US20120012284A1 - heat sink with staggered heat exchange elements - Google Patents

heat sink with staggered heat exchange elements Download PDF

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Publication number
US20120012284A1
US20120012284A1 US12/835,405 US83540510A US2012012284A1 US 20120012284 A1 US20120012284 A1 US 20120012284A1 US 83540510 A US83540510 A US 83540510A US 2012012284 A1 US2012012284 A1 US 2012012284A1
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Prior art keywords
heat exchange
row
exchange elements
elements
heat
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US12/835,405
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Todd Richard Salamon
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Nokia of America Corp
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Alcatel Lucent USA Inc
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Priority to US12/835,405 priority Critical patent/US20120012284A1/en
Assigned to ALCATEL-LUCENT USA, INCORPORATED reassignment ALCATEL-LUCENT USA, INCORPORATED ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: SALAMON, TODD RICHARD
Publication of US20120012284A1 publication Critical patent/US20120012284A1/en
Assigned to CREDIT SUISSE AG reassignment CREDIT SUISSE AG SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: ALCATEL-LUCENT USA INC.
Priority to US14/176,979 priority patent/US20140151012A1/en
Assigned to ALCATEL-LUCENT USA INC. reassignment ALCATEL-LUCENT USA INC. RELEASE BY SECURED PARTY (SEE DOCUMENT FOR DETAILS). Assignors: CREDIT SUISSE AG
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F5/00Elements specially adapted for movement
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F3/00Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • F28F3/02Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations
    • F28F3/04Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being integral with the element
    • F28F3/048Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being integral with the element in the form of ribs integral with the element or local variations in thickness of the element, e.g. grooves, microchannels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F13/00Arrangements for modifying heat-transfer, e.g. increasing, decreasing
    • F28F13/06Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media
    • F28F13/12Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media by creating turbulence, e.g. by stirring, by increasing the force of circulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0028Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for cooling heat generating elements, e.g. for cooling electronic components or electric devices
    • F28D2021/0029Heat sinks
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2275/00Fastening; Joining
    • F28F2275/02Fastening; Joining by using bonding materials; by embedding elements in particular materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2275/00Fastening; Joining
    • F28F2275/04Fastening; Joining by brazing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2275/00Fastening; Joining
    • F28F2275/06Fastening; Joining by welding
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4935Heat exchanger or boiler making

Definitions

  • the present disclosure is directed, in general, to a heat sink and methods of manufacture thereof.
  • Heat sinks are commonly used to increase the heat transfer area of an electronic device to decrease the thermal resistance between the device and cooling medium, e.g., air.
  • cooling medium e.g., air.
  • One embodiment is a heat sink comprising a base and a plurality of heat exchange elements.
  • the heat exchange elements are connected to and raised above, a surface of the base.
  • There is a first row of the heat exchange elements with each of the heat exchange elements having a long dimension that is substantially parallel to the long dimension of the other heat exchange elements of the first row and to the surface.
  • There is a second row of the heat exchange elements each of the heat exchange elements having a long dimension that is substantially parallel to the long dimension of the other heat exchange elements of the second row and to the surface.
  • the first row and the second row are substantially opposed to each other such that one set of ends of the heat exchange elements of the first row are staggered with respect to one set of ends of the heat exchange elements of the second row.
  • the apparatus comprises the above-described heat sink and a structure configured to produce heat, wherein the heat sink is coupled to the structure.
  • Another embodiment is a method of manufacturing a heat sink.
  • the method comprises forming a base and forming a plurality of heat exchange elements connected to and raised above, a surface of the base.
  • There is a first row of the heat exchange elements with each of the heat exchange elements having a long dimension that is substantially parallel to the long dimension of the other heat exchange elements of the first row and to the surface.
  • There is a second row of the heat exchange elements each of the heat exchange element having a long dimension that is substantially parallel to the long dimension of the other heat exchange elements of the second row and to the surface.
  • the first row and the second row are substantially opposed to each other such that one set of ends of the heat exchange elements of the first row are staggered with respect to one set of ends of the heat exchange elements of the second row.
  • FIG. 1 presents a perspective view of an example embodiment of the heat sink of the disclosure
  • FIG. 2 presents a plan view of the heat sink along view line 2 - 2 shown in FIG. 1 ;
  • FIG. 3 presents a sectional view of the heat sink along view line 3 - 3 shown in FIG. 1 ;
  • FIG. 4 presents a sectional view of the heat sink along view line 4 - 4 shown in FIG. 1 ;
  • FIGS. 5A-5E present plan views of alternative embodiments of the heat sink of the disclosure, analogous to the view presented in FIG. 2 ;
  • FIG. 6 presents a flow diagram of selected steps in an example method of manufacturing a heat sink of the disclosure, e.g., such as presented in FIGS. 1A-5E .
  • Embodiments of the disclosure benefit from the recognition that thermal boundary layers develop along the surfaces of a heat sink. Consequently, efficient heat transfer from the heat sink to the surrounding air can be deterred because the primary means of heat transfer from the slow air flowing in the boundary layer at the surface and the faster moving cold air in the space farther away from the surface is diffusion.
  • the embodiments described herein improve heat transfer efficiency by: i) increasing the turbulence (or mixing) of air located in the channels between the heat exchange elements of a heat sink; and ii) placing structures in a staggered fashion so as to ensure cooler air in the middle of channels contacts heat exchange elements directly. For instance, increased air turbulence helps mix the hotter air next to the heat exchange elements with the cooler air in the middle of channels, and thereby improve heat transfer.
  • the increased contact of cold air with heat exchange elements achieved by staggering the heat exchange elements in different rows as described herein, are believed in some cases to be capable of improving the cooling factor of a heat sink by up to about three times as compared to an analogous heat sink designs but without the staggered elements.
  • FIG. 1 presents a perspective view of one example embodiment of the heat sink of the disclosure.
  • FIG. 2 presents a plan view of the heat sink along view line 2 - 2 shown in FIG. 1 .
  • FIG. 3 presents a sectional view of the heat sink along view line 3 - 3 shown in FIG. 1 .
  • FIG. 4 presents a sectional view of the heat sink along view line 4 - 4 shown in FIG. 1 .
  • FIGS. 5A-5C present plan views of alternative embodiments of the heat sink of the disclosure analogous to the view presented in FIG. 2 .
  • the heat sink 100 comprises a base 105 and a plurality of heat exchange elements 110 .
  • the heat exchange elements 110 are connected to and raised above, a surface 120 of the base 105 .
  • Each of the heat exchange elements 110 of the first row 125 have a long dimension 130 that is substantially parallel to the long dimension 130 of other heat exchange elements 110 of the first row 125 , and, also substantially parallel to the surface 120 of the base 105 .
  • Each of the heat exchange elements 110 of the second row 127 have the long dimension 130 that is substantially parallel to the long dimension 130 of other heat exchange elements 110 of the second row 127 , and, also substantially parallel to the surface 120 of the base 105 .
  • the first row 125 and the second row 127 are substantially opposed to each other such that one set of ends 135 of the heat exchange elements 110 of the first row 125 are staggered with respect to one set of ends 137 of the heat exchange elements 110 of the second row 127 .
  • staggered means that the ends 137 of the heat exchange elements 110 of the second row 127 are substantially offset from the ends 135 of the heat exchange elements 110 of the first row 125 .
  • the adjacent the heat exchange elements 110 define a channel 140 , with a channel width 145 , in-between the adjacent the two heat exchange elements 110 .
  • the ends 137 of elements 110 in the second row 127 are considered to be staggered with respect to ends 135 of elements 110 in the first row 125 when the ends 137 are aligned with a central space 147 (e.g., a middle 80 percent, more preferably a middle 40 percent, and even more preferably, a middle 20 percent of the space 147 ; FIGS. 1-2 ) of the one of the channels 140 located between the ends 135 of elements 110 in the first row 125 .
  • a central space 147 e.g., a middle 80 percent, more preferably a middle 40 percent, and even more preferably, a middle 20 percent of the space 147 ; FIGS. 1-2
  • the height 150 of an element 110 might be longer than the long dimension 130 which, e.g., can correspond to a horizontal length of the element 110 .
  • the horizontal length which is substantially parallel to the base surface, is still the long dimension 130 in the plane of the base's surface 120 , e.g., because it is at least longer than the thickness 155 of the element 130 and because the height 150 dimension is perpendicular to the base's surface 120 .
  • Heat sink designs featuring heat exchange elements with parallel long dimensions can provide superior heat removal as compared to certain heat sink designs using a two-dimension array pin- or pillar-shaped heat exchange elements for configurations where the air flow is predominantly parallel to the base and the long dimension of the heat exchange elements described in the invention.
  • pin- or pillar-shaped heat exchange elements can provide superior heat removal as compared to certain heat sink designs described in this invention when the flow is predominantly parallel to the heat sink base and also orthogonal to the long dimension of the heat exchange elements, and also when the flow is predominantly orthogonal to the heat sink base.
  • the invention described herein is of interest to the case where the flow is predominantly parallel to the heat sink base and the long dimension of the heat exchange elements.
  • the heat exchange elements 110 are depicted as being rectangular-shaped planar fins.
  • a heat exchange element 110 design can be desirable, e.g., because such structures can be relatively simple and inexpensive to manufacture, or, because the air flow characteristics around such structures are relatively easy to simulate via computer modeling.
  • Examples of other heat exchange element designs are presented in patent application Ser. Nos. 12/165,063; 12/165,193; and 12/165,225, all of which are incorporated by reference herein in their entirety.
  • Non-limiting example designs include: bent or curved fins, fins that include flow diverters, monolithic structurally complex designs, or active heat sink designs.
  • the set of ends 135 of the heat exchange elements 110 of the first row 125 are separated from the set of ends 137 of the heat exchange elements 110 of the second row 127 by a gap 210 .
  • Including such an inter-row gap 210 can help reduce the overall pressure drop of air passing around the elements 110 , since the airflow field will tend to rearrange when air goes through the gap 210 from one row 125 to the other row 127 .
  • the gap 210 can also help the thermal boundary layer, which can develop next to the elements 110 , to renormalize.
  • a length 215 of the gap 210 between the set of ends 135 of elements 110 of the first row 125 and the set of ends 137 of elements 110 of the second row 127 can be up to about five times a channel width 125 between adjacent ones of elements 110 .
  • the gap 210 extends to an outer perimeter 220 of the base 105 .
  • the gap 220 is substantially centrally located over the base 105 (e.g., such as when the elements 110 of the first row 125 and the second row 127 all have the same long dimension 130 length).
  • the heat sink 100 can further including one or more vortex enhancers 510 located in the gap 210 .
  • the vortex enhancers 510 can be configured to direct air flow from channels 140 within the first row 125 of heat exchange elements 110 to channels 140 within the second row 127 of heat exchange elements 110 .
  • one or more of the elements 100 e.g., the entire first row 125 of elements 110 can itself be designed as vortex enhancers.
  • vortex enhancers can create vortices that are spatially and temporally varying and which enhance mixing of the cold air in the channel's middle and the hot air at the heat sink's surfaces.
  • Example vortex enhancer designs also known as vortex generators are presented in the above-incorporated U.S. patent application Ser. No. 12/165,225.
  • the set of ends 135 , 137 of the heat exchange elements of the first row 125 partially overlap with the set of ends 137 of the heat exchange elements 110 of the second row 127 .
  • a length 520 of the overlap between the set of ends 135 of the elements 110 of first row 125 with the set of ends 137 of elements 110 of the second row 127 is up to about five times a channel width 145 between adjacent ones of the heat exchange elements 110 .
  • the heat sink 100 can further including one or more additional rows 525 , 527 of the heat exchange elements 110 .
  • the heat sink 100 can further including one or more additional rows 525 , 527 of the heat exchange elements 110 .
  • a set of ends 530 of the heat exchange elements 110 of the additional row 525 are staggered with respect to a set of ends 535 of an opposing different additional row 527 .
  • a set of ends 540 of the heat exchange elements 110 of the additional row 525 are staggered with respect to a second set of ends 545 of the first row or the second row (e.g., second ends 545 of the elements of the second row 127 , as depicted in FIG. 5E ).
  • the set of ends 530 , 535 in the additional rows 525 , 527 can be separated by a gap 550 between the row 525 , 527 .
  • the set of ends 535 , 537 of the elements of the additional rows 525 , 527 can have overlap or be aligned, similar to that described in the context of in FIGS. 5C and 5D regarding example embodiments of the first and second rows 125 , 127 .
  • the channels 140 in the additional rows 525 , 527 are oriented substantially parallel with each other and with the channels 140 of the first and second rows 125 , 127 . Such configuration helps avoid air pressure drops which can decrease the heat sink's cooling performance. In other embodiments, however non-parallel channel orientations between rows could be used.
  • second ends 230 , 235 of the heat exchange elements 110 of the rows 125 , 127 can substantially extend to the outer perimeter 220 of the base 105 .
  • one or both of the second ends 230 , 235 may not extend to the perimeter 220 .
  • lengths of the long dimensions 130 of the heat exchange elements 110 of the first row 125 are substantially equal to each other (e.g., within 10 percent).
  • the lengths of the long dimensions 130 of the heat exchange elements 110 of the second row 127 can be substantially equal to each other, and in some cases, to lengths of the long dimensions 130 of the elements of the first row 125 .
  • the long dimension 130 of the elements 110 in the first or second row 125 , 127 may not be the same length within a row 125 (or row 127 ) or between different rows 125 , 127 .
  • the heat exchanger elements 110 are continuously connected to the base 105 . That is, the elements 110 and the base 105 are formed from the same work piece of starting material (e.g., aluminum and copper and their alloys, or steel, brass or silver).
  • the starting material can be a piece of metal which is shaped or machined, as further discussed below, to define the elements 110 and base 105 .
  • the elements 110 can be separately made and then coupled, as further discussed below, to the base 110 .
  • the elements 110 can have lengths 130 and heights 150 up to about 200 mm and thicknesses up to about 2 mm, with the height-to-length aspect ratio ranging from about 1:1 to 20:1, height-to-thickness aspect ratios ranging about from 1:1 to 500:1, and the channel width 145 ranging from about 1 to 20 mm. Proportionally greater sizes and spacing could be used in larger-scale cooling applications.
  • the apparatus 400 comprises a heat sink 100 , such as any of the embodiments of heat sinks 100 discussed in the context of FIGS. 1-5E .
  • the apparatus 400 also comprises a structure 410 configured to produce heat.
  • the heat sink 100 is coupled to the device 410 .
  • One skilled in the art would be familiar with the means to couple a heat sink to a structure so as to achieve efficient heat transfer.
  • the apparatus 400 can be an electrical device, and the heat generating structure 410 includes an integrated circuit, or, in other cases, a power supply of the electrical device.
  • the apparatus 400 can a heat exchanger and the heat generating structure 410 is a pipe that carries a heated fluid therein (e.g., water, air, refrigerant).
  • a plurality of heat sinks 100 can be thermally coupled to a heat pipe structure 410 that is configured to circulate fluid from another device that generates heat, e.g., a motor or electrical power supply (not shown).
  • heat pipes could be incorporated within the base 105 .
  • the base 105 and structure 410 are depicted as having a planar interface 415 , in other cases, the interface 415 could be non-planar (e.g., such as when the structure 410 is the wall of a cylindrical pipe).
  • FIG. 6 presents a flow diagram of selected steps in an example method 600 of manufacturing a heat sink 100 of the disclosure, such as any of the embodiments of heat sinks 100 discussed in the context of FIGS. 1-5E .
  • the method comprises a step 605 of forming a base 105 , and a step 610 of forming a plurality of heat exchange elements 110 , connected to and raised above, a surface 120 of the base 105 .
  • the elements 110 can be configured in any of the manners discussed herein.
  • forming the base 105 in step 605 includes machining a thin sheet of metal to the appropriate dimensions.
  • the base's thickness 160 may be on the order of about 1 to 10 mm.
  • the length 162 and width 164 can be on the order of 10 to 300 mm.
  • forming the base can include a step 615 of forming fluid flow conduits (e.g., pipes or chambers) within the base 105 .
  • fluid flow conduits e.g., pipes or chambers
  • fluid can be circulated through the conduits to facilitate cooling.
  • forming the base includes a step 620 of forming a heat exchange structure (e.g., a structure 410 such as discussed in the context of FIG. 4 ) wherein the base 105 is part of an outer surface of the heat exchange structure.
  • a heat exchange structure e.g., a structure 410 such as discussed in the context of FIG. 4
  • forming the plurality of elements 110 , connected to and raised above, the base's surface 120 in step 610 includes a step 625 of coupling the heat exchange elements 110 to the surface 120 .
  • the coupling step 625 can include coupling individual elements 110 , or preformed rows 125 , 127 of the elements 110 , to the surface 120 .
  • the preformed rows can comprise a metal sheet which is folded to form the elements 110 , and then the folded sheet can be coupled to the base 120 .
  • Non-limiting examples of coupling methods include epoxy bond, brazing, soldering, welding or various combinations thereof.
  • the forming step 610 can include a step 630 of shaping a same work piece that the base 105 is formed from.
  • a single metal sheet work piece can be shaped by skiving, machining, bending or stamping, the sheet to form the elements 110 .
  • a molten work piece can be shaped by extrusion or die casting, or, extrusion or die casting followed by post-extrusion machining, to form the elements 110 .

Abstract

Heat sink comprising a base and a plurality of heat exchange elements. The elements are connected to and raised above, a surface of the base. There is a first row of the elements, with each of the elements having a long dimension that is substantially parallel to the long dimension of the other elements of the first row and to the surface. There is a second row of the elements, each of the elements having a long dimension that is substantially parallel to the long dimension of the other elements of the second row and to the surface. The first row and the second row are substantially opposed to each other such that one set of ends of the elements of the first row are staggered with respect to one set of ends of the elements of the second row.

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • The present application is related to U.S. patent application Ser. No. ______ (docket no. 807926) to Salamon, entitled, “AIR JET ACTIVE HEAT SINK”, and which is commonly assigned with the present application, which is incorporated herein by reference in its entirety.
  • TECHNICAL FIELD OF THE INVENTION
  • The present disclosure is directed, in general, to a heat sink and methods of manufacture thereof.
  • BACKGROUND OF THE INVENTION
  • This section introduces aspects that may be helpful to facilitating a better understanding of the inventions. Accordingly, the statements of this section are to be read in this light. The statements of this section are not to be understood as admissions about what is in the prior art or what is not in the prior art.
  • Heat sinks are commonly used to increase the heat transfer area of an electronic device to decrease the thermal resistance between the device and cooling medium, e.g., air. There is a growing trend, however, for electronic devices to dissipate so much power that traditional heat sink designs are inadequate to sufficiently cool the device. Improved heat transfer efficiency from electronic devices would help extend the lifetime of such devices.
  • SUMMARY OF THE INVENTION
  • One embodiment is a heat sink comprising a base and a plurality of heat exchange elements. The heat exchange elements are connected to and raised above, a surface of the base. There is a first row of the heat exchange elements, with each of the heat exchange elements having a long dimension that is substantially parallel to the long dimension of the other heat exchange elements of the first row and to the surface. There is a second row of the heat exchange elements, each of the heat exchange elements having a long dimension that is substantially parallel to the long dimension of the other heat exchange elements of the second row and to the surface. The first row and the second row are substantially opposed to each other such that one set of ends of the heat exchange elements of the first row are staggered with respect to one set of ends of the heat exchange elements of the second row.
  • Another embodiment is an apparatus. The apparatus comprises the above-described heat sink and a structure configured to produce heat, wherein the heat sink is coupled to the structure.
  • Another embodiment is a method of manufacturing a heat sink. The method comprises forming a base and forming a plurality of heat exchange elements connected to and raised above, a surface of the base. There is a first row of the heat exchange elements, with each of the heat exchange elements having a long dimension that is substantially parallel to the long dimension of the other heat exchange elements of the first row and to the surface. There is a second row of the heat exchange elements, each of the heat exchange element having a long dimension that is substantially parallel to the long dimension of the other heat exchange elements of the second row and to the surface. The first row and the second row are substantially opposed to each other such that one set of ends of the heat exchange elements of the first row are staggered with respect to one set of ends of the heat exchange elements of the second row.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The embodiments of the disclosure are best understood from the following detailed description, when read with the accompanying FIGUREs. Some features in the figures may be described as “vertical” or “horizontal” for convenience in referring to those features. Such descriptions do not limit the orientation of such features with respect to the natural horizon or gravity. Various features may not be drawn to scale and may be arbitrarily increased or reduced in size for clarity of discussion. Reference is now made to the following descriptions taken in conjunction with the accompanying drawings, in which:
  • FIG. 1 presents a perspective view of an example embodiment of the heat sink of the disclosure;
  • FIG. 2 presents a plan view of the heat sink along view line 2-2 shown in FIG. 1;
  • FIG. 3 presents a sectional view of the heat sink along view line 3-3 shown in FIG. 1;
  • FIG. 4 presents a sectional view of the heat sink along view line 4-4 shown in FIG. 1;
  • FIGS. 5A-5E present plan views of alternative embodiments of the heat sink of the disclosure, analogous to the view presented in FIG. 2; and
  • FIG. 6 presents a flow diagram of selected steps in an example method of manufacturing a heat sink of the disclosure, e.g., such as presented in FIGS. 1A-5E.
  • DETAILED DESCRIPTION OF ILLUSTRATIVE EMBODIMENTS
  • The description and drawings merely illustrate the principles of the invention. It will thus be appreciated that those skilled in the art will be able to devise various arrangements that, although not explicitly described or shown herein, embody the principles of the invention and are included within its scope. Furthermore, all examples recited herein are principally intended expressly to be only for pedagogical purposes to aid the reader in understanding the principles of the invention and the concepts contributed by the inventor(s) to furthering the art, and are to be construed as being without limitation to such specifically recited examples and conditions. Moreover, all statements herein reciting principles, aspects, and embodiments of the invention, as well as specific examples thereof, are intended to encompass equivalents thereof. Additionally, the term, “or,” as used herein, refers to a non-exclusive or, unless otherwise indicated. Also, the various embodiments described herein are not necessarily mutually exclusive, as some embodiments can be combined with one or more other embodiments to form new embodiments.
  • Embodiments of the disclosure benefit from the recognition that thermal boundary layers develop along the surfaces of a heat sink. Consequently, efficient heat transfer from the heat sink to the surrounding air can be deterred because the primary means of heat transfer from the slow air flowing in the boundary layer at the surface and the faster moving cold air in the space farther away from the surface is diffusion.
  • The embodiments described herein improve heat transfer efficiency by: i) increasing the turbulence (or mixing) of air located in the channels between the heat exchange elements of a heat sink; and ii) placing structures in a staggered fashion so as to ensure cooler air in the middle of channels contacts heat exchange elements directly. For instance, increased air turbulence helps mix the hotter air next to the heat exchange elements with the cooler air in the middle of channels, and thereby improve heat transfer. The increased contact of cold air with heat exchange elements, achieved by staggering the heat exchange elements in different rows as described herein, are believed in some cases to be capable of improving the cooling factor of a heat sink by up to about three times as compared to an analogous heat sink designs but without the staggered elements.
  • One embodiment of the disclosure is a heat sink. FIG. 1 presents a perspective view of one example embodiment of the heat sink of the disclosure. FIG. 2 presents a plan view of the heat sink along view line 2-2 shown in FIG. 1. FIG. 3 presents a sectional view of the heat sink along view line 3-3 shown in FIG. 1. FIG. 4 presents a sectional view of the heat sink along view line 4-4 shown in FIG. 1. FIGS. 5A-5C present plan views of alternative embodiments of the heat sink of the disclosure analogous to the view presented in FIG. 2.
  • Turning to FIG. 1, the heat sink 100 comprises a base 105 and a plurality of heat exchange elements 110. The heat exchange elements 110 are connected to and raised above, a surface 120 of the base 105. There is first row 125 of the heat exchange elements 110 and a second row of the heat exchange elements 110. Each of the heat exchange elements 110 of the first row 125 have a long dimension 130 that is substantially parallel to the long dimension 130 of other heat exchange elements 110 of the first row 125, and, also substantially parallel to the surface 120 of the base 105. Each of the heat exchange elements 110 of the second row 127 have the long dimension 130 that is substantially parallel to the long dimension 130 of other heat exchange elements 110 of the second row 127, and, also substantially parallel to the surface 120 of the base 105. The first row 125 and the second row 127 are substantially opposed to each other such that one set of ends 135 of the heat exchange elements 110 of the first row 125 are staggered with respect to one set of ends 137 of the heat exchange elements 110 of the second row 127.
  • The term staggered as used herein means that the ends 137 of the heat exchange elements 110 of the second row 127 are substantially offset from the ends 135 of the heat exchange elements 110 of the first row 125. For instance, consider two adjacent the heat exchange elements 110 in either of the rows 125, 127. The adjacent the heat exchange elements 110 define a channel 140, with a channel width 145, in-between the adjacent the two heat exchange elements 110. The ends 137 of elements 110 in the second row 127 are considered to be staggered with respect to ends 135 of elements 110 in the first row 125 when the ends 137 are aligned with a central space 147 (e.g., a middle 80 percent, more preferably a middle 40 percent, and even more preferably, a middle 20 percent of the space 147; FIGS. 1-2) of the one of the channels 140 located between the ends 135 of elements 110 in the first row 125.
  • In some embodiment, the height 150 of an element 110 might be longer than the long dimension 130 which, e.g., can correspond to a horizontal length of the element 110. However, the horizontal length, which is substantially parallel to the base surface, is still the long dimension 130 in the plane of the base's surface 120, e.g., because it is at least longer than the thickness 155 of the element 130 and because the height 150 dimension is perpendicular to the base's surface 120.
  • Heat sink designs featuring heat exchange elements with parallel long dimensions, such as disclosed herein, can provide superior heat removal as compared to certain heat sink designs using a two-dimension array pin- or pillar-shaped heat exchange elements for configurations where the air flow is predominantly parallel to the base and the long dimension of the heat exchange elements described in the invention. In contrast, pin- or pillar-shaped heat exchange elements can provide superior heat removal as compared to certain heat sink designs described in this invention when the flow is predominantly parallel to the heat sink base and also orthogonal to the long dimension of the heat exchange elements, and also when the flow is predominantly orthogonal to the heat sink base. The invention described herein is of interest to the case where the flow is predominantly parallel to the heat sink base and the long dimension of the heat exchange elements.
  • For many of the example embodiments presented herein, such as in FIGS. 1-4, the heat exchange elements 110 are depicted as being rectangular-shaped planar fins. In some embodiments such a heat exchange element 110 design can be desirable, e.g., because such structures can be relatively simple and inexpensive to manufacture, or, because the air flow characteristics around such structures are relatively easy to simulate via computer modeling. In other embodiments, however, it may be advantageous for the heat exchange elements 110 to have other shapes. Examples of other heat exchange element designs are presented in patent application Ser. Nos. 12/165,063; 12/165,193; and 12/165,225, all of which are incorporated by reference herein in their entirety. Non-limiting example designs include: bent or curved fins, fins that include flow diverters, monolithic structurally complex designs, or active heat sink designs.
  • As illustrated in FIG. 2, in some embodiments, the set of ends 135 of the heat exchange elements 110 of the first row 125 are separated from the set of ends 137 of the heat exchange elements 110 of the second row 127 by a gap 210. Including such an inter-row gap 210 can help reduce the overall pressure drop of air passing around the elements 110, since the airflow field will tend to rearrange when air goes through the gap 210 from one row 125 to the other row 127. Additionally, the gap 210 can also help the thermal boundary layer, which can develop next to the elements 110, to renormalize.
  • To facilitate such advantages, in some embodiments, a length 215 of the gap 210 between the set of ends 135 of elements 110 of the first row 125 and the set of ends 137 of elements 110 of the second row 127 can be up to about five times a channel width 125 between adjacent ones of elements 110. In some preferred embodiments, the gap 210 extends to an outer perimeter 220 of the base 105. In some preferred embodiments, the gap 220 is substantially centrally located over the base 105 (e.g., such as when the elements 110 of the first row 125 and the second row 127 all have the same long dimension 130 length).
  • In some embodiments, there are additional structures that can be located in the gap 210 to facilitate increase air flow turbulence around the elements 110. For instance, as shown in FIG. 5A. The heat sink 100 can further including one or more vortex enhancers 510 located in the gap 210. The vortex enhancers 510 can be configured to direct air flow from channels 140 within the first row 125 of heat exchange elements 110 to channels 140 within the second row 127 of heat exchange elements 110. Of course, in still other embodiments, such as shown in FIG. 5B, one or more of the elements 100 (e.g., the entire first row 125 of elements 110 can itself be designed as vortex enhancers. One skilled in the art would understand that the vortex enhancers can create vortices that are spatially and temporally varying and which enhance mixing of the cold air in the channel's middle and the hot air at the heat sink's surfaces. Example vortex enhancer designs (also known as vortex generators) are presented in the above-incorporated U.S. patent application Ser. No. 12/165,225.
  • In some embodiments, however there is no gap between the ends 135, 137 of the elements 110 of the opposing rows 125, 127, such as discussed above in the context of FIG. 2. For instance, as illustrated in FIG. 5C, the set of ends 135, 137 of the heat exchange elements of the first row 125 partially overlap with the set of ends 137 of the heat exchange elements 110 of the second row 127. In some embodiments, as illustrated in FIG. 5C, a length 520 of the overlap between the set of ends 135 of the elements 110 of first row 125 with the set of ends 137 of elements 110 of the second row 127 is up to about five times a channel width 145 between adjacent ones of the heat exchange elements 110.
  • In yet other embodiments, such as shown in FIG. 5D there is neither a gap nor an overlap between the ends 135, 137 of the elements 110 of the opposing rows 125, 127. For instance, the ends 135, 137 of the elements 110 from the opposing rows 125, 127 can be substantially aligned with each other.
  • Some embodiments of the heat sink can include additional rows of heat exchange elements. For instance, as shown in FIG. 5E, the heat sink 100 can further including one or more additional rows 525, 527 of the heat exchange elements 110. Analogous to that discussed in the context of FIGS. 1 and 2, above, a set of ends 530 of the heat exchange elements 110 of the additional row 525, are staggered with respect to a set of ends 535 of an opposing different additional row 527.
  • Or, a set of ends 540 of the heat exchange elements 110 of the additional row 525 are staggered with respect to a second set of ends 545 of the first row or the second row (e.g., second ends 545 of the elements of the second row 127, as depicted in FIG. 5E). As also illustrated in FIG. 5E, the set of ends 530, 535 in the additional rows 525, 527 can be separated by a gap 550 between the row 525, 527. Or, there can be a gap 555 between one or more of the additional rows 525 and one of the first and second rows (e.g., there is a gap 555, between the set of second ends 540 of the elements 110 of the additional row 525 and the set of second ends 545 of the elements 110 of the second row 127. In still other embodiments, however, the set of ends 535, 537 of the elements of the additional rows 525, 527 can have overlap or be aligned, similar to that described in the context of in FIGS. 5C and 5D regarding example embodiments of the first and second rows 125, 127.
  • In some preferred embodiments, as also illustrated in FIG. 5E, the channels 140 in the additional rows 525, 527 are oriented substantially parallel with each other and with the channels 140 of the first and second rows 125, 127. Such configuration helps avoid air pressure drops which can decrease the heat sink's cooling performance. In other embodiments, however non-parallel channel orientations between rows could be used.
  • In some embodiments of the heat sink 100, as illustrated in FIG. 2, second ends 230, 235 of the heat exchange elements 110 of the rows 125, 127 can substantially extend to the outer perimeter 220 of the base 105. However, in other embodiments, one or both of the second ends 230, 235 may not extend to the perimeter 220.
  • In some embodiments of the heat sink 100, as illustrated in FIG. 2, lengths of the long dimensions 130 of the heat exchange elements 110 of the first row 125 are substantially equal to each other (e.g., within 10 percent). Similarly, the lengths of the long dimensions 130 of the heat exchange elements 110 of the second row 127 can be substantially equal to each other, and in some cases, to lengths of the long dimensions 130 of the elements of the first row 125. However, in other embodiments, the long dimension 130 of the elements 110 in the first or second row 125, 127 may not be the same length within a row 125 (or row 127) or between different rows 125, 127.
  • As illustrated in FIG. 3 and FIG. 4, in some embodiments of the heat sink 100, the heat exchanger elements 110 are continuously connected to the base 105. That is, the elements 110 and the base 105 are formed from the same work piece of starting material (e.g., aluminum and copper and their alloys, or steel, brass or silver). For instance, the starting material can be a piece of metal which is shaped or machined, as further discussed below, to define the elements 110 and base 105. In other embodiments, however the elements 110 can be separately made and then coupled, as further discussed below, to the base 110.
  • One skilled in the art would be familiar with the appropriate size and spacing of elements 110 to use for particular cooling applications. For instance, in certain micro-electronic applications, the elements 110 can have lengths 130 and heights 150 up to about 200 mm and thicknesses up to about 2 mm, with the height-to-length aspect ratio ranging from about 1:1 to 20:1, height-to-thickness aspect ratios ranging about from 1:1 to 500:1, and the channel width 145 ranging from about 1 to 20 mm. Proportionally greater sizes and spacing could be used in larger-scale cooling applications.
  • As further illustrated in FIG. 4, another embodiment of the disclosure is an apparatus 400. The apparatus 400 comprises a heat sink 100, such as any of the embodiments of heat sinks 100 discussed in the context of FIGS. 1-5E. The apparatus 400 also comprises a structure 410 configured to produce heat. The heat sink 100 is coupled to the device 410. One skilled in the art would be familiar with the means to couple a heat sink to a structure so as to achieve efficient heat transfer.
  • For instance, in some embodiments the apparatus 400 can be an electrical device, and the heat generating structure 410 includes an integrated circuit, or, in other cases, a power supply of the electrical device. In some embodiments, the apparatus 400 can a heat exchanger and the heat generating structure 410 is a pipe that carries a heated fluid therein (e.g., water, air, refrigerant). For instance, a plurality of heat sinks 100 can be thermally coupled to a heat pipe structure 410 that is configured to circulate fluid from another device that generates heat, e.g., a motor or electrical power supply (not shown). In other embodiments, however, heat pipes could be incorporated within the base 105. Although the base 105 and structure 410 are depicted as having a planar interface 415, in other cases, the interface 415 could be non-planar (e.g., such as when the structure 410 is the wall of a cylindrical pipe).
  • Another embodiment of the disclosure is a method of manufacturing a heat sink. FIG. 6 presents a flow diagram of selected steps in an example method 600 of manufacturing a heat sink 100 of the disclosure, such as any of the embodiments of heat sinks 100 discussed in the context of FIGS. 1-5E.
  • With continuing reference to FIGS. 1-5E throughout, the method comprises a step 605 of forming a base 105, and a step 610 of forming a plurality of heat exchange elements 110, connected to and raised above, a surface 120 of the base 105. The elements 110 can be configured in any of the manners discussed herein.
  • In some embodiments, forming the base 105 in step 605 includes machining a thin sheet of metal to the appropriate dimensions. E.g., for some electronic cooling applications, the base's thickness 160 (FIG. 1) may be on the order of about 1 to 10 mm. E.g., for some micro-electronic cooling applications the length 162 and width 164 can be on the order of 10 to 300 mm.
  • In some cases, forming the base (step 605) can include a step 615 of forming fluid flow conduits (e.g., pipes or chambers) within the base 105. During the heat sink's operation fluid can be circulated through the conduits to facilitate cooling.
  • In some cases, forming the base (step 605) includes a step 620 of forming a heat exchange structure (e.g., a structure 410 such as discussed in the context of FIG. 4) wherein the base 105 is part of an outer surface of the heat exchange structure.
  • In some embodiments, forming the plurality of elements 110, connected to and raised above, the base's surface 120 in step 610, includes a step 625 of coupling the heat exchange elements 110 to the surface 120.
  • The coupling step 625 can include coupling individual elements 110, or preformed rows 125, 127 of the elements 110, to the surface 120. For instance the preformed rows can comprise a metal sheet which is folded to form the elements 110, and then the folded sheet can be coupled to the base 120. Non-limiting examples of coupling methods include epoxy bond, brazing, soldering, welding or various combinations thereof.
  • In other embodiments, the forming step 610 can include a step 630 of shaping a same work piece that the base 105 is formed from. As a non-limiting example, a single metal sheet work piece can be shaped by skiving, machining, bending or stamping, the sheet to form the elements 110. As another non-limiting example, a molten work piece can be shaped by extrusion or die casting, or, extrusion or die casting followed by post-extrusion machining, to form the elements 110.
  • Although the embodiments have been described in detail, those of ordinary skill in the art should understand that they could make various changes, substitutions and alterations herein without departing from the scope of the disclosure.

Claims (20)

1. A heat sink, comprising:
a base; and
a plurality of heat exchange elements, connected to and raised above, a surface of said base, wherein
a first row of said heat exchange elements, with each of said heat exchange elements having a long dimension that is substantially parallel to said long dimension of said other heat exchange elements of said first row and to said surface,
a second row of said heat exchange elements, each of said heat exchange elements having a long dimension that is substantially parallel to said long dimension of other said heat exchange elements of said second row and to said surface, and
said first row and said second row are substantially opposed to each other such that one set of ends of said heat exchange elements of said first row are staggered with respect to one set of ends of said heat exchange elements of said second row.
2. The heat sink of claim 1, wherein said set of ends of said heat exchange elements of said first row are separated from said set of ends of said heat exchange elements of said second row by a gap.
3. The heat sink of claim 2, wherein a length of said gap between said set of ends of said first row and said set of ends of said second row is up to about five times a channel width between adjacent ones of said heat exchange elements.
4. The heat sink of claim 2, further including one or more vortex enhancers located in said gap, said vortex enhancers configured to create vortices and direct air flow from channels within said first row of heat exchange elements to channels within said second row of heat exchange elements.
5. The heat sink of claim 1, wherein one or more of said heat exchange elements of said first row or of said second row are configured as vortex enhancers.
6. The heat sink of claim 1, wherein said set of ends of said heat exchange elements of said first row partially overlap with said set of ends of said heat exchange elements of said second row.
7. The heat sink of claim 6, wherein a length of said overlap between said set of ends of said elements of said first row with said set of ends of said elements of said second row is up to about five times a channel width between adjacent ones of said heat exchange elements.
8. The heat sink of claim 1, further including one or more additional rows of said heat exchange elements wherein a set of ends of said heat exchange elements of said additional rows are staggered with respect to a set of ends of an opposing different additional rows, or, with respect to a second set of ends of said first row or of said second row.
9. The heat sink of claim 8, wherein channels between said heat exchange elements of said one or more additional rows of said heat exchange elements are oriented substantially parallel with channels between said heat exchange elements of said adjacent different additional rows and with channels between said heat exchange elements of said first and said second rows.
10. The heat sink of claim 1, wherein second ends of said heat exchange elements substantially extend to an outer perimeter of said base.
11. The heat sink of claim 1, wherein lengths of said long dimensions of said heat exchange elements of said first row are substantially equal to each other.
12. The heat sink of claim 1, wherein lengths of said long dimensions of said heat exchange elements of said second row are substantially equal to each other and to lengths of said long dimensions of said heat exchange elements of said first row.
13. The heat sink of claim 1, wherein said heat exchanger elements are continuously connected to said base.
14. The heat sink of claim 1, wherein said heat exchanger elements are coupled to said base.
15. An apparatus, comprising:
a heat sink, including:
a base; and
a plurality of heat exchange elements, connected to and raised above, a surface of said base, including:
a first row of said heat exchange elements, with each of said heat exchange elements having a long dimension that is substantially parallel to said long dimension of said other heat exchange elements of said first row and to said surface,
a second row of said heat exchange elements, each of said heat exchange elements having a long dimension that is substantially parallel to said long dimension of other said heat exchange elements of said second row and to said surface, and
said first row and said second row are substantially opposed to each other such that one set of ends of said heat exchange elements of said first row are staggered with respect to one set of ends of said heat exchange elements of said second row; and
a structure configured to produce heat, wherein said heat sink is coupled to said structure.
16. A method of manufacturing a heat sink, comprising:
forming a base; and
forming a plurality of heat exchange elements connected to and raised above, a surface of said base, including:
a first row of said heat exchange elements, with each of said heat exchange elements having a long dimension that is substantially parallel to said long dimension of said other heat exchange elements of said first row and to said surface,
a second row of said heat exchange elements, each of said heat exchange elements having a long dimension that is substantially parallel to said long dimension of other said heat exchange elements of said second row and to said surface, and
said first row and said second row are substantially opposed to each other such that one set of ends of said heat exchange elements of said first row are staggered with respect to one set of ends of said heat exchange elements of said second row.
17. The method of claim 16, wherein forming said base includes forming flow conduits within said base.
18. The method of claim 16, wherein forming said base includes forming a heat exchange structure wherein said base is part of an outer surface of said heat exchange device.
19. The method of claim 16, wherein forming said plurality of heat exchange elements connected to said base includes coupling said heat exchange elements to said surface.
20. The method of claim 16, wherein forming said plurality of heat exchange elements connected to said base includes shaping a same work piece that said base is formed from.
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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130114204A1 (en) * 2011-11-04 2013-05-09 Apple Inc. Heat removal system for computing systems
US20130168061A1 (en) * 2011-12-28 2013-07-04 Hon Hai Precision Industry Co., Ltd. Heat dissipation assembly
US20130250577A1 (en) * 2012-03-26 2013-09-26 Kabushiki Kaisha Toshiba Lighting unit and lighting device
CN103683557A (en) * 2012-08-31 2014-03-26 现代摩比斯株式会社 Cooling structure of stator
US20150369486A1 (en) * 2014-06-19 2015-12-24 Mitsubishi Hitachi Power Systems, Ltd. Heat-Transfer Device and Gas Turbine Combustor with Same
US9423189B2 (en) * 2012-11-19 2016-08-23 Acer Incorporated Fluid heat exchange apparatus
US20170231115A1 (en) * 2016-02-10 2017-08-10 Omron Automotive Electronics Co., Ltd. Cooler and flow path unit
JP2018063105A (en) * 2016-08-31 2018-04-19 ユニゾン・インダストリーズ,エルエルシー Engine heat exchanger and method of forming
US11125434B2 (en) * 2018-12-10 2021-09-21 Raytheon Technologies Corporation Preferential flow distribution for gas turbine engine component
US11209223B2 (en) * 2019-09-06 2021-12-28 Hamilton Sundstrand Corporation Heat exchanger vane with partial height airflow modifier
CN114152402A (en) * 2022-02-07 2022-03-08 中国空气动力研究与发展中心低速空气动力研究所 Wind tunnel test water content measuring device
US11965702B1 (en) * 2022-10-21 2024-04-23 Amulaire Thermal Technology, Inc. Low pressure drop automotive liquid-cooling heat dissipation plate and enclosed automotive liquid-cooling cooler having the same

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11639828B2 (en) * 2020-06-25 2023-05-02 Turbine Aeronautics IP Pty Ltd Heat exchanger

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3548927A (en) * 1968-11-29 1970-12-22 Intern Electronic Research Co Heat dissipating retainer for electronic component
US4009752A (en) * 1975-02-24 1977-03-01 Honeywell Information Systems Inc. Warp-resistant heat sink
US5021924A (en) * 1988-09-19 1991-06-04 Hitachi, Ltd. Semiconductor cooling device
US5194935A (en) * 1990-01-29 1993-03-16 Hitachi, Ltd. Plastic encapsulated semiconductor device and structure for mounting the same devices having particular radiating fin structure
US5518071A (en) * 1993-03-31 1996-05-21 Lee; Yong N. Heat sink apparatus
US6942025B2 (en) * 2000-09-20 2005-09-13 Degree Controls, Inc. Uniform heat dissipating and cooling heat sink

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1743861A (en) * 1925-09-25 1930-01-14 Arthur B Modine Radiator construction
US3524497A (en) * 1968-04-04 1970-08-18 Ibm Heat transfer in a liquid cooling system
US4984626A (en) * 1989-11-24 1991-01-15 Carrier Corporation Embossed vortex generator enhanced plate fin
WO1995025255A1 (en) * 1992-09-28 1995-09-21 Aavid Engineering, Inc. Apparatus and method for cooling heat generating electronic components in a cabinet
US6820682B2 (en) * 2000-12-19 2004-11-23 Denso Corporation Heat exchanger
TW200503608A (en) * 2003-07-15 2005-01-16 Ind Tech Res Inst Cooling plate having vortices generator
US20090065177A1 (en) * 2007-09-10 2009-03-12 Chien Ouyang Cooling with microwave excited micro-plasma and ions
US7961462B2 (en) * 2009-05-28 2011-06-14 Alcatel Lucent Use of vortex generators to improve efficacy of heat sinks used to cool electrical and electro-optical components

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3548927A (en) * 1968-11-29 1970-12-22 Intern Electronic Research Co Heat dissipating retainer for electronic component
US4009752A (en) * 1975-02-24 1977-03-01 Honeywell Information Systems Inc. Warp-resistant heat sink
US5021924A (en) * 1988-09-19 1991-06-04 Hitachi, Ltd. Semiconductor cooling device
US5194935A (en) * 1990-01-29 1993-03-16 Hitachi, Ltd. Plastic encapsulated semiconductor device and structure for mounting the same devices having particular radiating fin structure
US5518071A (en) * 1993-03-31 1996-05-21 Lee; Yong N. Heat sink apparatus
US6942025B2 (en) * 2000-09-20 2005-09-13 Degree Controls, Inc. Uniform heat dissipating and cooling heat sink

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130114204A1 (en) * 2011-11-04 2013-05-09 Apple Inc. Heat removal system for computing systems
US20130168061A1 (en) * 2011-12-28 2013-07-04 Hon Hai Precision Industry Co., Ltd. Heat dissipation assembly
US20130250577A1 (en) * 2012-03-26 2013-09-26 Kabushiki Kaisha Toshiba Lighting unit and lighting device
EP2644990A3 (en) * 2012-03-26 2013-11-13 Toshiba Lighting&Technology Corporation Lighting unit and lighting device
US9194568B2 (en) * 2012-03-26 2015-11-24 Toshiba Lighting & Technology Corporation Lighting unit and lighting device
CN103683557A (en) * 2012-08-31 2014-03-26 现代摩比斯株式会社 Cooling structure of stator
US9423189B2 (en) * 2012-11-19 2016-08-23 Acer Incorporated Fluid heat exchange apparatus
US10480789B2 (en) * 2014-06-19 2019-11-19 Mitsubishi Hitachi Power Systems, Ltd. Heat-transfer device and gas turbine combustor with same
US20150369486A1 (en) * 2014-06-19 2015-12-24 Mitsubishi Hitachi Power Systems, Ltd. Heat-Transfer Device and Gas Turbine Combustor with Same
US20170231115A1 (en) * 2016-02-10 2017-08-10 Omron Automotive Electronics Co., Ltd. Cooler and flow path unit
US10433457B2 (en) * 2016-02-10 2019-10-01 Omron Corporation Cooler and flow path unit
JP2018063105A (en) * 2016-08-31 2018-04-19 ユニゾン・インダストリーズ,エルエルシー Engine heat exchanger and method of forming
US10253785B2 (en) 2016-08-31 2019-04-09 Unison Industries, Llc Engine heat exchanger and method of forming
US10823201B2 (en) 2016-08-31 2020-11-03 Unison Industries, Llc Engine heat exchanger and method of forming
US11125434B2 (en) * 2018-12-10 2021-09-21 Raytheon Technologies Corporation Preferential flow distribution for gas turbine engine component
US11209223B2 (en) * 2019-09-06 2021-12-28 Hamilton Sundstrand Corporation Heat exchanger vane with partial height airflow modifier
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US11965702B1 (en) * 2022-10-21 2024-04-23 Amulaire Thermal Technology, Inc. Low pressure drop automotive liquid-cooling heat dissipation plate and enclosed automotive liquid-cooling cooler having the same

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