US20120043067A1 - Heat sink core member and its fabrication procedure - Google Patents

Heat sink core member and its fabrication procedure Download PDF

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Publication number
US20120043067A1
US20120043067A1 US12/885,573 US88557310A US2012043067A1 US 20120043067 A1 US20120043067 A1 US 20120043067A1 US 88557310 A US88557310 A US 88557310A US 2012043067 A1 US2012043067 A1 US 2012043067A1
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US
United States
Prior art keywords
heat sink
core member
tubular body
sink core
punch
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US12/885,573
Inventor
Tsung-Hsien Huang
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Individual
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Individual
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Publication of US20120043067A1 publication Critical patent/US20120043067A1/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/26Making specific metal objects by operations not covered by a single other subclass or a group in this subclass heat exchangers or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/10Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/12Tubular 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
    • F28F1/14Tubular 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 longitudinally
    • F28F1/20Tubular 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 longitudinally the means being attachable to the element
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/10Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/40Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only inside the tubular element
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/10Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/42Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being both outside and inside the tubular element
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L21/00Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
    • H01L21/02Manufacture or treatment of semiconductor devices or of parts thereof
    • H01L21/04Manufacture or treatment of semiconductor devices or of parts thereof the devices having at least one potential-jump barrier or surface barrier, e.g. PN junction, depletion layer or carrier concentration layer
    • H01L21/48Manufacture or treatment of parts, e.g. containers, prior to assembly of the devices, using processes not provided for in a single one of the subgroups H01L21/06 - H01L21/326
    • H01L21/4814Conductive parts
    • H01L21/4871Bases, plates or heatsinks
    • H01L21/4878Mechanical treatment, e.g. deforming
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L23/00Details of semiconductor or other solid state devices
    • H01L23/34Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements
    • H01L23/36Selection of materials, or shaping, to facilitate cooling or heating, e.g. heatsinks
    • H01L23/367Cooling facilitated by shape of device
    • H01L23/3672Foil-like cooling fins or heat sinks
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/10Heat sinks
    • 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
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L2924/00Indexing scheme for arrangements or methods for connecting or disconnecting semiconductor or solid-state bodies as covered by H01L24/00
    • H01L2924/0001Technical content checked by a classifier
    • H01L2924/0002Not covered by any one of groups H01L24/00, H01L24/00 and H01L2224/00
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4935Heat exchanger or boiler making
    • Y10T29/49377Tube with heat transfer means

Abstract

A heat sink core member made by: preparing a predetermined mass of aluminum block, extruding the aluminum block through an extruding machine into a tubular body having one close end wall and then punch-cutting the outside wall of the tubular body to form a plurality of densely distributed and equally spaced vertical retaining grooves. Radiation fins can easily be affixed to the vertical retaining grooves of the tubular body to form a heat sink.

Description

    BACKGROUND OF THE INVENTION
  • (a) Field of the Invention
  • The present invention relates to heat sink fabrication technology and more particularly to a method of making a heat sink core member by extruding a predetermined mass of aluminum block into a tubular body having one close end wall and then punch-cutting the outside wall of the tubular body to form a plurality of densely distributed and equally spaced vertical retaining grooves for easy mounting of radiation fins.
  • (b) Description of the Prior Art
  • A radiation fin type heat sink generally comprises a tubular core member and a plurality of radiation fins. The radiation fins are radially spaced around the periphery of the tubular core member. Because the radiation fins are integrally formed with the periphery of the tubular core member, the fabrication of the heat sink is complicated, and the cost is high. Further, due to technical limitation, the radiation fins have a thick wall thickness. In consequence, the heat sink is heavy. Due to a limited number of radiation fins, the heat dissipation efficiency of this kind of heat sink is limited.
  • During application, the tubular core member is attached with its one end to the heat source (CPU or LED device). A heat pipe may be attached to enhance heat dissipation performance. Further, the tubular core member may be made in the shape of a round tube, rectangular tube or polygonal tube.
  • There are known heat sinks in which the radiation fins are soldered to the periphery of the tubular core member. However, it takes much time and labor to solder every radiation fin to the periphery of the tubular core member. Before soldering, an electroplating technique may be necessary so that different metal materials can be soldered together. Further, this fabrication procedure is not environmentally friendly. Further, solder-bonding will lower heat transfer efficiency. Further, a heat sink may be directly cut from a solid aluminum block. This method wastes much labor and time and will produce many waste materials, increasing the cost considerably.
  • Further, a heat sink core member may be directly extruded from an aluminum ingot. This method is to extrude an aluminum ingot into a tubular member having longitudinal grooves spaced around the periphery. The tubular member is than cut into tubular core members subject to the desired length. Radiation fins are than fastened to the longitudinal grooves of each tubular core member. This fabrication procedure still has drawbacks as follows:
      • 1. Due to technical limitations, the number of the longitudinal grooves of the extruded heat sink core member is limited, and therefore only a limited number of radiation fins can be fastened to the periphery of the heat sink core member. When the number of the longitudinal grooves is increased, the wall structure of the heat sink core member under extrusion may be damaged.
      • 2. The finished heat sink core member is a hollow tubular member having two open ends. A plate member must be bonded to the heat sink core member to close its one end so that the blocked end of the heat sink core member can be attached to the heat source or used to support an attached member during application. However, because the plate member and the heat sink core member are not made integrally, a capillary effect will occur, lowering the heat transfer performance.
  • Therefore, it is desirable to provide a heat sink core member and its fabrication procedure that eliminates the drawbacks of the prior art designs and techniques.
  • SUMMARY OF THE INVENTION
  • The present invention has been accomplished under the circumstances in view. It is one object of the present invention to provide a heat sink core member fabrication procedure for making a heat sink core member by means of preparing a predetermined mass of aluminum block, and then extruding the aluminum block through an extruding machine into a tubular body having one close end wall and then punch-cutting the outside wall of the tubular body to form a plurality of densely distributed and equally spaced vertical retaining grooves. Thus, radiation fins can easily be affixed to the vertical retaining grooves of the tubular body to form a high-performance heat sink.
  • Using the heat sink core member fabrication procedure for making a heat sink core member of this application, the finished heat sink core member has a close end wall. As a result, the invention prevents a capillary effect, thus effectively facilitating heat transfer.
  • In the heat sink core member fabrication procedure for making a heat sink core member of the present application, the punch-cutting step may include three substeps, i.e., the coarse punch-cutting substep to punch-cut the outside wall of said tubular body into a predetermined number of rough grooves, the fine punch-cutting substep to punch-cut each said rough groove into a fine groove, and the superfine punch-cutting substep to punch-cut each said fine groove. These substeps are performed automatically for facilitating the fabrication and saving the fabrication time and labor.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a heat sink core member fabrication procedure in accordance with the present invention.
  • FIG. 2 is an alternate form of the heat sink core member fabrication procedure in accordance with the present invention.
  • FIG. 3 illustrates a circular aluminum block prepared according to the present invention.
  • FIG. 4 illustrates a rectangular aluminum block prepared according to the present invention.
  • FIG. 5 illustrates a round tubular body extruded according to the present invention.
  • FIG. 6 is a sectional view of FIG. 5.
  • FIG. 7 is a top view of FIG. 5.
  • FIG. 8 illustrates a rectangular tubular body extruded according to the present invention.
  • FIG. 9 is a sectional view of FIG. 8.
  • FIG. 10 is a top view of FIG. 8.
  • FIG. 11 is an oblique elevation of a round tube-like heat sink core member prepared according to the present invention.
  • FIG. 12 is a sectional view of FIG. 11.
  • FIG. 13 is a top view of FIG. 11.
  • FIG. 14 is an oblique elevation of a rectangular tube-like heat sink core member prepared according to the present invention.
  • FIG. 15 is a sectional view of FIG. 14.
  • FIG. 16 is a top view of FIG. 14.
  • FIG. 17 is a schematic sectional view, illustrating radiation fins inserted to the respective vertical retaining grooves of a round tube-like heat sink core member according to the present invention.
  • FIG. 18 corresponds to FIG. 17, illustrating the radiation fins affixed to the respective vertical retaining grooves.
  • FIG. 19 is an oblique elevation of a heat sink based on a round tube-like heat sink core member according to the present invention.
  • FIG. 20 is an oblique elevation of a heat sink based on a rectangular tube-like heat sink core member according to the present invention.
  • DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
  • As described in FIG. 1, a predetermined mass of aluminum block 1 (see FIG. 3 or FIG. 4) is extruded through an extruding machine into a tubular body 10 having one close end wall 11 (see FIGS. 5˜7 or FIGS. 8˜10), and then the outside wall of the tubular body 10 is punch-cut to form a plurality of vertical retaining grooves 12 that are equally spaced around the periphery in a densely distributed manner (see FIGS. 11˜13 or FIGS. 14˜16), and thus a heat sink core member 100 is obtained. Radiation fins 200 can then be fastened to the retaining grooves 12 of the heat sink core member 100 (see FIG. 17 or FIG. 18) to form a heat sink 300 (see FIG. 19 or FIG. 20).
  • The heat sink core member fabrication procedure includes the steps of:
      • (1) preparing a predetermined mass of aluminum block 1;
      • (2) extruding the aluminum block 1 through an extruding machine into a tubular body 10 having one close end wall 11; and
      • (3) punch-cutting the outside wall of the tubular body 10 to form a plurality of densely distributed and equally spaced vertical retaining grooves 12.
  • As described in FIG. 2, the step of punch-cutting the outside wall of the tubular body 10 includes the substeps of coarse punch-cutting, fine punch-cutting and superfine punch-cutting. The coarse punch-cutting substep is to punch-cut the outside wall of the tubular body 10 into a predetermined number of rough grooves. The fine punch-cutting substep is to punch-cut each rough groove into a fine groove substantially close to the predetermined size. The superfine punch-cutting substep is to punch-cut each fine groove again, modifying the size of each fine groove into one respective finished vertical retaining groove 12. By means of performing one coarse punch-cutting substep, at least one fine punch-cutting substep and at least one superfine punch-cutting substep, the outside wall of the tubular body 10 is rapidly and efficiently processed to form the desired, densely distributed and equally spaced vertical retaining grooves 12. These substeps are performed automatically for facilitating the fabrication and saving much the fabrication time and labor.
  • Further, during the extrusion step, vertical ribs 13 are formed on the inside wall of the tubular body 10 (see FIGS. 5˜7 or FIGS. 8˜10). Further, a hole-drilling step may be performed to make a mounting hole 14 on each vertical rib 13 (see FIG. 11 or FIG. 14), for mounting of an attached member. One or more mounting holes may be formed in the close end wall 11 of the tubular body 10 for the mounting of an attached member.
  • Further, the tubular body 10 can be made in any of a variety of shapes and dimensions. For example, the tubular body 10 can be shaped like a round tube as shown in FIGS. 5˜7. Alternatively, the tubular body 10 can be shaped like a rectangular tube as shown in FIGS. 8˜10.
  • Further, the radiation fins 200 to be fastened to the tubular body 10 can be made in any of a variety of shapes and sizes. However, the radiation fins 200 must be configured for press-fitting into or riveting to the vertical retaining grooves 12.
  • Further, the vertical retaining grooves 12 may be variously configured. Preferably, the outside wall of the tubular body 10 is so punch-cut that a first protruding portion 121 and a second protruding portion 122 are formed and disposed along two opposite lateral sides of each vertical retaining groove 12. After one radiation fin 200 is inserted into one vertical retaining groove 12, the adjacent first protruding portion 121 is deformed in the direction toward the adjacent second protruding portion 121 to have the radiation fin 200 be firmly seized in between the first protruding portion 121 and the second protruding portion 122 (see FIG. 18).
  • Although particular embodiments of the invention have been described in detail for purposes of illustration, various modifications and enhancements may be made without departing from the spirit and scope of the invention. Accordingly, the invention is not to be limited except as by the appended claims.

Claims (13)

What is claimed is:
1. A heat sink core member fabrication procedure, comprising the steps of:
(a) preparing a predetermined mass of aluminum block;
(b) extruding said aluminum block through an extruding machine into a tubular body having one close end wall; and
(c) punch-cutting the outside wall of said tubular body to form a plurality of densely distributed and equally spaced vertical retaining grooves.
2. The heat sink core member fabrication procedure as claimed in claim 1, wherein said step (c) comprises a coarse punch-cutting substep to punch-cut the outside wall of said tubular body into a predetermined number of rough grooves, a fine punch-cutting substep to punch-cut each said rough groove into a fine groove, and a superfine punch-cutting substep to punch-cut each said fine groove.
3. The heat sink core member fabrication procedure as claimed in claim 1, wherein said step (b) extrudes said aluminum block through an extruding machine into a tubular body having one close end wall and a plurality of vertical ribs on the inside wall thereof.
4. The heat sink core member fabrication procedure as claimed in claim 3, further comprising a substep of making a plurality of mounting holes on said vertical ribs after said step (b) and before said step (c).
5. The heat sink core member fabrication procedure as claimed in claim 1, further comprising a substep of making a plurality of mounting holes on said close end wall of said tubular body after said step (b) and before said step (c).
6. The heat sink core member fabrication procedure as claimed in claim 1, wherein said tubular body is in a shape of a round tube.
7. The heat sink core member fabrication procedure as claimed in claim 1, wherein said tubular body is in a shape of a rectangular tube.
8. A heat sink core member comprising a tubular body, a close end wall located on one end of said tubular body, and a plurality of vertical retaining grooves equally spaced around the periphery of said tubular body for the mounting of one radiation fin in each said vertical retaining groove.
9. The heat sink core member as claimed in claim 8, wherein said tubular body comprises a plurality of first protruding portions and a plurality of second protruding portions respectively extending along said vertical retaining grooves at two opposite sides.
10. The heat sink core member as claimed in claim 8, further comprising a plurality of vertical ribs axially formed on an inside wall of said tubular body and a mounting hole located on one end of each said vertical rib.
11. The heat sink core member as claimed in claim 8, further comprising a plurality of mounting holes located on said close end wall.
12. The heat sink core member as claimed in claim 8, wherein said tubular body is in a shape of a round tube.
13. The heat sink core member as claimed in claim 8, wherein said tubular body is in a shape of a rectangular tube.
US12/885,573 2010-08-20 2010-09-20 Heat sink core member and its fabrication procedure Abandoned US20120043067A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
TW099127906 2010-08-20
TW099127906A TW201043357A (en) 2010-08-20 2010-08-20 Core tube base for heat radiator and method for manufacturing the same

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US20120043067A1 true US20120043067A1 (en) 2012-02-23

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US (1) US20120043067A1 (en)
JP (1) JP2012044129A (en)
KR (1) KR20120018039A (en)
DE (2) DE202010008604U1 (en)
TW (1) TW201043357A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130229071A1 (en) * 2012-03-05 2013-09-05 Johnson Electric S.A. Electric motor
CN103406737A (en) * 2013-08-21 2013-11-27 安徽鸿路钢结构(集团)股份有限公司 Double-angle tubular pillar assembling method
US20180054978A1 (en) * 2016-08-30 2018-03-01 GE Lighting Solutions, LLC Luminaire including a heat dissipation structure
US11313631B2 (en) * 2020-07-07 2022-04-26 Hfc Industry Limited Composite heat sink having anisotropic heat transfer metal-graphite composite fins

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CN102527758B (en) * 2012-01-20 2014-12-03 东莞汉旭五金塑胶科技有限公司 Extrusion moulding die for aluminum base of radiator and manufacture method thereof
CN102699632B (en) * 2012-06-04 2014-07-09 宁波安拓实业有限公司 Process for manufacturing lining blank of damper

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US20050211416A1 (en) * 2003-10-17 2005-09-29 Kenya Kawabata Heat sink with fins and a method for manufacturing the same
US20060042777A1 (en) * 2004-08-31 2006-03-02 Delano Andrew D Heat sink fin with stator blade
US7028757B1 (en) * 2004-10-21 2006-04-18 Hewlett-Packard Development Company, L.P. Twin fin arrayed cooling device with liquid chamber
US7296619B2 (en) * 2004-10-21 2007-11-20 Hewlett-Packard Development Company, L.P. Twin fin arrayed cooling device with heat spreader
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US20090147520A1 (en) * 2007-12-07 2009-06-11 Fu Zhun Precision Industry (Shen Zhen) Co., Ltd. Led lamp with a heat sink
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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130229071A1 (en) * 2012-03-05 2013-09-05 Johnson Electric S.A. Electric motor
US9154013B2 (en) * 2012-03-05 2015-10-06 Johnson Electric S.A. Electric motor
CN103406737A (en) * 2013-08-21 2013-11-27 安徽鸿路钢结构(集团)股份有限公司 Double-angle tubular pillar assembling method
US20180054978A1 (en) * 2016-08-30 2018-03-01 GE Lighting Solutions, LLC Luminaire including a heat dissipation structure
US11134618B2 (en) * 2016-08-30 2021-10-05 Current Lighting Solutions, Llc Luminaire including a heat dissipation structure
US11313631B2 (en) * 2020-07-07 2022-04-26 Hfc Industry Limited Composite heat sink having anisotropic heat transfer metal-graphite composite fins

Also Published As

Publication number Publication date
DE102011000230A1 (en) 2012-02-23
TWI373385B (en) 2012-10-01
DE202010008604U1 (en) 2011-05-12
JP2012044129A (en) 2012-03-01
TW201043357A (en) 2010-12-16
KR20120018039A (en) 2012-02-29

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