cycles between 118 psig and 418 psig at a rate of 0.5 cycles/second without mechanical failure.
16. The heat exchanger of claim 15, wherein the heat exchanger is configured to receive a first fluid in the inner tube and second fluid in the annular portion, and the reinforcing sleeve enables to heat exchanger to operate with a pressure difference of at least 300 psi between the first and second fluids.
17. A method of making a heat exchanger tube comprising:
forming a inner tube comprising a first portion, a twisted portion, and a transition portion between the first portion and the twisted portion, and
forming a reinforcing sleeve over the transition portion.
18. The method of claim 17, further comprising disposing the inner tube and reinforcing sleeve in an outer tube to form an annular opening between the inner tube and the outer tube.
19. The method of claim 17 wherein the inner tube and the reinforcing sleeve comprise titanium.
20. The method of claim 17 wherein the first portion, twisted portion and transition portion are formed from a continuous segment of tube material.
21. The method of claim 17 wherein the transition portion includes a section of straight tube material and a section of twisted tube material, and the reinforcing sleeve is configured to protect a portion of the section of twisted tube material from fluid impingement.
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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110132028A1 (en) * 2009-12-05 2011-06-09 GM Global Technology Operations LLC Tubular heat exchanger for motor vehicle air conditioners
US20120192589A1 (en) * 2011-01-28 2012-08-02 Advanced Technical Solutions Gmbh Three-media evaporator for a cooling unit
EP2354743A3 (en) * 2010-01-15 2012-10-31 LG Electronics Inc. Double-pipe heat exchanger
US20120325450A1 (en) * 2010-08-20 2012-12-27 Tim Mimitz Connector for Tube-In-Tube Heat Exchanger and Methods of Making and Using Same
US20130192804A1 (en) * 2012-02-01 2013-08-01 Sumitomo Light Metal Industries, Ltd. Double pipe for heat exchanger
WO2013174652A1 (en) * 2012-05-22 2013-11-28 Robert Bosch Gmbh Device for heating a mixture, in particular a confectionery mixture, and method for producing said device
WO2014168725A1 (en) * 2013-03-15 2014-10-16 Turbotec Products, Inc. Heat exchanger containing multiple tubes, and method of making and using same
US20150359976A1 (en) * 2013-01-31 2015-12-17 Smiths Medical International Limited Medical infusion fluid heat exchange apparatus and warming systems
WO2016144912A3 (en) * 2015-03-06 2016-11-17 Energy Recovery Technology, Inc. Energy recovery in air conditioning and other energy producing systems
US20160348988A1 (en) * 2015-05-28 2016-12-01 Dometic Sweden Ab Corrosion Resistant Coaxial Heat Exchanger Assembly
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US20220290925A1 (en) * 2019-10-23 2022-09-15 Uacj Corporation Heat-transferring double pipe, inner pipe for heat-transferring double pipe, and manufacturing method thereof
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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105403093B (en) * 2015-12-10 2018-04-24 攀枝花市九鼎智远知识产权运营有限公司 High corrosion-proof titanium alloy heat exchanger

Citations (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US516206A (en) * 1894-03-13 Carl kellgren
US1804624A (en) * 1928-07-31 1931-05-12 Frigidaire Corp Refrigerating apparatus
US1861091A (en) * 1928-01-30 1932-05-31 Frigidaire Corp Of Dayton Refrigerating apparatus
US2422517A (en) * 1944-12-21 1947-06-17 Erwin G Baker Gas engine fuel induction means
US2774384A (en) * 1953-09-15 1956-12-18 Griscom Russell Co Heat exchanger u-tubes
US3468371A (en) * 1966-11-11 1969-09-23 Diedrich Menze Heat exchangers
US3566615A (en) * 1969-04-03 1971-03-02 Whirlpool Co Heat exchanger with rolled-in capillary for refrigeration apparatus
US3898428A (en) * 1974-03-07 1975-08-05 Universal Oil Prod Co Electric in line water heating apparatus
US3934617A (en) * 1974-08-26 1976-01-27 Controls Southeast, Inc. Corrugated jacketed pipe assembly having vented enclosures for connecting welds
US4222160A (en) * 1978-04-27 1980-09-16 Industrial Blast Coil Corporation Method of making heat exchange tubing assembly
US4307578A (en) * 1980-04-16 1981-12-29 Atlantic Richfield Company Heat exchanger efficiently operable alternatively as evaporator or condenser
DE3443085A1 (en) * 1983-12-07 1985-06-13 Kühner GmbH & Cie, 7155 Oppenweiler Double-tube heat exchanger
US4599773A (en) * 1979-10-11 1986-07-15 Thermodynetics Inc. Method of forming a multiple coil heat exchanger
US4798241A (en) * 1983-04-04 1989-01-17 Modine Manufacturing Mixed helix turbulator for heat exchangers
US4878537A (en) * 1986-05-27 1989-11-07 Level 1 Technologies Heat exchanger for physiological fluids
US4921041A (en) * 1987-06-23 1990-05-01 Actronics Kabushiki Kaisha Structure of a heat pipe
US5004046A (en) * 1990-06-11 1991-04-02 Thermodynetics, Inc. Heat exchange method and apparatus
US5004047A (en) * 1989-06-14 1991-04-02 Carrier Corporation Header for a tube-in-tube heat exchanger
US5307867A (en) * 1992-08-10 1994-05-03 Noritake Co., Limited Heat exchanger
US5409057A (en) * 1993-01-22 1995-04-25 Packless Metal Hose, Inc. Heat exchange element
US5487423A (en) * 1993-02-16 1996-01-30 Piscine Service Anjou Sa Heat exchanger
US5497824A (en) * 1990-01-18 1996-03-12 Rouf; Mohammad A. Method of improved heat transfer
US5533362A (en) * 1990-02-09 1996-07-09 Columbia Gas Of Ohio, Inc. Heat transfer apparatus for heat pumps
US5617916A (en) * 1993-07-21 1997-04-08 Babcock-Hitachi Kabushiki Kaisha Fin tube heat exchanger
JPH09126593A (en) * 1995-10-31 1997-05-16 Miura Co Ltd Antifreezing structure of heat exchanger for supercooling water
US5902038A (en) * 1997-10-09 1999-05-11 Curry; Ernest L. Lighted bicycle pedal
US5933953A (en) * 1997-03-17 1999-08-10 Carrier Corporation Method of manufacturing a heat transfer tube
US5992512A (en) * 1996-03-21 1999-11-30 The Furukawa Electric Co., Ltd. Heat exchanger tube and method for manufacturing the same
US6012514A (en) * 1997-11-26 2000-01-11 Swain; Robert L. B. Tube-in tube heat exchanger
US6206091B1 (en) * 1997-05-06 2001-03-27 United States Filter Corporation Process and apparatus for treating waste
US6293335B1 (en) * 1999-06-24 2001-09-25 Aquacal, Inc. Method and apparatus for optimizing heat transfer in a tube and shell heat exchanger
US20020157815A1 (en) * 2001-04-27 2002-10-31 Sutter Douglas E. Heat exchange tubing
US6530422B2 (en) * 1998-09-16 2003-03-11 China Petro-Chemical Corporation Heat exchanger tube, a method for making the same, and a cracking furnace or other tubular heat furnaces using the heat exchanger tube
US6664432B2 (en) * 2002-05-14 2003-12-16 Exxonmobil Research And Engineering Company Heat transfer in the acid catalyzed—effluent refrigerated alkylation process
JP2004239318A (en) * 2003-02-04 2004-08-26 Denso Corp Doubled pipe construction
US7062913B2 (en) * 1999-12-17 2006-06-20 The Ohio State University Heat engine
US20070187067A1 (en) * 2006-02-15 2007-08-16 Hitachi Cable, Ltd. Heat transfer tube and heat exchanger using same
US7290597B2 (en) * 2003-12-26 2007-11-06 Valeo Thermal Systems Japan Corporation Heat exchanger

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4118944A (en) * 1977-06-29 1978-10-10 Carrier Corporation High performance heat exchanger
US4305460A (en) * 1979-02-27 1981-12-15 General Atomic Company Heat transfer tube
US20030209345A1 (en) * 2002-05-07 2003-11-13 Zweig Mark Alan Tube-in-tube repairable heat exchanger with cross flow

Patent Citations (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US516206A (en) * 1894-03-13 Carl kellgren
US1861091A (en) * 1928-01-30 1932-05-31 Frigidaire Corp Of Dayton Refrigerating apparatus
US1804624A (en) * 1928-07-31 1931-05-12 Frigidaire Corp Refrigerating apparatus
US2422517A (en) * 1944-12-21 1947-06-17 Erwin G Baker Gas engine fuel induction means
US2774384A (en) * 1953-09-15 1956-12-18 Griscom Russell Co Heat exchanger u-tubes
US3468371A (en) * 1966-11-11 1969-09-23 Diedrich Menze Heat exchangers
US3566615A (en) * 1969-04-03 1971-03-02 Whirlpool Co Heat exchanger with rolled-in capillary for refrigeration apparatus
US3898428A (en) * 1974-03-07 1975-08-05 Universal Oil Prod Co Electric in line water heating apparatus
US3934617A (en) * 1974-08-26 1976-01-27 Controls Southeast, Inc. Corrugated jacketed pipe assembly having vented enclosures for connecting welds
US4222160A (en) * 1978-04-27 1980-09-16 Industrial Blast Coil Corporation Method of making heat exchange tubing assembly
US4599773A (en) * 1979-10-11 1986-07-15 Thermodynetics Inc. Method of forming a multiple coil heat exchanger
US4307578A (en) * 1980-04-16 1981-12-29 Atlantic Richfield Company Heat exchanger efficiently operable alternatively as evaporator or condenser
US4798241A (en) * 1983-04-04 1989-01-17 Modine Manufacturing Mixed helix turbulator for heat exchangers
DE3443085A1 (en) * 1983-12-07 1985-06-13 Kühner GmbH & Cie, 7155 Oppenweiler Double-tube heat exchanger
US4878537A (en) * 1986-05-27 1989-11-07 Level 1 Technologies Heat exchanger for physiological fluids
US4921041A (en) * 1987-06-23 1990-05-01 Actronics Kabushiki Kaisha Structure of a heat pipe
US5004047A (en) * 1989-06-14 1991-04-02 Carrier Corporation Header for a tube-in-tube heat exchanger
US5497824A (en) * 1990-01-18 1996-03-12 Rouf; Mohammad A. Method of improved heat transfer
US5533362A (en) * 1990-02-09 1996-07-09 Columbia Gas Of Ohio, Inc. Heat transfer apparatus for heat pumps
US5004046A (en) * 1990-06-11 1991-04-02 Thermodynetics, Inc. Heat exchange method and apparatus
US5307867A (en) * 1992-08-10 1994-05-03 Noritake Co., Limited Heat exchanger
US5409057A (en) * 1993-01-22 1995-04-25 Packless Metal Hose, Inc. Heat exchange element
US5487423A (en) * 1993-02-16 1996-01-30 Piscine Service Anjou Sa Heat exchanger
US5617916A (en) * 1993-07-21 1997-04-08 Babcock-Hitachi Kabushiki Kaisha Fin tube heat exchanger
JPH09126593A (en) * 1995-10-31 1997-05-16 Miura Co Ltd Antifreezing structure of heat exchanger for supercooling water
US5992512A (en) * 1996-03-21 1999-11-30 The Furukawa Electric Co., Ltd. Heat exchanger tube and method for manufacturing the same
US5933953A (en) * 1997-03-17 1999-08-10 Carrier Corporation Method of manufacturing a heat transfer tube
US6206091B1 (en) * 1997-05-06 2001-03-27 United States Filter Corporation Process and apparatus for treating waste
US5902038A (en) * 1997-10-09 1999-05-11 Curry; Ernest L. Lighted bicycle pedal
US6012514A (en) * 1997-11-26 2000-01-11 Swain; Robert L. B. Tube-in tube heat exchanger
US6530422B2 (en) * 1998-09-16 2003-03-11 China Petro-Chemical Corporation Heat exchanger tube, a method for making the same, and a cracking furnace or other tubular heat furnaces using the heat exchanger tube
US6293335B1 (en) * 1999-06-24 2001-09-25 Aquacal, Inc. Method and apparatus for optimizing heat transfer in a tube and shell heat exchanger
US7062913B2 (en) * 1999-12-17 2006-06-20 The Ohio State University Heat engine
US20020157815A1 (en) * 2001-04-27 2002-10-31 Sutter Douglas E. Heat exchange tubing
US6664432B2 (en) * 2002-05-14 2003-12-16 Exxonmobil Research And Engineering Company Heat transfer in the acid catalyzed—effluent refrigerated alkylation process
JP2004239318A (en) * 2003-02-04 2004-08-26 Denso Corp Doubled pipe construction
US7290597B2 (en) * 2003-12-26 2007-11-06 Valeo Thermal Systems Japan Corporation Heat exchanger
US20070187067A1 (en) * 2006-02-15 2007-08-16 Hitachi Cable, Ltd. Heat transfer tube and heat exchanger using same

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110132028A1 (en) * 2009-12-05 2011-06-09 GM Global Technology Operations LLC Tubular heat exchanger for motor vehicle air conditioners
EP2354743A3 (en) * 2010-01-15 2012-10-31 LG Electronics Inc. Double-pipe heat exchanger
US20120325450A1 (en) * 2010-08-20 2012-12-27 Tim Mimitz Connector for Tube-In-Tube Heat Exchanger and Methods of Making and Using Same
US20120192589A1 (en) * 2011-01-28 2012-08-02 Advanced Technical Solutions Gmbh Three-media evaporator for a cooling unit
US20130192804A1 (en) * 2012-02-01 2013-08-01 Sumitomo Light Metal Industries, Ltd. Double pipe for heat exchanger
WO2013174652A1 (en) * 2012-05-22 2013-11-28 Robert Bosch Gmbh Device for heating a mixture, in particular a confectionery mixture, and method for producing said device
US10363381B2 (en) * 2013-01-31 2019-07-30 Smiths Medical International Limited Medical infusion fluid heat exchange apparatus and warming systems
US20150359976A1 (en) * 2013-01-31 2015-12-17 Smiths Medical International Limited Medical infusion fluid heat exchange apparatus and warming systems
WO2014168725A1 (en) * 2013-03-15 2014-10-16 Turbotec Products, Inc. Heat exchanger containing multiple tubes, and method of making and using same
WO2016144912A3 (en) * 2015-03-06 2016-11-17 Energy Recovery Technology, Inc. Energy recovery in air conditioning and other energy producing systems
US20160348988A1 (en) * 2015-05-28 2016-12-01 Dometic Sweden Ab Corrosion Resistant Coaxial Heat Exchanger Assembly
WO2016189520A3 (en) * 2015-05-28 2017-03-02 Dometic Sweden Ab Corrosion resistant coaxial heat exchanger assembly
US10508867B2 (en) * 2015-05-28 2019-12-17 Dometic Sweden Ab Corrosion resistant coaxial heat exchanger assembly
EP4321828A3 (en) * 2015-05-28 2024-04-17 Dometic Sweden AB Corrosion resistant coaxial heat exchanger assembly
CN107270744A (en) * 2017-05-24 2017-10-20 浙江建春换热器有限公司 Efficient coaxial sleeve heat exchanger
US20220290925A1 (en) * 2019-10-23 2022-09-15 Uacj Corporation Heat-transferring double pipe, inner pipe for heat-transferring double pipe, and manufacturing method thereof
US20230003456A1 (en) * 2019-12-13 2023-01-05 Uacj Corporation Double pipe for heat exchanger
US12111117B2 (en) * 2019-12-13 2024-10-08 Uacj Corporation Double pipe for heat exchanger

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CA2710292A1 (en) 2009-07-02

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