EP2451604B1 - Copper alloy for heat exchanger tube - Google Patents

Copper alloy for heat exchanger tube Download PDF

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Publication number
EP2451604B1
EP2451604B1 EP10797826.4A EP10797826A EP2451604B1 EP 2451604 B1 EP2451604 B1 EP 2451604B1 EP 10797826 A EP10797826 A EP 10797826A EP 2451604 B1 EP2451604 B1 EP 2451604B1
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EP
European Patent Office
Prior art keywords
alloy
tube
copper
weight
inch
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EP10797826.4A
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German (de)
French (fr)
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EP2451604A4 (en
EP2451604A1 (en
Inventor
Parker M. Finney
Larz Ignberg
Anders Kamf
Tim Goebel
Eric Gong
Ed Rottman
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Virtus Precision Tube LLC
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Luvata Franklin Inc
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    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C9/00—Alloys based on copper
    • C22C9/02—Alloys based on copper with tin as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C9/00—Alloys based on copper
    • C22C9/06—Alloys based on copper with nickel or cobalt as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/08—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of copper or alloys based thereon
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F21/00—Constructions of heat-exchange apparatus characterised by the selection of particular materials
    • F28F21/08—Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
    • F28F21/081—Heat exchange elements made from metals or metal alloys
    • F28F21/085—Heat exchange elements made from metals or metal alloys from copper or copper alloys

Definitions

  • the present invention pertains generally to copper alloys and use of the copper alloys in tubes for heat exchangers. Specifically, the invention pertains to a high strength copper alloy tube that has desirable pressure fracture strength and processability properties.
  • the alloy is suitable to reduce thickness, and therefore, conserves material, for existing air conditioning and refrigeration (ACR) heat exchangers, and is suitable for use in a heat exchanger using a cooling medium such as CO 2 .
  • Heat exchangers for air conditioners may be constructed of a U-shaped copper tube bent like a hairpin and fins made from aluminum or aluminum alloy plate.
  • a copper tube used for the above type heat exchanger requires suitable conductivity, formability, and brazing properties.
  • HCFC hydro-chlorofluorocarbon
  • HCFC hydro-chlorofluorocarbon
  • Green refrigerants for example, CO 2 , which is a natural cooling medium, have been used for heat exchangers.
  • the condensing pressure during operation needs to be increased to use CO 2 as a cooling media to maintain the same heat transfer performance as HCFC-based fluorocarbons.
  • pressures at which these cooling media are used pressure of a fluid that flows in the heat exchanger tube
  • R22 gas cooler in CO 2
  • R22 a HCFC-based fluorocarbon
  • the CO 2 cooling medium needs to have a condensing pressure of about 7 to 10 MPa (supercritical state). Therefore, the operating pressures of the new cooling media are increased as compared with the operating pressure of the conventional cooling medium R22.
  • JP52145327 , JP1316431 , JP52145328 , JP4006234 , and JP6094390 disclose various copper alloys comprising nickel and/or tin in wide ranges, wherein the alloys are suitable for use in e.g. tubes used in heat exchangers.
  • the present invention provides a copper alloy, for use in heat exchanger tubes, having, for example, high tensile strength, excellent processability and good thermal conductivity.
  • the invention is defined in the claims.
  • the present invention provides tubes for ACR applications as defined in the claims comprising a copper alloy composition consisting of Cu, Ni, Sn, P and naturally occurring impurities.
  • the present invention provides a high strength alloy which can, for example, reduce the wall thickness and therefore reduce the cost associated with existing ACR tubing and/or provide ACR tubing capable of withstanding the increased pressures associated with cooling media such as CO 2 .
  • high strength it is meant that the alloy and/or tube made from the alloy has at least the levels of tensile strength and/or burst pressure and/or cycle fatigue failure set out herein.
  • the copper alloy can provide savings in material, costs, environmental impact and energy consumption.
  • the selected alloy should have appropriate material properties and perform well with regard to processability.
  • Important material properties include properties such as, for example, burst pressure/strength, ductility, conductivity, and cycle fatigue. The characteristics of the alloy and/or tube described herein are desirable so they can withstand ACR operating environments.
  • High tensile strength and high burst pressure are desirable tube properties because they define what operating pressure a tube can withstand before failing. For example, the higher the burst pressure, the more robust the tube design or for a given burst pressure minimum the present alloy allows for a thinner wall tube.
  • the alloy and/or tube comprising the alloy has, for example, a material tensile strength of a minimum of 262 MPa (38 ksi, kilo-pound per square inch).
  • the material tensile strength can be measured by methods known in the art such as, for example, the ASTM E-8 testing protocol.
  • the alloy and/or tube comprising the alloy has a material tensile strength of 269, 276, 283 or 290 MPa (39, 40, 41 or 42 ksi).
  • Ductility of the alloy and/or a tube made from the alloy is a desirable property because, in one embodiment, tubes need to be bent 180 degrees into hairpins without fracturing or wrinkling for use in the coil.
  • Elongation is an indicator of material ductility.
  • the alloy and/or tube comprising the alloy has, for example, an elongation of a minimum of 40 %. The elongation can be measured by methods known in the art such as, for example, the ASTM E-8 testing protocol.
  • the alloy and/or tube comprising the alloy has a minimum elongation of 41, 42, 43, 44, 45, 46, 47, 48, 49 or 50%.
  • Conductivity is a desirable property because it relates to heat transfer capability and therefore, it is a component of the efficiency of an ACR coil. Also, conductivity can be important for tube formation.
  • the alloy and/or tube comprising the alloy has, for example, a conductivity of a minimum of 35% IACS. The conductivity can be measured by methods known in the art such as, for example, the ASTM E-1004 testing protocol. In various embodiments, the alloy and/or tube comprising the alloy has a minimum conductivity of 36, 37, 38, 39, 40, 45, 50, 55, 60 or 65% (IACS).
  • the alloy and/or tube has, for example, at least equal resistance to cycle fatigue failure as the current alloy in use, e.g., C122 as shown in Table 2. Further, it is desirable that the alloy and/or tube has, for example, at least equivalent resistance against one or more types of corrosion (e.g., galvanic corrosion and formicary corrosion) as the current alloy in use, e.g., C122.
  • corrosion e.g., galvanic corrosion and formicary corrosion
  • a tube comprising an alloy of the present invention has improved softening resistance (which can be important for brazing) and/or increased fatigue strength relative to a standard copper tube, e.g., a tube made from C122.
  • a tube depicted in Figures 3(a) - (c) with reduced wall thickness t (relative to a tube comprising a conventional alloy, e.g., C122) comprising the present alloy has equal or improved burst pressure and/or cycle fatigue relative to tube comprising a conventional alloy, e.g., C122.
  • the tube wall thickness of a tube of the present invention is minimized relative to a standard tube, e.g. a C122 tube, which reduces total material cost, and both tubes exhibit the same burst pressure.
  • the tube wall thickness is at least 10, 15 or 20% less than a C122 tube, where both tubes have the same burst pressure.
  • the burst pressure can be measured by methods known in the art such as, for example, CSA-C22.2 No. 140.3 Clause 6.1 Strength Test - UL 207 Clause 13.
  • the cycle fatigue can be measured by methods known in the art such as, for example, CSA-C22.2 No. 140.3 Clause 6.4 Fatigue Test - UL 207 Clause 14.
  • the alloy of the present invention can be fabricated according to methods known in the art. During the alloy fabrication process and/or tube formation process, it can be important to control the temperature. Control of temperature can be important in keeping the elements in solution (preventing precipitation) and controlling grain size. For example, conductivity can increase and formability can suffer if processed incorrectly.
  • heat treatment in the production process will occur over a short time such that the temperature of the alloy and/or tube will be between 400-600 °C with a rapid (e.g., 10 to 500 °C/second) upward and downward ramping of the temperature.
  • the tube made from the alloy has a desired grain size, being from 1 micron to 50 microns, including all integers between 1 micron and 50 microns. In another embodiment, the grain size is from 10 microns to 25 microns. In yet another embodiment, the grain size is from 10 microns to 15 microns. The grain size can be measured by methods known in the art such as, for example, the ASTM E-112 testing protocol.
  • the alloy compositions of the present invention include the following where relative amounts of the components in the alloy are given as percentages by weight.
  • the ranges of percentage by weight include all fractions of a percent (including, but not limited to, tenths and hundredths of a percent) within the stated ranges.
  • the composition consists of copper, nickel, tin, phosphorus, and impurities.
  • the nickel is present in the range of 0.3% to 0.7%; tin in the range of 0.3% to 0.7%; phosphorus in the range of 0.01% to 0,07%; and its remainder is copper and impurities.
  • the composition of the alloy is CuNi(0.5)Sn(0.5)P(0.020).
  • the impurities can be, for example, naturally-occurring or occur as a result of processing.
  • impurities include, for example, zinc, iron and lead.
  • the impurities can be a maximum of 0.6 %. In various other embodiments, the impurities can be a maximum of 0.5, 0.45, 0.3, 0.2 or 0.1%.
  • Phosphorus is present in the range of 0.01% to 0.07%, and more specifically in the range of 0.015% to 0.030%, or at 0.02%. Without intending to be bound by any particular theory, it is considered that inclusion of an appropriate amount of phosphorus in the alloy increases the weldability of the alloy by effecting the flow characteristics and oxygen content of the metal, while addition of too much phosphorus leads to poor grain structure and unwanted precipitates.
  • composition of the alloy consists of Cu, Ni, Sn, P and impurities in the aforementioned ranges.
  • the alloy of the present invention may be produced for use by various processes such as cast and roll, extrusion or roll and weld.
  • the processing requirement includes, for example, brazeability. Brazing occurs when the tubes are connected as described below.
  • the alloy in the roll and weld process the alloy is cast into bars, roll reduced to thin gauge, heat treated, slit to size, embossed, formed into tube, welded, annealed, and packaged.
  • the alloy in the cast and roll process the alloy is cast into "mother" tube, drawn to size, annealed, machined to produce inner grooves, sized, annealed, and packaged.
  • the alloy in the extrusion process, the alloy is cast into a solid billet, reheated, extrusion pressed, drawn and grooved to final dimensions, annealed and packaged.
  • the present invention provides tubes as defined in the claims which are from 2.5 mm (0.100 inch) to 25 mm (1 inch) in outer diameter, including all fractions of an inch between 2.5 mm (0.100 inch) and 25 mm (1 inch), and have a wall thickness of from 0.10 mm (0.0004 inch) to 1.0 mm (0.040 inch) including all fractions of an inch between 0.10 mm (0.0004 inch) to 1.0 mm (0.040 inch).
  • tubes as defined in the claims which are from 2.5 mm (0.100 inch) to 25 mm (1 inch) in outer diameter, including all fractions of an inch between 2.5 mm (0.100 inch) and 25 mm (1 inch), and have a wall thickness of from 0.10 mm (0.0004 inch) to 1.0 mm (0.040 inch) including all fractions of an inch between 0.10 mm (0.0004 inch) to 1.0 mm (0.040 inch).
  • the tubes are used in ACR applications. It is desirable that the tubes have sufficient conductivity (e.g., so that the tubes can be joined by welding) and formability (e.g., ability to be shaped, e.g., bent, after formation of the tube). Also, it is desirable that the tubes have properties such that the tube can have internal groove enhancement.
  • One example of a process suited for the alloy of the present invention is a heat exchanger coil having tubes formed with a roll and weld process.
  • the copper alloy of the present invention is cast into slabs followed by hot and cold rolling into flat strips.
  • the cold rolled strips are soft annealed.
  • the soft annealed copper alloy strips are then formed into heat exchanger tubes by means of a continuous roll forming and weld process.
  • the tubes may be provided with internal enhancements such as grooves or ribs on the inside wall of the tube as will be evident to those of ordinary skill in the art.
  • the tubes are formed in a continuous roll and weld process and the output may be wound into a large coil. The large coil may then be moved to another area where the coil is cut into smaller sections and formed into the U or hairpin shape.
  • the hairpin is threaded into through-holes of aluminum fins and a jig is inserted into the U-shaped copper tube to expand the tube, thereby closely attaching the copper tube and the aluminum fin to each other. Then the open end of the U-shaped copper tube is expanded and a shorter hairpin similarly bent into a U-shape is inserted into the expanded end. The bent copper tube is brazed to the expanded open end using a brazing alloy thereby being connected to an adjacent hairpin to make a heat exchanger.
  • Material of a composition of Alloy B of 0.5 % Ni 0.5 % Sn and 0.020% P, denoted as CuNi(0.5)Sn(0.5) was produced in full production scale and formed to tubes using the roll and weld method.
  • the tubes were produced both in standard wall thickness (e.g., 0.300 mm (0.0118 inches)) and with 13 % lower wall thickness.
  • Mechanical properties of the tubes were tested using ASTM and UL (e.g., UL testing protocols and compared with tubes made of "present use" copper alloy C12200 with standard wall thickness. The results are shown in Table 2.
  • the alloy of the invention CuNi(0.5)Sn(0.5) has higher strength and higher burst pressure in standard wall thickness.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
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  • Metallurgy (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Conductive Materials (AREA)
  • Rigid Pipes And Flexible Pipes (AREA)

Description

    FIELD OF THE INVENTION
  • The present invention pertains generally to copper alloys and use of the copper alloys in tubes for heat exchangers. Specifically, the invention pertains to a high strength copper alloy tube that has desirable pressure fracture strength and processability properties. The alloy is suitable to reduce thickness, and therefore, conserves material, for existing air conditioning and refrigeration (ACR) heat exchangers, and is suitable for use in a heat exchanger using a cooling medium such as CO2.
  • BACKGROUND OF THE INVENTION
  • Heat exchangers for air conditioners may be constructed of a U-shaped copper tube bent like a hairpin and fins made from aluminum or aluminum alloy plate.
  • Accordingly, a copper tube used for the above type heat exchanger requires suitable conductivity, formability, and brazing properties.
  • HCFC (hydro-chlorofluorocarbon)-based fluorocarbons have been widely used for cooling media used for heat exchangers such as air conditioners. However, HCFC has a large ozone depleting potential such that other cooling media have been selected for environmental reasons. "Green refrigerants", for example, CO2, which is a natural cooling medium, have been used for heat exchangers.
  • The condensing pressure during operation needs to be increased to use CO2 as a cooling media to maintain the same heat transfer performance as HCFC-based fluorocarbons. Usually in a heat exchanger, pressures at which these cooling media are used (pressure of a fluid that flows in the heat exchanger tube) become maximized in a condenser (gas cooler in CO2). In this condenser or gas cooler, for example, R22 (a HCFC-based fluorocarbon) has a condensing pressure of about 1.8 MPa. On the other hand, the CO2 cooling medium needs to have a condensing pressure of about 7 to 10 MPa (supercritical state). Therefore, the operating pressures of the new cooling media are increased as compared with the operating pressure of the conventional cooling medium R22.
  • Due to the increased pressure and to some loss of strength due to brazing in some tube forming processes, conventional copper materials have to be made thicker thereby increasing the weight of the tube and therefore the material costs associated with the tube.
  • JP52145327 , JP1316431 , JP52145328 , JP4006234 , and JP6094390 disclose various copper alloys comprising nickel and/or tin in wide ranges, wherein the alloys are suitable for use in e.g. tubes used in heat exchangers.
  • What is needed is a heat exchanger tube that has high tensile strength, excellent processability and good thermal conductivity that is suitable for reducing the wall thickness, and therefore, the material costs, for ACR heat exchangers and that is suitable for withstanding high pressure applications with new "green" cooling media such as CO2.
  • BRIEF SUMMARY OF THE INVENTION
  • The present invention provides a copper alloy, for use in heat exchanger tubes, having, for example, high tensile strength, excellent processability and good thermal conductivity. The invention is defined in the claims.
  • The present invention provides tubes for ACR applications as defined in the claims comprising a copper alloy composition consisting of Cu, Ni, Sn, P and naturally occurring impurities.
  • BRIEF DESCRIPTION OF THE DRAWINGS
    • Figure 1. Graphical representation of relative metal value per meter (feet) vs. copper price for a presently used alloy, C122, at standard wall thickness compared with an alloy of the present invention CuNi(0.5)Sn(0.5) at reduced wall thickness.
    • Figure 2. Graphical representation of tensile strength and conductivity for tested alloys as a function of Ni and Sn contents. Sn has a greater influence on both strength and conductivity.
    • Figures 3(a) - (c). Graphical representation of various views of a tube according to an embodiment of the present invention. Figure (a) is a perspective view; Figure (b) is a cross-section of the tube of (a) as viewed along a longitudinal axis; and Figure (c) is a cross-section of the tube of (a) and (b) as viewed along an axis normal to the longitudinal axis.
    DETAILED DESCRIPTION OF THE INVENTION
  • The present invention provides a high strength alloy which can, for example, reduce the wall thickness and therefore reduce the cost associated with existing ACR tubing and/or provide ACR tubing capable of withstanding the increased pressures associated with cooling media such as CO2. By, high strength it is meant that the alloy and/or tube made from the alloy has at least the levels of tensile strength and/or burst pressure and/or cycle fatigue failure set out herein. The copper alloy can provide savings in material, costs, environmental impact and energy consumption.
  • In order to provide a copper alloy for a heat exchanger tube, which can, for example, be used with cooling media such as CO2, the selected alloy should have appropriate material properties and perform well with regard to processability. Important material properties include properties such as, for example, burst pressure/strength, ductility, conductivity, and cycle fatigue. The characteristics of the alloy and/or tube described herein are desirable so they can withstand ACR operating environments.
  • High tensile strength and high burst pressure are desirable tube properties because they define what operating pressure a tube can withstand before failing. For example, the higher the burst pressure, the more robust the tube design or for a given burst pressure minimum the present alloy allows for a thinner wall tube. A correlation exists between tensile strength and burst pressure. The alloy and/or tube comprising the alloy has, for example, a material tensile strength of a minimum of 262 MPa (38 ksi, kilo-pound per square inch). The material tensile strength can be measured by methods known in the art such as, for example, the ASTM E-8 testing protocol. In various embodiments, the alloy and/or tube comprising the alloy has a material tensile strength of 269, 276, 283 or 290 MPa (39, 40, 41 or 42 ksi).
  • Ductility of the alloy and/or a tube made from the alloy is a desirable property because, in one embodiment, tubes need to be bent 180 degrees into hairpins without fracturing or wrinkling for use in the coil. Elongation is an indicator of material ductility. The alloy and/or tube comprising the alloy has, for example, an elongation of a minimum of 40 %. The elongation can be measured by methods known in the art such as, for example, the ASTM E-8 testing protocol. In various embodiments, the alloy and/or tube comprising the alloy has a minimum elongation of 41, 42, 43, 44, 45, 46, 47, 48, 49 or 50%.
  • Conductivity is a desirable property because it relates to heat transfer capability and therefore, it is a component of the efficiency of an ACR coil. Also, conductivity can be important for tube formation. The alloy and/or tube comprising the alloy has, for example, a conductivity of a minimum of 35% IACS. The conductivity can be measured by methods known in the art such as, for example, the ASTM E-1004 testing protocol. In various embodiments, the alloy and/or tube comprising the alloy has a minimum conductivity of 36, 37, 38, 39, 40, 45, 50, 55, 60 or 65% (IACS).
  • The alloy and/or tube has, for example, at least equal resistance to cycle fatigue failure as the current alloy in use, e.g., C122 as shown in Table 2. Further, it is desirable that the alloy and/or tube has, for example, at least equivalent resistance against one or more types of corrosion (e.g., galvanic corrosion and formicary corrosion) as the current alloy in use, e.g., C122.
  • In one embodiment, a tube comprising an alloy of the present invention has improved softening resistance (which can be important for brazing) and/or increased fatigue strength relative to a standard copper tube, e.g., a tube made from C122.
  • In one embodiment, a tube depicted in Figures 3(a) - (c) with reduced wall thickness t (relative to a tube comprising a conventional alloy, e.g., C122) comprising the present alloy has equal or improved burst pressure and/or cycle fatigue relative to tube comprising a conventional alloy, e.g., C122. For example, the tube wall thickness of a tube of the present invention is minimized relative to a standard tube, e.g. a C122 tube, which reduces total material cost, and both tubes exhibit the same burst pressure. In various embodiments, the tube wall thickness is at least 10, 15 or 20% less than a C122 tube, where both tubes have the same burst pressure. The burst pressure can be measured by methods known in the art such as, for example, CSA-C22.2 No. 140.3 Clause 6.1 Strength Test - UL 207 Clause 13. The cycle fatigue can be measured by methods known in the art such as, for example, CSA-C22.2 No. 140.3 Clause 6.4 Fatigue Test - UL 207 Clause 14.
  • The alloy of the present invention can be fabricated according to methods known in the art. During the alloy fabrication process and/or tube formation process, it can be important to control the temperature. Control of temperature can be important in keeping the elements in solution (preventing precipitation) and controlling grain size. For example, conductivity can increase and formability can suffer if processed incorrectly.
  • For example, to maintain both the desired grain size and prevent precipitate formation in the alloy fabrication and/or tube formation processes, heat treatment in the production process will occur over a short time such that the temperature of the alloy and/or tube will be between 400-600 °C with a rapid (e.g., 10 to 500 °C/second) upward and downward ramping of the temperature.
  • It The tube made from the alloy has a desired grain size, being from 1 micron to 50 microns, including all integers between 1 micron and 50 microns. In another embodiment, the grain size is from 10 microns to 25 microns. In yet another embodiment, the grain size is from 10 microns to 15 microns. The grain size can be measured by methods known in the art such as, for example, the ASTM E-112 testing protocol.
  • The alloy compositions of the present invention include the following where relative amounts of the components in the alloy are given as percentages by weight. The ranges of percentage by weight include all fractions of a percent (including, but not limited to, tenths and hundredths of a percent) within the stated ranges.
  • The composition consists of copper, nickel, tin, phosphorus, and impurities. The nickel is present in the range of 0.3% to 0.7%; tin in the range of 0.3% to 0.7%; phosphorus in the range of 0.01% to 0,07%; and its remainder is copper and impurities. In one embodiment, the composition of the alloy is CuNi(0.5)Sn(0.5)P(0.020).
  • The impurities can be, for example, naturally-occurring or occur as a result of processing. Examples of impurities include, for example, zinc, iron and lead. The impurities can be a maximum of 0.6 %. In various other embodiments, the impurities can be a maximum of 0.5, 0.45, 0.3, 0.2 or 0.1%.
  • Phosphorus is present in the range of 0.01% to 0.07%, and more specifically in the range of 0.015% to 0.030%, or at 0.02%. Without intending to be bound by any particular theory, it is considered that inclusion of an appropriate amount of phosphorus in the alloy increases the weldability of the alloy by effecting the flow characteristics and oxygen content of the metal, while addition of too much phosphorus leads to poor grain structure and unwanted precipitates.
  • The composition of the alloy consists of Cu, Ni, Sn, P and impurities in the aforementioned ranges.
  • The alloy of the present invention may be produced for use by various processes such as cast and roll, extrusion or roll and weld. The processing requirement includes, for example, brazeability. Brazing occurs when the tubes are connected as described below.
  • Generally, in the roll and weld process the alloy is cast into bars, roll reduced to thin gauge, heat treated, slit to size, embossed, formed into tube, welded, annealed, and packaged. Generally, in the cast and roll process the alloy is cast into "mother" tube, drawn to size, annealed, machined to produce inner grooves, sized, annealed, and packaged. Generally, in the extrusion process, the alloy is cast into a solid billet, reheated, extrusion pressed, drawn and grooved to final dimensions, annealed and packaged.
  • In one aspect the present invention provides tubes as defined in the claims which are from 2.5 mm (0.100 inch) to 25 mm (1 inch) in outer diameter, including all fractions of an inch between 2.5 mm (0.100 inch) and 25 mm (1 inch), and have a wall thickness of from 0.10 mm (0.0004 inch) to 1.0 mm (0.040 inch) including all fractions of an inch between 0.10 mm (0.0004 inch) to 1.0 mm (0.040 inch). One advantage of the present invention is that thinner walled tubes can be used in ACR applications. This leads to reduced materials costs (see Figure 1).
  • The tubes are used in ACR applications. It is desirable that the tubes have sufficient conductivity (e.g., so that the tubes can be joined by welding) and formability (e.g., ability to be shaped, e.g., bent, after formation of the tube). Also, it is desirable that the tubes have properties such that the tube can have internal groove enhancement.
  • One example of a process suited for the alloy of the present invention is a heat exchanger coil having tubes formed with a roll and weld process. In an initial step, the copper alloy of the present invention is cast into slabs followed by hot and cold rolling into flat strips. The cold rolled strips are soft annealed. The soft annealed copper alloy strips are then formed into heat exchanger tubes by means of a continuous roll forming and weld process. Before the roll forming and welding process the tubes may be provided with internal enhancements such as grooves or ribs on the inside wall of the tube as will be evident to those of ordinary skill in the art. The tubes are formed in a continuous roll and weld process and the output may be wound into a large coil. The large coil may then be moved to another area where the coil is cut into smaller sections and formed into the U or hairpin shape.
  • In order to construct a heat exchanger, the hairpin is threaded into through-holes of aluminum fins and a jig is inserted into the U-shaped copper tube to expand the tube, thereby closely attaching the copper tube and the aluminum fin to each other. Then the open end of the U-shaped copper tube is expanded and a shorter hairpin similarly bent into a U-shape is inserted into the expanded end. The bent copper tube is brazed to the expanded open end using a brazing alloy thereby being connected to an adjacent hairpin to make a heat exchanger.
  • The following Example is presented to further describe the present invention and is not intended to be in any way limiting.
  • EXAMPLE
  • Copper alloys with different Ni and Sn contents were produced in pilot scale and mechanical and physical properties tested, see Table 1.
  • The results was plotted versus the amount ofNi or Sn, see Figure 2. All tested alloys meet a desired minimum conductivity of 35 % IACS. The mechanical properties of a minimum tensile strength of 262 MPa (38 ksi) is achieved for all tested alloys. In order to meet desired strength and conductivity the tested composition contained 0.2% to 1.0 % by weight for both Ni and Sn.
  • Material of a composition of Alloy B of 0.5 % Ni 0.5 % Sn and 0.020% P, denoted as CuNi(0.5)Sn(0.5) was produced in full production scale and formed to tubes using the roll and weld method. The tubes were produced both in standard wall thickness (e.g., 0.300 mm (0.0118 inches)) and with 13 % lower wall thickness. Mechanical properties of the tubes were tested using ASTM and UL (e.g., UL testing protocols and compared with tubes made of "present use" copper alloy C12200 with standard wall thickness. The results are shown in Table 2. The alloy of the invention CuNi(0.5)Sn(0.5) has higher strength and higher burst pressure in standard wall thickness. For tubes produced with reduced wall thickness the burst pressure for an alloy of the present invention (CuNi(0.5)Sn(0.5)) is still higher compared with C 122 at standard wall thickness. Table 1. Mechanical properties and conductivity for tested alloys at different Ni and Sn contents.
    Alloy no Ni Sn P TS Parallel E Parallel TS Transverse E Transverse Electrical Conductivity
    (%) (%) (%) (MPa (ksi)) (%) (MPa (ksi)) (%) (% IACS)
    A 0.2 0.2 0.026 272 (39.4) 48.0 262 (38.0) 47.9 65
    B 0.5 0.5 0.020 283 (41.1) 44.2 282 (40.9) 46.7 51
    C 1.0 0.5 0.028 291 (42.2) 44.1 291 (42.2) 46.3 42
    D 0.8 1.2 0.025 321 (46.6) 46.3 317 (46.0) 47.9 35
    E 1.7 1.2 0.020 345 (50.0) 43.0 - - 35
    Table 2. Mechanical properties of tubes made of an alloy of the invention (CuNi0.5Sn0.5) compared with current standard alloy C12200 (Cu-DHP).
    Alloy Wall thickness of tube Grain size Tensile strength Elongation Burst pressure Conductivity Cycle Fatigue
    (mm) (MPa (ksi)) (%) (MPa (psi)) (% IACS)
    CuNi0.5Sn0.5 Standard 0.015 274 (39.7) 46 16.9 (2450) 52 Pass
    CuNi0.5Sn0.5 87 % of standard 0.015 274 (39.7) 50 13.7(1980) 52 Pass
    C12200 Standard 0.020 239 (34.7) 47 13.4 (1950) 83 Pass

Claims (6)

  1. An ACR tube for use in an air conditioning and refrigeration (ACR) heat exchanger, wherein the tube comprises a copper alloy consisting of:
    a) nickel at from 0.3% to 0.7% by weight;
    b) tin at from 0.3% to 0.7% by weight; and
    c) phosphorus at from 0.01% to 0.07% by weight,
    wherein the remainder of the alloy is copper and naturally-occurring impurities are present at a maximum of 0.6 % by weight;
    the alloy has a grain size of from 1 micron to 50 microns; and the tube has a wall thickness of from 0.10 mm (0.004 inch) to 1.0 mm (0.040 inch).
  2. The ACR tube of claim1, wherein the tube comprises a copper alloy consisting of:
    a) nickel at from 0.3% to 0.7% by weight;
    b) tin at from 0.3% to 0.7% by weight; and
    c) phosphorus at from 0.01% to 0.07% by weight,
    wherein the remainder of the alloy is copper;
    the alloy has a grain size of from 1 micron to 50 microns; and the tube has a wall thickness of from 0.10 mm (0.004 inch) to 1.0 mm (0.040 inch).
  3. The ACR tube of claim 1 or 2, wherein the nickel is present at 0.5% by weight, and wherein the tin is present at 0.5% by weight.
  4. The ACR tube of claim 1 or 2, wherein the phosphorus is present in the alloy at 0.020% by weight.
  5. The ACR tube of claim 1 or 2, wherein the alloy has a grain size of 10 microns to 25 microns.
  6. The ACR tube of claim 1 or 2, wherein the tube has an outer diameter of from 2.5 mm (0.100 inch) to 25 mm (1 inch).
EP10797826.4A 2009-07-10 2010-07-08 Copper alloy for heat exchanger tube Not-in-force EP2451604B1 (en)

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US22467109P 2009-07-10 2009-07-10
PCT/US2010/041313 WO2011005926A1 (en) 2009-07-10 2010-07-08 Copper alloy for heat exchanger tube

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EP2451604A4 EP2451604A4 (en) 2013-04-10
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BR112012000607A8 (en) 2018-02-06
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WO2011005926A1 (en) 2011-01-13
US20110005739A1 (en) 2011-01-13
JP2012532990A (en) 2012-12-20
CN102470471A (en) 2012-05-23
MY173128A (en) 2019-12-30
ES2649557T3 (en) 2018-01-12
MX2012000544A (en) 2012-07-20
BR112012000607B1 (en) 2019-03-06
JP2015178679A (en) 2015-10-08
CA2767242A1 (en) 2011-01-13
JP6087982B2 (en) 2017-03-01
MX340861B (en) 2016-07-28
EP2451604A1 (en) 2012-05-16
CA2767242C (en) 2016-09-27
US20160363397A1 (en) 2016-12-15
CN107739880A (en) 2018-02-27

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