GB1572475A - Heat transfer tube and method of making same - Google Patents

Heat transfer tube and method of making same Download PDF

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Publication number
GB1572475A
GB1572475A GB17512/77A GB1751277A GB1572475A GB 1572475 A GB1572475 A GB 1572475A GB 17512/77 A GB17512/77 A GB 17512/77A GB 1751277 A GB1751277 A GB 1751277A GB 1572475 A GB1572475 A GB 1572475A
Authority
GB
United Kingdom
Prior art keywords
tube
finning
fins
heat transfer
insert
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB17512/77A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Honeywell UOP LLC
Original Assignee
UOP LLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by UOP LLC filed Critical UOP LLC
Publication of GB1572475A publication Critical patent/GB1572475A/en
Expired legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C37/00Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape
    • B21C37/06Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape of tubes or metal hoses; Combined procedures for making tubes, e.g. for making multi-wall tubes
    • B21C37/15Making tubes of special shape; Making tube fittings
    • B21C37/20Making helical or similar guides in or on tubes without removing material, e.g. by drawing same over mandrels, by pushing same through dies ; Making tubes with angled walls, ribbed tubes and tubes with decorated walls
    • B21C37/207Making helical or similar guides in or on tubes without removing material, e.g. by drawing same over mandrels, by pushing same through dies ; Making tubes with angled walls, ribbed tubes and tubes with decorated walls with helical guides
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C37/00Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape
    • B21C37/06Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape of tubes or metal hoses; Combined procedures for making tubes, e.g. for making multi-wall tubes
    • B21C37/15Making tubes of special shape; Making tube fittings
    • B21C37/151Making tubes with multiple passages
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/26Making specific metal objects by operations not covered by a single other subclass or a group in this subclass heat exchangers or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/10Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/42Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being both outside and inside the tubular element
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F13/00Arrangements for modifying heat-transfer, e.g. increasing, decreasing
    • F28F13/06Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media

Description

(54) HEAT TRANSFER TUBE AND METHOD OF MAKING SAME (71) We, UOP INC, a corporation.
organized under the laws of the State of Delaware United States of America, of Ten UOP Plaza, Algonquin & Mt. Prospect Roads, Des Plaines, Illinois, 60016, United States of America, do hereby declare the invention, for which we pray that a patent may be granted to us, and the method by which it is to be performed, to be particularly described in and by the following statement: BACKGROUND OF THE INVENTION This invention relates to a heat transfer tube and particularly to a tube which has increased internal surface area as compared to a plain tube. U.S. Patents 2,960,114 and 3,696,863 each disclose a composite assem bly comprising a tube and an externally rib bed or finned insert core and discuss the desirability of providing such a core for enhancing the internal heat transfer coeffi cient of a tube in certain refrigeration appli cations.The earlier of the aforesaid patents teaches the locking of the inside tube wall and the fins on the core in tight mechanical relationship by means of longitudinal flutes formed in the smooth external pipe surface in the region between adjacent pairs of internal fins. The later patent teaches that a ribbed or finned insert core can be placed inside an outer tube which has been previously exter nally firmed. The core is then mechanically bonded to the previously finned outer tube - by grooving the annular, transversely arranged external fins in a general longitudi nal direction at a plurality of locations around the circumference of the tube. The grooving serves to divide each annular fin into a plurality of separate fins in a common plane.
SUMMARY It is among the objects of the present invention to provide an improved, externally finned heat transfer tube and a method of making same wherein a tube having an outer smooth surface is finned and mechanically locked to a coaxially positioned finned insert member in a single operation using conventional finning equipment.
In the preferred method of the present invention, a finned insert, usually formed of aluminum, is loosely placed inside a length of tubing, usually copper. The tubing is then finned in a known manner by fin forming tools, such as the disc type tools disclosed in U.S. Patent 3,383,893 whose subject matter is incorporated by reference herein. Since the ribs or fins of the insert support the inner tube wall at a plurality of locations, the mandrel pin which is normally used during tube finning to prevent the tube wall from collapsing can be omitted. The radial inward pressures applied to the tube by the finning discs serve to crimp the tube around the insert by reducing the internal diameter of the tube and forcing its inner wall into contact with the outer tips of the ribs or fins on the insert.
Preferably, the finning pressures are sufficient to cause the tips of the insert ribs to become partially embedded in the inner wall of the tube during the crimping. The tube is also lengthened during the finning process.
BRIEF DESCRIPTION OF THE DRAW INGS Figure 1 shows a fragmentary perspective view of a tube in accordance with the present invention; Figure 2 is an end cross sectional view taken on line 2-2 of Figure 1; Figure 3 is an end view of an insert member; Figure 4 is an end view of a tube member; Figure 5 is a partially broken away perspective view showing the insert of Figure 3 and the tube of Figure 4 after they have been telescopically assembled to each other; Figure 6 is a partially broken away perspective view of a finning machine (with one arbor removed for clarity) which can be used to externally fin the assembly of Figure 5; and Figure 7 is a side view showing the insert and tube assembly of Figure 5 following its partial passage to the right through the finning apparatus of Figure 6.
DETAILED DESCRIPTION Figure 1 shows an improved heat transfer tube, in particular a chiller tube, made in accordance with the present invention. The improved tube indicated generally at 10 comprises an insert member indicated generally at 12 (Figure 3) which is preferably formed of an aluminum alloy such as type 6063 and extruded into a shape comprising a core portion 14 having a plurality of ribs or fins 16 extending radially outwardly therefrom. Surrounding the insert member 12 is a tubular member indicated generally at 18 (Figure 4) which initially has a smooth outer surface 20 and a smooth inner surface 22. To produce the finished finned tube 10, the insert member 12 is placed inside the tube 18 so as to be spaced from the ends of the hube 18 as shown in Figure 5.The assembly of Figure 5 is then placed in a finning apparatus such as the three arbor structure disclosed in the aforementioned Patent No. 3,383,893 or in the four arbor apparatus 33 (one arbor has been omitted for clarity) shown in Figure 6.
The finning apparatus 33 includes two sets of variable diameter finning discs. The final sets of discs 36 are positioned downstream (in the direction of tube movement) of the initial sets of discs 46, the initial and final discs of each arbor 38, 40 and 42 being mounted coaxially. The arbors are positioned on a plurality of cam arms 48 for movement toward and away from the axis of the tube 18. The assembly shown in Figure 5 is transformed into the shape shown in Figure 1 as the tube 18 is crimped around the insert member 12 by being fed from left to right through the apparatus 33. In order to provide unfinned plane end portions 18', 18" on the tube, as shown in Figure 7, the finning discs 36, 46 are not moved into the tube 18 until a suitable length of plane end tube 18' is moved past them.At this point, the final discs 36 are brought slowly into contact with the work until they are at their final depth of penetration. From this point onward the initial finning discs 46 will proceed to engage the smooth tube portions proceeding from the left. When fins have been formed to the desired axial length the cam arms 48 are rotated in order to cause the finning discs 36, 46 to withdraw from the work piece and leave the trailing end of the tubes 18" with a smooth unfinned surface.
Although finning is usually done with a mandrel bar inside the tube to resist the tremendous forces applied by the finning discs we have found that it is possible to utilize the insert member 12 as a mandrel. Since the insert member 12 can only resist forces applied radially inwardly along its ribs 16, the inner tube wall 22' tends to assume a straight profile between adjacent fins 16.
Naturally, the outside cross section of the heat exchange member 10 also tends to assume a similar shape so that it has a somewhat polygonal configuration. Preferably, the fins 30 are formed to a sufficient depth to cause enough pressure to be applied to the tube 18 to cause its internal diameter to be reduced to a dimension smaller than the outer diameter of the fin tips 16' on the insert member 12. This diameter reduction causes the tube wall to move radially inwardly of the fin tips sufficiently to cause the fin tips 16' to be embedded in the inner tube wall 22'. This embedment provides a very firm locking of the insert to the tube and enhances the transfer of heat between the insert and the tube.
The forces produced by the finning operation normally induces a twist in the tube being firmed. Naturally, the twisting of the tube will cause a generally identical twisting of the insert member 12. Depending upon the amount of twist or lack thereof desired in the insert member of the final product, it is possible to pretwist the insert member in one direction or another or leave it straight before it is assembled inside the tube.
From the preceding description one can appreciate that the method of our invention enables a finned insert tube to be made in a single finning operation rather than require the use of two operations as in the aforementioned prior art patent wherein the tube was finned in a first operation and then additional grooving operations were necessary to provide a locking of the insert member to the tube. Furthermore, our one-step operation is less costly and can be done on conventional finning equipment rather than require additional equipment. Finally, the continuous pressure applied during finning causes a much firmer engagement between the tube and insert fin member than is possible by longitudinally grooving an already finned tube. This tighter bonding enhances heat transfer from the ribs of the insert member to the metal body of the tube and thus increases the overall efficiency of the tube.
WHAT WE CLAIM IS: 1. A method of making a heat transfer tube having inner and outer fins comprising the steps of inserting a core member having a plurality of radially extending longitudinal fins inside a smooth surfaced cylindrical tube and subjecting at least a portion of the outside surface of the composite assembly to a plurality of finning tools so as to produce external fins on the tube and reduce its internal diameter to a dimension less than the external diameter of the finned core member.
2. The method of Claim 1 wherein said external fins are helically arranged and generally transverse to the axis of the tube.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (12)

**WARNING** start of CLMS field may overlap end of DESC **. Figure 7 is a side view showing the insert and tube assembly of Figure 5 following its partial passage to the right through the finning apparatus of Figure 6. DETAILED DESCRIPTION Figure 1 shows an improved heat transfer tube, in particular a chiller tube, made in accordance with the present invention. The improved tube indicated generally at 10 comprises an insert member indicated generally at 12 (Figure 3) which is preferably formed of an aluminum alloy such as type 6063 and extruded into a shape comprising a core portion 14 having a plurality of ribs or fins 16 extending radially outwardly therefrom. Surrounding the insert member 12 is a tubular member indicated generally at 18 (Figure 4) which initially has a smooth outer surface 20 and a smooth inner surface 22. To produce the finished finned tube 10, the insert member 12 is placed inside the tube 18 so as to be spaced from the ends of the hube 18 as shown in Figure 5.The assembly of Figure 5 is then placed in a finning apparatus such as the three arbor structure disclosed in the aforementioned Patent No. 3,383,893 or in the four arbor apparatus 33 (one arbor has been omitted for clarity) shown in Figure 6. The finning apparatus 33 includes two sets of variable diameter finning discs. The final sets of discs 36 are positioned downstream (in the direction of tube movement) of the initial sets of discs 46, the initial and final discs of each arbor 38, 40 and 42 being mounted coaxially. The arbors are positioned on a plurality of cam arms 48 for movement toward and away from the axis of the tube 18. The assembly shown in Figure 5 is transformed into the shape shown in Figure 1 as the tube 18 is crimped around the insert member 12 by being fed from left to right through the apparatus 33. In order to provide unfinned plane end portions 18', 18" on the tube, as shown in Figure 7, the finning discs 36, 46 are not moved into the tube 18 until a suitable length of plane end tube 18' is moved past them.At this point, the final discs 36 are brought slowly into contact with the work until they are at their final depth of penetration. From this point onward the initial finning discs 46 will proceed to engage the smooth tube portions proceeding from the left. When fins have been formed to the desired axial length the cam arms 48 are rotated in order to cause the finning discs 36, 46 to withdraw from the work piece and leave the trailing end of the tubes 18" with a smooth unfinned surface. Although finning is usually done with a mandrel bar inside the tube to resist the tremendous forces applied by the finning discs we have found that it is possible to utilize the insert member 12 as a mandrel. Since the insert member 12 can only resist forces applied radially inwardly along its ribs 16, the inner tube wall 22' tends to assume a straight profile between adjacent fins 16. Naturally, the outside cross section of the heat exchange member 10 also tends to assume a similar shape so that it has a somewhat polygonal configuration. Preferably, the fins 30 are formed to a sufficient depth to cause enough pressure to be applied to the tube 18 to cause its internal diameter to be reduced to a dimension smaller than the outer diameter of the fin tips 16' on the insert member 12. This diameter reduction causes the tube wall to move radially inwardly of the fin tips sufficiently to cause the fin tips 16' to be embedded in the inner tube wall 22'. This embedment provides a very firm locking of the insert to the tube and enhances the transfer of heat between the insert and the tube. The forces produced by the finning operation normally induces a twist in the tube being firmed. Naturally, the twisting of the tube will cause a generally identical twisting of the insert member 12. Depending upon the amount of twist or lack thereof desired in the insert member of the final product, it is possible to pretwist the insert member in one direction or another or leave it straight before it is assembled inside the tube. From the preceding description one can appreciate that the method of our invention enables a finned insert tube to be made in a single finning operation rather than require the use of two operations as in the aforementioned prior art patent wherein the tube was finned in a first operation and then additional grooving operations were necessary to provide a locking of the insert member to the tube. Furthermore, our one-step operation is less costly and can be done on conventional finning equipment rather than require additional equipment. Finally, the continuous pressure applied during finning causes a much firmer engagement between the tube and insert fin member than is possible by longitudinally grooving an already finned tube.This tighter bonding enhances heat transfer from the ribs of the insert member to the metal body of the tube and thus increases the overall efficiency of the tube. WHAT WE CLAIM IS:
1. A method of making a heat transfer tube having inner and outer fins comprising the steps of inserting a core member having a plurality of radially extending longitudinal fins inside a smooth surfaced cylindrical tube and subjecting at least a portion of the outside surface of the composite assembly to a plurality of finning tools so as to produce external fins on the tube and reduce its internal diameter to a dimension less than the external diameter of the finned core member.
2. The method of Claim 1 wherein said external fins are helically arranged and generally transverse to the axis of the tube.
3. The method of Claim 1 or Claim 2
wherein sufficient radial force is applied to the tube during the finning operation to cause the tube wall to tend to become straight, in transverse axial cross-section, in those portions of its circumference which are located between the longitudinal fins on said core member.
4. The method of Claim 3 wherein said radial force is sufficient to cause the tips of said longitudinal fins to become partially embedded in the inner wall surface of said tube.
5. An improved heat transfer tube comprising an inner core portion having a plural- ity of generally longitudinal fins and a tubular outer portion having smooth cylindrical end portions and a helical transverse externally finned portion intermediate the ends thereof, the inner walls of said finned portion having portions located between each adjacent pair of longitudinal fins at a radial distance from the axis of the core which is less than the radial distance to the tips of the longitudinal fins.
6. An improved heat transfer tube in accordance with Claim 5 wherein the crosssectional configuration of the inner tube wall in said finned portion is generally polygonal.
7. An improved heat transfer tube in accordance with Claim 5 or Claim 6 wherein the external helical fins on said finned portion have a peripheral edge which is continuous and uninterrupted.
8. An improved heat transfer tube in accordance with Claim 5, 6 or 7 wherein the core portion and tubular portion comprise different metals.
9. A method of making a heat transfer tube having inner and outer fins which method comprises introducing into a tube of generally uniform circular cross-section a core member comprising a plurality of generally longitudinal fins each of which is directed in a generally radial fashion and treating the outer surface of at least a region of the tube extending around its circumference to form the region with external fins and to effect crimping of the tube around said core member in the said region.
10. A method as claimed in any one of Claims 1 to 4 and 9, substantially as hereinbefore described with reference to the accompanying drawings.
11. A heat transfer tube whenever obtained by a method as claimed in any one of claims 1 to 4, 9 and 10.
12. A heat transfer tube as claimed in claim 5, substantially as hereinbefore described with reference to, and as illustrated in, Figures 1 to 5 and 7 of the accompanying drawings.
GB17512/77A 1976-04-28 1977-04-27 Heat transfer tube and method of making same Expired GB1572475A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US68100676A 1976-04-28 1976-04-28

Publications (1)

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GB1572475A true GB1572475A (en) 1980-07-30

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GB17512/77A Expired GB1572475A (en) 1976-04-28 1977-04-27 Heat transfer tube and method of making same

Country Status (18)

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JP (1) JPS52133156A (en)
AR (1) AR212360A1 (en)
AU (1) AU510153B2 (en)
BE (1) BE853787A (en)
BR (1) BR7702662A (en)
CA (1) CA1096147A (en)
DE (1) DE2717802B2 (en)
ES (1) ES458227A1 (en)
FR (1) FR2349812A1 (en)
GB (1) GB1572475A (en)
IN (1) IN146417B (en)
IT (1) IT1115901B (en)
LU (1) LU77201A1 (en)
MX (1) MX144667A (en)
NL (1) NL7704575A (en)
PH (1) PH17527A (en)
SU (1) SU724092A3 (en)
ZA (1) ZA772383B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2280256A (en) * 1993-07-23 1995-01-25 Graeme Donald Marshall Fluid channelling member for use in heat transfer tubes
GB2604379A (en) * 2021-03-04 2022-09-07 Free Running Buildings Ltd Heat Exchanger for Building Ventilator

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2522548B1 (en) * 1982-03-05 1985-09-06 Kuibyshevsky Aviat Institu METHOD FOR MANUFACTURING MULTI-CHANNEL TUBES, DIE FOR IMPLEMENTING SAME, AND MULTI-CHANNEL TUBES OBTAINED BY SAID METHOD
JPS63126780U (en) * 1987-02-05 1988-08-18
AT405881B (en) * 1998-03-05 1999-12-27 Vaillant Gmbh HEAT EXCHANGER
KR20020048366A (en) * 2002-06-04 2002-06-22 핀튜브텍(주) Fin tube type heat exchanger and airconditioner and refrigerator using the heat exchanger
KR100469321B1 (en) * 2001-12-08 2005-02-02 핀튜브텍(주) A Fin-Tube Type Heat Exchanger And Manufacturing Method Thereof
KR20030038599A (en) * 2003-04-16 2003-05-16 위성점 A pipe for a refrigerating machine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2280256A (en) * 1993-07-23 1995-01-25 Graeme Donald Marshall Fluid channelling member for use in heat transfer tubes
GB2604379A (en) * 2021-03-04 2022-09-07 Free Running Buildings Ltd Heat Exchanger for Building Ventilator
GB2604379B (en) * 2021-03-04 2024-01-03 Free Running Buildings Ltd Heat Exchanger for Building Ventilator

Also Published As

Publication number Publication date
AU2447577A (en) 1978-10-26
LU77201A1 (en) 1977-08-17
CA1096147A (en) 1981-02-24
NL7704575A (en) 1977-11-01
ES458227A1 (en) 1978-02-16
MX144667A (en) 1981-11-09
PH17527A (en) 1984-09-13
AR212360A1 (en) 1978-06-30
DE2717802B2 (en) 1981-02-05
FR2349812B1 (en) 1980-04-25
ZA772383B (en) 1978-03-29
IT1115901B (en) 1986-02-10
AU510153B2 (en) 1980-06-12
FR2349812A1 (en) 1977-11-25
DE2717802A1 (en) 1977-11-17
SU724092A3 (en) 1980-03-25
BE853787A (en) 1977-08-16
IN146417B (en) 1979-05-26
BR7702662A (en) 1978-01-17
JPS52133156A (en) 1977-11-08

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee