Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F28—HEAT EXCHANGE IN GENERAL
  • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
  • F28F1/00—Tubular elements; Assemblies of tubular elements
  • F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
  • F28F1/40—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only inside the tubular element
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
  • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
  • B23P15/26—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass heat exchangers or the like
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F28—HEAT EXCHANGE IN GENERAL
  • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
  • F28F1/00—Tubular elements; Assemblies of tubular elements
  • F28F1/08—Tubular elements crimped or corrugated in longitudinal section
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F28—HEAT EXCHANGE IN GENERAL
  • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
  • F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
  • F28F13/02—Arrangements for modifying heat-transfer, e.g. increasing, decreasing by influencing fluid boundary
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F28—HEAT EXCHANGE IN GENERAL
  • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
  • F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
  • F28F13/06—Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media
  • F28F13/12—Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media by creating turbulence, e.g. by stirring, by increasing the force of circulation
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F28—HEAT EXCHANGE IN GENERAL
  • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
  • F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
  • F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
  • F28D2021/0068—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for refrigerant cycles
• • 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
  • F28F21/084—Heat exchange elements made from metals or metal alloys from aluminium or aluminium alloys
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F28—HEAT EXCHANGE IN GENERAL
  • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
  • F28F2210/00—Heat exchange conduits
  • F28F2210/06—Heat exchange conduits having walls comprising obliquely extending corrugations, e.g. in the form of threads

Definitions

• the present disclosure relates to a heat transfer tube including axial and non-axial grooves therein.
• Copper tubing is generally used for condenser tubing in, for example, an air conditioner, refrigerator, or heat pump. While copper provides excellent heat transfer, copper is an expensive material. Thus, materials such as aluminum are now being used to form condenser tubing.
• the present disclosure provides a heat transfer tube.
• the heat transfer tube includes an inner surface including a plurality of grooves.
• the plurality of grooves includes at least primary grooves and secondary grooves, wherein the primary grooves extend along a length of the tube, and the secondary grooves intersect the primary grooves.
• the heat transfer tube may include secondary grooves that are helically formed.
• the heat transfer tube may also include tertiary grooves that intersect at least the primary grooves.
• the tertiary grooves may intersect the secondary grooves.
• the tertiary grooves may be helically formed.
• the heat transfer tube may include aluminum.
• the present disclosure also provides a method of forming a heat transfer tube.
• the method includes extruding a tube including a plurality of axial primary grooves on an inner surface thereof; and forming a plurality of secondary grooves on the inner surface using a first forming tool, wherein the secondary grooves intersect the primary grooves.
• the ridges between the primary grooves may be deformed to partially or completely block the primary grooves.
• the first forming tool may include a plurality of threads at a first pitch and a first height.
• the first forming tool may include expanding tools or cams that press the secondary grooves into the tube
• the first forming tool may form the secondary grooves in a helical orientation that may be either continuous or discontinuous, forming discrete rings or other paths.
• a plurality of tertiary grooves may also be formed on the inner surface using a second forming tool.
• the tertiary grooves may intersect the primary grooves.
• the tertiary grooves may intersect the secondary grooves.
• the second forming tool may include a plurality of threads at a second pitch and a second height and/or a different shape than the first forming tool.
• the secondary grooves and the tertiary grooves may each be helically formed.
• the method may also include a step of cutting a length of tube from the extruded tube.
• the length of tube may be cut from the extruded tube before forming the secondary grooves.
• the length of tube may be cut from the extruded tube after forming the secondary grooves.
• the method may also include bending the heat transfer tube into a hairpin tube.
• the heat transfer tube may include aluminum.
• the present disclosure also provides heat transfer tube having an inner surface including a plurality of grooves, wherein the plurality of grooves including at least primary grooves and secondary grooves.
• the primary grooves each extend helically in an axial direction along and defined by a length of the tube and are open in a radial direction toward a center of the tube. Adjacent primary grooves are separated by a ridge.
• each of the primary grooves are entirely blocked in the axial direction of the tube without being blocked in the radial direction by a material of the ridge that separates the adjacent primary grooves that is deformed into one of the adjacent primary grooves.
• the secondary grooves may be helically formed.
• the inner surface may also include tertiary grooves that intersect at least the primary grooves.
• the tertiary grooves may also intersect the secondary grooves.
• the tertiary grooves may be helically formed.
• the heat transfer tube may include aluminum.
• each of the deformations of the ridges that separate adjacent primary grooves may be oriented in a same direction.
• a depth of the secondary grooves may be greater than a depth of the primary grooves.
• the present disclosure also provides heat transfer tube having an inner surface including a plurality of grooves, wherein the plurality of grooves including at least primary grooves and secondary grooves.
• the primary grooves each extend helically in an axial direction along and defined by a length of the tube and are open in a radial direction toward a center of the tube. Adjacent primary grooves being separated by a ridge.
• the secondary grooves intersect the primary grooves, and at locations where the secondary grooves intersect the primary grooves, each of the primary grooves are at least partially blocked in the axial direction of the tube without being blocked in the radial direction by a material of the ridge that separates adjacent primary grooves that is deformed into one of the adjacent primary grooves.
• a depth of the secondary grooves may be greater than a depth of the primary grooves.
• Each of the primary grooves may be entirely blocked in the axial direction of the tube without being blocked in the radial direction by the deformation of the ridge that separates the adjacent primary grooves.
• the present disclosure also provides a heat transfer tube having an inner surface including a plurality of grooves, wherein the plurality of grooves including at least primary grooves and secondary grooves.
• the primary grooves each extend helically in an axial direction along a length of the tube and are open in a radial direction toward a center of the tube.
• the secondary grooves intersect the primary grooves.
• each of the primary grooves are at least partially blocked in the axial direction of the tube without being blocked in the radial direction by a deformation of a ridge that separates adjacent primary grooves, and a depth of the secondary grooves is greater than a depth of the primary grooves.
• Each of the primary grooves may be entirely blocked in the axial direction of the tube without being blocked in the radial direction by the deformation of the ridge that separates the adjacent primary grooves.
• each of the deformations of the ridges that separate adjacent primary grooves are oriented in a same direction.
• Figure 1 is a cross-sectional view of an exemplary heat transfer tube according to a principle of the present disclosure
• Figure 2 is a perspective view of a section of an exemplary heat transfer tube according to a principle of the present disclosure
• Figure 3 is a perspective view of a forming tool used to form grooves in a heat transfer tube according to a principle of the present disclosure
• Figure 4 is a perspective view of a section of another exemplary heat transfer tube according to a principle of the present disclosure.
• Figure 5 is a micrograph of a section of an exemplary heat transfer tube according to a principle of the present disclosure, wherein in the process of forming the secondary grooves, the primary grooves are substantially blocked by material deformed from the ridges between primary grooves;
• Figure 6 is a micrograph of a section of an exemplary heat transfer tube according to a principle of the present disclosure, wherein in the process of forming the secondary grooves, the ridges between primary grooves are deformed to protrude into the primary groove without substantially blocking the groove;
• Figure 7 is a graph illustrating heat transfer results from a 7mm tube utilizing refrigerant 410a, wherein the secondary grooves have a different depth in comparison to the primary grooves, where the percent depth pertains to the percent the secondary groove cuts into the ridge between the primary grooves (e.g. at 30%, the secondary groove cuts through the top 30% of the ridge, and at 100%, the secondary groove cuts completely through the ridge with both primary and secondary grooves having the same depth);
• Figure 8 is a graph illustrating heat transfer results from a 7mm tube utilizing refrigerant 410a, wherein a tube including primary grooves is compared to a tube including primary grooves and secondary grooves, and compared to a tube including primary grooves, secondary grooves, and tertiary grooves;
• Figure 9 is a graph illustrating heat transfer results from a 7mm tube utilizing refrigerant 410a, wherein a tube including primary grooves is compared to the tube illustrated in Figure 5, and compared to the tube illustrated in Figure 6;
• Figures 10 and 11 are perspective views of sections of additional exemplary heat transfer tubes according to a principle of the present disclosure.
• Figure 1 illustrates a tube 10 including a plurality of primary grooves 12 separated by ridges 13.
• Tube 10 is generally cylindrically shaped and includes an outer surface 14 that defines an outer diameter OD, and an inner surface 16 defining an inner diameter ID.
• Tube 10 may be formed from materials such as copper, aluminum, stainless steel, or any other material known to one skilled in the art.
• tube 10 is used for carrying a refrigerant in an air conditioner condenser, an evaporator, or heat pump.
• Tube 10 may be extruded to include primary grooves 12.
• Primary grooves 12, as illustrated, are axial grooves 12 that assist in increasing the inner surface area of tube 10. It should be understood, however, that primary grooves 12 can be helically formed without departing from the scope of the present disclosure ( Figures 10 and 11). By increasing the inner surface area of tube 10, a greater amount of heat transfer can occur between the refrigerant carried by tube 10 and tube 10.
• the number and size of grooves 12 can be variable. As illustrated in Figure 1, tube 10 includes fifty-eight primary grooves 12. Tube 10, however, can include a greater or less number of primary grooves 12 without departing from the scope of the present disclosure.
• primary grooves 12 are illustrated as including a rounded bottom 18, it should be understood that primary grooves 12 can be square shaped, oval-shaped, or V-shaped without departing from the scope of the present disclosure.
• Tube 10 has a thickness T in the range of about a third of an inch. Tube 10, however, can have a greater or lesser thickness as desired.
• tube 10 can be further processed to include secondary grooves 20.
• secondary grooves 20 are non-axially formed so as to intersect primary grooves 12.
• the use of secondary grooves 20 along with primary grooves 12 creates a complex inner surface 16 that maximizes heat transfer between the refrigerant carried by tube 10 and tube 10.
• Secondary grooves 20 may be formed orthogonal to primary grooves 12, or secondary grooves 20 can be helically formed to intersect primary grooves 12.
• the secondary grooves 20 may be continuously formed or discontinuously formed down the length of the tube 10.
• FIG. 3 illustrates a forming tool 22 that may be used to form secondary grooves 20.
• Forming tool 22 includes a proximal portion 24 that is driven by a rotating tool (not shown), and forming tool 22 includes a distal portion 26.
• Distal portion 26 of forming tool 22 also includes a threading 28 that, as forming tool 22 is rotated, will form secondary grooves 20 in tube 10.
• a pitch or spacing S between threads 30 can be modified, as desired. Further, a height FI of threads 30 can be adjusted, as desired.
• height FI of threads 30 can be formed greater than, equal to, or less a depth D of primary grooves 12 such that secondary grooves 20 have a different depth (e.g., greater or lesser) in comparison to a depth of primary grooves 12. Differing the depth of secondary grooves 20 can affect heat exchange between the refrigerant and the tube 10. As best shown in Figure 7, when secondary grooves 20 have a depth that is 30% of the depth of the primary grooves 12, heat transfer is increased. Figure 7 also shows that secondary grooves 20 that have a depth this 50% or 100% of the depth of the primary grooves 12 also increases heat exchange between the refrigerant and the tube 10.
• an angle a at which threads 30 are arranged relative to an axis A of forming tool 22 can be adjusted as desired.
• each of the spacing S, height FI, and angle a can be selected and adjusted based on the inner diameter ID of tube 10, and the desired flow rate of the refrigerant in tube 10.
• the secondary grooves 20 may also be formed with a variety of tools that can be placed in the tube to deform the primary grooves, resulting in secondary grooves 20.
• tube 10 may include primary grooves 12, secondary grooves 20, and tertiary grooves 32. Similar to secondary grooves 20, tertiary grooves 32 are non-axially formed so as to intersect primary grooves 12. Tertiary grooves 32 may also intersect secondary grooves 20. The use of tertiary grooves 32 along with primary grooves 12 and secondary grooves 20 creates a complex inner surface 16 that maximizes heat transfer between the refrigerant carried by tube 10 and tube 10. Tertiary grooves 32 may be formed orthogonal to primary grooves 12, or tertiary grooves 32 can be helically formed to intersect primary grooves 12.
• tertiary grooves 32 may be formed with a forming tool 22 similar to that used to form secondary grooves 20, with the spacing S, height FI, and angle a being differed.
• the tertiary grooves 32 may have a completely different shape or follow an entirely different path than the primary grooves 12 and secondary grooves 20, and may be continuously formed or discontinuously formed.
• primary grooves 12 (which travel from left to right in Figures 5 and 6) may be entirely blocked ( Figure 5) or partially blocked ( Figure 6) by formation of the secondary grooves 20 and/or the tertiary grooves 32.
• tool 22 used to form second grooves 20 and/or tertiary grooves 32 can deform ridges 13 between primary grooves 12 during formation of the secondary grooves 20 and/or the tertiary grooves 32 such that portions of ridges 13 are deformed or forced into primary grooves 12.
• the use of secondary grooves 20 and/or tertiary grooves 32 assists in improving the heat transfer characteristics of tube 10 as much as 30% in comparison to a tube 10 including only axial primary grooves or only helical primary grooves.
• the refrigerant flow tends to settle into and follow the grooves, which forms a refrigerant boundary layer within the tube that resists and/or restricts heat transfer between the refrigerant and the tube.
• the use of secondary grooves 20 and/or tertiary grooves 32 disrupts the flow of the refrigerant through primary grooves 12 to prevent formation of a refrigerant boundary layer.
• the flow of the refrigerant is disrupted by the intersection of the primary grooves 12 by each of the secondary grooves 20 and/or the tertiary grooves 32, which causes the refrigerant flow to break off from primary grooves 20 and also creates turbulence in the refrigerant flow that enhances heat transfer.
• a length of tube (e.g., 500 feet) is extruded to include primary grooves 12 that are either axial or helical.
• a desired length of tube 10 is selected, and the desired length is cut from the length of tube.
• a secondary process is then conducted to form secondary grooves 20 and/or tertiary grooves 32.
• a forming tool 22 is selected having the desired spacing S, height H, and angle a of threads 30.
• Forming tool 22 is inserted into tube 10 and rotated to form secondary grooves 20 and/or tertiary grooves 32.
• a single pass of multiple forming tools 22, or multiple passes of multiple forming tools 22 can be done to form secondary and/or tertiary grooves 20 and 32.
• tube 10 can also include any number of grooves (not shown), etc.
• the tube 10 may then be bent into a desired configuration (e.g., a hairpin). Alternatively, tube 10 may be bent into the desired configuration prior to forming secondary and/or tertiary grooves 20 and 32.
• the second processing can occur before or after tube 10 is cut from the length of tube, and before or after lubricant is applied to tube 10 that is used during expansion of tube 10.
• the secondary grooves 20 may formed in a continuous fashion (e.g. drawing) before cutting the tube 10 to final length.
• the forming tool may be designed in a way that the tool is self-rotating in the continuous process, simplifying the process.
• the continuous process may be performed in conjunction with other existing processes, such as extrusion or cutting, or performed as a standalone coil to coil operation.

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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)
• Metal Extraction Processes (AREA)
• Rigid Pipes And Flexible Pipes (AREA)

Priority Applications (5)

Applications Claiming Priority (2)

Publications (1)

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ID=76478013

Family Applications (1)

Country Status (6)

Citations (5)

• 2020
  • 2020-12-18 MX MX2022007765A patent/MX2022007765A/es unknown
  • 2020-12-18 EP EP20903875.1A patent/EP4078063A4/en active Pending
  • 2020-12-18 CN CN202080088998.9A patent/CN115244354A/zh active Pending
  • 2020-12-18 BR BR112022012070A patent/BR112022012070A2/pt unknown
  • 2020-12-18 JP JP2022537433A patent/JP2023508887A/ja active Pending
  • 2020-12-18 WO PCT/US2020/065856 patent/WO2021127340A1/en unknown

Patent Citations (5)

Non-Patent Citations (1)

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