US3265127A - Heat exchange element - Google Patents
Heat exchange element Download PDFInfo
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- US3265127A US3265127A US317638A US31763863A US3265127A US 3265127 A US3265127 A US 3265127A US 317638 A US317638 A US 317638A US 31763863 A US31763863 A US 31763863A US 3265127 A US3265127 A US 3265127A
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- louvers
- fins
- fin
- heat exchange
- adjacent
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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
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/126—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element consisting of zig-zag shaped fins
- F28F1/128—Fins with openings, e.g. louvered fins
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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
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/24—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely
- F28F1/32—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely the means having portions engaging further tubular elements
- F28F1/325—Fins with openings
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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
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/34—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending obliquely
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- 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
- Y10T29/49373—Tube joint and tube plate structure
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- 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
- Y10T29/49377—Tube with heat transfer means
- Y10T29/49378—Finned tube
Definitions
- This invention relates to heat exchange devices and particularly to a novel heat exchange element which forms an integral part of a fin assembly or spacer strip for use in a device wherein heat exchange is effected between fluids, as, for example, in automobile radiators and heaters. More particularly, this invention relates to a louvered heat exchange fin wherein adjacent louvers extend from opposite sides of the otherwise essentially planar body.
- the fin of this invention is hereinafter described in relation to its use as a part of the main cooling system of an engine.
- an engine cooling radiator ordinarily includes an inlet'tank and an outlet tank for suitable connection with the water jacket of the engine, and a core or heat dissipating unit interposed between the two tanks for the travel of water in thin streams from one tank to the other through a number of spaced passageways or water tubes of suitable heat exchange material. Between each pair of these water conduits flows an air stream to take up or absorb heat carried by the water.
- a heat exchange and spacer element comprising a thin strip of suitable metal or alloy, e.g., copper, brass, etc., is interposed between the water tubes and folded back and forth so as to divide the air passageway into a multiplicity of air cells of substantially equal dimensions.
- the portion extending between folds or major corrugations may be referred to as a heat exchange fin, a fin proper or merely a fin.
- the material extending between each of two adjacent fins may be referred to as a connecting member, it being understood that the fin strip is of unitary construction.
- FIGURE 1 is a partially completed front view of an automobile radiator illustrating one use for the fin assembly of this invent-ion;
- FIGURE 2 is a perspective view of a portion of a fin assembly or spacer strip constructed in accordance with the present invention
- FIGURE 3 is a front elevational view of the fin structure shown in FIGURE 2;
- FIGURE 4 is a semidiagrammatic transverse section Patented August 9, 1966 taken approximately on line 4-4 of FIGURE 3 showing the alignment of alternating louvers in relation to the planar base of the fin of which they form a part and in relation to the corresponding louvers of adjacent fins;
- FIGURE 5 is a fragmentary perspective View of a portion of an automobile radiator employing the fin strip of this invention and illustrating the alternation of converging and diverging sections within the air passageways formed by the fin strips and the adjacent water tubes;
- FIGURE 6 is a representative flow diagram illustrating the flow of air through and between adjacent air passageways formed with the fin strip of this invention.
- the radiator assembly includes a heat dissipating unit of core 11 having at opposite ends a top tank or inlet header 13 and a bottom tank or outlet header 15, adapted for connection, respectively, with the discharge and intake conduits of a cylinder block cooling jacket.
- the core is made up of a number of fluid passageways or water tubes 17 spaced apart by fin strips or heat exchange spacer strips 19.
- the fin strip shown in the drawing is of folded or corrugated outline providing a series of fins 21 bet-ween the folds or connecting members 23.
- the strips 19 therefore extend between each pair of water tubes 17 and divide the space into a plurality of relatively small air cells, passageways or conduits 25.
- the opposite edges or front and rear faces of the core assembly are dipped first in a fiux and then in molten solder to set the margins or ends of the walls of the water tubes where necessary and to join the fin strips to the walls.
- Pin 21 comprises a planar base or body having a plurality of transversely aligned louvers 27 which may be formed by slitting the planar base and turning the metal abutting one major side of the opening out of the base plane.
- the slits or windows 29 place adjacent passageways in fluid communication with each other and preferably are substantially equidistant from each other, the edge opposite the corresponding louver being substantially perpendicular to the longitudinal axis of the fin proper and substantially parallel to the longitudinal axis of the fin strip.
- alternate louvers are turned from the base plane in opposite directions. The order of louver alignment on adjacent fins is reversed.
- 'Two adjacent fins form two sides of an air passageway which is completed by one of the water tubes and the connecting element between such fins.
- This passageway is substantially triangular in cross section with such section taken on or along a line parallel to the longitudinal axis of the fin strip.
- the alternation of louver alignment on each fin with a reverse alignment on the fin forming the opposing wall of the passageway provides a passageway that is alternately converging and diverging in width. Since this alternation continues with each succeeding fin within the fin strip, a row of passageways are provided wherein the converging sections of a given passageway are in line with the diverging sections of the adjacent passageways. This arrangement provides a maximum number of converging and diverg ing passageways with any given number of louvers per fin.
- louvers stimulates turbulence by wake flow from the converging louver and wall effect of the diverging louver.
- the alternately constricted and expanded air passages together with the inner communication between such passages provide a high level of turbulence with alternation of positive and negative pressure gradients within each passageway, such alternation being reversed in adjacent passageways.
- level of turbulence as employed herein is interchangeable with intensity of turbulence and refers to the root mean square of the instantaneous velocity fluctuation divided by the mean velocity.
- Example Fins designed in accordance with this invention were tested with a variety of conventional radiator fin designs to evaluate their effectiveness for creating turbulence in an air stream.
- a hot wire anemometer is an instrument by which the velocities in a moving fluid are determined by the cooling effect of the stream on a thin electrically heated element positioned therein.
- the sensing element was of platinum and had an average diameter of 0.00015 inch.
- the anemometer includes a probe to hold the sensing element in the fluid stream, a controlled source for electrically heating the sensing element, precision equipment for measuring D.C. electrical values, e.g., a precision galvanometer or bridge circuit, an amplifier and a recording device for measuring A.C.
- a second control fin employed planar fins with terminal louvers extending outward from one side of the base plane, a center portion supporting louvers turned from the base plane in a direction opposite the terminal louvers and intermediate louvers on either side of the center portion each of which are pivoted from the planar body so that each extended through the base plane to protrude on the two opposite sides thereof.
- This fin is hereinafter termed Fin B.
- a third control fin was a species of the common serpentine or bump fin wherein the width of the winding air passageways are essentially constant. This fin is hereinafter termed Fin C.
- the control fins provided passageways illustrated by the following profiles:
- the counterlouvered fins of this invention provide a high level of turbulence when interposed in an air stream and thus permit high utilization of the air stream for heat exchange.
- a heat exchange and spacer element for use in a passageway between and in heat exchange relationship with conduits of a heat exchange device, said element comprising a corrugated metal strip having a plurality of slitted fins separated by connecting members and being constructed and arranged to divide said passageway into Fin B a plurality of smaller intercommunicating air passageways of substantially equal dimensions, said fins consisting of a substantially planar base having a plurality of slits therein extending through and in transverse relationship to the longitudinal axis of said fins with each end thereof terminating within said planar base and a plurality of louvers turned out of the base plane adjacent said slits in a manner such that alternate louvers extend from said base plane on opposite sides thereof, the directional alternation of the louvers of each fin being in reverse order with respect to the alternation of the louvers of the fins adjacent thereto thereby providing said air passageways with alternately converging and diverging sections.
- a heat exchange and spacer element for use in a passageway between and in heat exchange relationship with conduits of a heat exchange device, said element comprising a folded metal strip having a plurality of slitted fins separated by connecting members and being constructed and arranged to divide said passageway into a plurality of smaller intercommunicating air passageways of substantially equal dimensions, said fins consisting of a substantially planar base having a plurality of slits therein extending through and in transverse relationship to the longitudinal axis of said fins with each end thereof terminating within said planar base and a plurality of louvers turned out of the base plane adjacent said slits in a manner such that alternate louvers extend from said fin on opposites sides thereof, the directional alternation of the louvers of each fin being in reverse order with respect to the alternation of the louvers of the fins adjacent thereto thereby providing said air passageways with alternately converging and diverging sections, the alternation of said converging and diverging sections in a given air passageway being in reverse order with respect to
- a tube separator comprising a strip of metal providing heat exchange surface common to a pair of adjacent tubes and dividing the space there between into a plurality of intercommunicating air pas sageways, said strip of metal comprising a plurality of slitted fins separated by connecting members, said fins consisting of a substantially planar base having a plurality of slits therein extending through and in transverse relationship to the longitudinal axis of said fins with each end thereof terminating within said planar base and a plurality of louvers turned out of the base plane adjacent said slits in a manner such that alternate louvers extend from said fin on opposite sides thereof, the directional alternation of the louvers of each fin being in reverse order with respect to the alternation of the louvers of the fins adjacent thereto thereby providing said air passageways with alternately converging and diverging sections.
- a tube separator comprising a Fin C strip of metal providing heat exchange surface common to a pair of adjacent tubes and dividing the space therebetween into a plurality of intercommunicating air passageways, said strip of metal comprising a plurality of slitted fins separated by connecting members, said fins consisting of a substantially planar base having a plurality of slits therein extending through and in transverse relationship to the longitudinal axis of said fins with each end thereof terminating within said planar base and a plurality of louvers turned out of the base plane adjacent said slits in a manner such that alternate louvers extend from said fin on opposite sides thereof, the directional alternation of the louvers of each fin being in reverse order with respect to the alternation of the louvers of the fins adjacent thereto thereby providing said air passageways with alternately converging and diverging sections, the alternation of said converging and diverging sections in a given air passageway being in reverse order with respect to the converging and diverging sections of the air
- a tube separator comprising a strip of metal providing heat exchange surface common to a pair of adjacent tubes and dividing the space therebetween into a plurality of intercommunicating air passageways, said strip of metal comprising -a plurality of slitted fins separated by connecting members, said fins consisting of a substantially planar Ibase having a plurality of slits therein extending through and intransverse relationship to the longitudinal axis of said fins with each end thereof terminating within said planar base and a plurality of louvers turned out of the base plane adjacent said slits in a manner such that alternate louvers extend from said fin on opposite sides thereof, the directional alternation of the louvers of each fin being in reverse order with respect to the alternation of the louvers of the fins adjacent thereto thereby providing said air passageways with alternately converging and diverging sections.
- a tube separator comprising a strip of metal providing heat exchange surface common to a pair of adjacent tubes and dividing the space therebetween into a plurality of intercommunicating air passageways, said strip of metal comprising a plurality of slitted fins separated by connecting members, said fins consisting of a substantially planar base having a plurality of slits therein extending through and in transverse relationship to the longitudinal axis of said fins with each end thereof terminating within said planar base and from which a plurality of louvers turned out of the base plane adjacent said slits in a manner such that alternate louvers extend from said fin on opposite sides thereof, the directional alternation of the louvers of each fin being in reverse order with respect to the alternation of the louvers of the fins adjacent thereto thereby providing said air passageways with alternately converging and diverging sections, the alternation of said converging and diverging sections in a given air passageway being in reverse order with respect to the converging and diverging sections of the air
- a heat exchange and spacer element for use in a passageway between and in heat exchange relationship with conduits of a heat exchange device, said element comprising a corrugated metal strip having a plurality of slitted fins separated by connecting members and being constructed and arranged to divide said passageway into a plurality of smaller intercommunicating air passageways of substantially equal dimensions, each of said fins consisting of a substantially planar base having a plurality of slits therein extending through and in transverse relationship to the longitudinal axis of said fins with each end thereof terminating within said planar base and a single louver associated with each of said slits, each of said louvers being integral with said planar base, describing one side of the slit with which it is associated, and turned out of the base plane of said planar base in a manner such that alternate louvers of a given fin extend from said base plane on opposite sides thereof, the directional alternation of the louvers of each fin being in reverse order with respect to the alternation of the louvers of the fins adjacent there
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- Engineering & Computer Science (AREA)
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- Thermal Sciences (AREA)
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- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Description
Aug. 9, 1966 H. A. NICK OL ETAL HEAT EXCHANGE ELEMENT 2 Sheets-Sheet 1 Filed Oct. 21, 1963 HE/Vky A i CK L 1966 H. A. NICKOL ETAL. 3, 65, 7
HEAT EXCHANGE ELEMENT Filed Oct. 21, 1963 2 Sheets-Sheet 2 w R. 7M4
ATTOR/VIYS United States Patent 3,265,127 HEAT EXCHANGE ELEMENT Henry A. Nickol, Livonia, and Sylvester J. Battisti, Wayne, Mich, assignors to Ford Motor Company, Dear-born, MiclL, a corporation of Delaware Filed Oct. 21, 1963, Ser. No. 317,638 7 Claims. (Cl. 165-152) This invention relates to heat exchange devices and particularly to a novel heat exchange element which forms an integral part of a fin assembly or spacer strip for use in a device wherein heat exchange is effected between fluids, as, for example, in automobile radiators and heaters. More particularly, this invention relates to a louvered heat exchange fin wherein adjacent louvers extend from opposite sides of the otherwise essentially planar body.
For purposes of illustration, the fin of this invention is hereinafter described in relation to its use as a part of the main cooling system of an engine.
Although details of construction may vary, an engine cooling radiator ordinarily includes an inlet'tank and an outlet tank for suitable connection with the water jacket of the engine, and a core or heat dissipating unit interposed between the two tanks for the travel of water in thin streams from one tank to the other through a number of spaced passageways or water tubes of suitable heat exchange material. Between each pair of these water conduits flows an air stream to take up or absorb heat carried by the water. A heat exchange and spacer element comprising a thin strip of suitable metal or alloy, e.g., copper, brass, etc., is interposed between the water tubes and folded back and forth so as to divide the air passageway into a multiplicity of air cells of substantially equal dimensions. The portion extending between folds or major corrugations may be referred to as a heat exchange fin, a fin proper or merely a fin. The material extending between each of two adjacent fins may be referred to as a connecting member, it being understood that the fin strip is of unitary construction.
It is one object of this invention to provide an improved fin structure for use in a heat exchange device as hereinafter described which will increase the heat absorption of an air stream passing through such device by increasing the turbulence level of the air flow therethrough.
It is another object of this invention to provide an improved heat exchange structure wherein adjacent fins each have louvers aligned so as to provide an air passageway therebetween of alternating diverging and converging sections.
Other objects and advantages of this invention will be obvious to those skilled in the art from the following description and the accompanying drawings wherein:
FIGURE 1 is a partially completed front view of an automobile radiator illustrating one use for the fin assembly of this invent-ion;
FIGURE 2 is a perspective view of a portion of a fin assembly or spacer strip constructed in accordance with the present invention;
FIGURE 3 is a front elevational view of the fin structure shown in FIGURE 2;
FIGURE 4 is a semidiagrammatic transverse section Patented August 9, 1966 taken approximately on line 4-4 of FIGURE 3 showing the alignment of alternating louvers in relation to the planar base of the fin of which they form a part and in relation to the corresponding louvers of adjacent fins;
FIGURE 5 is a fragmentary perspective View of a portion of an automobile radiator employing the fin strip of this invention and illustrating the alternation of converging and diverging sections within the air passageways formed by the fin strips and the adjacent water tubes; and
FIGURE 6 is a representative flow diagram illustrating the flow of air through and between adjacent air passageways formed with the fin strip of this invention.
Referring now to the drawings, the radiator assembly, as will be readily understood, includes a heat dissipating unit of core 11 having at opposite ends a top tank or inlet header 13 and a bottom tank or outlet header 15, adapted for connection, respectively, with the discharge and intake conduits of a cylinder block cooling jacket. For the flow of cooling medium from one tank to the other, the core is made up of a number of fluid passageways or water tubes 17 spaced apart by fin strips or heat exchange spacer strips 19. The fin strip shown in the drawing is of folded or corrugated outline providing a series of fins 21 bet-ween the folds or connecting members 23. The strips 19 therefore extend between each pair of water tubes 17 and divide the space into a plurality of relatively small air cells, passageways or conduits 25. Ordinarily, the opposite edges or front and rear faces of the core assembly are dipped first in a fiux and then in molten solder to set the margins or ends of the walls of the water tubes where necessary and to join the fin strips to the walls.
Attention is now directed to the novel design of the fin proper and specifically to FIGURES 2, 4, 5 and 6 of the drawing. Pin 21 comprises a planar base or body having a plurality of transversely aligned louvers 27 which may be formed by slitting the planar base and turning the metal abutting one major side of the opening out of the base plane. The slits or windows 29 place adjacent passageways in fluid communication with each other and preferably are substantially equidistant from each other, the edge opposite the corresponding louver being substantially perpendicular to the longitudinal axis of the fin proper and substantially parallel to the longitudinal axis of the fin strip. On a given fin, alternate louvers are turned from the base plane in opposite directions. The order of louver alignment on adjacent fins is reversed.
'Two adjacent fins form two sides of an air passageway which is completed by one of the water tubes and the connecting element between such fins. This passageway is substantially triangular in cross section with such section taken on or along a line parallel to the longitudinal axis of the fin strip. The alternation of louver alignment on each fin with a reverse alignment on the fin forming the opposing wall of the passageway provides a passageway that is alternately converging and diverging in width. Since this alternation continues with each succeeding fin within the fin strip, a row of passageways are provided wherein the converging sections of a given passageway are in line with the diverging sections of the adjacent passageways. This arrangement provides a maximum number of converging and diverg ing passageways with any given number of louvers per fin. This arrangement of louvers stimulates turbulence by wake flow from the converging louver and wall effect of the diverging louver. The alternately constricted and expanded air passages together with the inner communication between such passages provide a high level of turbulence with alternation of positive and negative pressure gradients within each passageway, such alternation being reversed in adjacent passageways.
The term level of turbulence as employed herein is interchangeable with intensity of turbulence and refers to the root mean square of the instantaneous velocity fluctuation divided by the mean velocity.
Example Fins designed in accordance with this invention were tested with a variety of conventional radiator fin designs to evaluate their effectiveness for creating turbulence in an air stream.
The tests were carried out in a low turbulence wind tunnel, i.e., background turbulence of about 0.28% throughout the several tests. A hot wire anemometer is an instrument by which the velocities in a moving fluid are determined by the cooling effect of the stream on a thin electrically heated element positioned therein. In these tests the sensing element was of platinum and had an average diameter of 0.00015 inch. The anemometer includes a probe to hold the sensing element in the fluid stream, a controlled source for electrically heating the sensing element, precision equipment for measuring D.C. electrical values, e.g., a precision galvanometer or bridge circuit, an amplifier and a recording device for measuring A.C. electrical signals, e.g., an oscilloscope or root mean square meter, and a second air channel for correlation studies. The filament size permits sensitive measurement of fluctuations in the flow pattern. These measurements were electrically recorded. In the first test readings were taken at a number of different depths within the air passageway. This procedure was duplicated as were all other procedures for each succeeding test.
One of the control fins tested employed planar fins without louvers and is hereinafter termed Fin A. A second control fin employed planar fins with terminal louvers extending outward from one side of the base plane, a center portion supporting louvers turned from the base plane in a direction opposite the terminal louvers and intermediate louvers on either side of the center portion each of which are pivoted from the planar body so that each extended through the base plane to protrude on the two opposite sides thereof. This fin is hereinafter termed Fin B. A third control fin was a species of the common serpentine or bump fin wherein the width of the winding air passageways are essentially constant. This fin is hereinafter termed Fin C. The control fins provided passageways illustrated by the following profiles:
Fin A The turbulence intensity provided by the best of the controls was less than one fifth of that provided by the fin of this invention.
From the foregoing it will be evident that the counterlouvered fins of this invention provide a high level of turbulence when interposed in an air stream and thus permit high utilization of the air stream for heat exchange.
We claim:
1. A heat exchange and spacer element for use in a passageway between and in heat exchange relationship with conduits of a heat exchange device, said element comprising a corrugated metal strip having a plurality of slitted fins separated by connecting members and being constructed and arranged to divide said passageway into Fin B a plurality of smaller intercommunicating air passageways of substantially equal dimensions, said fins consisting of a substantially planar base having a plurality of slits therein extending through and in transverse relationship to the longitudinal axis of said fins with each end thereof terminating within said planar base and a plurality of louvers turned out of the base plane adjacent said slits in a manner such that alternate louvers extend from said base plane on opposite sides thereof, the directional alternation of the louvers of each fin being in reverse order with respect to the alternation of the louvers of the fins adjacent thereto thereby providing said air passageways with alternately converging and diverging sections.
2. A heat exchange and spacer element for use in a passageway between and in heat exchange relationship with conduits of a heat exchange device, said element comprising a folded metal strip having a plurality of slitted fins separated by connecting members and being constructed and arranged to divide said passageway into a plurality of smaller intercommunicating air passageways of substantially equal dimensions, said fins consisting of a substantially planar base having a plurality of slits therein extending through and in transverse relationship to the longitudinal axis of said fins with each end thereof terminating within said planar base and a plurality of louvers turned out of the base plane adjacent said slits in a manner such that alternate louvers extend from said fin on opposites sides thereof, the directional alternation of the louvers of each fin being in reverse order with respect to the alternation of the louvers of the fins adjacent thereto thereby providing said air passageways with alternately converging and diverging sections, the alternation of said converging and diverging sections in a given air passageway being in reverse order with respect to the converging and diverging sections of the air passageways adjacent thereto.
3. In a radiator core, a tube separator comprising a strip of metal providing heat exchange surface common to a pair of adjacent tubes and dividing the space there between into a plurality of intercommunicating air pas sageways, said strip of metal comprising a plurality of slitted fins separated by connecting members, said fins consisting of a substantially planar base having a plurality of slits therein extending through and in transverse relationship to the longitudinal axis of said fins with each end thereof terminating within said planar base and a plurality of louvers turned out of the base plane adjacent said slits in a manner such that alternate louvers extend from said fin on opposite sides thereof, the directional alternation of the louvers of each fin being in reverse order with respect to the alternation of the louvers of the fins adjacent thereto thereby providing said air passageways with alternately converging and diverging sections.
4. In a radiator core, a tube separator comprising a Fin C strip of metal providing heat exchange surface common to a pair of adjacent tubes and dividing the space therebetween into a plurality of intercommunicating air passageways, said strip of metal comprising a plurality of slitted fins separated by connecting members, said fins consisting of a substantially planar base having a plurality of slits therein extending through and in transverse relationship to the longitudinal axis of said fins with each end thereof terminating within said planar base and a plurality of louvers turned out of the base plane adjacent said slits in a manner such that alternate louvers extend from said fin on opposite sides thereof, the directional alternation of the louvers of each fin being in reverse order with respect to the alternation of the louvers of the fins adjacent thereto thereby providing said air passageways with alternately converging and diverging sections, the alternation of said converging and diverging sections in a given air passageway being in reverse order with respect to the converging and diverging sections of the air passageways adjacent thereto.
5. In an automobile heater core, a tube separator comprising a strip of metal providing heat exchange surface common to a pair of adjacent tubes and dividing the space therebetween into a plurality of intercommunicating air passageways, said strip of metal comprising -a plurality of slitted fins separated by connecting members, said fins consisting of a substantially planar Ibase having a plurality of slits therein extending through and intransverse relationship to the longitudinal axis of said fins with each end thereof terminating within said planar base and a plurality of louvers turned out of the base plane adjacent said slits in a manner such that alternate louvers extend from said fin on opposite sides thereof, the directional alternation of the louvers of each fin being in reverse order with respect to the alternation of the louvers of the fins adjacent thereto thereby providing said air passageways with alternately converging and diverging sections.
6. In an automobile heater core, a tube separator comprising a strip of metal providing heat exchange surface common to a pair of adjacent tubes and dividing the space therebetween into a plurality of intercommunicating air passageways, said strip of metal comprising a plurality of slitted fins separated by connecting members, said fins consisting of a substantially planar base having a plurality of slits therein extending through and in transverse relationship to the longitudinal axis of said fins with each end thereof terminating within said planar base and from which a plurality of louvers turned out of the base plane adjacent said slits in a manner such that alternate louvers extend from said fin on opposite sides thereof, the directional alternation of the louvers of each fin being in reverse order with respect to the alternation of the louvers of the fins adjacent thereto thereby providing said air passageways with alternately converging and diverging sections, the alternation of said converging and diverging sections in a given air passageway being in reverse order with respect to the converging and diverging sections of the air passageways adjacent thereto.
7. A heat exchange and spacer element for use in a passageway between and in heat exchange relationship with conduits of a heat exchange device, said element comprising a corrugated metal strip having a plurality of slitted fins separated by connecting members and being constructed and arranged to divide said passageway into a plurality of smaller intercommunicating air passageways of substantially equal dimensions, each of said fins consisting of a substantially planar base having a plurality of slits therein extending through and in transverse relationship to the longitudinal axis of said fins with each end thereof terminating within said planar base and a single louver associated with each of said slits, each of said louvers being integral with said planar base, describing one side of the slit with which it is associated, and turned out of the base plane of said planar base in a manner such that alternate louvers of a given fin extend from said base plane on opposite sides thereof, the directional alternation of the louvers of each fin being in reverse order with respect to the alternation of the louvers of the fins adjacent thereto thereby providing said intercommunicating air passageways with alternately converging and diverging sections throughout the entire length of said passageway.
References Cited by the Examiner UNITED STATES PATENTS 1,800,853 4/1931 Yeager l152 1,906,077 4/1933 Modine -122 1,969,439 8/1934 Wentworth et al. 165-152 2,011,853 8/1935 Emmons 165153 2,016,822 10/1935 Przyborowski 165153 2,063,757 12/1936 Sanders l65153 3,003,749 8/1961 Morse 165l52 FOREIGN PATENTS 341,247 1/ 1931 Great Britain.
ROBERT A. OLEARY, Primary Examiner.
CHARLES SUKALO, FREDERICK L. MATTESON.
JR., Examiners.
T. W. STREULE, Assistant Examiner.
Claims (1)
1. A HEAT EXCHANGE AND SPACER ELEMENT FOR USE IN A PASSAGEWAY BETWEEN AND IN HEAT EXCHANGE RELATIONSHIP WITH CONDUITS OF A HEAT EXCHANGE DEVICE SAID ELEMENT COMPRISING A CORRUGATED METAL STRIP HAVING A PLURALITY OF SLITTED FINS SEPARATED BY CONNECTING MEMBERS AND BEING CONSTRUCTED AND ARRANGED TO DIVIDE SAID PASSAGEWAYS INTO A PLURALITY OF SMALLER INTERCOMMUNICATING AIR PASSAGEWAYS OF SUBSTANTIALLY EQUAL DIMENSIONS, SAID FINS CONSISTING OF A SUBSTANTIALLY PLANAR BASE AND PLURALITY OF SLITS THEREIN EXTENDING THROUGH AND IN TRAVERSE RELATIONSHIP TO THE LONGITUDINAL AXIS OF SAID FINS WITH EACH END THEREOF TERMINATING WITHIN A PLANAR BASE AND A PLURALITY OF LOUVERS TURNED OUT OF BASE PLATE ADJACENT SAID SLITS IN A MANNER SUCH THAN ALTERNATE LOUVERS EXTEND FROM SAID BASE PLANE ON OPPOSITE SIDES THEREOF, THE DIRECTIONAL ALTERNATION OF THE LOUVERS OF EACH FIN BEING IN REVERSE ORDER WITH RESPECT TO THE ALTERNATION OF THE LOUVERS OF THE FINS ADJACENT THERETO THEREBY PROVIDING SAID AIR PASSAGEWAYS WITH ALTERNATELY CONVERGING AND DIVERGING SECTIONS.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US317638A US3265127A (en) | 1963-10-21 | 1963-10-21 | Heat exchange element |
GB36069/64A GB1030379A (en) | 1963-10-21 | 1964-09-03 | Heat exchanger |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US317638A US3265127A (en) | 1963-10-21 | 1963-10-21 | Heat exchange element |
Publications (1)
Publication Number | Publication Date |
---|---|
US3265127A true US3265127A (en) | 1966-08-09 |
Family
ID=23234587
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US317638A Expired - Lifetime US3265127A (en) | 1963-10-21 | 1963-10-21 | Heat exchange element |
Country Status (2)
Country | Link |
---|---|
US (1) | US3265127A (en) |
GB (1) | GB1030379A (en) |
Cited By (51)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3380518A (en) * | 1965-02-26 | 1968-04-30 | Canteloube Andre | Finned heat exchanger |
US3521707A (en) * | 1967-09-13 | 1970-07-28 | Ass Eng Ltd | Heat exchangers |
JPS5293846U (en) * | 1976-01-10 | 1977-07-13 | ||
JPS5293844U (en) * | 1976-01-10 | 1977-07-13 | ||
JPS5293843U (en) * | 1976-01-10 | 1977-07-13 | ||
EP0005959A1 (en) * | 1978-05-31 | 1979-12-12 | Armstrong Engineering Limited | Heat exchanger fins and apparatus for making same |
DE2834422A1 (en) * | 1978-08-05 | 1980-02-28 | Daimler Benz Ag | Air cooled radiator for vehicle IC engine - has vortex in air flow created by driving fan oppositely to baffles carried by heat exchanger |
US4262659A (en) * | 1980-01-24 | 1981-04-21 | Valley Industries, Inc. | Solar radiation absorbing panel |
US4469168A (en) * | 1980-02-27 | 1984-09-04 | Hitachi, Ltd. | Fin assembly for heat exchangers |
FR2576094A1 (en) * | 1985-01-15 | 1986-07-18 | Sanden Corp | SERPENTINE-TYPE HEAT EXCHANGER USING WING PLATES WITH HOLES |
US4614230A (en) * | 1983-07-29 | 1986-09-30 | Mitsubishi Denki Kabushiki Kaisha | Heat exchanger |
US4615384A (en) * | 1983-06-30 | 1986-10-07 | Nihon Radiator Co., Ltd. | Heat exchanger fin with louvers |
US4621687A (en) * | 1984-10-11 | 1986-11-11 | Nihon Radiator Co., Ltd. | Flat tube heat exchanger having corrugated fins with louvers |
US4796694A (en) * | 1985-08-26 | 1989-01-10 | Nihon Radiator Co., Ltd. | Cooling fin for heat exchanger |
US4958681A (en) * | 1989-08-14 | 1990-09-25 | General Motors Corporation | Heat exchanger with bypass channel louvered fins |
US5062475A (en) * | 1989-10-02 | 1991-11-05 | Sundstrand Heat Transfer, Inc. | Chevron lanced fin design with unequal leg lengths for a heat exchanger |
US5150596A (en) * | 1991-07-11 | 1992-09-29 | General Motors Corporation | Heat transfer fin with dammed segments |
DE4142019A1 (en) * | 1991-12-19 | 1993-06-24 | Behr Gmbh & Co | SHAFT RIB FOR FLAT TUBE HEAT EXCHANGER |
DE19501532A1 (en) * | 1994-01-21 | 1995-07-27 | Honda Motor Co Ltd | Heat exchanger with exchange elements for fluid |
US5634270A (en) * | 1994-03-15 | 1997-06-03 | Behr Heat Transfer Systems, Inc. | Method for making off-set louvered heat exchanger fin |
US5669438A (en) * | 1996-08-30 | 1997-09-23 | General Motors Corporation | Corrugated cooling fin with louvers |
US5704417A (en) * | 1996-08-23 | 1998-01-06 | Gas Research Institute | Perforated fin heat and mass transfer device |
US5730214A (en) * | 1997-01-16 | 1998-03-24 | General Motors Corporation | Heat exchanger cooling fin with varying louver angle |
US5787972A (en) * | 1997-08-22 | 1998-08-04 | General Motors Corporation | Compression tolerant louvered heat exchanger fin |
WO1998050746A1 (en) * | 1997-05-07 | 1998-11-12 | Valeo Klimatechnik Gmbh & Co. Kg | Zigzag blade as ribbing for motor vehicle flat tube heat exchangers |
US6170566B1 (en) * | 1999-12-22 | 2001-01-09 | Visteon Global Technologies, Inc. | High performance louvered fin for a heat exchanger |
US6314752B1 (en) | 1998-12-18 | 2001-11-13 | The Ohio State University Research Foundation | Mass and heat transfer devices and methods of use |
US20040250811A1 (en) * | 2003-06-10 | 2004-12-16 | Moravec Donald W. | Deep fat fryer burner tube insert for enhanced heat transfer |
US6957694B2 (en) * | 2001-03-16 | 2005-10-25 | Calsonic Kansei Corporation | Core structure of integral heat-exchanger |
US20050252640A1 (en) * | 2004-05-13 | 2005-11-17 | Juei-Chi Chang | Finned heat dissipation module having flow guide |
DE102005007692A1 (en) * | 2005-02-18 | 2006-08-31 | Behr Gmbh & Co. Kg | Shaft rib for a cooling system |
US20070012430A1 (en) * | 2005-07-18 | 2007-01-18 | Duke Brian E | Heat exchangers with corrugated heat exchange elements of improved strength |
EP1898464A1 (en) * | 2005-06-27 | 2008-03-12 | Kabushiki Kaisha Toyota Jidoshokki | Heat sink for power module |
WO2009015805A1 (en) * | 2007-07-31 | 2009-02-05 | Behr Gmbh & Co. Kg | Fin for a heat exchanger |
US20090173479A1 (en) * | 2008-01-09 | 2009-07-09 | Lin-Jie Huang | Louvered air center for compact heat exchanger |
US20110036551A1 (en) * | 2009-08-11 | 2011-02-17 | Trane International Inc. | Louvered Plate Fin |
US20110247791A1 (en) * | 2010-04-13 | 2011-10-13 | Danfoss Sanhua (Hangzhou) Micro Channel Heat Exchanger Co., Ltd. | Heat exchanger |
US20130118479A1 (en) * | 2010-05-27 | 2013-05-16 | Commissariat A L'energie Atomique Et Aux Energies Alternatives | Module for a thermal absorber of a solar receiver, absorber comprising at least one such module and receiver comprising at least one such absorber |
EP2402699A3 (en) * | 2010-06-29 | 2014-04-09 | Sanhua Holding Group Co., Ltd. | Fin and heat exchanger comprising the same |
EP2463903A4 (en) * | 2009-08-07 | 2015-03-04 | Furukawa Sky Aluminum Corp | Heat sink |
CN105157465A (en) * | 2015-10-12 | 2015-12-16 | 山东大学 | Right-angle plate-type fin provided with stabs |
CN105157459A (en) * | 2015-10-12 | 2015-12-16 | 山东大学 | Right angle plate-fin type heat exchanger with spikes for non-azeotropic multicomponent mixture condensation |
CN105180692A (en) * | 2015-10-12 | 2015-12-23 | 山东大学 | Trapezoidal plate-fin heat exchanger provided with stabs |
CN105180690A (en) * | 2015-10-12 | 2015-12-23 | 山东大学 | Trapezoidal plate fin type heat exchanger provided with stabs and used for condensation of non-azeotropic multi-component mixture |
CN105241294A (en) * | 2015-10-12 | 2016-01-13 | 山东大学 | Triangular protruding stab plate-fin heat exchanger |
US20160061537A1 (en) * | 2014-08-28 | 2016-03-03 | Delphi Technologies, Inc. | Heat exchanger fin retention feature |
DE102015205902A1 (en) * | 2015-04-01 | 2016-10-06 | Mahle International Gmbh | Rib for a heat exchanger |
US20170105322A1 (en) * | 2013-03-15 | 2017-04-13 | A.K. Stamping Company, Inc. | Aluminum EMI / RF Shield |
US9752833B2 (en) | 2010-06-21 | 2017-09-05 | Sanhua (Hangzhou) Micro Channel Heat Exchange Co., Ltd | Heat exchanger |
DE102016213197A1 (en) * | 2016-07-19 | 2018-01-25 | Mahle International Gmbh | Corrugated rib of a heat exchanger and heat exchanger |
US11039550B1 (en) * | 2020-04-08 | 2021-06-15 | Google Llc | Heat sink with turbulent structures |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE759255A (en) * | 1969-12-03 | 1971-04-30 | Chausson Usines Sa | CORRUGATED DISSIPATOR FOR RADIATOR HARNESS WITH TUBES AND DISSIPATORS AND PROCESS FOR ITS MANUFACTURING |
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GB341247A (en) * | 1929-12-28 | 1931-01-15 | Gallay Sa | Improvements in or relating to heat exchangers |
US1800853A (en) * | 1930-03-14 | 1931-04-14 | Fedders Mfg Co Inc | Radiator core |
US1906077A (en) * | 1925-09-25 | 1933-04-25 | Modine Mfg Co | Radiator |
US1969439A (en) * | 1933-09-22 | 1934-08-07 | Wentworth | Radiator |
US2011853A (en) * | 1932-07-25 | 1935-08-20 | Gen Motors Corp | Radiator core |
US2016822A (en) * | 1932-02-19 | 1935-10-08 | Przyborowski Stanislaus | Radiator |
US2063757A (en) * | 1934-12-29 | 1936-12-08 | Gen Motors Corp | Radiator core |
US3003749A (en) * | 1957-09-09 | 1961-10-10 | Modine Mfg Co | Automotive strip serpentine fin |
-
1963
- 1963-10-21 US US317638A patent/US3265127A/en not_active Expired - Lifetime
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US1906077A (en) * | 1925-09-25 | 1933-04-25 | Modine Mfg Co | Radiator |
GB341247A (en) * | 1929-12-28 | 1931-01-15 | Gallay Sa | Improvements in or relating to heat exchangers |
US1800853A (en) * | 1930-03-14 | 1931-04-14 | Fedders Mfg Co Inc | Radiator core |
US2016822A (en) * | 1932-02-19 | 1935-10-08 | Przyborowski Stanislaus | Radiator |
US2011853A (en) * | 1932-07-25 | 1935-08-20 | Gen Motors Corp | Radiator core |
US1969439A (en) * | 1933-09-22 | 1934-08-07 | Wentworth | Radiator |
US2063757A (en) * | 1934-12-29 | 1936-12-08 | Gen Motors Corp | Radiator core |
US3003749A (en) * | 1957-09-09 | 1961-10-10 | Modine Mfg Co | Automotive strip serpentine fin |
Cited By (69)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3380518A (en) * | 1965-02-26 | 1968-04-30 | Canteloube Andre | Finned heat exchanger |
US3521707A (en) * | 1967-09-13 | 1970-07-28 | Ass Eng Ltd | Heat exchangers |
JPS5293846U (en) * | 1976-01-10 | 1977-07-13 | ||
JPS5293844U (en) * | 1976-01-10 | 1977-07-13 | ||
JPS5293843U (en) * | 1976-01-10 | 1977-07-13 | ||
EP0005959A1 (en) * | 1978-05-31 | 1979-12-12 | Armstrong Engineering Limited | Heat exchanger fins and apparatus for making same |
DE2834422A1 (en) * | 1978-08-05 | 1980-02-28 | Daimler Benz Ag | Air cooled radiator for vehicle IC engine - has vortex in air flow created by driving fan oppositely to baffles carried by heat exchanger |
US4262659A (en) * | 1980-01-24 | 1981-04-21 | Valley Industries, Inc. | Solar radiation absorbing panel |
US4469168A (en) * | 1980-02-27 | 1984-09-04 | Hitachi, Ltd. | Fin assembly for heat exchangers |
US4615384A (en) * | 1983-06-30 | 1986-10-07 | Nihon Radiator Co., Ltd. | Heat exchanger fin with louvers |
US4614230A (en) * | 1983-07-29 | 1986-09-30 | Mitsubishi Denki Kabushiki Kaisha | Heat exchanger |
US4621687A (en) * | 1984-10-11 | 1986-11-11 | Nihon Radiator Co., Ltd. | Flat tube heat exchanger having corrugated fins with louvers |
FR2576094A1 (en) * | 1985-01-15 | 1986-07-18 | Sanden Corp | SERPENTINE-TYPE HEAT EXCHANGER USING WING PLATES WITH HOLES |
US4796694A (en) * | 1985-08-26 | 1989-01-10 | Nihon Radiator Co., Ltd. | Cooling fin for heat exchanger |
US4958681A (en) * | 1989-08-14 | 1990-09-25 | General Motors Corporation | Heat exchanger with bypass channel louvered fins |
US5062475A (en) * | 1989-10-02 | 1991-11-05 | Sundstrand Heat Transfer, Inc. | Chevron lanced fin design with unequal leg lengths for a heat exchanger |
US5150596A (en) * | 1991-07-11 | 1992-09-29 | General Motors Corporation | Heat transfer fin with dammed segments |
DE4142019A1 (en) * | 1991-12-19 | 1993-06-24 | Behr Gmbh & Co | SHAFT RIB FOR FLAT TUBE HEAT EXCHANGER |
US5361829A (en) * | 1991-12-19 | 1994-11-08 | Behr Gmbh & Co. | Corrugated fin for flat-tube heat exchangers |
DE19501532A1 (en) * | 1994-01-21 | 1995-07-27 | Honda Motor Co Ltd | Heat exchanger with exchange elements for fluid |
US5558156A (en) * | 1994-01-21 | 1996-09-24 | Honda Giken Kogyo Kabushiki | Heat exchanger |
DE19501532C2 (en) * | 1994-01-21 | 1998-01-29 | Honda Motor Co Ltd | Heat exchanger |
US5634270A (en) * | 1994-03-15 | 1997-06-03 | Behr Heat Transfer Systems, Inc. | Method for making off-set louvered heat exchanger fin |
US5704417A (en) * | 1996-08-23 | 1998-01-06 | Gas Research Institute | Perforated fin heat and mass transfer device |
US5669438A (en) * | 1996-08-30 | 1997-09-23 | General Motors Corporation | Corrugated cooling fin with louvers |
EP0826942A2 (en) | 1996-08-30 | 1998-03-04 | General Motors Corporation | Corrugated cooling fin with louvers |
EP0826942A3 (en) * | 1996-08-30 | 1998-07-08 | General Motors Corporation | Corrugated cooling fin with louvers |
US5730214A (en) * | 1997-01-16 | 1998-03-24 | General Motors Corporation | Heat exchanger cooling fin with varying louver angle |
WO1998050746A1 (en) * | 1997-05-07 | 1998-11-12 | Valeo Klimatechnik Gmbh & Co. Kg | Zigzag blade as ribbing for motor vehicle flat tube heat exchangers |
US5787972A (en) * | 1997-08-22 | 1998-08-04 | General Motors Corporation | Compression tolerant louvered heat exchanger fin |
US6314752B1 (en) | 1998-12-18 | 2001-11-13 | The Ohio State University Research Foundation | Mass and heat transfer devices and methods of use |
US6170566B1 (en) * | 1999-12-22 | 2001-01-09 | Visteon Global Technologies, Inc. | High performance louvered fin for a heat exchanger |
US20060016585A1 (en) * | 2001-03-16 | 2006-01-26 | Calsonic Kansei Corporation | Core structure of integral heat-exchanger |
US6957694B2 (en) * | 2001-03-16 | 2005-10-25 | Calsonic Kansei Corporation | Core structure of integral heat-exchanger |
US20040250811A1 (en) * | 2003-06-10 | 2004-12-16 | Moravec Donald W. | Deep fat fryer burner tube insert for enhanced heat transfer |
US20050252640A1 (en) * | 2004-05-13 | 2005-11-17 | Juei-Chi Chang | Finned heat dissipation module having flow guide |
US7140423B2 (en) * | 2004-05-13 | 2006-11-28 | Mitac Technology Corp. | Finned heat dissipation module having flow guide |
DE102005007692A1 (en) * | 2005-02-18 | 2006-08-31 | Behr Gmbh & Co. Kg | Shaft rib for a cooling system |
EP1898464A1 (en) * | 2005-06-27 | 2008-03-12 | Kabushiki Kaisha Toyota Jidoshokki | Heat sink for power module |
US8411438B2 (en) | 2005-06-27 | 2013-04-02 | Kabushiki Kaisha Toyota Jidoshokki | Heat sink for power module |
EP1898464A4 (en) * | 2005-06-27 | 2009-09-02 | Toyota Jidoshokki Kk | Heat sink for power module |
US20090302458A1 (en) * | 2005-06-27 | 2009-12-10 | Hidehito Kubo | Heat Sink For Power Module |
US20070012430A1 (en) * | 2005-07-18 | 2007-01-18 | Duke Brian E | Heat exchangers with corrugated heat exchange elements of improved strength |
WO2009015805A1 (en) * | 2007-07-31 | 2009-02-05 | Behr Gmbh & Co. Kg | Fin for a heat exchanger |
US20100193172A1 (en) * | 2007-07-31 | 2010-08-05 | Hermann Knaus | Fin for a heat exchanger |
CN101790671B (en) * | 2007-07-31 | 2012-06-27 | 贝洱两合公司 | Fin for a heat exchanger |
US20090173479A1 (en) * | 2008-01-09 | 2009-07-09 | Lin-Jie Huang | Louvered air center for compact heat exchanger |
EP2463903A4 (en) * | 2009-08-07 | 2015-03-04 | Furukawa Sky Aluminum Corp | Heat sink |
US20110036551A1 (en) * | 2009-08-11 | 2011-02-17 | Trane International Inc. | Louvered Plate Fin |
US8267160B2 (en) * | 2009-08-11 | 2012-09-18 | Trane International Inc. | Louvered plate fin |
US9528770B2 (en) * | 2010-04-13 | 2016-12-27 | Sanhua (Hangzhou) Micro Channel Heat Exchanger Co. | Heat exchanger |
US20110247791A1 (en) * | 2010-04-13 | 2011-10-13 | Danfoss Sanhua (Hangzhou) Micro Channel Heat Exchanger Co., Ltd. | Heat exchanger |
US20130118479A1 (en) * | 2010-05-27 | 2013-05-16 | Commissariat A L'energie Atomique Et Aux Energies Alternatives | Module for a thermal absorber of a solar receiver, absorber comprising at least one such module and receiver comprising at least one such absorber |
US9752833B2 (en) | 2010-06-21 | 2017-09-05 | Sanhua (Hangzhou) Micro Channel Heat Exchange Co., Ltd | Heat exchanger |
EP2402699A3 (en) * | 2010-06-29 | 2014-04-09 | Sanhua Holding Group Co., Ltd. | Fin and heat exchanger comprising the same |
US20170105322A1 (en) * | 2013-03-15 | 2017-04-13 | A.K. Stamping Company, Inc. | Aluminum EMI / RF Shield |
US20160061537A1 (en) * | 2014-08-28 | 2016-03-03 | Delphi Technologies, Inc. | Heat exchanger fin retention feature |
US10139172B2 (en) * | 2014-08-28 | 2018-11-27 | Mahle International Gmbh | Heat exchanger fin retention feature |
DE102015205902A1 (en) * | 2015-04-01 | 2016-10-06 | Mahle International Gmbh | Rib for a heat exchanger |
CN105241294A (en) * | 2015-10-12 | 2016-01-13 | 山东大学 | Triangular protruding stab plate-fin heat exchanger |
CN105180690A (en) * | 2015-10-12 | 2015-12-23 | 山东大学 | Trapezoidal plate fin type heat exchanger provided with stabs and used for condensation of non-azeotropic multi-component mixture |
CN105241294B (en) * | 2015-10-12 | 2017-04-12 | 山东大学 | Triangular protruding stab plate-fin heat exchanger |
CN105180692A (en) * | 2015-10-12 | 2015-12-23 | 山东大学 | Trapezoidal plate-fin heat exchanger provided with stabs |
CN105157459A (en) * | 2015-10-12 | 2015-12-16 | 山东大学 | Right angle plate-fin type heat exchanger with spikes for non-azeotropic multicomponent mixture condensation |
CN105157465A (en) * | 2015-10-12 | 2015-12-16 | 山东大学 | Right-angle plate-type fin provided with stabs |
DE102016213197A1 (en) * | 2016-07-19 | 2018-01-25 | Mahle International Gmbh | Corrugated rib of a heat exchanger and heat exchanger |
US11039550B1 (en) * | 2020-04-08 | 2021-06-15 | Google Llc | Heat sink with turbulent structures |
US11574850B2 (en) | 2020-04-08 | 2023-02-07 | Google Llc | Heat sink with turbulent structures |
TWI829560B (en) * | 2020-04-08 | 2024-01-11 | 美商谷歌有限責任公司 | Heat sink with turbulent structures |
Also Published As
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