US2611585A - Heat exchanger - Google Patents
Heat exchanger Download PDFInfo
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- US2611585A US2611585A US17899A US1789948A US2611585A US 2611585 A US2611585 A US 2611585A US 17899 A US17899 A US 17899A US 1789948 A US1789948 A US 1789948A US 2611585 A US2611585 A US 2611585A
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- tube
- heat
- fin
- members
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- 239000012530 fluid Substances 0.000 description 15
- 229910052751 metal Inorganic materials 0.000 description 9
- 239000002184 metal Substances 0.000 description 9
- 238000010276 construction Methods 0.000 description 7
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 239000000463 material Substances 0.000 description 2
- 239000003507 refrigerant Substances 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 229940000425 combination drug Drugs 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- OWFXIOWLTKNBAP-UHFFFAOYSA-N isoamyl nitrite Chemical compound CC(C)CCON=O OWFXIOWLTKNBAP-UHFFFAOYSA-N 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 229910000679 solder Inorganic materials 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
- F28F13/06—Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L53/00—Heating of pipes or pipe systems; Cooling of pipes or pipe systems
- F16L53/30—Heating of pipes or pipe systems
- F16L53/32—Heating of pipes or pipe systems using hot fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D7/00—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D7/0008—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one medium being in heat conductive contact with the conduits for the other medium
- F28D7/0016—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one medium being in heat conductive contact with the conduits for the other medium the conduits for one medium or the conduits for both media being bent
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D7/00—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D7/02—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being helically coiled
- F28D7/024—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being helically coiled the conduits of only one medium being helically coiled tubes, the coils having a cylindrical configuration
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F7/00—Elements not covered by group F28F1/00, F28F3/00 or F28F5/00
- F28F7/02—Blocks traversed by passages for heat-exchange media
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2255/00—Heat exchanger elements made of materials having special features or resulting from particular manufacturing processes
- F28F2255/14—Heat exchanger elements made of materials having special features or resulting from particular manufacturing processes molded
- F28F2255/146—Heat exchanger elements made of materials having special features or resulting from particular manufacturing processes molded overmolded
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2275/00—Fastening; Joining
- F28F2275/02—Fastening; Joining by using bonding materials; by embedding elements in particular materials
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S165/00—Heat exchange
- Y10S165/355—Heat exchange having separate flow passage for two distinct fluids
- Y10S165/442—Conduits
- Y10S165/451—Conduits including bent conduits
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4935—Heat exchanger or boiler making
- Y10T29/49362—Tube wound about tube
Definitions
- This invention relates to the transfer of heat from one fluid to another, and more in particular to highly efficient heat-exchange units and the method of makingthe same.
- An object of this invention is to provide a heat exchange assembly whereby heat is transferred from one material to another in an extremely heat-exchange units of the above character in a.
- the invention accordingly consists in the features of construction, combinations of elements, arrangements of parts and in the several steps and relation andorder of each of the same to one or more of the others, all as will be illustratively described herein, and the scope of the application of which will'be indicated in the fol:- lowing claims.
- FIG. 1 is a side plan view with portions broken away of a heat-exchange unit constituting one embodiment of the invention
- Figure 2 is an enlarged sectional view on the line 2-2 of Figure 1'; 1 A
- Figure 3 is an enlarged sectional view on the line 3--3 of Figure 1 showing only the central portion of the unit.
- Figure 4 is a top plan view. of the unit of Fig- 4O urel. v.
- an elongated cylinder or tube 2 has coiled about it a spiral tube 4 which formsfive complete'turns betweenits flareden'ds 6' and 8. .
- the ends of tube2 are reducedat l and"l2,,and except for these reduced ends, substantially the entire tube 2 and substantially the entire length of tube 4 are embedded in a cast aluminum block-l4; block I4 is cylindrical with two protrusions I6 and 18 at the ends surrounding theportions of tube'4' ad- A further 0b-"" jac'ent ends 6 and B.
- tube 4 is somewhat ovalin-*cross-section-,- having been originally circular in cross-section, and; hen having been deformedto the oval shape when wound into aspiral: r
- a heat-exchange assembly 20 Positioned within tube 2 is a heat-exchange assembly 20 which is formed by a central expanded tube 22 and a fin construction 24.
- the structure of fin construction 24 is best shown in Figure 3 where it is seen that it is formed from a corrugated sheet of metal bent into cylindrical form. There are 21 flat fin portions or corrugations, and the corrugations originally forming the edges of the sheet are-overlapped to form a single fin portion so that there are ten pairs of fiat fin portions symmetrically positioned in the annular space between tubes 2 and 22.
- Each of these flat fin portions is positioned substantially radially with respect to tubes 2 and 22, and in this form they extend tangentially with respect to an imaginary cylinder the diameter of which is approximately one-half the diameter of tube 22.
- tube 2 originally has its ends of the same diameter as its main body portion and tube 22 is of slightly smaller diameter than here appears; thus, fin construction 24 and tube 22 are readily positioned within tube 2.
- the two tubes and the fin construction then are held fixed and tube 22 is expanded to the diameter shown. This expanding is performed by drawing through the tube a cylindrical die of greater diameter than the original internal diameter of tube 22.
- tube 22 is expanded so that it continually presses outwardly against each fin portion, and expands the fin construction 24 with considerable force against the inner surface of tube 2.
- an extremely rigid heat transfer assembly is provided within tube 2, and each of the fin portions is in good heat contacting relationship with tube 2 as well as with tube 22.
- tube 4 which has-been wound into a spiral in a mandril, is slippedinto place.
- the tube assembly thus formed is then positioned within amold and the block of aluminumis cast around it.
- tube 4 is in intimate contact a with tube 2 and the aluminum fills into the cracks at the edges of tube 4 sufficiently to avoid any cavity.
- Block [4 not only provides for the even distribution and transfer of heat between tube '2 and tube'4, but the blockalso provides; a heat carry-over so that fluid is cooled evenly in one tube and heated evenly in another. tube without minor fluctuations in temperature in the one is a tendency for the entirewall of tube 2 tube maintained at substantially the same tempera-- ture.
- the gas passing through tube 2 is-carried in assembly within said annular chamber and comprising sheet metal corrugations each of which is substantially straight and is non-distortable and extends longitudinally of said chamber bridging the space between said rigid members and is connected to the next adjacent corrugation by a trough-like connecting portion-whichpresents a straight portion-in contact with a surface of one of said members, the distance between said rigid cylindrical members being such that each of said trough-like connecting portions is distorted and each of said trough-like connecting portions is subjected-to substantial compressive forces which I tare applied at the inner and outer peripheries of the passageways between the fins of fin construe tion 24 as well as through tube 22, and'there'is" a minimum resistance to flow.
- -tubes ⁇ , 4- and 22 and fin construction 24 are, of copper and the passageways for the refrigerant arefree of other materials such as solder andpthe like. to be. of: advantage in the adaptation of this invention to certain "uses. 7 r
- heat exchange apparatus of: the type whereina fiuid'i's subjected'to a heatv transfer operation, the combina tion of, a pair of concentrically positioned rig-idmembers; defining a substantially annular chamber for the flow-of the fluid to be subjectedfto a heat'transfer operation, and anannular'rnetallic fin assembly within said chamber and comprising sheet metal corrugations each of which issubstantially straight and .tion which presentsastraight portion incontact V wima surface of one-of said membera the distance between said rigid members :b 'eing.
- annular chamber both of which chambers are transfer operation, and an annular metallic fin for the flowof :flu-id-to. be” subjected to ,a hea-t said fin assembly by said rigid members.
- annular metallic finassembly within said chamber and comprising sheet metal corrugations each of which is substantially rectangular and straight and is not distorted and extends longitudinally of said chamber bridging the space between said rigid members andis connected to the next adjacent oorrugation by a trough-like connecting portion Which3presents a straight portion'in contact with atsurface of one of said cylindrical members,
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Thermal Sciences (AREA)
- Geometry (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Description
Sept. 23, 1952 c. BOLING HEAT EXCHANGER Filed March 30, 1948 INVENTOR Patented Sept. 23, 1952 HEAT EXCHANGER Cecil Boling, Brewster, N. Y., assignor to-The Heat-X-Changer. 00., Inc., Brewster, N. Y., a corporation of New York Application March 30, 1948, Serial No. 17,899
8 Claims. (Cl. 257241) This invention relates to the transfer of heat from one fluid to another, and more in particular to highly efficient heat-exchange units and the method of makingthe same.
An object of this invention is to provide a heat exchange assembly whereby heat is transferred from one material to another in an extremely heat-exchange units of the above character in a.
simple manner which is inexpensive and yet thoroughly practical in every respect. These and other objects will be in part obvious and in part pointed out below.
The invention accordingly consists in the features of construction, combinations of elements, arrangements of parts and in the several steps and relation andorder of each of the same to one or more of the others, all as will be illustratively described herein, and the scope of the application of which will'be indicated in the fol:- lowing claims. y
In the drawing: r Figure 1 is a side plan view with portions broken away of a heat-exchange unit constituting one embodiment of the invention;
Figure 2 is an enlarged sectional view on the line 2-2 of Figure 1'; 1 A
Figure 3 is an enlarged sectional view on the line 3--3 of Figure 1 showing only the central portion of the unit; and,
Figure 4 is a top plan view. of the unit of Fig- 4O urel. v.
Referring to Figure 1 of the drawing, an elongated cylinder or tube 2 has coiled about it a spiral tube 4 which formsfive complete'turns betweenits flareden'ds 6' and 8. .The ends of tube2 are reducedat l and"l2,,and except for these reduced ends, substantially the entire tube 2 and substantially the entire length of tube 4 are embedded in a cast aluminum block-l4; block I4 is cylindrical with two protrusions I6 and 18 at the ends surrounding theportions of tube'4' ad- A further 0b-"" jac'ent ends 6 and B. "As shown best in Figure 2.
Positioned within tube 2 is a heat-exchange assembly 20 which is formed by a central expanded tube 22 and a fin construction 24. The structure of fin construction 24 is best shown in Figure 3 where it is seen that it is formed from a corrugated sheet of metal bent into cylindrical form. There are 21 flat fin portions or corrugations, and the corrugations originally forming the edges of the sheet are-overlapped to form a single fin portion so that there are ten pairs of fiat fin portions symmetrically positioned in the annular space between tubes 2 and 22. Each of these flat fin portions is positioned substantially radially with respect to tubes 2 and 22, and in this form they extend tangentially with respect to an imaginary cylinder the diameter of which is approximately one-half the diameter of tube 22.
During manufacture, tube 2 originally has its ends of the same diameter as its main body portion and tube 22 is of slightly smaller diameter than here appears; thus, fin construction 24 and tube 22 are readily positioned within tube 2. The two tubes and the fin construction then are held fixed and tube 22 is expanded to the diameter shown. This expanding is performed by drawing through the tube a cylindrical die of greater diameter than the original internal diameter of tube 22. Thus, tube 22 is expanded so that it continually presses outwardly against each fin portion, and expands the fin construction 24 with considerable force against the inner surface of tube 2. In this way an extremely rigid heat transfer assembly is provided within tube 2, and each of the fin portions is in good heat contacting relationship with tube 2 as well as with tube 22.
After the expanding of tube 22 the ends of tube 2 are reduced and tube 4, which has-been wound into a spiral in a mandril, is slippedinto place. The tube assembly thus formed is then positioned within amold and the block of aluminumis cast around it. The aluminumbonds to the entire embedded surfaces of tubes 2 and 4 and provides excellent heat transfer relationship between the aluminum and each of these tubes. As shown best in Figure 3, tube 4 is in intimate contact a with tube 2 and the aluminum fills into the cracks at the edges of tube 4 sufficiently to avoid any cavity. Block [4 not only provides for the even distribution and transfer of heat between tube '2 and tube'4, but the blockalso provides; a heat carry-over so that fluid is cooled evenly in one tube and heated evenly in another. tube without minor fluctuations in temperature in the one is a tendency for the entirewall of tube 2 tube maintained at substantially the same tempera-- ture.
The gas passing through tube 2 is-carried in assembly within said annular chamber and comprising sheet metal corrugations each of which is substantially straight and is non-distortable and extends longitudinally of said chamber bridging the space between said rigid members and is connected to the next adjacent corrugation by a trough-like connecting portion-whichpresents a straight portion-in contact with a surface of one of said members, the distance between said rigid cylindrical members being such that each of said trough-like connecting portions is distorted and each of said trough-like connecting portions is subjected-to substantial compressive forces which I tare applied at the inner and outer peripheries of the passageways between the fins of fin construe tion 24 as well as through tube 22, and'there'is" a minimum resistance to flow. Some of the heat from tube 2 is picked up directly by the refrigerant gas, but the major portion of the heat passes by conduction from tube 2 to the various fin portionswith this heat transfer being facilitated'by the excellent contact which is provided betweenttube' 2 and the corrugation ridgesor fin edges. An additional amount of heat passes from the fin portionsto the gas while the remainder-of: theyheat is transferred from the fin to tube22 and thence to the gas around and mainly withinthistube. I n
In this embodiment-tubes}, 4- and 22 and fin construction 24 are, of copper and the passageways for the refrigerant arefree of other materials such as solder andpthe like. to be. of: advantage in the adaptation of this invention to certain "uses. 7 r
As many possible embodiments may bemade of the mechanical features of the above invention This has proved and as the art" hereindescribed might be varied in variousparts; allwithoutdeparting from the scope of the invention; itzis'to be understood that all matter hereina-bove set forth, or shown in the accompanying drawings is to be interpreted as illustrative and not ina limiting sense.
Iclaim: 1
V 1". In: heat exchange: apparatus of: the type whereina fiuid'i's subjected'to a heatv transfer operation, the combina tion of, a pair of concentrically positioned rig-idmembers; defining a substantially annular chamber for the flow-of the fluid to be subjectedfto a heat'transfer operation, and anannular'rnetallic fin assembly within said chamber and comprising sheet metal corrugations each of which issubstantially straight and .tion which presentsastraight portion incontact V wima surface of one-of said membera the distance between said rigid members :b 'eing. such that each ofsaid trough-like: connecting portions is distorted and-each of saidtroughelike connecting portions issubj'ectedcto substantial compressive forces which are applied at the inner and: outer peripheries of said fin assembly by said. rigid members. 7
H -2. In heat exchangelapparatus of the; type wherein" a fluid, is subjected to aheat transfer operation, the'zcombination of, a .pair of hollow concentrically positioned rigid cylindrical .mem-
bers defininga; cylindrical central chamber; and
an annular chamber. both of which chambers are transfer operation, and an annular metallic fin for the flowof :flu-id-to. be" subjected to ,a hea-t said fin assembly by said rigid members.
wherein 'a' fl'uidis subjected to a heat transfer operation, the combination of, a pair of concentrically positioned rigid cylindrical members defining-a substantially annular chamber between the-cuter surface ofthe smaller of said members and the inner surface of the larger of said members, saidmembers providing for the flow through saidannular chamber of thefluid to be subjected to a heat transfer. operation, an annular metallic finassembly within said chamber and comprising sheet metal corrugations each of which is substantially rectangular and straight and is not distorted and extends longitudinally of said chamber bridging the space between said rigid members andis connected to the next adjacent oorrugation by a trough-like connecting portion Which3presents a straight portion'in contact with atsurface of one of said cylindrical members,
being such thatreach .of said trough-like connecting portions is, distortedand each of said trough-like connecting portions 'is subjected ,to substantial compressive'forces-which are applied at-the inner and outer peripheries of said fin assembly by said cylindrical members, and means exteriorly of the larger of sai'dcylindrical .members and providing a' passageway-fora second fluid and providing for the transfer of heat between fluid fl'oWing-through' said cylindrical members and said secondfluid. 1
4. Inheat exchange apparatus of the type wherein a fluid is subjected to a heat transfer operation, the combination of, a pair ofconcentrically positioned hollow rigid cylindrical members defining a substantially annular chamber between the outersurface of the smaller of said members and the inner surface of the larger of said members and a cylindrical passageway within the smaller of said memberssaid members providing for the flow through said annular chamber and said" cylindrical passageway of fluid to be subjected to'a heat transferoperation, an annular metallic fin assembly within said chamber and comprising sheet metal corruga= tio'ns. each of which isfsubstantially rectangular and straight and is j bt j distorted and extends longitudinally ofsaid'charfiber bridging the space between 'said rigid'inember's and is connected toji the nextadjacentcorrugation :bya trough like;v connecting portion which resents a straight portion in contactwith a surface ofone of said cylindrical iifeirlbers, the distance between said cylindrical members being such that each of said trough dike connecting: portions is distorted and each of said tro'ugh like connecting portions, is subjected =tosubstantial compressive forces which are applied atf the inner" anapu er peripheries of said fin assemblyby s ai d'cylind'ri cal members, and heat transfer means" in intimate contact with the outer surface of the larger of said cylindrical members and providing a. passageway for a second fluid and providing for the transfer of heat between fluid flowing through said cylindrical members and said second fluid.
5. In heat exchange apparatus of the type wherein a fluid is subjected to a heat transfer operation, the combination of, a pair of concentrically positioned rigid members defining a substantially annular chamber for the fiow of the fluid to be subjected to a. heat transfer operation, an annular metallic fin assembly within said chamber and comprising sheet metal corrugations each of which is substantially straight and is non-distortable and extends longitudinally of said chamber bridging the space between said rigid members and is connected to the next adjacent corrugation by a trough-like connecting portion which presents a straight portion in contact with a surface of one of said members, the distance between said rigid members being such that each of said trough-like connecting portions is distorted and each of said troughlike connecting portions is subjected to substantial compressive forces which are applied at the inner and outer peripheries of said fin assembly by said rigid members, a tube formed into a spiral and closely hugging the outer surface of the larger of said rigid members, and a block of aluminum substantially enclosing said larger rigid member and said tube.
6. Apparatus as described in claim 5 wherein said spiral tube is substantially oval in crosssection, and wherein said fin assembly is formed by a single sheet of corrugated metal.
7. Apparatus as described in claim 6 wherein said rigid members are sheet metal cylinders and the larger of said cylinders has its ends reduced in diameter and projecting from said block of a uminium.-
8. In heat exchange apparatus of the type wherein a fluid is subjected to a heat transfer operation, the combination of, a pair of concentrically positioned rigid members defining a substantially annular chamber for the flow of the fluid to be subjected to a heat transfer operation, and an annular metallic fin assembly within said chamber and comprising a sheet of metal formed into corrugations each of which is substantially rectangular and straight and is non-distortable and extends longitudinally of said chamber bridging the space between said rigid members, each of said corrugations being connected to the next adjacent corrugation by a trough-like connecting portion which presents a straight portion in contact with a surface of one of said members, the distance between said rigid members being such that each of said troughlike connecting portions is distorted from its original shape and each of said trough-like connecting portions is subjected to substantial compressive forces which are applied at the inner and outer peripheries of said fin assembly by said rigid members.
CECIL BOLING.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 660,292 Durr Oct. 23, 1900 1,270,198 Parkhurst June 18, 1918 1,584,772 Hyde May. 18, 1926 2,004,389 Jones June 11, 1935 2,206,826 Hopper July 2, 1940 2,324,395 Hoop July 13, 1943
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US17899A US2611585A (en) | 1948-03-30 | 1948-03-30 | Heat exchanger |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US17899A US2611585A (en) | 1948-03-30 | 1948-03-30 | Heat exchanger |
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US2611585A true US2611585A (en) | 1952-09-23 |
Family
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US17899A Expired - Lifetime US2611585A (en) | 1948-03-30 | 1948-03-30 | Heat exchanger |
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Cited By (51)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2693026A (en) * | 1950-02-17 | 1954-11-02 | Modine Mfg Co | Method of making concentric tubes with radial fins |
US2703921A (en) * | 1949-04-14 | 1955-03-15 | Brown Fintube Co | Method of making internally finned tubes |
US2722733A (en) * | 1950-11-08 | 1955-11-08 | Cleaver Brooks Co | Method of making heat exchanger tube |
US2876630A (en) * | 1955-02-18 | 1959-03-10 | Dunham Bush Inc | Refrigeration system including defrosting apparatus |
US2985435A (en) * | 1956-08-27 | 1961-05-23 | Gross Frank Robert | Heat-transfer apparatus |
US3163996A (en) * | 1963-03-11 | 1965-01-05 | Whirlpool Co | Tubular evaporator |
US3173196A (en) * | 1959-11-02 | 1965-03-16 | Fromson H A | Method of producing a double-walled tube with one of the tubes having integral therewith projecting fin means radially separating the tubes |
US3197975A (en) * | 1962-08-24 | 1965-08-03 | Dunham Bush Inc | Refrigeration system and heat exchangers |
US3201861A (en) * | 1960-03-31 | 1965-08-24 | Fromson H A | Method of making a double-walled tube |
US3250322A (en) * | 1964-02-07 | 1966-05-10 | Texas Instruments Inc | Corrosive fluid heat exchanger |
US3269422A (en) * | 1963-01-09 | 1966-08-30 | Moore & Co Samuel | Composite tubing product and apparatus and method for manufacturing the same |
US3315703A (en) * | 1967-04-25 | Matthews etal composite tubing product | ||
US3400737A (en) * | 1966-07-07 | 1968-09-10 | Moore & Co Samuel | Composite tubing product and apparatus for manufacturing the same |
US3498371A (en) * | 1967-06-12 | 1970-03-03 | Alfred E Zygiel | Heat transfer device |
US3857680A (en) * | 1970-11-03 | 1974-12-31 | Getters Spa | Catalyst cartridge |
US3890104A (en) * | 1970-11-03 | 1975-06-17 | Getters Spa | Catalytic cartridge |
US4015567A (en) * | 1975-05-12 | 1977-04-05 | Jan Wassing | Gasoline preheater |
US4094358A (en) * | 1975-04-02 | 1978-06-13 | Societe Anonyme Francaise Du Ferodo | Liquid cooling apparatus |
DE3114556A1 (en) * | 1981-03-10 | 1982-09-30 | Injecta AG, Teufenthal, Aargau | Liquid-cooled electric subassembly, and method for producing it |
US4397288A (en) * | 1981-05-01 | 1983-08-09 | Phillips Temro, Inc. | Diesel fuel warmer |
US4559999A (en) * | 1983-04-08 | 1985-12-24 | Shiley, Inc. | Heat exchanger for extracorporeal circuit |
US4643001A (en) * | 1984-07-05 | 1987-02-17 | Air Products And Chemicals, Inc. | Parallel wrapped tube heat exchanger |
EP0305854A2 (en) * | 1987-08-29 | 1989-03-08 | Müller, Jörg Dieter Fritz | Heating device for diesel oil or heating oil for an engine or a burner |
US4917179A (en) * | 1987-05-22 | 1990-04-17 | Beckman Instruments, Inc. | Thermoelectric cooling design |
US5596973A (en) * | 1995-06-05 | 1997-01-28 | Grice; Franklin R. | Fuel expander |
US5724478A (en) * | 1996-05-14 | 1998-03-03 | Truheat Corporation | Liquid heater assembly |
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US6363737B1 (en) * | 2000-03-07 | 2002-04-02 | Robby D. Raney | Heat exchanger and method of use therefor |
US20040154787A1 (en) * | 2003-02-06 | 2004-08-12 | Modine Manufacturing Company | Heat exchanger |
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US20060205332A1 (en) * | 2005-03-11 | 2006-09-14 | Flow International Corporation | Method to remove meat from crabs |
US7220381B2 (en) | 2001-06-15 | 2007-05-22 | Avure Technologies Incorporated | Method for high pressure treatment of substances under controlled temperature conditions |
US20070119578A1 (en) * | 2004-02-06 | 2007-05-31 | Yutaka Shibata | Hot water supply heat exchanger |
US20080149309A1 (en) * | 2005-03-25 | 2008-06-26 | Tsinghua University | Hot Water Heat Transfer Pipe |
US20090038302A1 (en) * | 2006-03-16 | 2009-02-12 | Takeshi Yamada | Exhaust gas heat recovery device |
US20100175689A1 (en) * | 2009-01-13 | 2010-07-15 | Hamilton Sundstrand Corporation | Catalyzed hot gas heating system for pipes |
US20110280554A1 (en) * | 2010-05-12 | 2011-11-17 | Schlipf Andreas | High-performance flow heater |
US20120063754A1 (en) * | 2010-09-13 | 2012-03-15 | Tokyo Electron Limited | Liquid Heating Unit, Liquid Processing Apparatus Including the Same, and Liquid Processing Method |
US20140367476A1 (en) * | 2013-06-18 | 2014-12-18 | Airbus Helicopters | System for heating the cabin of an aircraft provided with an annular heat exchanger around the exhause nozzle |
US20150122459A1 (en) * | 2013-11-06 | 2015-05-07 | Carrier Corporation | Brazed heat exchanger design |
JP2015152226A (en) * | 2014-02-14 | 2015-08-24 | 日本電熱株式会社 | liquid heating device |
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US10514210B2 (en) | 2014-12-31 | 2019-12-24 | Ingersoll-Rand Company | Fin-tube heat exchanger |
US20200079544A1 (en) * | 2017-05-10 | 2020-03-12 | Gea Food Solutions Weert B.V. | Heating means for a flow wrapper |
US10995998B2 (en) * | 2015-07-30 | 2021-05-04 | Senior Uk Limited | Finned coaxial cooler |
US11333440B2 (en) * | 2019-12-07 | 2022-05-17 | John Richard Nobile | Compact thin-film heat recovery device for showers |
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US2703921A (en) * | 1949-04-14 | 1955-03-15 | Brown Fintube Co | Method of making internally finned tubes |
US2693026A (en) * | 1950-02-17 | 1954-11-02 | Modine Mfg Co | Method of making concentric tubes with radial fins |
US2722733A (en) * | 1950-11-08 | 1955-11-08 | Cleaver Brooks Co | Method of making heat exchanger tube |
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US2985435A (en) * | 1956-08-27 | 1961-05-23 | Gross Frank Robert | Heat-transfer apparatus |
US3173196A (en) * | 1959-11-02 | 1965-03-16 | Fromson H A | Method of producing a double-walled tube with one of the tubes having integral therewith projecting fin means radially separating the tubes |
US3201861A (en) * | 1960-03-31 | 1965-08-24 | Fromson H A | Method of making a double-walled tube |
US3197975A (en) * | 1962-08-24 | 1965-08-03 | Dunham Bush Inc | Refrigeration system and heat exchangers |
US3269422A (en) * | 1963-01-09 | 1966-08-30 | Moore & Co Samuel | Composite tubing product and apparatus and method for manufacturing the same |
US3163996A (en) * | 1963-03-11 | 1965-01-05 | Whirlpool Co | Tubular evaporator |
US3250322A (en) * | 1964-02-07 | 1966-05-10 | Texas Instruments Inc | Corrosive fluid heat exchanger |
US3400737A (en) * | 1966-07-07 | 1968-09-10 | Moore & Co Samuel | Composite tubing product and apparatus for manufacturing the same |
US3498371A (en) * | 1967-06-12 | 1970-03-03 | Alfred E Zygiel | Heat transfer device |
US3857680A (en) * | 1970-11-03 | 1974-12-31 | Getters Spa | Catalyst cartridge |
US3890104A (en) * | 1970-11-03 | 1975-06-17 | Getters Spa | Catalytic cartridge |
US4094358A (en) * | 1975-04-02 | 1978-06-13 | Societe Anonyme Francaise Du Ferodo | Liquid cooling apparatus |
US4015567A (en) * | 1975-05-12 | 1977-04-05 | Jan Wassing | Gasoline preheater |
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US4397288A (en) * | 1981-05-01 | 1983-08-09 | Phillips Temro, Inc. | Diesel fuel warmer |
US4559999A (en) * | 1983-04-08 | 1985-12-24 | Shiley, Inc. | Heat exchanger for extracorporeal circuit |
US4643001A (en) * | 1984-07-05 | 1987-02-17 | Air Products And Chemicals, Inc. | Parallel wrapped tube heat exchanger |
US4917179A (en) * | 1987-05-22 | 1990-04-17 | Beckman Instruments, Inc. | Thermoelectric cooling design |
EP0305854A2 (en) * | 1987-08-29 | 1989-03-08 | Müller, Jörg Dieter Fritz | Heating device for diesel oil or heating oil for an engine or a burner |
EP0305854A3 (en) * | 1987-08-29 | 1989-11-15 | Müller, Jörg Dieter Fritz | Heating device for diesel oil or heating oil for an engine or a burner |
US5596973A (en) * | 1995-06-05 | 1997-01-28 | Grice; Franklin R. | Fuel expander |
US5724478A (en) * | 1996-05-14 | 1998-03-03 | Truheat Corporation | Liquid heater assembly |
US20010041206A1 (en) * | 1998-06-18 | 2001-11-15 | Chidambaram Raghavan | Method and apparatus for pressure processing a pumpable substance |
EP1035387A1 (en) | 1999-03-10 | 2000-09-13 | Speciality Equipment Companies Inc. | High efficiency refrigeration system |
US6253573B1 (en) | 1999-03-10 | 2001-07-03 | Specialty Equipment Companies, Inc. | High efficiency refrigeration system |
EP1052469A1 (en) * | 1999-05-11 | 2000-11-15 | Euradus | Heat exchange module |
FR2793547A1 (en) * | 1999-05-11 | 2000-11-17 | Euradus | THERMAL EXCHANGE MODULE |
US6363737B1 (en) * | 2000-03-07 | 2002-04-02 | Robby D. Raney | Heat exchanger and method of use therefor |
US6804459B2 (en) * | 2001-06-15 | 2004-10-12 | Flow International Corporation | Method and apparatus for changing the temperature of a pressurized fluid |
US7220381B2 (en) | 2001-06-15 | 2007-05-22 | Avure Technologies Incorporated | Method for high pressure treatment of substances under controlled temperature conditions |
US20040154787A1 (en) * | 2003-02-06 | 2004-08-12 | Modine Manufacturing Company | Heat exchanger |
US6988542B2 (en) | 2003-02-06 | 2006-01-24 | Modine Manufacturing Company | Heat exchanger |
WO2004072563A1 (en) * | 2003-02-06 | 2004-08-26 | Modine Manufacturing Company | Heat exchanger |
US8162034B2 (en) | 2003-07-28 | 2012-04-24 | Bonner Michael R | Thermal inner tube |
US20060225865A1 (en) * | 2003-07-28 | 2006-10-12 | Bonner Michael R | Thermal inner tube |
WO2005013329A3 (en) * | 2003-07-28 | 2005-06-02 | St Clair Systems Inc | Thermal inner tube |
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US20070119578A1 (en) * | 2004-02-06 | 2007-05-31 | Yutaka Shibata | Hot water supply heat exchanger |
US20060205332A1 (en) * | 2005-03-11 | 2006-09-14 | Flow International Corporation | Method to remove meat from crabs |
US8215380B2 (en) * | 2005-03-25 | 2012-07-10 | Tsinghua University | Hot water heat transfer pipe |
US20080149309A1 (en) * | 2005-03-25 | 2008-06-26 | Tsinghua University | Hot Water Heat Transfer Pipe |
US20090038302A1 (en) * | 2006-03-16 | 2009-02-12 | Takeshi Yamada | Exhaust gas heat recovery device |
US8297049B2 (en) * | 2006-03-16 | 2012-10-30 | Toyota Jidosha Kabushiki Kaisha | Exhaust gas heat recovery device |
US20100175689A1 (en) * | 2009-01-13 | 2010-07-15 | Hamilton Sundstrand Corporation | Catalyzed hot gas heating system for pipes |
US8925543B2 (en) * | 2009-01-13 | 2015-01-06 | Aerojet Rocketdyne Of De, Inc. | Catalyzed hot gas heating system for pipes |
US20110280554A1 (en) * | 2010-05-12 | 2011-11-17 | Schlipf Andreas | High-performance flow heater |
US20120063754A1 (en) * | 2010-09-13 | 2012-03-15 | Tokyo Electron Limited | Liquid Heating Unit, Liquid Processing Apparatus Including the Same, and Liquid Processing Method |
US8670656B2 (en) * | 2010-09-13 | 2014-03-11 | Tokyo Electron Limited | Liquid heating unit, liquid processing apparatus including the same, and liquid processing method |
US20140367476A1 (en) * | 2013-06-18 | 2014-12-18 | Airbus Helicopters | System for heating the cabin of an aircraft provided with an annular heat exchanger around the exhause nozzle |
US9623723B2 (en) * | 2013-06-18 | 2017-04-18 | Airbus Helicopters | System for heating the cabin of an aircraft provided with an annular heat exchanger around the exhaust nozzle |
US20150122459A1 (en) * | 2013-11-06 | 2015-05-07 | Carrier Corporation | Brazed heat exchanger design |
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US10514210B2 (en) | 2014-12-31 | 2019-12-24 | Ingersoll-Rand Company | Fin-tube heat exchanger |
US10995998B2 (en) * | 2015-07-30 | 2021-05-04 | Senior Uk Limited | Finned coaxial cooler |
US20180051934A1 (en) * | 2016-08-16 | 2018-02-22 | Hamilton Sundstrand Corporation | Heat exchangers with multiple flow channels |
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