US2775433A - Finned tube spacing supports - Google Patents

Finned tube spacing supports Download PDF

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US2775433A
US2775433A US377388A US37738853A US2775433A US 2775433 A US2775433 A US 2775433A US 377388 A US377388 A US 377388A US 37738853 A US37738853 A US 37738853A US 2775433 A US2775433 A US 2775433A
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tubes
tube
strip
fins
finned
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William F Matheny
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/007Auxiliary supports for elements
    • F28F9/013Auxiliary supports for elements for tubes or tube-assemblies
    • F28F9/0138Auxiliary supports for elements for tubes or tube-assemblies formed by sleeves for finned tubes
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4935Heat exchanger or boiler making
    • Y10T29/49377Tube with heat transfer means
    • Y10T29/49378Finned tube
    • Y10T29/49382Helically finned

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  • the present invention consists in new and useful improvements in tube spacing supports and the method of applying the same, whereby the individual tubes aremaintained in uniformly spaced relation in the housingand at the same time, damage to the helical fins surrounding the tubes is prevented.
  • any two adjacent finned tubes must be held apart a sufiicient distance to permit the tubes to be moved longitudinally with respect to one another during assembly and to' prevent the fins on adjacent tubes' from locking together.
  • a tube banding device which is adapted toembr-ace the peripheral edgesof the helical fin at predetermined-spaced intervals on the heat exchanger tubes.
  • a strip of metal of a width to embrace several convolutions of a helical -fin is secured around the finned tube.
  • Molten lead, solder, or other'suitablemetalhaving a low meltingpoint is poured into a "hole irijthe'strip and flows intofthe spacesbetween certain'ofthe helical fins so as to provide a cylindiicalbodywithin the-bound- 7 2,775,433 Patented Dem--25,- 1956 ing strip which completely encircles the tube between the fins, after solidification.
  • This solidified metallic body and the strip which bounds it forms a rigid'support between the fins and the tube proper, relieving the fins of all strain at these points.
  • these metal-filled bands eliminate the need of otherspacing and'supporting means and greatly facilitate theremoval of defective tubes from a heat exchanger unit by minimizing the number of other tubes which must be removed to. gain access to the defective tube.
  • Another object of the invention is to arrange tube bandingdevices such as just described, at uniformly spaced intervals on each of a series of tubes to be used in a heat exchanger chamber, so that when the tubes are arranged in superimposed rows, the corresponding banding devices of adjacent tubes lie in abutting relation, the peripheries of the helical fins of adjacent tubes being spaced apart laterally for a distance determined by the thickness of the banding strip.
  • a further object of the invention is to provide a banding strip of modified cross sectional profile, for use when it is desired to space the tubes laterally a distance greater than the thickness of the banding strip.
  • Figure 1 is an end view of a heat exchanger chamber showing a series of finned tubes and their supporting bands.
  • Figure 2 is a transverse sectional view taken on line 2-2 of Figure 1, showing the lateral relationship of a series of tubes supported in accordance with this invention.
  • Figure 3 is a perspective view showing one form of banding strip before it is applied to the tube.
  • Figure 4 is an enlarged transverse sectional view through a finned tube, showing the banding strip in the course of application.
  • Figure 4A is detail view showing the joined ends of the strip after a preliminary bending and. before cornpressing.
  • Figure 5 is a diagrammatic illustration of one form of clamping device which may be employed in applying and locking the banding strip on the periphery of the helical fins.
  • Figure 6 is a longitudinal sectional view through a section of finned tubing, showing a channeled banding strip of the type used to increase the distance between two adjacent tubes and Figure 7 is a similar view showing a plain banding strip.
  • the numeral '10 generally represents a conventional helical finned tube consisting of the central tube proper 11, the periphery of which is'encircled from end to end by a helical fin strip 12 which is firmly secured to the tube proper by various known methods.
  • a series of layers or horizontal rows of these tubes 10 are superimposed in a heat exchanger chamber A, the wall B of which is'o'pen toexpose the finned tubes so that cooling air may be forced or drawn through the chamber, over the tubes and between the spaces and convolutions of the helical fins.
  • these parallel rows of tubes 10 are connected in series so that the fluid to be cooled can be drawn or forced continuously back and forth through the tubes until the entire'series has been encountered.
  • the tubes in order to obtain 'themaximum benefit of the cooling air drawn through the chamber A, it is desirable to have the tubes arranged as closely together as possible while at the same time permitting suflicient space between the tubes to accommodate the passage of air therethrough. It is to facilitate this arrangement of tubes in close proximity, thatthe improved tube banding device or spacing support of the present invention is employed.
  • this tube spacing support consists of a metal strip 13 of a length to completely encircle a finned tube in close engagement with the peripheral edges of of its helical fin and of suflicient width to overlie several of the convolutions of the fin.
  • a plurality of strips 13 are arranged in predetermined longitudinal spaced relation on each of the tubes to be placed in the chamber A, such spacing being uniform on all tubes so that when the tubes are superimposed the supporting contact between the tubes is borne by the peripheries of adjacent bands 13.
  • each tube is supported by the engagement of its bands with the corresponding bands of adjacent tubes and the tubes are spaced apart laterally a distance determined by the thickness of the strip 13.
  • the metal of the strips 13 may vary in thickness to meet requirements of use, but it has been found that a strip .016 inch in thickness is generally satisfactory for this type of installation.
  • Each of the strips 13 is provided at a point intermediate its longitudinal edges, with an aperture 16 which as will later appear, is adapted to permit the pouring of molten lead or solder into the area bounded by the strip, which flows around the periphery of the tube proper 11 and fills the space between the convolutions of one or more of the fins with a metal mass or body 17.
  • the molten metal is introduced at substantially the central portion of the bounding strip, it has a tendency to initially flow'beyond the longitudinal limits required. However, the metal cools rapidly and progressively dams up the narrow spaces between the fins, so that the ultimate mass 17 fills only the desired number of spaces.
  • this body of metal 17 forms a rigid supporting bushing or washer which extends radially from the tube 11 to the periphery of the helical fin and together with the surrounding strip 13, is adapted to bear considerable weight without in any way deforming the helical fins of adjacent tubes.
  • the various rows of tubes 10 can be arranged in staggered relation as shown in Figure 2, withoutdanger of injury to the helical fins of any of the tubes.
  • the bands or strips 13 have a plain crosssectional profile as shown in Figure 7 as the spacing afforded by the thickness of two contacting bands is sufficient. However, in some instances it is desirable to space the tubes as much as A inch apart. This cannot practically be accomplished by the use of thicker bands because bands of the required thickness would offer such a resistance when applied to the fins, that the fins would be deformed.
  • the radical ribs 13a of any two adjacent bands serve as lateral abutments and support the tubes at a spacing distance determined by the depth of the channels 13a.
  • the body of metal 17 fills the space between the tube 11 and the web of the channel 13a and provides an extended rigid supporting washer or bushing.
  • the transverse thickness of the metal body 17 may vary from the distance between two adjacent fins, to the convolutions of several fins, depending upon the quantity of molten metal poured into the band.
  • a pair of suitable pliers is applied to the engaging flanges 14-15, to bend the ends over slightly at reversed, coacting acute angles as shown in Fig. 4A. As will later appear, this angular arrangement facilitates the clamping of the band in tight engagement with the fins.
  • This fixture C preferably consists of a pair of upper and lower jaw members 18 and 19, hingedly connected as at 20 and having a handle 21 fixed to the upper jaw.
  • the opposed faces of the jaws are respectively provided with concave recesses 22, having a radius to accommodate the peripheries of the finned tube with a band encircling the same.
  • the recess 22 of jaw member 18 embraces the overlapping end of the strip and as the fixture jaws are closed, a lever action is started on the connected flanges of the strip.
  • the closing jaws bend the connected flanges of the strip and as the underlying angular flange 14 is bent in a counter-clockwise are about the base of its angle, it pulls the over-lying angular flange 15 with it and tightens the band around the tube.
  • the angular flanges 14-15 are flattened and embedded slightly into the periphery of the adjacent finned tube so as to slightly deform the fin at this point. This not only locks the ends of the strip 13 together but by embedding them slightly into the periphery of the fin tube, longitudinal movement of the strip on the fin, is prevented during the metal pouring operation.
  • molten lead or solder is poured into the opening 16 and flows around the fin 12, completely filling one or two of the convolutions of the fin as previously described.
  • the channel 13a may be applied to the strip 13 in any suitable manner such for example as by a die or by rolling the channel into the strip and the depth of the channel can be predetermined to give the required tube spacing.
  • a radial spacing support forming device comprising a band of flexible metal encircling a portion of said tube and engaging the peripheral edges of a group of adjacent fins, a central annular channel extending around said band, spaced radially from the peripheral edges of said fins, the meeting edges of said band being interconnected by overlapping, transverse flanges bent upon one another, and an opening through the web of said channel to facilitate the flowing of molten metal within the, band and between said fins, to provide when hardened, a mass of metal extending radially from the tube to the inner face of said web.
  • a heat exchanger including a chamber having 1 a series of parallel finned tubes arranged in superimtudinally spaced intervals on each tube, each support comprising a flexible metal band encircling said tube and engaging the peripheral edges of a group of adjacent finned portions, a central annular channel extending around each band, radially spaced from the peripheral edges of said fins, an annular mass of metal surrounding References Cited in the file of this patent UNITED STATES PATENTS 1,455,028 McCord May 15, 1923 1,782,260 Franquet et al Nov. 18, 1930 2,146,614 Bergdoll Feb. 7, 1939 2,179,530 Townsend Nov.

Description

Dec. 25, 1956 w. F. MATHENY 2,775,433
FINNED TUBE SPACING SUPPORTS Filed Aug. 31, 1953 H i=- -5 7- W i- J IN VEN TOR.
WILL/AM I. MATHENY.
ATTORNEY United States PatentO' FINNED TUBE SPACING SUPPORTS William F. Matheny, Tulsa,0kla. Application August 31, 1953, Serial No. 377,388 2 Claims. (Cl. 257-26216) More particularly, the present invention consists in new and useful improvements in tube spacing supports and the method of applying the same, whereby the individual tubes aremaintained in uniformly spaced relation in the housingand at the same time, damage to the helical fins surrounding the tubes is prevented.
Heretofore, in heat exchangers of this general type the tubes have been supported by transverse racks arranged at spaced intervals throughout the length of the chamber and having apertures through which the finned tubes extend. In some intsances," a seriesof strips have been extended'transversely of the chamber between the various rows of tubes in order to afford lateral support.
' In heat exchangers of the type employing air as the cooling medium, it is desirable to maintain the tubes in relatively close proximity so that all of the cooling air will pass through the fins, taking maximum advantage of the cooling medium. In someinstances, it is desirable that' this spacing of the tubes be as close as .030 inch. At the same time, any two adjacent finned tubes must be held apart a sufiicient distance to permit the tubes to be moved longitudinally with respect to one another during assembly and to' prevent the fins on adjacent tubes' from locking together.
Experience has shown that when using a series of supporting sheets or racks with perforations to receive the finned tubes, it is practically impossible to arrange the 7 apertures in sufficiently closely spaced relation to take full benefit of the'rnaximum fiow of cooling air and also afford a sufiiciently strong rack to give adequate support to the tubes.
A further disadvantage of heat exchangersemploying transverse racks 'or those with supporting bars between each row of tubes, has been the difficulty of removing and replacing individual tubes. The tubes must always be taken out from between the headersvand if for example, a tube in the-second or third row is defective, all
of the tubes in the rows above, must first be removed in order to removethe rack or spacing bars and gain access to thedefective tube.
It is'therefore the primary object-of-the present invention to overcome these disadvantages andto thisend Ihave provided a tube banding device which is adapted toembr-ace the peripheral edgesof the helical fin at predetermined-spaced intervals on the heat exchanger tubes. A strip of metal of a width to embrace several convolutions of a helical -fin is secured around the finned tube. Molten lead, solder, or other'suitablemetalhaving a low meltingpoint, is poured into a "hole irijthe'strip and flows intofthe spacesbetween certain'ofthe helical fins so as to provide a cylindiicalbodywithin the-bound- 7 2,775,433 Patented Dem--25,- 1956 ing strip which completely encircles the tube between the fins, after solidification. This solidified metallic body and the strip which bounds it forms a rigid'support between the fins and the tube proper, relieving the fins of all strain at these points. Furthermore, these metal-filled bands eliminate the need of otherspacing and'supporting means and greatly facilitate theremoval of defective tubes from a heat exchanger unit by minimizing the number of other tubes which must be removed to. gain access to the defective tube.
Another object of the invention is to arrange tube bandingdevices such as just described, at uniformly spaced intervals on each of a series of tubes to be used in a heat exchanger chamber, so that when the tubes are arranged in superimposed rows, the corresponding banding devices of adjacent tubes lie in abutting relation, the peripheries of the helical fins of adjacent tubes being spaced apart laterally for a distance determined by the thickness of the banding strip.
A further object of the invention is to provide a banding strip of modified cross sectional profile, for use when it is desired to space the tubes laterally a distance greater than the thickness of the banding strip.
With the above and other objects in view which will appear as the description proceeds, the invention consists in the novel features herein set forth, illustrated in the accompanying drawings and more particularly'pointed out in the appended claims.
Referring to the drawings in which numerals of like character designate similar parts throughout the several views,
Figure 1 is an end view of a heat exchanger chamber showing a series of finned tubes and their supporting bands.
Figure 2 is a transverse sectional view taken on line 2-2 of Figure 1, showing the lateral relationship of a series of tubes supported in accordance with this invention.
Figure 3 is a perspective view showing one form of banding strip before it is applied to the tube.
Figure 4 is an enlarged transverse sectional view through a finned tube, showing the banding strip in the course of application.
Figure 4A is detail view showing the joined ends of the strip after a preliminary bending and. before cornpressing.
Figure 5 is a diagrammatic illustration of one form of clamping device which may be employed in applying and locking the banding strip on the periphery of the helical fins.
. Figure 6 is a longitudinal sectional view through a section of finned tubing, showing a channeled banding strip of the type used to increase the distance between two adjacent tubes and Figure 7 is a similar view showing a plain banding strip.
In the drawings, the numeral '10 generally represents a conventional helical finned tube consisting of the central tube proper 11, the periphery of which is'encircled from end to end by a helical fin strip 12 which is firmly secured to the tube proper by various known methods. In accordance with this'invention a series of layers or horizontal rows of these tubes 10 are superimposed in a heat exchanger chamber A, the wall B of which is'o'pen toexpose the finned tubes so that cooling air may be forced or drawn through the chamber, over the tubes and between the spaces and convolutions of the helical fins. It will of course be understood that these parallel rows of tubes 10 are connected in series so that the fluid to be cooled can be drawn or forced continuously back and forth through the tubes until the entire'series has been encountered. i
As previously'indicated, in order to obtain 'themaximum benefit of the cooling air drawn through the chamber A, it is desirable to have the tubes arranged as closely together as possible while at the same time permitting suflicient space between the tubes to accommodate the passage of air therethrough. It is to facilitate this arrangement of tubes in close proximity, thatthe improved tube banding device or spacing support of the present invention is employed.
In its simplest form, as illustrated in Figure 7 this tube spacing support consists of a metal strip 13 of a length to completely encircle a finned tube in close engagement with the peripheral edges of of its helical fin and of suflicient width to overlie several of the convolutions of the fin. One particular method of applying and locking these banding strips around the peripheries of the helical fin will be described later on but at this point it is suflicient to note that a plurality of strips 13 are arranged in predetermined longitudinal spaced relation on each of the tubes to be placed in the chamber A, such spacing being uniform on all tubes so that when the tubes are superimposed the supporting contact between the tubes is borne by the peripheries of adjacent bands 13. In other words, each tube is supported by the engagement of its bands with the corresponding bands of adjacent tubes and the tubes are spaced apart laterally a distance determined by the thickness of the strip 13.
The metal of the strips 13 may vary in thickness to meet requirements of use, but it has been found that a strip .016 inch in thickness is generally satisfactory for this type of installation.
Each of the strips 13 is provided at a point intermediate its longitudinal edges, with an aperture 16 which as will later appear, is adapted to permit the pouring of molten lead or solder into the area bounded by the strip, which flows around the periphery of the tube proper 11 and fills the space between the convolutions of one or more of the fins with a metal mass or body 17. When the molten metal is introduced at substantially the central portion of the bounding strip, it has a tendency to initially flow'beyond the longitudinal limits required. However, the metal cools rapidly and progressively dams up the narrow spaces between the fins, so that the ultimate mass 17 fills only the desired number of spaces. It will be apparent that when this body of metal 17 has solidified, it forms a rigid supporting bushing or washer which extends radially from the tube 11 to the periphery of the helical fin and together with the surrounding strip 13, is adapted to bear considerable weight without in any way deforming the helical fins of adjacent tubes. Thus,
in order to take full benefit of the area of the chamber A, the various rows of tubes 10 can be arranged in staggered relation as shown in Figure 2, withoutdanger of injury to the helical fins of any of the tubes.
Ordinarily the bands or strips 13 have a plain crosssectional profile as shown in Figure 7 as the spacing afforded by the thickness of two contacting bands is sufficient. However, in some instances it is desirable to space the tubes as much as A inch apart. This cannot practically be accomplished by the use of thicker bands because bands of the required thickness would offer such a resistance when applied to the fins, that the fins would be deformed.
To increase the spacing between the individual tubes a greater distance than that afforded by the thickness of two contacting strips 13 I have designed a band of modified cross-section and in this connection attention is directed to Figures 3 and 6 of the drawings. Here it will be seen that the strip 13 is provided intermediate its longitudinal edges, with an outwardly directed channel 13a which extend-s the length of the strip and'when applied to the periphery of the helical fin provides an annular rib which extends radially beyond the fin engaging edges of the strip as best seen in Figure 6.
With this structure, the radical ribs 13a of any two adjacent bands, serve as lateral abutments and support the tubes at a spacing distance determined by the depth of the channels 13a. In this form, the body of metal 17 fills the space between the tube 11 and the web of the channel 13a and provides an extended rigid supporting washer or bushing.
With either form of band, the transverse thickness of the metal body 17 may vary from the distance between two adjacent fins, to the convolutions of several fins, depending upon the quantity of molten metal poured into the band.
While the strips may be applied to the tubes and locked in place in various ways, one method which has proven satisfactory, is illustrated in Figures 3, 4 and 5. Here it will be seen that the longitudinal extremities of the strip 13 are bent transversely to provide oppositely directed right angular connecting flanges 14 and 15. The straight strip as shown in Figure 3 is first placed in any suitable die or fixture to form a U-shape having a radius to accommodate the peripheral edges of a helical finned tube. The U-shaped band is then applied to the tube and its opposite ends are bent around the tube until the angular flanges 14 and 15 are brought into operative engagement as seen in Figure 4. At this point, a pair of suitable pliers, is applied to the engaging flanges 14-15, to bend the ends over slightly at reversed, coacting acute angles as shown in Fig. 4A. As will later appear, this angular arrangement facilitates the clamping of the band in tight engagement with the fins.
The finned tube 10 and the partially locked band 13 are then placed in a suitable fixture generally indicated by the letter C, to complete the locking of the strip on the helical fins. This fixture C preferably consists of a pair of upper and lower jaw members 18 and 19, hingedly connected as at 20 and having a handle 21 fixed to the upper jaw. The opposed faces of the jaws are respectively provided with concave recesses 22, having a radius to accommodate the peripheries of the finned tube with a band encircling the same. With the engaging ends 14-15 of the banding strip in the relationship shown in Fig. 4A, the recess 22 of jaw member 18 embraces the overlapping end of the strip and as the fixture jaws are closed, a lever action is started on the connected flanges of the strip. The closing jaws bend the connected flanges of the strip and as the underlying angular flange 14 is bent in a counter-clockwise are about the base of its angle, it pulls the over-lying angular flange 15 with it and tightens the band around the tube. Simultaneously with this constricting leverage action, the angular flanges 14-15 are flattened and embedded slightly into the periphery of the adjacent finned tube so as to slightly deform the fin at this point. This not only locks the ends of the strip 13 together but by embedding them slightly into the periphery of the fin tube, longitudinal movement of the strip on the fin, is prevented during the metal pouring operation.
This method of applying and locking the bands on the tube makes it possible to employ band materials such as aluminum, which do not readily lend themselves to soldering. Furthermore, it avoids the lumps of solder which would result from the use of a soldere djoint at the ends of the encircling band.
After the strip 13 has been applied in this manner, molten lead or solder is poured into the opening 16 and flows around the fin 12, completely filling one or two of the convolutions of the fin as previously described.
The channel 13a may be applied to the strip 13 in any suitable manner such for example as by a die or by rolling the channel into the strip and the depth of the channel can be predetermined to give the required tube spacing.
It will thus be seen that with the present invention, the difliculties heretofore encountered by the necessity of employing transverse spacers in the form of perforated sheets or racks, are eliminated and a maximum benefit of cooling surface for a given chamber area can be made available. Furthermore, these supporting bands or spacers greatly facilitate the installation and removal of individual finned tubes, as only those tubes immediately above a defective tube need be taken out to gain access to the tube to be removed and replaced.
While this invention was primarily designed for the purpose of spacing helical finned tubes in a heat exchanger chamber, it will be apparent that the use of these banding strips will also make it possible to transport tube sections from place to place, either in or out of containers, without injury to the fins.
From the foregoing it is believed that my invention may be readily understood by those skilled in the art without further description, it being borne in mind that numerous changes may be made in the details disclosed, without departing from the spirit of the invention as set forth in the following claims.
What I claim is:
1. In a finned tube for heat exchangers, including a tube portion having a series of radial fins, a radial spacing support forming device, comprising a band of flexible metal encircling a portion of said tube and engaging the peripheral edges of a group of adjacent fins, a central annular channel extending around said band, spaced radially from the peripheral edges of said fins, the meeting edges of said band being interconnected by overlapping, transverse flanges bent upon one another, and an opening through the web of said channel to facilitate the flowing of molten metal within the, band and between said fins, to provide when hardened, a mass of metal extending radially from the tube to the inner face of said web.
2. In a heat exchanger, including a chamber having 1 a series of parallel finned tubes arranged in superimtudinally spaced intervals on each tube, each support comprising a flexible metal band encircling said tube and engaging the peripheral edges of a group of adjacent finned portions, a central annular channel extending around each band, radially spaced from the peripheral edges of said fins, an annular mass of metal surrounding References Cited in the file of this patent UNITED STATES PATENTS 1,455,028 McCord May 15, 1923 1,782,260 Franquet et al Nov. 18, 1930 2,146,614 Bergdoll Feb. 7, 1939 2,179,530 Townsend Nov. 14, 1939 2,241,209 Lea May 6, 1941 2,243,593 Zallea May 27, 1941 2,362,694 Hill Nov. 14, 1944 2,402,209 Ryder June 18, 1946 2,404,575 Hill July 23, 1946 2,434,519 Raskin Jan. 13, 1948 2,535,669 Clay Dec. 26, 1950 FOREIGN PATENTS 110,125 Great Britain Oct. 11, 1917 532,968 Great Britain Feb. 4, 1941
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3180405A (en) * 1959-03-11 1965-04-27 Itt Condensers
US3420296A (en) * 1967-04-28 1969-01-07 Happy Co Finned tube protector band
US4095648A (en) * 1976-07-01 1978-06-20 Hudson Products Corporation Tube bundles
US20110289775A1 (en) * 2008-08-08 2011-12-01 Delphi Technologies, Inc. Method and apparatus for bending a micro-channel heat exchanger

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GB110125A (en) * 1917-06-09 1917-10-11 Arthur Tate Simpson Improvements in Apparatus for Cooling the Cylinders of Internal-combustion Engines.
US1455028A (en) * 1921-09-12 1923-05-15 Alvin C Mccord Air-cooled engine cylinder and method of making same
US1782260A (en) * 1928-06-16 1930-11-18 Franquet Jean Removable radiating device for the cooling of spark plugs
US2146614A (en) * 1936-07-31 1939-02-07 York Ice Machinery Corp Condenser and method of making the same
US2179530A (en) * 1935-12-18 1939-11-14 Albert J Townsend Method of forming finned tubing or the like
GB532968A (en) * 1938-09-01 1941-02-04 British Thomson Houston Co Ltd Improvements in and relating to tubular surface coolers
US2241209A (en) * 1940-06-08 1941-05-06 Edward S Lea Finned condenser tube
US2243593A (en) * 1938-08-12 1941-05-27 James P Zallea Heat exchanger
US2362694A (en) * 1942-02-02 1944-11-14 Calumet And Hecla Cons Copper Method of manufacturing tubes for heat exchange devices
US2402209A (en) * 1944-06-29 1946-06-18 Support for finned tubes
US2404575A (en) * 1943-06-21 1946-07-23 Calumet And Hecla Cons Copper Method of manufacturing finned tubes with support engaging bearing portions
US2434519A (en) * 1942-04-18 1948-01-13 Raskin Walter Heat exchange conduit with a spiral fin having a capillary groove
US2535669A (en) * 1945-08-07 1950-12-26 Hartford Nat Bank & Trust Co Electric discharge tube and means for cooling the anode thereof

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB110125A (en) * 1917-06-09 1917-10-11 Arthur Tate Simpson Improvements in Apparatus for Cooling the Cylinders of Internal-combustion Engines.
US1455028A (en) * 1921-09-12 1923-05-15 Alvin C Mccord Air-cooled engine cylinder and method of making same
US1782260A (en) * 1928-06-16 1930-11-18 Franquet Jean Removable radiating device for the cooling of spark plugs
US2179530A (en) * 1935-12-18 1939-11-14 Albert J Townsend Method of forming finned tubing or the like
US2146614A (en) * 1936-07-31 1939-02-07 York Ice Machinery Corp Condenser and method of making the same
US2243593A (en) * 1938-08-12 1941-05-27 James P Zallea Heat exchanger
GB532968A (en) * 1938-09-01 1941-02-04 British Thomson Houston Co Ltd Improvements in and relating to tubular surface coolers
US2241209A (en) * 1940-06-08 1941-05-06 Edward S Lea Finned condenser tube
US2362694A (en) * 1942-02-02 1944-11-14 Calumet And Hecla Cons Copper Method of manufacturing tubes for heat exchange devices
US2434519A (en) * 1942-04-18 1948-01-13 Raskin Walter Heat exchange conduit with a spiral fin having a capillary groove
US2404575A (en) * 1943-06-21 1946-07-23 Calumet And Hecla Cons Copper Method of manufacturing finned tubes with support engaging bearing portions
US2402209A (en) * 1944-06-29 1946-06-18 Support for finned tubes
US2535669A (en) * 1945-08-07 1950-12-26 Hartford Nat Bank & Trust Co Electric discharge tube and means for cooling the anode thereof

Cited By (5)

* Cited by examiner, † Cited by third party
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US3420296A (en) * 1967-04-28 1969-01-07 Happy Co Finned tube protector band
US4095648A (en) * 1976-07-01 1978-06-20 Hudson Products Corporation Tube bundles
US20110289775A1 (en) * 2008-08-08 2011-12-01 Delphi Technologies, Inc. Method and apparatus for bending a micro-channel heat exchanger
US9415436B2 (en) * 2008-08-08 2016-08-16 Mahle International Gmbh Method and apparatus for bending a micro-channel heat exchanger

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