WO2022184473A1 - Conduit dilatable et système d'installation de conduits dilatables dans des échangeurs de chaleur - Google Patents
Conduit dilatable et système d'installation de conduits dilatables dans des échangeurs de chaleur Download PDFInfo
- Publication number
- WO2022184473A1 WO2022184473A1 PCT/EP2022/054114 EP2022054114W WO2022184473A1 WO 2022184473 A1 WO2022184473 A1 WO 2022184473A1 EP 2022054114 W EP2022054114 W EP 2022054114W WO 2022184473 A1 WO2022184473 A1 WO 2022184473A1
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- WO
- WIPO (PCT)
- Prior art keywords
- pipe
- protrusions
- expandable
- expansion bullet
- expansion
- Prior art date
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- 238000009434 installation Methods 0.000 title claims abstract description 11
- 238000012546 transfer Methods 0.000 claims abstract description 43
- 239000004411 aluminium Substances 0.000 claims abstract description 24
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 24
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 22
- 229910000838 Al alloy Inorganic materials 0.000 claims abstract description 18
- 239000011248 coating agent Substances 0.000 claims description 11
- 238000000576 coating method Methods 0.000 claims description 11
- 238000009827 uniform distribution Methods 0.000 claims description 5
- 239000012530 fluid Substances 0.000 description 10
- 230000008901 benefit Effects 0.000 description 7
- 230000004907 flux Effects 0.000 description 7
- 239000000463 material Substances 0.000 description 7
- 238000009833 condensation Methods 0.000 description 6
- 230000005494 condensation Effects 0.000 description 6
- 238000001704 evaporation Methods 0.000 description 6
- 230000008020 evaporation Effects 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 4
- 238000012360 testing method Methods 0.000 description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 3
- 229910052802 copper Inorganic materials 0.000 description 3
- 239000010949 copper Substances 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 229910003460 diamond Inorganic materials 0.000 description 3
- 239000010432 diamond Substances 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
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- 238000010586 diagram Methods 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000003507 refrigerant Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- IHPYMWDTONKSCO-UHFFFAOYSA-N 2,2'-piperazine-1,4-diylbisethanesulfonic acid Chemical compound OS(=O)(=O)CCN1CCN(CCS(O)(=O)=O)CC1 IHPYMWDTONKSCO-UHFFFAOYSA-N 0.000 description 1
- 239000007990 PIPES buffer Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000012809 cooling fluid Substances 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
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- 238000005336 cracking Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D39/00—Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders
- B21D39/08—Tube expanders
- B21D39/20—Tube expanders with mandrels, e.g. expandable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D39/00—Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders
- B21D39/06—Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders of tubes in openings, e.g. rolling-in
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D39/00—Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders
- B21D39/08—Tube expanders
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/02—Making other particular articles heat exchangers or parts thereof, e.g. radiators, condensers fins, headers
- B21D53/08—Making other particular articles heat exchangers or parts thereof, e.g. radiators, condensers fins, headers of both metal tubes and sheet metal
- B21D53/085—Making other particular articles heat exchangers or parts thereof, e.g. radiators, condensers fins, headers of both metal tubes and sheet metal with fins places on zig-zag tubes or parallel tubes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/24—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely
- F28F1/32—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely the means having portions engaging further tubular elements
- F28F1/325—Fins with openings
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2275/00—Fastening; Joining
- F28F2275/12—Fastening; Joining by methods involving deformation of the elements
- F28F2275/125—Fastening; Joining by methods involving deformation of the elements by bringing elements together and expanding
Definitions
- This invention relates to a system for installation of expandable pipes in heat exchangers especially aluminium or aluminium alloy expandable pipes.
- the invention also relates to expandable aluminium or aluminium alloy pipes suitable to be installed in such a system, and an expansion bullet suitable for use to install expandable pipes, especially expandable aluminium or aluminium alloy pipes, in such a system.
- Heat exchangers of various kinds depend of the ability to transfer heat from one medium to another, so as to be able to lead away heat, or to provide heat from and to various locations and devices. Heat exchangers may be manufactured in various shapes, types and forms. Metal, having high heat conductivity, and being a commonly used construction material, is often used for manufacturing of heat exchangers.
- a fluid is often provided to a pipe or similar, wherein said pipe is in contact with flanges and/or heat sinks, providing an indirect coupling of the fluid in said pipe and a medium and/or device coupled to said flanges and/or heat sinks. By pumping said fluid within said pipe, the basic principle of a heat exchanger is provided.
- a method to achieve said contact is to provide an expandable pipe into an opening of a plurality of metal fins, and then expanding the pipe to push it towards said fins.
- the metal fins may then lead heat to or from the pipe, which pipe houses a flow of a suitable heat conductive fluid.
- Such expandable pipe is often paired with a so called expansion bullet, which bullet is pushed through the expandable pipe, wherein said pipe is expanded to an increased diameter that engage the surrounding metal fins firmly.
- Such pipes are furthermore often provided with inner heat transfer protrusions, arranged to engage the expansion bullet when in mechanical contact thereto, and transfer the mechanical energy from the expansion bullet to the wall of the pipe and push said wall outwards, making it expand.
- heat transfer protrusions may, for example, be provided as inwardly directed protrusions from the wall of the pipe, projecting and protruding inwards towards the hollow interior of the pipe where they will be engaged by the tapered expansion bullet when being installed.
- Document JP2011208823 A discloses a system comprising expandable pipes and expansion bullets.
- inwardly directed projections in known expandable pipes may also be deformed when engaged by the expansion bullet, leading to some extent of the mechanical energy provided by means of the expansion bullet to be lost, relative to the intended object of expanding the pipe. Furthermore, the more such projections get deformed, the lower their surface area will be, which in turn also lowers the heat transfer capabilities of the pipe, as such projections also will be exposed to the heating or cooling fluid within the pipe when the heat exchanger is used.
- the disclosure herein aims to combat such drawback of prior art, and provide a system for installation of expandable aluminium or aluminium alloy pipes in heat exchangers, wherein such pipes will achieve an improved expansion and in turn a higher heat transfer within said heat exchangers.
- a system for installation of expandable aluminium material or aluminium alloy pipes in a heat exchanger comprises at least one aluminium or aluminium alloy expandable pipe (hereafter generally denoted “expandable pipe” or simply “pipe” unless otherwise specified) and at least one expansion bullet, said at least one expansion bullet comprising an elongated body with a tapered front portion and a curved portion having a curved shape.
- the at least one expansion bullet is arranged to be inserted in the at least one expandable pipe, which is performed during installations of the expandable pipe in a heat exchanger configured for such an expandable pipe.
- the at least one expandable pipe has a first outer diameter when in a first state, and achieves a second outer diameter when expanded by means of the expansion bullet. Said expansion is achieved after said expansion bullet has been inserted and forced through a hollow interior of said expandable pipe.
- the at least one expandable pipe further comprises elongated inner protrusions, arranged at an inner wall of said pipe, extending along a length of the pipe, and protruding inwards towards a centre line of the pipe.
- the protrusions are configured to transfer an outwards directed force from the expansion bullet for expanding the expandable pipe to the second diameter, wherein the number of protrusions is between 30 and 49. In an embodiment the number of protrusions is between 35 and 45.
- protrusion should be understood to include "fin”.
- Such a system comprising at least one expansion bullet together with at least one expandable pipe having a number of protrusions between 30 and 49 will result in an installation of expandable pipes in a heat exchanger with an increased heat transfer coefficient of the expandable pipes.
- an effective heat exchanger is achieved both for evaporation and condensation.
- the number of protrusions between 30 and 49 will result in an increased heat transfer coefficient of the pipe, since a significant volume of the fluid, flowing in the pipe will flow in the space (may also be denoted grooves) created between the protrusions.
- the space between the protrusions will have a shape and a volume, which result in a large heat transfer coefficient of the expanded pipes.
- the number of protrusions is between 30 and 49 and the outer diameter of the expandable pipe before expansion is between 7 mm to 7.5 mm, a large heat transfer coefficient of the expanded pipes is achieved. From 35 to 45 protrusions and grooves has been found to perform especially well. Especially, in an embodiment wherein the number of protrusions is 35 to 45 and the outer diameter of the expandable pipe before expansion is in the range of 7 mm to 7.1 mm, a large heat transfer coefficient of the expanded pipes is achieved.
- the number of protrusions is between 30 and 49, such as between 35 and 45, a large enough number of protrusions are provided to split the expanding force between them with regards to contact points, which results in a uniformly expanded pipe, a large enough number of protrusions to make each individual protrusion small enough to not exhibit a too strong structural integrity with regards to be able to be slightly deformed when reaching maximum expansion. Further, a reduced number of protrusions may decrease the pressure drop within the pipes and result in an increased heat transfer coefficient of the pipe and thus a more effective heat exchanger.
- the outwards directed force during expansion of the expandable pipe is achieved by means of the curved portion of the expansion bullet, wherein the angled surface of said tapered front and curved portion engages the protrusions, and then pushes them outwards when they slide along said angled surface until they reach an outer wall of the body of the expansion bullet.
- the surface of the expansion bullet may comprise a coating in order to reduce friction between the bullet and the elongated inner protrusions.
- the coating may be a DLC, a Diamond Like Coating.
- a lubricant may be applied between the expansion bullet and the expandable pipe during the expansion of the expandable pipe.
- the expansion bullet may have an elongated solid body or be provided with an axial bore for connecting the expansion bullet to a rod.
- a diameter of the outer wall of the body of the expansion bullet is configured to be larger than a diameter of a virtual circle enclosed by tips of the inner protrusions.
- the radius of curvature of the curved shape of the curved portion is between 5 mm and 20 mm.
- Such a system comprising an expansion bullet with a radius of curvature of the curved shape of the curved portion between 5 mm and 20 mm together with an expandable pipe result in an installation of expandable pipes in a heat exchanger with an increased heat transfer coefficient of the expandable pipes.
- an effective heat exchanger is achieved both for evaporation and condensation.
- the large amount of force results in a strong outward directed force and thus a solid contact with outer exterior elements of a heat exchanger in which such a pipe is installed.
- the lower amount of deformation further results in a larger intact surface area of said protrusions, wherein heat transfer is increased further.
- a small deformation of each protrusion may be acceptable and still achieve large heat transfer coefficient characteristics of the expandable pipe.
- Arranging the protrusions in a pattern provides an increased efficiency as, a uniform distribution of the protrusions distributes the outwardly directed forces uniformly around the circumference of the pipe.
- a helically arranged shape of the orientation of the protrusions will result in an angled directed deformation rather than a pure compression deformation, leaving a larger surface area of such deformed protrusions within the pipe.
- the expansion bullet is arranged to be inserted in the pipe and thereafter passing through the pipe for expanding the outer wall of the pipe.
- the outer wall of the entire length of the pipe may be expanded by passing the expansion bullet through the pipe.
- the bullet is inserted in one end opening of the pipe and exits the pipe from another end opening or returned to the first end opening of the pipe by pulling after expansion.
- the expansion bullet is passed through the pipe by a force acting on the expansion bullet.
- the force acting on the expansion coincide with the extension of a centre line of the expansion bullet.
- the radius of curvature of the curved shape of the curved portion is between 5 mm and 10 mm.
- This range and specific radius of curvature of the curved shape of the curved portion may engage the protrusions of the expandable pipe such that a low amount of deformation of said protrusions is achieved during expansion of the pipe.
- the curved shape of the curved portion of the expansion bullet may have the specific radius of curvature of 7 mm.
- This specific radius of curvature of the curved shape of the curved portion may engage the protrusions of the expandable pipe such that a low amount of deformation of said protrusions is achieved during expansion of the pipe.
- a taper angle of the tapered front portion is between 9.5° and 12.5°.
- the curved portion has a maximal outer diameter at one point along the length of the expansion bullet.
- the point of maximal outer diameter is located at a distance from a front end of the expansion bullet and along a centre line of the expansion bullet ,the distance being in the range of 50% to 90% of the entire length of the expansion bullet.
- This location of the point of maximal outer diameter may engage the protrusions of the expandable pipe such that a low amount of deformation of said protrusions is achieved during expansion of the pipe.
- the distance is located between 60% and 75% of the entire length of the expansion bullet.
- each inner protrusion of the expandable pipe comprises a flat or curved abutment surface, arranged at a tip portion of said protrusion, wherein said abutment surface is configured to engage an outer surface of the expansion bullet.
- each inner protrusion comprises a substantially rectangular cross section, said cross section being taken perpendicular to the centre line of the at least one pipe.
- each inner protrusion comprises a substantially tapered cross section, said cross section being taken in a plane perpendicular to the centre line of the at least one pipe, and wherein each inner protrusion tapering in the direction of the centre line with a taper angle between 15°- 40°, such as between 20°- 30°.
- each inner protrusion creates a space (groove) between the protrusions which have a shape and a volume, which result in a large heat transfer coefficient of the expanded pipes. Further, a tapered configuration of each inner protrusion will result in a large resistance against deformation by the influence of the expanding force from the expansion bullet.
- Each inner protrusion may taper in the direction of the centre line with a taper angle between 15°- 40°, such as 20°-30°. Protrusions having said taper angle may have an extraordinary large resistance against deformation by the influence of the expanding force from the expansion bullet.
- each inner protrusion has a root width between 0.2 mm - 0.3 mm.
- the angular distance between two protrusions arranged adjacent to each other is between 8°-10°, such as 9°.
- each inner protrusion will create a space between the protrusions with a shape and a volume, which result in a large heat transfer coefficient of the expanded pipes.
- each protrusion is configured to be deformed less than 15% from the initial shape of the protrusion, after the pipe has been expanded to the second diameter.
- the inner protrusions are arranged in a pattern at the inner wall.
- the protrusions may be uniformly arranged parallel to the centre line of the pipe.
- the pattern comprises a uniform distribution of helically arranged protrusions, relative to the centre line of the at least one pipe.
- a helical pattern has the advantage that forces from the expansion bullet acting on the inner protrusions will be directed in a direction separate from the extending direction of the inner protrusions. Such a directed force will, when reaching deformation with regards to the inner protrusions, bend the inner protrusions rather than compressing them in parallel with their extending directions. Slightly bend protrusions will thus retain more of their original shape, and provide an improved heat transfer within the pipe due to providing a larger interacting surface area between the inner protrusions and a fluid within the pipe. Further, the helical pattern will create annular flow with centrifugal forces driving the liquid phase of the fluid to the bottom of the space between the inner protrusions, hence augment the heat transfer.
- the helix angle of the helical pattern is 1° - 50°, preferably 10° - 40°.
- the helix angle of the helical pattern may be 15°, 18°, 28° or 40°. For each of these specific helix angles, exceptional good results and characteristics to the end product of a fully assembled heat exchanger is achieved.
- the expandable pipe is made of aluminium material or aluminium alloy, which is a very suitable material, with regards to mechanical and heat transfer properties. Aluminium and aluminium alloys are malleable as a construction material, making it ideal to use in an expanding pipe, where sufficient expansion may be reached without the risk of cracking. Aluminium and aluminium alloys further have the beneficial material property of passively oxidising, wherein microscopic cracks and similar will create an oxide film passively, which oxide film prevents and/or slows failure mechanics such as crack corrosion and similar processes. Even further, aluminium and aluminium alloys have suitable heat transfer properties to be used as material in a heat exchanger.
- the disclosure also relates to an expandable aluminium material or aluminium alloy pipe suitable to be installed in a heat exchanger.
- the expandable aluminium or aluminium alloy pipe may be arranged to be installed in a system according to the first aspect and the embodiments of the system.
- the expandable pipe has a first outer diameter when in a first state and achieves a second outer diameter when expanded by means of an expansion bullet being inserted and forced through the hollow interior of the pipe.
- the expandable pipe comprises elongated inner protrusions, arranged at the inner wall of the expandable pipe.
- the elongated inner protrusions extend along a length of the expandable pipe, and protrude inwardly towards a centre line of the expandable pipe.
- the protrusions are configured to transfer an outwardly directed force from the expansion bullet for expanding the pipe to the second diameter.
- the number of said protrusions is between 30 and 49. In an embodiment the number of protrusions is between 35 and 45.
- the diameter of the expandable pipe, before expansion is between 7 mm and 7.5 mm, such as between 7 mm and 7.1 mm.
- each of the inner protrusions comprise a flat or curved abutment surface, arranged at a tip portion of said protrusion, which are configured to engage an outer surface of the expansion bullet being forced therethrough.
- the width of the tip portion of the protrusions should be between 0.08 mm and 0.2 mm.
- each inner protrusion comprises a substantially rectangular cross section, said cross section being taken perpendicular to the centre line of the pipe.
- each inner protrusion comprises a substantially tapered cross section, said cross section being taken in a plane perpendicular to the centre line of the pipe, and where each inner protrusion is tapering in the direction of the centre line with a taper angle (l) between 15°- 40°, preferably between 20°- 30°.
- each inner protrusion has a root width (d) between 0.2 mm - 0.4 mm.
- the angular distance (d) between two protrusions arranged adjacent to each other is between 8°- 10°.
- each protrusion is configured to be deformed less than 15% from the initial shape of the protrusion, after the pipe has been expanded to the second diameter.
- the inner protrusions are arranged in a pattern at the inner wall, which pattern comprises a uniform distribution.
- the protrusions can be arranged in a parallel pattern or helical pattern, relative to the centre line of the pipe.
- the helix angle (a) of the helical pattern may be 1° - 50°, preferably 10° - 40°.
- the helix angle (a) of the helical pattern may be 15°, 18°, 28° or 40°.
- the disclosure also relates to an expansion bullet suitable for use in the system according to the first aspect and embodiments thereof.
- the expansion bullet comprises an elongated body with a tapered front portion and a curved portion having a curved shape.
- the expansion bullet may comprise an elongated tubular body with a tapered front portion and a curved portion having a curved shape.
- the radius of curvature of the curved shape of the curved portion is between 5 mm and 20 mm, such as between 6 mm and 10 mm.
- a taper angle (b) of the tapered front portion is between 9.5° and 12.5°.
- the curved portion has a maximal outer diameter at one point along the length of the expansion bullet.
- the point of maximal outer diameter may be located at a distance from a front end of the expansion bullet and along a centre line of the expansion bullet, where the distance may be in the range of 50% to 90% of the entire length of the expansion bullet. In an embodiment, the distance is located between 60% and 75% of the entire length of the expansion bullet.
- an outer surface of the expansion bullet may comprise a friction reducing coating.
- the surface of the expansion bullet may comprise the coating in order to reduce friction between the bullet and the elongated inner protrusions.
- the coating may be a DLC, a Diamond Like Coating.
- Fig. 1 shows a schematic depiction of a heat exchanger in a perspective view, assembled by means of the system according to the disclosure
- Fig. 2a shows schematic depiction of a cross-sectional view of an expandable pipe, according to an example of the disclosure
- Fig. 2b shows a detail view of the cross-sectional view of the expandable pipe in fig. 2a
- Figs. 3a and 3b show diagrams of the heat transfer coefficient in evaporation condition and condensation condition, respectively, for different pipes at different mass flux
- Figs. 4a and 4b show schematic depictions of longitudinal cross-sectional views of portions of an expandable pipe, according to examples of the disclosure.
- Fig. 5 shows a schematic depiction of a longitudinal cross-sectional view of an expansion bullet configured for use in the system, according to an example.
- Fig. 1 shows a schematic depiction of a heat exchanger 1 in a perspective view.
- the heat exchanger 1 is to be perceived as being assembled by means of the system 2 described throughout the disclosure herein, and thus comprising parts defined by any variation of the various examples as described herein.
- the heat exchanger 1 comprises a plurality of plate elements, hereafter called fins 4. Said fins 4 are, as depicted in fig. 1, provided with three through holes 6, through which an expandable pipe 8 may be inserted. In fig. 1 three such pipes 8 are to be perceived as already being installed into the fins 4.
- pre-formed half circle hairpin shaped pipes 8 may be connected to the end portions of the pipes 8 as depicted, so as to achieve a single fluid circuit utilizing all three pipes 8 herein, or each pipe 8 may be used as an individual circuit, depending on the design and desired properties of the assembled heat exchanger 1.
- the system 2 is configured for installation of the expandable pipes 8 in the heat exchanger 1.
- Said system 2 comprises at least one expandable pipe 8 and an expansion bullet 10, comprising an elongated body 12 with a tapered front portion 14 and a radius of curvature, arranged to be inserted in the at least one pipe 8.
- an expansion bullet 10 is described with reference to fig. 5.
- the at least one expandable pipe 8 has a first outer diameter D1 when in a first state, and achieves a second outer diameter D2 when expanded by means of the bullet 10, after said expansion bullet 10 has been inserted and forced through a hollow interior of said pipe 8.
- the heat exchanger 1 depicted in fig. 1 is to be understood as already installed, wherein the pipes 8 are to be perceived as being in their expanded state, and thus sitting flush with the holes 6 in the fins 4 of the heat exchanger 1, wherein the pipes 8 herein having their second outer diameters D2.
- the at least one expandable pipe 8 further comprises elongated inner protrusions 16, arranged at an inner wall 17 of said pipe 8.
- Said protrusions 16 extend along a length of the pipes 8, and protrude inwards towards a centre line Cl of the pipes 8.
- the protrusions 16 are configured to transfer an outwards directed force from the expansion bullet 10 for expanding the pipe 8 to the second diameter. Such a force is achieved when the inner protrusions 16 engage the tapered front portion 14 of the expansion bullet 10, and then slide along said tapered front portion 14 until they reach the elongated body 12, which body comprises an outer diameter that forces the inner protrusions 16 to move outwards and thus expand the pipe 8 until it fits firmly inside the holes 6 of the fins 4.
- the inner protrusions 16 are arranged in a pattern 13 at the inner wall 17, which pattern 13 comprises a uniformly distribution of helically arranged protrusions 16, relative the centre line Cl of the at least one pipe 8. It should thus be obvious that the tapered front portion 14 of the expansion bullet 10 will act on the inner protrusions 16 in a direction that is separate from the extending direction of the inner protrusions 16. This means that when the expansion of the pipe 8 is stopped by means of the variable diameter of the pipe 8 reaching the fins 4, any further movement of the expansion bullet 10 within the pipe 8 will result in deformation of the inner protrusions 16 instead of further moving them outwards.
- the deformation on the inner protrusions 16 may be continuous during the expansion after the bullet surface has engaged the protrusions.
- the through holes 6 of fin may be provided with a diameter of 7.3 mm.
- the expected outer diameter of the pipe 8 after expansion may be about 7.42 mm.
- Fig. 2a shows schematic depiction of a cross-sectional view of an expandable pipe, according to an example of the disclosure
- Fig. 2a depicts a cross-sectional view taken perpendicular to the centre line Cl of the pipe 8, more clearly showing the inner protrusions 16 with regards to their distribution and shape.
- Each inner protrusion 16 may, as depicted in fig. 2a, comprise a substantially flat or curved abutment surface 18, arranged at a tip portion 15 of said protrusion 16.
- Such an abutment surface 18 is configured to receive an outer surface 20 of the expansion bullet 10.
- the example of the expandable pipe 8 as depicted in fig. 2a comprises a total of 40 inner protrusions 16, spaced uniformly around the circumference of the expandable pipe 8.
- each protrusion 16 may of course be modified depending on the number of protrusions 16 comprised in the pipe 8, and other total amounts of protrusions 16 is possible to utilize without deviating from the scope of protection defined by the disclosure herein.
- Other examples of the expandable pipe 8 may have a number of inner protrusions 16 in the range of about 30 to 49. Further examples of the expandable pipe 8 may have a number of inner protrusions 16 in the range of about 35 to 45.
- Such inner protrusions 16 may thus be altered with regards to their shape and size, so as to achieve a large enough accumulative abutment surface 18 area, and to withstand the forces applied from the expansion bullet 10 when in use.
- the first outer diameter D1 of the expandable pipe may be in the range of 7 mm to 7.1 mm before expansion.
- Each inner protrusion 16 may, as seen in fig. 2a, comprise a substantially rectangular cross section, said cross section being taken perpendicular to the centre line Cl of the at least one pipe 8.
- a slight tapering to sidewalls 22 of said protrusions 16 may be present. Such slight tapering may provide benefits to the manufacturing of such a pipe 8, as the pipe 8 is round and thus the inner wall 17 to which the inner protrusions 16 are connected to is concave with regards to the extending direction of the inner protrusions 16.
- Such a shape as described here above is structurally rigid and may transfer a large enough force to the outer wall 19 of the expansion pipe 8 without deforming too much.
- material usage may be reduced and manufacturing may be simplified, providing a cost effective product.
- Fig. 2b shows a detail view of the cross-sectional view of the expandable pipe in fig. 2a.
- the detail view in fig. 2b represents the details within the small circle in fig. 2a.
- the inner protrusion 16 comprises a substantially tapered cross section, said cross section being taken perpendicular to the centre line Cl of the at least one pipe 8, and wherein each inner protrusion 16 tapering in the direction of the centre line Cl with a taper angle l, which may be between 15°- 40°.
- the height h of the inner protrusion 16 may be in the range 0.1 mm - 0.4 mm.
- the space between the protrusions 16 will have a shape and a volume, which result in a large heat transfer coefficient of the expanded pipes 8.
- Figs. 3a and 3b show diagrams of the heat transfer coefficient HTC for different pipes in evaporation condition and condensation condition, respectively, at different mass flux. Test results of the heat transfer coefficient at different mass flux for different expandable pipes at evaporation are shown in fig. 3a.
- the expandable pipe 8 in aluminium with 40 inner protrusions has a larger heat transfer coefficient for all different mass flux comparing to expandable pipes with 50 inner protrusions of aluminium and copper. Further, the expandable pipe in aluminium with a smooth inner surface and without inner protrusions has lowest heat transfer coefficient. All the expandable pipes had an outer diameter of 7 mm.
- the evaporation test in fig. 3a was performed at 10° C. The fluid flowing within the pipes was a refrigerant.
- Fig. 4a depicts a schematic longitudinal cross-sectional view of a portion of a pipe 8, taken along the centre line Cl of said pipe 8 when the helix angle a is 0°.
- the helix angle a of the helical pattern 13 may preferably be in the range of about 1° to about 50°, which is illustrated in fig. 4b by the helix angle a therein, wherein may be perceived to be shifted within said defined range.
- the protrusions extend in a parallel with the centre line Cl of the pipe.
- the helix angle a of the helical pattern 13 is 18°, as an example.
- Fig. 5 shows a schematic depiction of a longitudinal cross-sectional view of an expansion bullet 10 configured for use in the system 2.
- the expansion bullet 10 comprising an elongated tubular body 12 with a tapered front portion 14 and a curved portion 30 having a curved shape 32.
- the expansion bullet 10 is arranged to be inserted in the pipe 8 and thereafter passing through the pipe 8 for expanding the outer wall 19 of the pipe 8.
- the outer wall 19 of the entire length of the pipe 8 may be expanded by passing the expansion bullet 10 through the pipe 8.
- the bullet 10 is inserted in one end opening of the pipe 8, and exit the pipe 8 in another end opening or returned to the first end opening of the pipe by pulling after expansion.
- the expansion bullet 10 is passed through the pipe 8 by a force acting on the expansion bullet 10.
- the force acting on the expansion bullet 10 coincide with the extension of a centre line C2 of the expansion bullet 10.
- a first part 24 of the expansion bullet 10 has the shape of a truncated cone 26.
- a base 28 of the truncated cone 26 is arranged adjacent to a second curved part 30 of the expansion bullet 10.
- the second part 30 of the expansion bullet 10 has curved shape 32, provided with a maximal outer diameter D3 at one point 34 along the length LI of the expansion bullet 10.
- the point 34 of maximal outer diameter D3 at a distance L2 from a front end 36 of the expansion bullet 10 and along the centre line C2 may be located in the range of 50% to 90% of the entire length of the expansion bullet 10 based on the radius of curvature. In fig. 5 this point of maximal outer diameter D3 at the distance D2 from the front end 36 of the expansion bullet 10 and along the centre line C2 is located 67% of the entire length of the expansion bullet 10.
- the radius R of curvature of the curved shape 32 of the curved portion 30 is between 5 and 20 mm. There may be a relationship between the taper angle of the tapered front portion and the radius of curvature of the curved shape of the curved portion. The taper angle may increase as the radius of curvature increases. The tapered front portion may be eliminated at a radius at 9.8 mm. The tapered front portion may decrease as the radius of curvature decreases. According to an example, the radius R of curvature of the curved shape 32 of the curved portion 30 is 7 mm and a taper angle b of the tapered front portion 14 is 11.9°.
- the expansion bullet engages the inner protrusions with a low angle, providing a low deformation at the initial engagement, which in turn easily allows the expansion bullet to slide in within the expandable pipe.
- the inner protrusions may then gradually be subjected to more force, forcing the pipe to expand in a smooth transition between its two diameters.
- the outwards directed expansion force from the expansion bullet 10 acting on the protrusions 16 in the pipe 8 is achieved by means of the tapered front portion 14 of the expansion bullet 10, which has the shape of a truncated cone 26.
- the outer surface 20 of said truncated cone 20 engages the protrusions 16, which are pushed outwards when sliding along said outer surface 20 until they slide up on the curved shaped 32 second part 30 of the expansion bullet 10.
- the surface 20 of the expansion bullet 10 may comprise a coating 38 in order to reduce friction between the bullet 10 and the elongated inner protrusions 16.
- the coating 38 may be a DLC, a Diamond Like Coating.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Thermal Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
L'invention concerne un système d'installation de conduits en aluminium ou en alliage d'aluminium dilatables dans un échangeur de chaleur, comprenant au moins un conduit dilatable et au moins une balle de dilatation présentant un corps allongé doté d'une partie avant conique et d'une partie incurvée ayant une forme incurvée, conçue pour être insérée dans ledit conduit dilatable, au moins, ledit conduit dilatable a un premier diamètre extérieur dans un premier état, et atteint un second diamètre extérieur lorsqu'il est dilaté au moyen de la balle de dilatation, après l'introduction de ladite balle de dilatation et son forçage dans l'intérieur creux dudit conduit dilatable, ledit conduit dilatable, au moins, comprend en outre des parties saillantes internes allongées, disposées au niveau d'une paroi interne dudit conduit dilatable, s'étendant sur une longueur du conduit dilatable, et faisant saillie vers l'intérieur vers une ligne centrale du conduit dilatable, les parties saillantes, au nombre de 30 à 49, étant conçues pour transférer une force dirigée vers l'extérieur par la balle de dilatation pour élargir le conduit dilatable jusqu'à atteindre le second diamètre.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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SE2150224 | 2021-03-01 | ||
SE2150224-0 | 2021-03-01 |
Publications (1)
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WO2022184473A1 true WO2022184473A1 (fr) | 2022-09-09 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/EP2022/054114 WO2022184473A1 (fr) | 2021-03-01 | 2022-02-18 | Conduit dilatable et système d'installation de conduits dilatables dans des échangeurs de chaleur |
Country Status (2)
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CN (1) | CN217303714U (fr) |
WO (1) | WO2022184473A1 (fr) |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5381600A (en) * | 1993-10-06 | 1995-01-17 | Ford Motor Company | Heat exchanger and method of making the same |
US6026892A (en) * | 1996-09-13 | 2000-02-22 | Poongsan Corporation | Heat transfer tube with cross-grooved inner surface and manufacturing method thereof |
JP2005288502A (ja) * | 2004-03-31 | 2005-10-20 | Kobelco & Materials Copper Tube Inc | 拡管用工具およびそれを使用した拡管方法 |
JP2011208823A (ja) | 2010-03-29 | 2011-10-20 | Furukawa Electric Co Ltd:The | 熱交換器の製造方法 |
WO2014130281A1 (fr) * | 2013-02-21 | 2014-08-28 | Carrier Corporation | Structures de tuyau pour échangeur de chaleur |
JP2015062951A (ja) * | 2013-08-29 | 2015-04-09 | 三菱アルミニウム株式会社 | アルミニウムまたはアルミニウム合金製伝熱管の拡管方法 |
-
2021
- 2021-04-01 CN CN202120667680.8U patent/CN217303714U/zh active Active
-
2022
- 2022-02-18 WO PCT/EP2022/054114 patent/WO2022184473A1/fr active Application Filing
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5381600A (en) * | 1993-10-06 | 1995-01-17 | Ford Motor Company | Heat exchanger and method of making the same |
US6026892A (en) * | 1996-09-13 | 2000-02-22 | Poongsan Corporation | Heat transfer tube with cross-grooved inner surface and manufacturing method thereof |
JP2005288502A (ja) * | 2004-03-31 | 2005-10-20 | Kobelco & Materials Copper Tube Inc | 拡管用工具およびそれを使用した拡管方法 |
JP2011208823A (ja) | 2010-03-29 | 2011-10-20 | Furukawa Electric Co Ltd:The | 熱交換器の製造方法 |
WO2014130281A1 (fr) * | 2013-02-21 | 2014-08-28 | Carrier Corporation | Structures de tuyau pour échangeur de chaleur |
JP2015062951A (ja) * | 2013-08-29 | 2015-04-09 | 三菱アルミニウム株式会社 | アルミニウムまたはアルミニウム合金製伝熱管の拡管方法 |
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