US3636982A - Internal finned tube and method of forming same - Google Patents

Internal finned tube and method of forming same Download PDF

Info

Publication number
US3636982A
US3636982A US11623A US3636982DA US3636982A US 3636982 A US3636982 A US 3636982A US 11623 A US11623 A US 11623A US 3636982D A US3636982D A US 3636982DA US 3636982 A US3636982 A US 3636982A
Authority
US
United States
Prior art keywords
fins
core portion
fin
tubular member
fin member
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 - Lifetime
Application number
US11623A
Inventor
Charles E Drake
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.)
HARSCH Corp (HARSCO)
Original Assignee
PATTERSON KELLEY CO
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 PATTERSON KELLEY CO filed Critical PATTERSON KELLEY CO
Application granted granted Critical
Publication of US3636982A publication Critical patent/US3636982A/en
Assigned to HARSCH CORPORATION (HARSCO) reassignment HARSCH CORPORATION (HARSCO) ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: PATTERSON-KELLEY COMPANY THE, INC.
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F28F1/40Tubular 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

Definitions

  • the core portion is composed of a plurality of axially spaced segments, and the fins bridge a space between and interconnect adjacent segments.
  • the space between adjacent segments establishes communication across the core portion between flow paths bounded radially of the core portion by the tubular member and fins.
  • the core portion is segmented subsequent to extrusion forming of the fin member by directing a cutting member into engagement with the core portion along a line extending transversely of the fin member.
  • the tubular heat exchanger disclosed by the aforementioned patent are the arranging of the fins in a spiraled relationship relative to the longitudinal axis of the fin member and the provision of openings at axially spaced locations in the fins immediately adjacent the inner surface of the tubular member.
  • the openings establish communication between adjacent flow paths defined by the tubular member and the fins, whereas movement of the medium through the openings is encouraged by the centrifugal forces acting upon the medium as a result of the spiraling of the fins.
  • the provision of openings in the fins adjacent the inner surface of the tubular member is intended to prevent unequal ratios of refrigerant and gas from existing in the various flow paths in an effort to maintain the heat absorbing characteristics of the heat exchanger consistent throughout the circumference of the tubular member.
  • the present invention relates to an improved fin-type tube heat exchanger of the type described in U.S. Pat. No. 3,394,736 and to a method of forming same. More particularly, the present invention provides an improved fin member construction, which insures uniform heat characteristics throughout the circumferential dimension of the tubular member, while overcoming the disadvantages inherent in prior art constructions.
  • the fin member is provided with a core portion composed of a plurality of segments, which are interconnected in axially spaced relationship by the fins.
  • the space between adjacent segments is effective to simultaneously establish free flow communication between all of the flow paths defined by the fin and tubular members, thereby resulting in uniform heat exchange conditions within the several fiow paths regardless of number.
  • the free inner edges of portions of the fins bridging the space between adjacent segments define notches, which open towards the space and serve to facilitate flow between adjacent flow paths bounded by fins with which the notches are associated.
  • the nonnotched portions of the fins, which bridge the space between adjacent segments, cooperate to maintain rigidity of the fin member. Furthermore, with this construction there exists no fin areas which are readily subject to being deformed out of the plane of its associated fin, during the notch forming or subsequent fin member handling operations.
  • the core portion of an extrusion formed fin member may be segmented and the fins simultaneously notched by a single material removing operation, thereby greatly facilitating and reducing the cost of manufacture of the present heat exchanger.
  • FIG. l is a perspective view of a fin member constructed in accordance with the present invention.
  • FIG. 2 is an elevational, sectional view of a heat exchanger constructed in accordance with the present invention
  • FIG. 3 is a sectional view taken generally along the line 3-3 in FIG. 2;
  • FIG. 4 is a sectionalized perspective view taken generally along the line ll-4i in FIG. I;
  • FIG. 5 is a sectional view of a fin member illustrating the preferred mode of segmenting the core portion thereof and simultaneously forming notches in the fins.
  • a tubular fin type heat exchanger formed in accordance with the present invention which is generally designated as l in FIGS. 2 and 3, comprises a tubular member 2 and a fin member 3 located within the tubular member.
  • Tubular member 2 is defined by cylindrical inner and outer surfaces 5 and 6, respectively, and preferably formed of a relatively soft metal, such as copper or aluminum, having a high coefi'lciency of thermal conductivity.
  • fin member 3 in its preferred form comprises an axially extending core portion 3 and a plurality of fins I0, which are integral with and extend radially from core portion 8.
  • fin member 3 is spiraled with respect to its longitudinal axis, that is each of fins I0 is spiraled in a longitudinal direction about the axis of core 8.
  • Fins It may be, as desired, spiraled during fin member forming or by a subsequent operation. In practice, it has been found that for a fin member having an overall diameter of about 0.6 inch, a one complete spiral for every 2 feet of linear length of the fin member produces advantageous results.
  • Fin member 3 is preferably formed by an extrusion process from a metal having a high coefficiency of thermal conductivity.
  • the material of fin member 3 is preferably of a greater hardness than the material of tubular member 2 in order to permit proper interference fit to be accomplished in the manner to be hereinafter described.
  • the tubular member is formed of copper and the fin member is formed of an alloy having a greater hardness than that of copper, such as one of the aluminum alloys 63S-T5, 63ST6 or 63S-T2. properly aged.
  • Fins 10 which may be three or more in number depending on the requirements of the heat exchanger, are preferably equally spaced about the axis of core portion 8, and are formed with a generally T-shaped section on the radially outer boundary edges thereof, as indicated at U.
  • the T-shaped section increases the circumferential length of the fin edges and thereby greatly increases the area of contact between the tubular and fin members when assembled.
  • fin member 3 is located within tubular member 2 and the tubular member thereafter radially contracted, as by a drawing operation, so as to bring tube inner surface 5 into interference fit relationship with fin edges 12.
  • tube 1 With tube 1 assembled in this manner, there are defined a plurality of flow paths M for heat exchange medium, which are bounded outwardly of core portion 8 by adjacent pairs of fins 10 and the tube inner surface 5.
  • heat exchangers of the type thus far described are employed for chilling or refrigeration purposes, and a suitable refrigerant comprises the heat exchange medium which is to be passed through flow paths M.
  • Refrigerant is normally in the form of a gas having particles of liquid entrained therein.
  • heat exchangers formed in accordance with the present invention may be employed in any heat transfer application, wherein a material is passed through flow paths 14.
  • tube 1 As thus far described, are conventional, and are shown only for purposes of illustration. Thus, it will be appreciated that applicants invention, which will now be described in detail, may be employed with heat exchangers, wherein fin members having any desired number of fins, wherein the fins are of any desired cross-sectional configuration and are either straight or spiraled; and wherein the fin member is formed by means other than an extrusion operation and joined to the tubular member in any desired fashion.
  • core portion 8 is composed of a plurality of segments, designated generally at 8a, 8b and 8c in FIGS. 1 and 2, which are interconnected in an axially spaced relationship by fins 10.
  • the space or opening between the ends of adjacent segments, which is generally indicated at 16 serves to simultaneously establish communication across core portion 8 between all of flow paths 14.
  • heat exchange media may be uniformly distributed throughout the cross-sectional configuration of the heat exchange tube, thereby insuring that the heat absorbing characteristics of the heat exchanger will remain constant throughout the circumferential dimension of tubular member 2.
  • notches 18 open into space 16 and serve to greatly facilitate the flow of heat exchange medium both between relatively remote flow paths across core portion 8 and between pairs of adjacent flow paths bounded by the fins with which the notches are associated.
  • notches 18 adjacent the radially inner edges of fins l0 permits a substantially greater amount of fin material to be removed without objectionably reducing the elastic strength of fin member 3, than would be the case if notches were to be arranged adjacent the radially outer edges of fins 10.
  • the radial depth of notches 18 may exceed 50 percent of the radial dimension of their associated fins, thereby insuring equalizing flow between the several flow paths at each point along the heat exchanger at which core portion 8 is segmented.
  • FIG. 5 illustrates the preferred mode of segmenting core portion 8 and/or simultaneously segmenting the core portion and forming notches 18 in all of fins 10.
  • a fin member is laid in a suitable jig, not shown, and a single hole" is formed therein by moving a suitable metal cutting device of circular cross section, such as a drill, shown in phantom at 20 along a line, which is substantially normal to the axis of core portion 8 and substantially bisects the angle defined by a pair of adjacent fins. Any burrs produced during the cutting operation would be removed in order to prevent blockage of the notches and/or flow paths.
  • a suitable metal cutting device of circular cross section such as a drill
  • material may be removed from the fin members to form opening 16 and/or notches of any desired configuration and in any suitable manner, such as for instance by punching or flame cutting operations.
  • cuts may be made along lines at angles other than to the axis of the core portion, so long as the strength of the fin members is not critically diminished, as by cutting through the radially outer boundary edges of the fins.
  • the "single hole. forming operation preferably results in both the segmenting of the core portion and notching of the fins.
  • the spacing between openings formed by the single hole forming operation described is normally on the order of about 6 to 8 inches for a five finned fin member having nominally one complete spiral for every 2 feet of length, depending on the accuracy of the spiraling operation. Of course, opening spacings less or greater than that described may be employed depending on heat exchange operating requirements.
  • fluid communication across the core portion may be provided by a grouping of two or more closely adjacent single holes at each station lengthwise of the fin member at which it is desired to obtain uniform heat exchange conditions.
  • each hole is preferably clear through" the core portion and provides notches in all of the fins, since otherwise maximum possible efficiency is not realized.
  • any given station lengthwise of the fin member by replacing a single hole" opening or a grouping thereof with a slot opening or axially spaced slot openings, which are preferably elongated in a direction lengthwise of the fin member.
  • Slot openings may be formed by milling or grinding operations, as well as any of the cutting operations mentioned above.
  • materials other than those specifically discussed above may be employed in forming the tubular and fin members.
  • a heat exchange tube construction including an outer tubular member, and an internal fin member disposed within and extending axially of said tubular member, said fin member having a central core portion and a plurality of fins joined to and extending radially from said core portion, said fins being elongated axially of said core portion and each being radially outwardly bounded by an outer edge portion, said fin outer edge portions being joined to an inner surface of said tubular member for providing an intimate heat-conductive engagement between said fin member and said tubular member, the improvement wherein:
  • said core portion is composed of a plurality of axially spaced segments, and said fins bridge a space between and interconnect adjacent segments, said space between adjacent sion of their associated fins.

Abstract

A tube-type heat exchanger wherein a fin member, including a central core portion and a plurality of fins extending radially therefrom, is located within a tube such that the fins have a close interference fit with the inner wall of the tube. The core portion is composed of a plurality of axially spaced segments, and the fins bridge a space between and interconnect adjacent segments. The space between adjacent segments establishes communication across the core portion between flow paths bounded radially of the core portion by the tubular member and fins. The core portion is segmented subsequent to extrusion forming of the fin member by directing a cutting member into engagement with the core portion along a line extending transversely of the fin member.

Description

i Ttet Uralre Jan. 25, 197' INTERNAL MNNIEID TUBE AND METHU U1 1F URN/TING SAME [72] Inventor: Charles E. Drake, Stroudsburg, Pa.
[73] Assignee: The Pattersnn-llfielley (10., inc., East Stroudsburg, Pa.
[22] Filed: Feb. 16, 11970 211 App]. No.: 11,623
[52] US. Cl ..138/38, 165/109, 165/179, 165/186 [51] lint. Cl ..F28i13/112 [58] Field 011 Search ..165/109, 179, 186; 138/38 [56] References Cited UNITED STATES PATENTS 2,895,508 7/1959 Drake ..165/109 2,869,836 1/1959 l-luet ..165/179 2,864,405 12/1958 Young 165/109 Primary Examiner-Charles Sukalo I Att0rneyBean & Bean [57] ABSTRACT A tube-type heat exchanger wherein a fin member, including a central core portion and a plurality of fins extending radially therefrom, is located within a tube such that the fins have a close interference fit with the inner wall of the tube. The core portion is composed of a plurality of axially spaced segments, and the fins bridge a space between and interconnect adjacent segments. The space between adjacent segments establishes communication across the core portion between flow paths bounded radially of the core portion by the tubular member and fins.
The core portion is segmented subsequent to extrusion forming of the fin member by directing a cutting member into engagement with the core portion along a line extending transversely of the fin member.
4 Claims, 5 Drawing Figures INTERNAL lFlNNElD TUBE AND METHOD OF llFORMlING SAME BACKGROUND OF THE INVENTION In U.S. Pat. No. 3,394,736 there is disclosed a fin-type heat exchanger, wherein a fin member having a central core portion and a plurality of fine extending radially therefrom is placed within a tubular member and the tubular member swaged, drawn, or otherwise reduced in diameter so as to form an intimate interference engagement between the radial outer edges of the fins and the inner surface of the tubular member. By interconnecting the fin and tubular members in this manner, there is obtained a very effective heat transfer connection. Heat exchangers of this type have found use in refrigeration systems, wherein the medium to be cooled is exposed to the exterior of the tubular member and refrigerant is passed through the tubular member along flow paths defined by the fins.
Primary features of the tubular heat exchanger disclosed by the aforementioned patent are the arranging of the fins in a spiraled relationship relative to the longitudinal axis of the fin member and the provision of openings at axially spaced locations in the fins immediately adjacent the inner surface of the tubular member. The openings establish communication between adjacent flow paths defined by the tubular member and the fins, whereas movement of the medium through the openings is encouraged by the centrifugal forces acting upon the medium as a result of the spiraling of the fins. The provision of openings in the fins adjacent the inner surface of the tubular member is intended to prevent unequal ratios of refrigerant and gas from existing in the various flow paths in an effort to maintain the heat absorbing characteristics of the heat exchanger consistent throughout the circumference of the tubular member.
One drawback of the above mentioned heat exchanger is its increased construction costs, due to the fact that each fin opening requires a separate punching or other machining operation. Furthermore, care must be exercised during the fin opening forming operation and subsequent fin member handling operations to prevent deformation of the radially outer free edge areas of the fins immediately adjacent the openings. Such deformation of the fins would tend to interfere with or prevent insertion and/or joining of the fin member with the tubular member, and if not corrected prior to joining of the members would result in partial blockage of the refrigerant flow paths into which the deformed areas of the fins extend.
Further, normal refrigerant flow rates do not for practical I purposes, permit a single set of fin openings arranged at any given point along the heat exchanger to equalize conditions existing in all of the flow paths at such point. This problem becomes increasingly acute as the number of fins or How paths increases, since equalizing of conditions may require the passage of medium transversely of several adjacent flow paths. While uniform conditions could of course be established by increasing the number of openings per unit length of the heat exchanger, the machine costs would likely render the resultant heat exchanger financially noncompetitive with similar but less effective products.
SUMMARY OF THE INVENTION The present invention relates to an improved fin-type tube heat exchanger of the type described in U.S. Pat. No. 3,394,736 and to a method of forming same. More particularly, the present invention provides an improved fin member construction, which insures uniform heat characteristics throughout the circumferential dimension of the tubular member, while overcoming the disadvantages inherent in prior art constructions.
in accordance with the present invention the fin member is provided with a core portion composed of a plurality of segments, which are interconnected in axially spaced relationship by the fins. The space between adjacent segments is effective to simultaneously establish free flow communication between all of the flow paths defined by the fin and tubular members, thereby resulting in uniform heat exchange conditions within the several fiow paths regardless of number.
In the preferred form of the invention, the free inner edges of portions of the fins bridging the space between adjacent segments define notches, which open towards the space and serve to facilitate flow between adjacent flow paths bounded by fins with which the notches are associated. The nonnotched portions of the fins, which bridge the space between adjacent segments, cooperate to maintain rigidity of the fin member. Furthermore, with this construction there exists no fin areas which are readily subject to being deformed out of the plane of its associated fin, during the notch forming or subsequent fin member handling operations.
It is a specific feature of the present invention that the core portion of an extrusion formed fin member may be segmented and the fins simultaneously notched by a single material removing operation, thereby greatly facilitating and reducing the cost of manufacture of the present heat exchanger.
DRAWINGS The nature and mode of operation ofthe present invention will be more fully described in the following detailed description taken with the accompanying drawings, wherein:
FIG. l is a perspective view of a fin member constructed in accordance with the present invention;
FIG. 2 is an elevational, sectional view of a heat exchanger constructed in accordance with the present invention;
FIG. 3 is a sectional view taken generally along the line 3-3 in FIG. 2;
FIG. 4 is a sectionalized perspective view taken generally along the line ll-4i in FIG. I; and
FIG. 5 is a sectional view of a fin member illustrating the preferred mode of segmenting the core portion thereof and simultaneously forming notches in the fins.
DETAILED DESCRIPTION A tubular fin type heat exchanger formed in accordance with the present invention, which is generally designated as l in FIGS. 2 and 3, comprises a tubular member 2 and a fin member 3 located within the tubular member.
Tubular member 2 is defined by cylindrical inner and outer surfaces 5 and 6, respectively, and preferably formed of a relatively soft metal, such as copper or aluminum, having a high coefi'lciency of thermal conductivity.
Now referring particularly to FIGS. ll-3, it will be understood that fin member 3 in its preferred form comprises an axially extending core portion 3 and a plurality of fins I0, which are integral with and extend radially from core portion 8. Preferably, fin member 3 is spiraled with respect to its longitudinal axis, that is each of fins I0 is spiraled in a longitudinal direction about the axis of core 8. Fins It) may be, as desired, spiraled during fin member forming or by a subsequent operation. In practice, it has been found that for a fin member having an overall diameter of about 0.6 inch, a one complete spiral for every 2 feet of linear length of the fin member produces advantageous results.
Fin member 3 is preferably formed by an extrusion process from a metal having a high coefficiency of thermal conductivity. The material of fin member 3 is preferably of a greater hardness than the material of tubular member 2 in order to permit proper interference fit to be accomplished in the manner to be hereinafter described. Normally, the tubular member is formed of copper and the fin member is formed of an alloy having a greater hardness than that of copper, such as one of the aluminum alloys 63S-T5, 63ST6 or 63S-T2. properly aged.
Fins 10, which may be three or more in number depending on the requirements of the heat exchanger, are preferably equally spaced about the axis of core portion 8, and are formed with a generally T-shaped section on the radially outer boundary edges thereof, as indicated at U. The T-shaped section increases the circumferential length of the fin edges and thereby greatly increases the area of contact between the tubular and fin members when assembled.
' To assemble heat exchanger tube 1, fin member 3 is located within tubular member 2 and the tubular member thereafter radially contracted, as by a drawing operation, so as to bring tube inner surface 5 into interference fit relationship with fin edges 12. With tube 1 assembled in this manner, there are defined a plurality of flow paths M for heat exchange medium, which are bounded outwardly of core portion 8 by adjacent pairs of fins 10 and the tube inner surface 5.
Conventionally, heat exchangers of the type thus far described are employed for chilling or refrigeration purposes, and a suitable refrigerant comprises the heat exchange medium which is to be passed through flow paths M. Refrigerant is normally in the form of a gas having particles of liquid entrained therein. However, it will be understood that heat exchangers formed in accordance with the present invention may be employed in any heat transfer application, wherein a material is passed through flow paths 14.
It will be understood that the specific structural features of tube 1, as thus far described, are conventional, and are shown only for purposes of illustration. Thus, it will be appreciated that applicants invention, which will now be described in detail, may be employed with heat exchangers, wherein fin members having any desired number of fins, wherein the fins are of any desired cross-sectional configuration and are either straight or spiraled; and wherein the fin member is formed by means other than an extrusion operation and joined to the tubular member in any desired fashion.
In accordance with the present invention, core portion 8 is composed of a plurality of segments, designated generally at 8a, 8b and 8c in FIGS. 1 and 2, which are interconnected in an axially spaced relationship by fins 10. The space or opening between the ends of adjacent segments, which is generally indicated at 16 serves to simultaneously establish communication across core portion 8 between all of flow paths 14. As a result, heat exchange media may be uniformly distributed throughout the cross-sectional configuration of the heat exchange tube, thereby insuring that the heat absorbing characteristics of the heat exchanger will remain constant throughout the circumferential dimension of tubular member 2.
As a practical matter, except where the diameter of core 8 is relatively large as compared to the overall diameter of fin member 3 such that fins 10 cover only a relatively limited portion of the surface of the core portion, it is necessary to provide notches 18 adjacent the radially inner edges of those portions of fins 10, which bridge between adjacent core portion segments. As will appear from FIGS. 1-4, notches 18 open into space 16 and serve to greatly facilitate the flow of heat exchange medium both between relatively remote flow paths across core portion 8 and between pairs of adjacent flow paths bounded by the fins with which the notches are associated.
The positioning of notches 18 adjacent the radially inner edges of fins l0 permits a substantially greater amount of fin material to be removed without objectionably reducing the elastic strength of fin member 3, than would be the case if notches were to be arranged adjacent the radially outer edges of fins 10. When fin member 3 is formed of common aluminum alloys mentioned above, the radial depth of notches 18 may exceed 50 percent of the radial dimension of their associated fins, thereby insuring equalizing flow between the several flow paths at each point along the heat exchanger at which core portion 8 is segmented.
Moreover, by positioning notches 18 in the manner described, there exists no projecting or unsupported comers adjacent the notches, which would be subject to deformation during the notch forming or subsequent fin member handling operations.
FIG. 5 illustrates the preferred mode of segmenting core portion 8 and/or simultaneously segmenting the core portion and forming notches 18 in all of fins 10. In the simplest form of this operation, a fin member is laid in a suitable jig, not shown, and a single hole" is formed therein by moving a suitable metal cutting device of circular cross section, such as a drill, shown in phantom at 20 along a line, which is substantially normal to the axis of core portion 8 and substantially bisects the angle defined by a pair of adjacent fins. Any burrs produced during the cutting operation would be removed in order to prevent blockage of the notches and/or flow paths. Of course, it will be understood that material may be removed from the fin members to form opening 16 and/or notches of any desired configuration and in any suitable manner, such as for instance by punching or flame cutting operations. As will be apparent, cuts may be made along lines at angles other than to the axis of the core portion, so long as the strength of the fin members is not critically diminished, as by cutting through the radially outer boundary edges of the fins.
It will be understood that the "single hole. forming operation preferably results in both the segmenting of the core portion and notching of the fins. The spacing between openings formed by the single hole forming operation described is normally on the order of about 6 to 8 inches for a five finned fin member having nominally one complete spiral for every 2 feet of length, depending on the accuracy of the spiraling operation. Of course, opening spacings less or greater than that described may be employed depending on heat exchange operating requirements.
As will be apparent from viewing FIG. 5, a disparity between the sizes of notches 18 formed in the respective fins of a five-finned member illustrated results from a single hole forming operation. However, as a practical matter. slight disparities in notch sizes obtained by forming a single hole" in fin members having 3, 4 or 5 fins does not unduly reduce efficiency of their operation. Of course, efficiency is maximized by employing a cutting tool whose diameter is limited only by the requirement that a notch formed by any given fin will have an effective radial dimension less than that which would result in damage to the fin, and by performing material removing operation through the fin member at the same or substantially the same point along a line bisecting the angle defined by more than one pair of adjacent fins.
Alternatively, fluid communication across the core portion may be provided by a grouping of two or more closely adjacent single holes at each station lengthwise of the fin member at which it is desired to obtain uniform heat exchange conditions. When employing groupings of holes, each hole is preferably clear through" the core portion and provides notches in all of the fins, since otherwise maximum possible efficiency is not realized.
Also, it is within the scope of the present invention to provide for fluid communication at any given station lengthwise of the fin member, by replacing a single hole" opening or a grouping thereof with a slot opening or axially spaced slot openings, which are preferably elongated in a direction lengthwise of the fin member. Slot openings may be formed by milling or grinding operations, as well as any of the cutting operations mentioned above. Of course it will be understood that materials other than those specifically discussed above may be employed in forming the tubular and fin members.
I claim:
1. In a heat exchange tube construction including an outer tubular member, and an internal fin member disposed within and extending axially of said tubular member, said fin member having a central core portion and a plurality of fins joined to and extending radially from said core portion, said fins being elongated axially of said core portion and each being radially outwardly bounded by an outer edge portion, said fin outer edge portions being joined to an inner surface of said tubular member for providing an intimate heat-conductive engagement between said fin member and said tubular member, the improvement wherein:
said core portion is composed of a plurality of axially spaced segments, and said fins bridge a space between and interconnect adjacent segments, said space between adjacent sion of their associated fins.
3. The improvement in a heat exchange tube according to claim 1, wherein said core portion and said fins are integrally formed.
d. The improvement in a heat exchange tube according to claim 3, wherein said fins are spiraled relative to the longitudinal axis of said fin member.

Claims (4)

1. In a heat exchange tube construction including an outer tubular member, and an internal fin member disposed within and extending axially of said tubular member, said fin member having a central core portion and a plurality of fins joined to and extending radially from said core portion, said fins being elongated axially of said core portion and each being radially outwardly bounded by an outer edge portion, said fin outer edge portions being joined to an inner surface of said tubular member for providing an intimate heat-conductive engagement between said fin member and said tubular member, the improvement wherein: said core portion is composed of a plurality of axially spaced segments, and said fins bridge a space between and interconnect adjacent segments, said space between adjacent segments establishing communication across said core portion between flow paths bounded radially of said core portion by said tubular member and said fins.
2. The improvement in a heat exchange tube according to claim 1, wherein portions of said fins bridging said space are radially inwardly bounded by free inner edge portions, said inner edge portions defining notches opening towards said space and having radial dimensions less than the radial dimension of their associated fins.
3. The improvement in a heat exchange tube according to claim 1, wherein said core portion and said fins are integrally formed.
4. The improvement in a heat exchange tube according to claim 3, wherein said fins are spiraled relative to the longitudinal axis of said fin member.
US11623A 1970-02-16 1970-02-16 Internal finned tube and method of forming same Expired - Lifetime US3636982A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1162370A 1970-02-16 1970-02-16

Publications (1)

Publication Number Publication Date
US3636982A true US3636982A (en) 1972-01-25

Family

ID=21751264

Family Applications (1)

Application Number Title Priority Date Filing Date
US11623A Expired - Lifetime US3636982A (en) 1970-02-16 1970-02-16 Internal finned tube and method of forming same

Country Status (2)

Country Link
US (1) US3636982A (en)
CA (1) CA934749A (en)

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4132264A (en) * 1974-12-20 1979-01-02 Ecodyne Corporation Plastic heat exchange tube
US4190105A (en) * 1976-08-11 1980-02-26 Gerhard Dankowski Heat exchange tube
US4296539A (en) * 1978-01-27 1981-10-27 Kobe Steel, Limited Heat transfer tubing for natural gas evaporator
EP0121079A1 (en) * 1983-03-30 1984-10-10 Süddeutsche Kühlerfabrik Julius Fr. Behr GmbH & Co. KG Heat exchanger
US4678548A (en) * 1986-07-21 1987-07-07 Aluminum Company Of America Corrosion-resistant support apparatus and method of use for inert electrodes
US4685514A (en) * 1985-12-23 1987-08-11 Aluminum Company Of America Planar heat exchange insert and method
US4702312A (en) * 1986-06-19 1987-10-27 Aluminum Company Of America Thin rod packing for heat exchangers
US4705106A (en) * 1986-06-27 1987-11-10 Aluminum Company Of America Wire brush heat exchange insert and method
US6481492B1 (en) * 1998-09-16 2002-11-19 China Petro-Chemical Corp. And Others Heat exchanger tube, a method for making the same, and a cracking furnace or other tubular heat furnaces using the heat exchanger tube
US6615911B1 (en) * 2002-03-07 2003-09-09 Delphi Technologies, Inc. High performance liquid-cooled heat sink with twisted tape inserts for electronics cooling
US20030209469A1 (en) * 2002-05-07 2003-11-13 Westlake Technology Corporation Cracking of hydrocarbons
US20040173520A1 (en) * 2003-03-06 2004-09-09 Nguyen Ledu Quoc Plastic extruded center tube profile and method of manufacture
US20050014102A1 (en) * 2003-06-12 2005-01-20 Wolfgang Harbeck Recuperator burner including recuperator
US20070224565A1 (en) * 2006-03-10 2007-09-27 Briselden Thomas D Heat exchanging insert and method for fabricating same
DE102006016559A1 (en) * 2006-04-07 2007-10-11 Air Liquide Deutschland Gmbh Heat exchanger for a mobile refrigerated vehicle
US20080141706A1 (en) * 2006-11-22 2008-06-19 Johnson Controls Technology Company Multichannel Evaporator with Flow Mixing Manifold
US20080141708A1 (en) * 2006-11-22 2008-06-19 Johnson Controls Technology Company Space-Saving Multichannel Heat Exchanger
DE102007011203A1 (en) * 2007-03-06 2008-09-11 Schako Klima Luft Ferdinand Schad Kg Zweigniederlassung Kolbingen Pipe for delivery of heat to a room, or removal of heat from the room has elongated insert with radial vanes
US20090050307A1 (en) * 2005-12-05 2009-02-26 Joachim Franke Steam Generator Pipe, Associated Production Method and Continuous Steam Generator
US20100050685A1 (en) * 2008-08-28 2010-03-04 Johnson Controls Technology Company Multichannel Heat Exchanger with Dissimilar Flow
ITMI20102048A1 (en) * 2010-11-04 2012-05-05 Unical Ag Spa OPTIMIZATION DEVICE FOR HEAT TRANSMISSION IN TUBE OF CONVEYANCE OF FUMES IN HEAT EXCHANGE APPLIANCE.
US20140205425A1 (en) * 2013-01-18 2014-07-24 Hamilton Sundstrand Space Systems International Oil cooling arrangement and method of cooling oil
US20150211807A1 (en) * 2014-01-29 2015-07-30 Trane International Inc. Heat Exchanger with Fluted Fin
US20160070319A1 (en) * 2014-09-08 2016-03-10 Ashwin Bharadwaj Heat sink
EP3208560A4 (en) * 2014-10-16 2018-06-27 Daikin Industries, Ltd. Refrigerant flow divider
US20180252475A1 (en) * 2015-08-25 2018-09-06 Danfoss Micro Channel Heat Exchanger (Jiaxing) Co., Ltd. Heat exchange tube for heat exchanger, heat exchanger and assembly method thereof
US20200132347A1 (en) * 2018-10-25 2020-04-30 Heatcraft Refrigeration Products Llc Evaporator coil insert
US10782072B2 (en) * 2014-04-16 2020-09-22 Enterex America LLC Counterflow helical heat exchanger

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2864405A (en) * 1957-02-25 1958-12-16 Young Radiator Co Heat exchanger agitator
US2869836A (en) * 1956-05-28 1959-01-20 Huet Andre Tubular heat exchanger with cores
US2895508A (en) * 1955-11-23 1959-07-21 Patterson Kelley Company Inc Heat exchange conduit

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2895508A (en) * 1955-11-23 1959-07-21 Patterson Kelley Company Inc Heat exchange conduit
US2869836A (en) * 1956-05-28 1959-01-20 Huet Andre Tubular heat exchanger with cores
US2864405A (en) * 1957-02-25 1958-12-16 Young Radiator Co Heat exchanger agitator

Cited By (54)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4132264A (en) * 1974-12-20 1979-01-02 Ecodyne Corporation Plastic heat exchange tube
US4190105A (en) * 1976-08-11 1980-02-26 Gerhard Dankowski Heat exchange tube
US4296539A (en) * 1978-01-27 1981-10-27 Kobe Steel, Limited Heat transfer tubing for natural gas evaporator
US4367791A (en) * 1978-01-27 1983-01-11 Kobe Steel, Ltd. Heat transfer tubing for natural gas evaporator
EP0121079A1 (en) * 1983-03-30 1984-10-10 Süddeutsche Kühlerfabrik Julius Fr. Behr GmbH & Co. KG Heat exchanger
US4524823A (en) * 1983-03-30 1985-06-25 Suddeutsch Kuhlerfabrik Julius Fr. Behr GmbH & Co. KG Heat exchanger having a helical distributor located within the connecting tank
US4685514A (en) * 1985-12-23 1987-08-11 Aluminum Company Of America Planar heat exchange insert and method
US4702312A (en) * 1986-06-19 1987-10-27 Aluminum Company Of America Thin rod packing for heat exchangers
US4705106A (en) * 1986-06-27 1987-11-10 Aluminum Company Of America Wire brush heat exchange insert and method
US4678548A (en) * 1986-07-21 1987-07-07 Aluminum Company Of America Corrosion-resistant support apparatus and method of use for inert electrodes
US6481492B1 (en) * 1998-09-16 2002-11-19 China Petro-Chemical Corp. And Others Heat exchanger tube, a method for making the same, and a cracking furnace or other tubular heat furnaces using the heat exchanger tube
US6530422B2 (en) 1998-09-16 2003-03-11 China Petro-Chemical Corporation Heat exchanger tube, a method for making the same, and a cracking furnace or other tubular heat furnaces using the heat exchanger tube
US6615911B1 (en) * 2002-03-07 2003-09-09 Delphi Technologies, Inc. High performance liquid-cooled heat sink with twisted tape inserts for electronics cooling
US20030209469A1 (en) * 2002-05-07 2003-11-13 Westlake Technology Corporation Cracking of hydrocarbons
US20040173520A1 (en) * 2003-03-06 2004-09-09 Nguyen Ledu Quoc Plastic extruded center tube profile and method of manufacture
US7108139B2 (en) * 2003-03-06 2006-09-19 Purolator Filters Na Llc Plastic extruded center tube profile and method of manufacture
US20050014102A1 (en) * 2003-06-12 2005-01-20 Wolfgang Harbeck Recuperator burner including recuperator
US20090050307A1 (en) * 2005-12-05 2009-02-26 Joachim Franke Steam Generator Pipe, Associated Production Method and Continuous Steam Generator
US20070224565A1 (en) * 2006-03-10 2007-09-27 Briselden Thomas D Heat exchanging insert and method for fabricating same
US8162040B2 (en) 2006-03-10 2012-04-24 Spinworks, LLC Heat exchanging insert and method for fabricating same
DE102006016559A1 (en) * 2006-04-07 2007-10-11 Air Liquide Deutschland Gmbh Heat exchanger for a mobile refrigerated vehicle
US20080148760A1 (en) * 2006-11-22 2008-06-26 Johnson Controls Technology Company Multichannel Heat Exchanger With Dissimilar Tube Spacing
US7895860B2 (en) 2006-11-22 2011-03-01 Johnson Controls Technology Company Multichannel evaporator with flow mixing manifold
US20080141686A1 (en) * 2006-11-22 2008-06-19 Johnson Controls Technology Company Multichannel Evaporator With Flow Mixing Multichannel Tubes
US20080141709A1 (en) * 2006-11-22 2008-06-19 Johnson Controls Technology Company Multi-Block Circuit Multichannel Heat Exchanger
US20080141525A1 (en) * 2006-11-22 2008-06-19 Johnson Controls Technology Company Method for Making a Shaped Multichannel Heat Exchanger
US20080141707A1 (en) * 2006-11-22 2008-06-19 Johnson Controls Technology Company Multichannel Evaporator with Flow Separating Manifold
US20080141708A1 (en) * 2006-11-22 2008-06-19 Johnson Controls Technology Company Space-Saving Multichannel Heat Exchanger
US20090288440A1 (en) * 2006-11-22 2009-11-26 Johnson Controls Technology Company Multichannel Heat Exchanger with Dissimilar Tube Spacing
US20080141706A1 (en) * 2006-11-22 2008-06-19 Johnson Controls Technology Company Multichannel Evaporator with Flow Mixing Manifold
US7677057B2 (en) 2006-11-22 2010-03-16 Johnson Controls Technology Company Multichannel heat exchanger with dissimilar tube spacing
US7757753B2 (en) 2006-11-22 2010-07-20 Johnson Controls Technology Company Multichannel heat exchanger with dissimilar multichannel tubes
US7802439B2 (en) 2006-11-22 2010-09-28 Johnson Controls Technology Company Multichannel evaporator with flow mixing multichannel tubes
US7832231B2 (en) 2006-11-22 2010-11-16 Johnson Controls Technology Company Multichannel evaporator with flow separating manifold
US8281615B2 (en) 2006-11-22 2012-10-09 Johnson Controls Technology Company Multichannel evaporator with flow mixing manifold
US20110132587A1 (en) * 2006-11-22 2011-06-09 Johnson Controls Technology Company Multichannel Evaporator with Flow Mixing Manifold
US7980094B2 (en) 2006-11-22 2011-07-19 Johnson Controls Technology Company Multichannel heat exchanger with dissimilar tube spacing
DE102007011203A1 (en) * 2007-03-06 2008-09-11 Schako Klima Luft Ferdinand Schad Kg Zweigniederlassung Kolbingen Pipe for delivery of heat to a room, or removal of heat from the room has elongated insert with radial vanes
US20100050685A1 (en) * 2008-08-28 2010-03-04 Johnson Controls Technology Company Multichannel Heat Exchanger with Dissimilar Flow
US8938988B2 (en) 2008-08-28 2015-01-27 Johnson Controls Technology Company Multichannel heat exchanger with dissimilar flow
US8234881B2 (en) 2008-08-28 2012-08-07 Johnson Controls Technology Company Multichannel heat exchanger with dissimilar flow
ITMI20102048A1 (en) * 2010-11-04 2012-05-05 Unical Ag Spa OPTIMIZATION DEVICE FOR HEAT TRANSMISSION IN TUBE OF CONVEYANCE OF FUMES IN HEAT EXCHANGE APPLIANCE.
WO2012059250A1 (en) * 2010-11-04 2012-05-10 Unical Ag S.P.A. Device for optimizing the transmission of heat in a pipe for conveying exhaust gases in a heat exchange apparatus
US20140205425A1 (en) * 2013-01-18 2014-07-24 Hamilton Sundstrand Space Systems International Oil cooling arrangement and method of cooling oil
US20150211807A1 (en) * 2014-01-29 2015-07-30 Trane International Inc. Heat Exchanger with Fluted Fin
US10782072B2 (en) * 2014-04-16 2020-09-22 Enterex America LLC Counterflow helical heat exchanger
US20160070319A1 (en) * 2014-09-08 2016-03-10 Ashwin Bharadwaj Heat sink
US10103081B2 (en) * 2014-09-08 2018-10-16 Ashwin Bharadwaj Heat sink
EP3208560A4 (en) * 2014-10-16 2018-06-27 Daikin Industries, Ltd. Refrigerant flow divider
US20180252475A1 (en) * 2015-08-25 2018-09-06 Danfoss Micro Channel Heat Exchanger (Jiaxing) Co., Ltd. Heat exchange tube for heat exchanger, heat exchanger and assembly method thereof
US10690420B2 (en) * 2015-08-25 2020-06-23 Danfoss Micro Channel Heat Exchanger (Jiaxing) Co., Ltd. Heat exchange tube for heat exchanger, heat exchanger and assembly method thereof
US20200132347A1 (en) * 2018-10-25 2020-04-30 Heatcraft Refrigeration Products Llc Evaporator coil insert
US11009271B2 (en) * 2018-10-25 2021-05-18 Heatcraft Refrigeration Products Llc Evaporator coil insert
US11885539B2 (en) 2018-10-25 2024-01-30 Heatcraft Refrigeration Products Llc Evaporator coil insert

Also Published As

Publication number Publication date
CA934749A (en) 1973-10-02

Similar Documents

Publication Publication Date Title
US3636982A (en) Internal finned tube and method of forming same
KR950014055B1 (en) Heat exchanger tube
US3394736A (en) Internal finned tube
US5669441A (en) Heat transfer tube and method of manufacture
US5722485A (en) Louvered fin heat exchanger
US2929408A (en) Fin construction
AR044266A2 (en) METHOD OF MANUFACTURE OF A HEAT EXCHANGER
US3668757A (en) Method of forming a heat exchanger
US6167950B1 (en) Heat transfer tube
US3223153A (en) Fin and tube type heat exchanger
US2216778A (en) Heat exchange member and method of making
US3983932A (en) Heat exchanger
JP3947158B2 (en) Heat exchanger
US2535721A (en) Cylindrical heat exchanger
US4393926A (en) Clover heat exchanger core
US4554969A (en) Coaxial finned tube heat exchanger
US3763930A (en) Heat exchanger
JPS6020094A (en) Heat exchanger
JPS5933450B2 (en) Tube expansion and internal grooving device for heat transfer tubes for heat exchangers
JPH02213694A (en) Fin tube type heat exchanger
SU361377A1 (en) SHELL-TUBE HEAT EXCHANGER
US2173665A (en) Finned tube construction
JPS63279094A (en) Heat exchanger
JPS6314091A (en) Heat transfer pipe
JPS61147096A (en) Cooler

Legal Events

Date Code Title Description
AS Assignment

Owner name: HARSCH CORPORATION (HARSCO), HARRISBURG, PA, A COR

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:PATTERSON-KELLEY COMPANY THE, INC.;REEL/FRAME:004377/0507

Effective date: 19850227