US20050284616A1 - Advanced microelectronic heat dissipation package and method for its manufacture - Google Patents

Advanced microelectronic heat dissipation package and method for its manufacture Download PDF

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US20050284616A1
US20050284616A1 US11/141,885 US14188505A US2005284616A1 US 20050284616 A1 US20050284616 A1 US 20050284616A1 US 14188505 A US14188505 A US 14188505A US 2005284616 A1 US2005284616 A1 US 2005284616A1
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heat
chip
copper
feedstock
cavities
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US11/141,885
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Randall German
Lye-King Tan
John Johnson
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Advanced Materials Technology Pte Ltd
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Advanced Materials Technology Pte Ltd
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    • 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
    • H01L23/42Fillings or auxiliary members in containers or encapsulations selected or arranged to facilitate heating or cooling
    • H01L23/427Cooling by change of state, e.g. use of heat pipes
    • 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
    • F28D15/00Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • F28D15/0275Arrangements for coupling heat-pipes together or with other structures, e.g. with base blocks; Heat pipe cores
    • 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
    • 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
    • F28D15/00Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • F28D2015/0225Microheat pipes
    • 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
    • Y10T29/49353Heat pipe device making

Definitions

  • the invention relates to the general field of microelectronics with particular reference to packaging and heat dissipation.
  • microelectronic devices are running into basic barriers related to heat dissipation.
  • Options under exploration include active and passive packaging designs.
  • the active designs require fans or pumps to circulate fluids for heat extraction, often leading to heat generation, power drain, and new failure modes.
  • the alternative is to move into passive designs, such as fins to radiate heat into the enclosure.
  • High thermal conductivity materials are desirable for heat dissipation, and current favorites include tungsten-copper, molybdenum-copper, and aluminum or copper. The latter choices suffer from high thermal expansion coefficients which induce a new failure mechanism through thermal fatigue, associated with turning on (heating up) and turning off (cooling down) an electronic device. In order to sustain the desired thermal expansion match with silicon while maximizing thermal conductivity, the top materials then tend to be heavy, expensive, and modest in thermal conductivity. Only diamond provides a high thermal conductivity with low thermal expansion, but its cost is prohibitive.
  • two-material powder injection molding This step toward functionality directly built into a device has potential benefits in microelectronic packaging.
  • the walls might be fabricated from a good glass-sealing alloy, such as kovar, while the base would be fabricated from a low thermal expansion material, such as tungsten-copper.
  • tungsten-copper is capable of thermal conductivities in the 200 W/m/K range. This is still half that possible with pure copper, but, again, still fails to satisfy the thermal expansion requirement.
  • diamond can achieve 2000 W/m/K.
  • the present invention makes use of two-material powder injection molding to implement a different approach to this problem.
  • This process has been described in application Ser. No. 09/733,527 Dec. 11, 2000 “Method to form multi-material components”. Briefly, this process shows how powder injection molding may be used to form a continuous body having multiple parts, each of which has different physical properties such as magnetic characteristics or hardness. This is accomplished through careful control of the relative shrinkage rates of these various parts. Additionally, care is taken to ensure that only certain selected physical properties are allowed to differ between the parts while others may be altered through relatively small changes in the composition of the feedstocks used.
  • Another object of at least one embodiment of the present invention has been that said heat pipe be readily made part of a package suitable for housing, and rapidly removing, heat generated by a semiconductor chip.
  • a further object of at least one embodiment of the present invention has been to provide a process for manufacturing said chip package.
  • the lower portion of the package is formed first as an initial green part which includes one or more cavities.
  • the latter if their dimensions exceed about 1,000 microns, are then filled with a feedstock that is designed to produce a porous material lining after sintering. Cavities with dimensions less than about 1,000 microns may be left unfilled.
  • a working fluid is introduced into the cavities and sealed, thereby forming one or more heat pipes located directly below the chip. The latter is sealed inside an enclosure. During operation, heat generated by the chip is efficiently transferred to points outside the enclosure. A process for manufacturing the structure is described.
  • FIG. 1 is a plan view of the structure of the present invention.
  • FIG. 4 is an isometric representation of FIGS. 1, 2 , and 3 .
  • FIG. 5 is a flow chart summarizing the principal steps of the process of the present invention.
  • the present invention discloses a novel functional design that is material based on selective porosity embedded at desired locations in a microelectronic package. These are placed directly in the microelectronic package under the semiconductor chip to afford the greatest heat dissipation.
  • the purpose of the selective porosity is to enable wicking of the condensed working fluid, such-as alcohol or water, from a cold region back to a hot region.
  • the liquid phase evaporates from the hot region, thereby consuming the enthalpy (heat content) of evaporation.
  • the vapor now migrates through a channel to a cold region where it redeposits the enthalpy via condensation.
  • Heat pipes Such behavior is well known as heat pipe technology, such heat pipes being used as structures for the transport of heat via evaporation and condensation of a working fluid in a porous pipe or wick. Heat pipes can deliver from 50,000 to 200,000 W/m/K in equivalent thermal conductivity.
  • the present invention teaches how two-material injection molding technology can be applied to the fabrication of high heat dissipation microelectronic packages. This is achieved by first injection molding the housing with cavities located in appropriate places.
  • One means for achieving this goal would be to use a sacrificial material insert in the mold, but a preferred means is to use the two-color metal powder injection molding technology already known to AMT.
  • a low packing density powder feedstock is injection molded into the pattern of the heat pipe located in the overall package.
  • Controlled porosity and pore size are possible by selection of the proper metal powder size and powder to polymer ratio. Additional control can be achieved by inclusion of sacrificial particles in the feedstock. The latter route provides precise control over the pore size and porosity, independent of the metal powder size, since the concentration and size of the sacrificial particles are independently controlled when batching the feedstock.
  • the component is subjected to normal debinding and sintering cycles. After sintering, the second material regions will be incompletely sintered, leaving behind the desired porosity and pores for the eventual creation of high thermal conductivity heat pipes. A working fluid is then dosed into the pores and the pore channels sealed by solder, plugging, or other mechanical or standard means. Since heat pipes dissipate 100 times more heat than diamond, the resulting microelectronic packages can far exceed what can be attained with current designs.
  • the approach taken by the present invention allows the fabrication of more complicated patterns, including curved and conformal cooling passages. Additionally, the present invention allows the fabrication of lightweight devices from aluminum or other low-density materials for portable devices, such as cellular telephones and laptop computers.
  • FIG. 1 shown there is a plan view of the structure. Its principal parts are a solid body 11 within which there are cavities such as 12 . These cavities have been lined with porous material 15 which is saturated with a working fluid. The unfilled portions of the cavities are open vapor channels.
  • the manufacturing process starts with the preparation of a feedstock made up of particles of the material from which solid body 11 is to be constructed, as well as a suitable binder (and possibly, for some materials, a fluxing agent).
  • suitable materials for these particles include, but are not limited to, copper, aluminum, tungsten, tungsten-copper, kovar, stainless steel, or nickel alloys.
  • the particles are carefully chosen for their ability to sinter density to near 100% of the materials theoretical density. Generally, this requires a mean particle size less than 30 ⁇ m, but is material dependent. For example, tungsten-based materials generally require a mean particle size less 5 ⁇ m.
  • Suitable binder materials include combinations of waxes, organic polymers, and surface active agents, such as stearic acid. These binders are melted and the particles are uniformly dispersed within them. Typically, the particles compose 50-65 percent of the total volume of feedstock while the binder composes the rest.
  • inserts Prior to injection of the feedstock, inserts are added to the mold. These have the shape of the cavities 12 that are to be formed and are placed in the appropriate locations. At this stage, the cavities will always have at least one open end although more complicated designs may require two or more open ends per cavity. Typically, a simple straight cavity as exemplified by 12 in the figures would be between about 2 and 8 mm wide, 2 and 5 mm deep, and between 12 and 60 mm long.
  • a second set of inserts Prior to injection of the second feedstock, a second set of inserts are added to the green body. These have the shape of the vapor channels within the cavities 12 that are to be left open. They may be made out of the same types of sacrificial or reusable materials as the first set of inserts. With the second feedstock heated and the initial green body with insert(s) in place, a second molding under pressure takes place, resulting in the formation of the final green body. Cavities with dimensions less than about 1000 ⁇ m can be left unfilled.
  • the process now continues with routine removal of all binding materials from the final green body resulting in the formation of a skeleton structure.
  • the latter is then sintered to form the final body.
  • the step of sintering consists of heating at a temperature and time and in an atmosphere that depends on the composition of the body.
  • a copper body is sintered at a temperature between about 900 and 1070° C. for between 5 and 120 minutes in an atmosphere of hydrogen.
  • an important feature of the process is the control of the nature and concentration of the various binders used to form the feedstocks so as to ensure that porous and dense portions of the structure shrink by the same amount during sintering. Details about this aspect of the invention can be found in the aforementioned application Ser. No. 09/733,527 filed Dec. 11, 2000.
  • the next step is the introduction of a working fluid into the cavity so that it may function as a wick.
  • the working fluid must have a triple point below its operational temperature and a critical point above its operational temperature. Typically, the working fluid will have a triple point below 20° C. and a critical point above 100° C.
  • Examples of liquids suitable for use as a working fluid include, but are not limited to, water, ammonia, acetone, and alcohol.
  • the working fluid occupies enough of the cavity volume to saturate the wick. This is accomplished by first evacuating the cavity under vacuum, charging the cavity with the fluid, then sealing all open ends with plugs 13 , thereby forming the heat pipe. Possible ways to seal the cavities include, but are not limited to, epoxying, welding, crimping, soldering, and press fitting.
  • Enclosure 14 is then formed on the upper surface of body 11 . This is best seen in FIG. 2 which is a cross-section taken through 2 - 2 in FIG. 1 . Enclosure 14 is placed directly over one or more of the heat pipes. Cross-section 3 - 3 can be viewed in FIG. 3 which also shows the direction of heat flow.
  • hot spot 31 generally the underside of a chip
  • heat is transferred by conduction through solid body 11 to the porous wick 32 where it causes the working fluid to evaporate and expand along the vapor space in directions 33 , carrying the heat with it.
  • the hot vapor passes outside the sphere of influence of hot spot 31 it condenses back to liquid, as symbolized by arrows 34 . As the liquid concentration builds up there, capillary forces draw it back through the porous wick 32 toward hot spot 31 where the cycle can begin again.
  • FIG. 4 is an isometric view of the structure showing a chip 41 in place inside enclosure 14 . Not shown in FIG. 4 are contact pads, formed inside enclosure 14 to receive chip 41 , together with leads, connected to these contact pads that extend away from the chip to terminate outside the enclosure.
  • a 99.85% pure copper powder with a mean particle size of 15 ⁇ m is mixed with an organic binder composed of paraffin wax, micropulver wax, polyethylene, and stearic acid to form a first feedstock.
  • Said 15 ⁇ m copper powder comprises 50 volume percent of the said first feedstock.
  • a 99.88% pure copper powder with a mean particle size of 50 ⁇ m is mixed with the same binder composition to form a second feedstock.
  • Said 50 ⁇ m copper powder comprises 35 vol. % of the said second feedstock.
  • the first feedstock is molded into the shape of a cylindrical housing measuring 18 mm long and 12.5 mm in diameter.
  • a cylindrical steel insert forms a cavity measuring 16 mm long and 5 mm in diameter.
  • a 16 mm long and 3 mm in diameter insert consisting of polyethylene and 20% paraffin wax is then added to the cavity of the green housing and the second feedstock is molded into the open portion of the cavity.
  • the green body is freed of all organic binder by heating in a controlled furnace over a period of 25 hours at 600° C. in a hydrogen atmosphere.
  • the debound body is heated to 1050° C. at a rate of 350° C./hr in a hydrogen atmosphere. After sintering at 1050° C. for two hours, the furnace is allowed to cool. This results in a housing with a density of about 8.6 g/cm 3 , which is close to its theoretical density, and a porous layer within the housing with a density of about 60% of theoretical.

Abstract

Heat dissipation during the operation of integrated circuit chips is an old problem that continues to get worse. The present invention significantly ameliorates this by placing an embedded heat pipe directly beneath the chip. Using powder injection molding, the lower portion of the package is formed first as an initial green part which includes one or more cavities. The latter are then lined with a feedstock that is designed to produce a porous material after sintering, at which time a working fluid is introduced into the porous cavities and sealed, thereby forming one or more heat pipes located directly below the chip. The latter is then sealed inside an enclosure. During operation, heat generated by the chip is efficiently transferred to points outside the enclosure. A process for manufacturing the structure is also described.

Description

    FIELD OF THE INVENTION
  • The invention relates to the general field of microelectronics with particular reference to packaging and heat dissipation.
  • BACKGROUND OF THE INVENTION
  • As the world moves towards higher performance communication and computer systems, microelectronic devices are running into basic barriers related to heat dissipation. Options under exploration include active and passive packaging designs. The active designs require fans or pumps to circulate fluids for heat extraction, often leading to heat generation, power drain, and new failure modes. The alternative is to move into passive designs, such as fins to radiate heat into the enclosure.
  • High thermal conductivity materials are desirable for heat dissipation, and current favorites include tungsten-copper, molybdenum-copper, and aluminum or copper. The latter choices suffer from high thermal expansion coefficients which induce a new failure mechanism through thermal fatigue, associated with turning on (heating up) and turning off (cooling down) an electronic device. In order to sustain the desired thermal expansion match with silicon while maximizing thermal conductivity, the top materials then tend to be heavy, expensive, and modest in thermal conductivity. Only diamond provides a high thermal conductivity with low thermal expansion, but its cost is prohibitive.
  • In recent years, we have made progress in designing improved functionality into a structure through the combination of two different materials using a process termed two-material powder injection molding. This step toward functionality directly built into a device has potential benefits in microelectronic packaging. The walls might be fabricated from a good glass-sealing alloy, such as kovar, while the base would be fabricated from a low thermal expansion material, such as tungsten-copper. However, even these two-material combinations are limited by the thermal conductivity of the base. Currently, tungsten-copper is capable of thermal conductivities in the 200 W/m/K range. This is still half that possible with pure copper, but, again, still fails to satisfy the thermal expansion requirement. We note that diamond can achieve 2000 W/m/K.
  • As will become clear later, the present invention makes use of two-material powder injection molding to implement a different approach to this problem. This process has been described in application Ser. No. 09/733,527 Dec. 11, 2000 “Method to form multi-material components”. Briefly, this process shows how powder injection molding may be used to form a continuous body having multiple parts, each of which has different physical properties such as magnetic characteristics or hardness. This is accomplished through careful control of the relative shrinkage rates of these various parts. Additionally, care is taken to ensure that only certain selected physical properties are allowed to differ between the parts while others may be altered through relatively small changes in the composition of the feedstocks used.
  • A routine search of the prior art was performed and the following U.S. Patents were found to be of interest:
  • U.S. Pat. No. 6,410,982 (Brownell et al.); U.S. Pat. No. 6,321,452 (Lin); U.S. Pat. No. 6,385,044 (Colbert at al); U.S. Pat. No. 6,370,749 (Tseng et al.); U.S. Pat. No. 6,303,191 (Henne et al.); U.S. Pat. No. 6,293,333 (Ponnappan et al.); U.S. Pat. No. 6,230,407 (Akutsu); and U.S. Pat. No. 6,070,654 (Ito).
  • Additionally, the following publications were discovered during our search:
  • 1. B. R. Babin, G. P. Peterson, and D. Wu, “Steady-State Modeling and Testing of a Micro Heat Pipe,” Journal of Heat Transfer, vol. 112, August 1990, pp. 595-601.
  • 2. J. P. Longtin, B. Badran, and F. M. Gemer, “A One-Dimensional Model of a Micro Heat Pipe During Steady State Operation,” Journal of Heat Transfer, vol. 116, August 1994, pp. 709-715.
  • 3. L. W. Swanson, “Heat Pipes,” The CRC Handbook of Thermal Engineering, F. Kreith (ed.) CRC Press, NY, 2000, pp. 4.419-4.429.
  • SUMMARY OF THE INVENTION
  • It has been an object of at least one embodiment of the present invention to provide a heat pipe that can be cheaply produced and readily miniaturized.
  • Another object of at least one embodiment of the present invention has been that said heat pipe be readily made part of a package suitable for housing, and rapidly removing, heat generated by a semiconductor chip.
  • Still another object of at least one embodiment of the present invention has been to provide a process for manufacturing said heat pipe.
  • A further object of at least one embodiment of the present invention has been to provide a process for manufacturing said chip package.
  • These objects have been achieved by placing an embedded heat pipe directly beneath the chip. Using powder injection molding, the lower portion of the package is formed first as an initial green part which includes one or more cavities. The latter, if their dimensions exceed about 1,000 microns, are then filled with a feedstock that is designed to produce a porous material lining after sintering. Cavities with dimensions less than about 1,000 microns may be left unfilled. After sintering, a working fluid is introduced into the cavities and sealed, thereby forming one or more heat pipes located directly below the chip. The latter is sealed inside an enclosure. During operation, heat generated by the chip is efficiently transferred to points outside the enclosure. A process for manufacturing the structure is described.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a plan view of the structure of the present invention.
  • FIGS. 2 and 3 are cross-sections through two different planes of the structure seen in FIG. 1.
  • FIG. 4 is an isometric representation of FIGS. 1, 2, and 3.
  • FIG. 5 is a flow chart summarizing the principal steps of the process of the present invention.
  • DESCRIPTION OF THE PREFERRED EMBODIMENTS
  • The present invention discloses a novel functional design that is material based on selective porosity embedded at desired locations in a microelectronic package. These are placed directly in the microelectronic package under the semiconductor chip to afford the greatest heat dissipation. The purpose of the selective porosity is to enable wicking of the condensed working fluid, such-as alcohol or water, from a cold region back to a hot region. The liquid phase evaporates from the hot region, thereby consuming the enthalpy (heat content) of evaporation. The vapor now migrates through a channel to a cold region where it redeposits the enthalpy via condensation. Such behavior is well known as heat pipe technology, such heat pipes being used as structures for the transport of heat via evaporation and condensation of a working fluid in a porous pipe or wick. Heat pipes can deliver from 50,000 to 200,000 W/m/K in equivalent thermal conductivity.
  • Structures of the type described above are relatively expensive and not well suited for incorporation in a microelectronic packaging scheme. The present invention teaches how two-material injection molding technology can be applied to the fabrication of high heat dissipation microelectronic packages. This is achieved by first injection molding the housing with cavities located in appropriate places. One means for achieving this goal would be to use a sacrificial material insert in the mold, but a preferred means is to use the two-color metal powder injection molding technology already known to AMT.
  • In this latter case, hard tooling inserts form the cooling pattern during the first molding. In the second stage of injection molding, a low packing density powder feedstock is injection molded into the pattern of the heat pipe located in the overall package. Controlled porosity and pore size are possible by selection of the proper metal powder size and powder to polymer ratio. Additional control can be achieved by inclusion of sacrificial particles in the feedstock. The latter route provides precise control over the pore size and porosity, independent of the metal powder size, since the concentration and size of the sacrificial particles are independently controlled when batching the feedstock.
  • After the second step in injection molding, the component is subjected to normal debinding and sintering cycles. After sintering, the second material regions will be incompletely sintered, leaving behind the desired porosity and pores for the eventual creation of high thermal conductivity heat pipes. A working fluid is then dosed into the pores and the pore channels sealed by solder, plugging, or other mechanical or standard means. Since heat pipes dissipate 100 times more heat than diamond, the resulting microelectronic packages can far exceed what can be attained with current designs.
  • The approach taken by the present invention allows the fabrication of more complicated patterns, including curved and conformal cooling passages. Additionally, the present invention allows the fabrication of lightweight devices from aluminum or other low-density materials for portable devices, such as cellular telephones and laptop computers.
  • We will describe the present invention in terms of a process for its manufacture. This description will also further clarify the structure of the present invention. Referring now to FIG. 1, shown there is a plan view of the structure. Its principal parts are a solid body 11 within which there are cavities such as 12. These cavities have been lined with porous material 15 which is saturated with a working fluid. The unfilled portions of the cavities are open vapor channels.
  • The manufacturing process starts with the preparation of a feedstock made up of particles of the material from which solid body 11 is to be constructed, as well as a suitable binder (and possibly, for some materials, a fluxing agent). Suitable materials for these particles include, but are not limited to, copper, aluminum, tungsten, tungsten-copper, kovar, stainless steel, or nickel alloys. The particles are carefully chosen for their ability to sinter density to near 100% of the materials theoretical density. Generally, this requires a mean particle size less than 30 μm, but is material dependent. For example, tungsten-based materials generally require a mean particle size less 5 μm. Suitable binder materials include combinations of waxes, organic polymers, and surface active agents, such as stearic acid. These binders are melted and the particles are uniformly dispersed within them. Typically, the particles compose 50-65 percent of the total volume of feedstock while the binder composes the rest.
  • Prior to injection of the feedstock, inserts are added to the mold. These have the shape of the cavities 12 that are to be formed and are placed in the appropriate locations. At this stage, the cavities will always have at least one open end although more complicated designs may require two or more open ends per cavity. Typically, a simple straight cavity as exemplified by 12 in the figures would be between about 2 and 8 mm wide, 2 and 5 mm deep, and between 12 and 60 mm long. The inserts may be made of sacrificial materials such as organic polymers, including polyethylene, polypropylene, and polystyrene, so that the cavity is formed when they are removed through liquefaction, vaporization, or chemical action, or they may be made out of materials, such as bronze, steel, or alumina, which allows them to be removed intact for later reuse. The latter type of insert is to be preferred, for economic reasons, unless the shape of the cavity is such that the insert cannot be removed without changing the cavity's shape. With the feedstock heated and the insert(s) in place, molding under pressure takes place, resulting in the formation of the initial green body.
  • Cavities with dimensions greater than about 1000 μm in the green body are now partially filled with a second feedstock which was previously prepared from particles having a mean diameter between about 40 and 200 μm, uniformly dispersed within a suitable binder. Suitable materials for these particles include, but are not limited to copper, aluminum, tungsten, tungsten-copper, kovar, stainless steel, or nickel alloys. The larger size of the particles here ensures that the material that will be obtained after sintering will be porous. An additional degree of pore size control may be achieved by adding to the second feedstock particles of a sacrificial material such as graphite, which evacuates the structure during sintering, leaving behind voids. Typically, the volume fraction of the non-sacrificial particles in the mix is 30-40 percent of the total volume of the feedstock.
  • Prior to injection of the second feedstock, a second set of inserts are added to the green body. These have the shape of the vapor channels within the cavities 12 that are to be left open. They may be made out of the same types of sacrificial or reusable materials as the first set of inserts. With the second feedstock heated and the initial green body with insert(s) in place, a second molding under pressure takes place, resulting in the formation of the final green body. Cavities with dimensions less than about 1000 μm can be left unfilled.
  • The process now continues with routine removal of all binding materials from the final green body resulting in the formation of a skeleton structure. The latter is then sintered to form the final body. The step of sintering consists of heating at a temperature and time and in an atmosphere that depends on the composition of the body. For example, a copper body is sintered at a temperature between about 900 and 1070° C. for between 5 and 120 minutes in an atmosphere of hydrogen. Note that an important feature of the process (though not part of the present invention) is the control of the nature and concentration of the various binders used to form the feedstocks so as to ensure that porous and dense portions of the structure shrink by the same amount during sintering. Details about this aspect of the invention can be found in the aforementioned application Ser. No. 09/733,527 filed Dec. 11, 2000.
  • The next step is the introduction of a working fluid into the cavity so that it may function as a wick. The working fluid must have a triple point below its operational temperature and a critical point above its operational temperature. Typically, the working fluid will have a triple point below 20° C. and a critical point above 100° C. Examples of liquids suitable for use as a working fluid include, but are not limited to, water, ammonia, acetone, and alcohol. The working fluid occupies enough of the cavity volume to saturate the wick. This is accomplished by first evacuating the cavity under vacuum, charging the cavity with the fluid, then sealing all open ends with plugs 13, thereby forming the heat pipe. Possible ways to seal the cavities include, but are not limited to, epoxying, welding, crimping, soldering, and press fitting.
  • Enclosure 14 is then formed on the upper surface of body 11. This is best seen in FIG. 2 which is a cross-section taken through 2-2 in FIG. 1. Enclosure 14 is placed directly over one or more of the heat pipes. Cross-section 3-3 can be viewed in FIG. 3 which also shows the direction of heat flow. Starting at hot spot 31 (generally the underside of a chip) heat is transferred by conduction through solid body 11 to the porous wick 32 where it causes the working fluid to evaporate and expand along the vapor space in directions 33, carrying the heat with it. Once the hot vapor passes outside the sphere of influence of hot spot 31 it condenses back to liquid, as symbolized by arrows 34. As the liquid concentration builds up there, capillary forces draw it back through the porous wick 32 toward hot spot 31 where the cycle can begin again.
  • The process concludes with the step of mounting the chip on the upper surface of body 11, using a high thermal conductivity medium, such as silver-filled epoxy, followed by sealing of enclosure 12 (with the chip inside it). Optionally, a high conductivity material such as helium may be sealed inside 14 together with the chip. FIG. 4 is an isometric view of the structure showing a chip 41 in place inside enclosure 14. Not shown in FIG. 4 are contact pads, formed inside enclosure 14 to receive chip 41, together with leads, connected to these contact pads that extend away from the chip to terminate outside the enclosure.
  • EXAMPLE
  • A 99.85% pure copper powder with a mean particle size of 15 μm is mixed with an organic binder composed of paraffin wax, micropulver wax, polyethylene, and stearic acid to form a first feedstock. Said 15 μm copper powder comprises 50 volume percent of the said first feedstock. A 99.88% pure copper powder with a mean particle size of 50 μm is mixed with the same binder composition to form a second feedstock. Said 50 μm copper powder comprises 35 vol. % of the said second feedstock. The first feedstock is molded into the shape of a cylindrical housing measuring 18 mm long and 12.5 mm in diameter.
  • A cylindrical steel insert forms a cavity measuring 16 mm long and 5 mm in diameter. A 16 mm long and 3 mm in diameter insert consisting of polyethylene and 20% paraffin wax is then added to the cavity of the green housing and the second feedstock is molded into the open portion of the cavity. The green body is freed of all organic binder by heating in a controlled furnace over a period of 25 hours at 600° C. in a hydrogen atmosphere. The debound body is heated to 1050° C. at a rate of 350° C./hr in a hydrogen atmosphere. After sintering at 1050° C. for two hours, the furnace is allowed to cool. This results in a housing with a density of about 8.6 g/cm3, which is close to its theoretical density, and a porous layer within the housing with a density of about 60% of theoretical.
  • Good bonding is observed between the porous layer and housing surface. This housing can then be charged with water and sealed for operation as a heat pipe for removing heat from a semiconductor chip, placed in an enclosure on one end of the cylindrical structure. The effectiveness of this design for power dissipation was confirmed by calculations that show that, at a nominal operating temperature of 40° C., the package is capable of transporting over 100 W of waste heat away from the chip. A flow chart for the above process in presented in FIG. 5.

Claims (6)

1-21. (canceled)
22. A heat pipe, for use with integrated circuits, comprising:
a solid body wherein is located a fully enclosed cavity whose diameter exceeds 1,000 microns, said cavity being lined with a porous material; and
a working fluid in said cavity.
23. The heat pipe described in claim 22 wherein said solid body is selected from the group consisting of copper, aluminum, tungsten, tungsten-copper, kovar, stainless steel, and nickel alloys.
24. The heat pipe described in claim 22 wherein said porous material is selected from the group consisting of copper, aluminum, tungsten, tungsten-copper, kovar, stainless steel, and nickel alloys.
25. The heat pipe described in claim 22 wherein said working fluid is selected from the group consisting of water, ammonia, acetone, and alcohol.
26-31. (canceled)
US11/141,885 2001-08-28 2005-06-01 Advanced microelectronic heat dissipation package and method for its manufacture Abandoned US20050284616A1 (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100139888A1 (en) * 2008-12-08 2010-06-10 Fu Zhun Precision Industry (Shen Zhen) Co., Ltd. Heat spreader and heat dissipation device using same
CN105157460A (en) * 2015-08-24 2015-12-16 东华大学 Pulsating heat pipe heat exchanger with ammonia water as media and stainless steel as materials

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004077051A (en) * 2002-08-20 2004-03-11 Sony Corp Heat transport device and its manufacturing method
KR100609014B1 (en) * 2004-02-27 2006-08-03 삼성전자주식회사 Thin film heat spreader and method for manufacturing the same
US7286359B2 (en) * 2004-05-11 2007-10-23 The U.S. Government As Represented By The National Security Agency Use of thermally conductive vias to extract heat from microelectronic chips and method of manufacturing
JP4714434B2 (en) 2004-07-20 2011-06-29 古河スカイ株式会社 Heat pipe heat sink
US20100229394A1 (en) * 2004-12-31 2010-09-16 Industrial Technology Research Institute Method for fabricating wick microstructures in heat pipes
TWI276767B (en) * 2004-12-31 2007-03-21 Ind Tech Res Inst Forming method for the micro wick structure inside the heat pipe
TWI288224B (en) * 2005-04-08 2007-10-11 Asustek Comp Inc Manufacturing method of heat pipe
CN1329707C (en) * 2005-06-28 2007-08-01 杨洪武 Wicking and bracing frame for inner cavity of integrated heat pipe radiator
TW200706100A (en) * 2005-07-29 2007-02-01 Hon Hai Prec Ind Co Ltd Heat sink
TWI317414B (en) * 2005-10-21 2009-11-21 Foxconn Tech Co Ltd Sintered heat pipe and method for manufacturing the same
US20080105413A1 (en) * 2006-10-16 2008-05-08 Yu-Huang Peng Manufacturing Method of Water Block
JP5112101B2 (en) * 2007-02-15 2013-01-09 株式会社東芝 Semiconductor package
US8356410B2 (en) * 2007-06-13 2013-01-22 The Boeing Company Heat pipe dissipating system and method
US20100028192A1 (en) * 2008-08-04 2010-02-04 Foxconn Technology Co., Ltd. Method for manufacturing a plate-type heat pipe
TW201113494A (en) * 2009-10-08 2011-04-16 Ying-Tung Chen Heat dissipation structure and manufacturing method thereof
US8759843B2 (en) 2011-08-30 2014-06-24 Abl Ip Holding Llc Optical/electrical transducer using semiconductor nanowire wicking structure in a thermal conductivity and phase transition heat transfer mechanism
US8723205B2 (en) 2011-08-30 2014-05-13 Abl Ip Holding Llc Phosphor incorporated in a thermal conductivity and phase transition heat transfer mechanism
US8710526B2 (en) 2011-08-30 2014-04-29 Abl Ip Holding Llc Thermal conductivity and phase transition heat transfer mechanism including optical element to be cooled by heat transfer of the mechanism
DE102012205590B4 (en) * 2012-04-04 2023-11-02 Robert Bosch Gmbh Arrangement with a power semiconductor, a circuit carrier, a capillary and/or porous body and a heat sink, method for producing an arrangement and method for operating cooling of a power semiconductor by means of a heat transport medium
CN103415192B (en) * 2013-08-20 2015-09-23 南京理工大学 Vapor chamber heat pipe/microchannel cold plates composite construction temperature equalization system
US9903275B2 (en) 2014-02-27 2018-02-27 Pratt & Whitney Canada Corp. Aircraft components with porous portion and methods of making
US9517507B2 (en) 2014-07-17 2016-12-13 Pratt & Whitney Canada Corp. Method of shaping green part and manufacturing method using same
US11397057B2 (en) * 2014-09-26 2022-07-26 Asia Vital Components Co., Ltd. Vapor chamber structure
WO2016071324A1 (en) * 2014-11-03 2016-05-12 At & S Austria Technologie & Systemtechnik Aktiengesellschaft Hermetically sealed heat pipe structure synthesized with support structure and method for producing it
US20160263656A1 (en) 2015-03-12 2016-09-15 Pratt & Whitney Canada Corp. Method of forming a component from a green part
BE1024200B1 (en) * 2016-05-13 2017-12-12 Centre De Recherches Metallurgiques Asbl - Centrum Voor Research In De Metallurgie Vzw DYNAMIC THERMAL CONTROL SYSTEM THROUGH PHASE CHANGE MATERIALS
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Citations (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3762011A (en) * 1971-12-16 1973-10-02 Trw Inc Method of fabricating a capillary heat pipe wick
US4106188A (en) * 1976-04-19 1978-08-15 Hughes Aircraft Company Transistor cooling by heat pipes
US4274479A (en) * 1978-09-21 1981-06-23 Thermacore, Inc. Sintered grooved wicks
US4588023A (en) * 1980-06-16 1986-05-13 Showa Aluminum Corporation Device for releasing heat
US4770238A (en) * 1987-06-30 1988-09-13 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Capillary heat transport and fluid management device
US4880052A (en) * 1989-02-27 1989-11-14 Thermacore, Inc. Heat pipe cooling plate
US4929414A (en) * 1988-10-24 1990-05-29 The United States Of America As Represented By The Secretary Of The Air Force Method of manufacturing heat pipe wicks and arteries
US4975225A (en) * 1989-03-07 1990-12-04 United Technologies Corporation Manufacture of monolithic, stiff, lightweight ceramic articles
USH971H (en) * 1988-10-24 1991-10-01 The United States Of America As Represented By The Secretary Of The Air Force Regidized porous material and method
US5253702A (en) * 1992-01-14 1993-10-19 Sun Microsystems, Inc. Integral heat pipe, heat exchanger, and clamping plate
US5283715A (en) * 1992-09-29 1994-02-01 International Business Machines, Inc. Integrated heat pipe and circuit board structure
US5317805A (en) * 1992-04-28 1994-06-07 Minnesota Mining And Manufacturing Company Method of making microchanneled heat exchangers utilizing sacrificial cores
US5325913A (en) * 1993-06-25 1994-07-05 The United States Of America As Represented By The Secretary Of The Navy Module cooling system
US5355942A (en) * 1991-08-26 1994-10-18 Sun Microsystems, Inc. Cooling multi-chip modules using embedded heat pipes
US5598632A (en) * 1994-10-06 1997-02-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method for producing micro heat panels
US5660229A (en) * 1992-04-22 1997-08-26 Sunkyong Industries Co., Ltd. Plate type heat transfer device
US5697428A (en) * 1993-08-24 1997-12-16 Actronics Kabushiki Kaisha Tunnel-plate type heat pipe
US5880524A (en) * 1997-05-05 1999-03-09 Intel Corporation Heat pipe lid for electronic packages
US5933323A (en) * 1997-11-05 1999-08-03 Intel Corporation Electronic component lid that provides improved thermal dissipation
US5956229A (en) * 1998-04-01 1999-09-21 Intel Corporation Injection molded thermal interface system
US6032726A (en) * 1997-06-30 2000-03-07 Solid State Cooling Systems Low-cost liquid heat transfer plate and method of manufacturing therefor
US6059001A (en) * 1994-04-15 2000-05-09 The United States Of America As Represented By The Secretary Of The Air Force Apparatus for manufacturing microtubes with axially variable geometries
US6062302A (en) * 1997-09-30 2000-05-16 Lucent Technologies Inc. Composite heat sink
US6070654A (en) * 1998-04-03 2000-06-06 Nissho Iwai Corporation Heat pipe method for making the same and radiating structure
US6133631A (en) * 1997-05-30 2000-10-17 Hewlett-Packard Company Semiconductor package lid with internal heat pipe
US6178088B1 (en) * 1998-01-27 2001-01-23 Lucent Technologies Inc. Electronic apparatus
US6191946B1 (en) * 2000-01-03 2001-02-20 Thermal Corp. Heat spreader with excess solder basin
US6194066B1 (en) * 1991-04-24 2001-02-27 The United States Of America As Represented By The Secretary Of The Air Force Microscopic tube devices and method of manufacture
US6230407B1 (en) * 1998-07-02 2001-05-15 Showa Aluminum Corporation Method of checking whether noncondensable gases remain in heat pipe and process for producing heat pipe
US6260613B1 (en) * 1999-01-05 2001-07-17 Intel Corporation Transient cooling augmentation for electronic components
US6282913B1 (en) * 1999-06-11 2001-09-04 Mitsubishi Denki Kabushiki Kaisha Water vaporization type cooling apparatus for heat-generating unit
US6293333B1 (en) * 1999-09-02 2001-09-25 The United States Of America As Represented By The Secretary Of The Air Force Micro channel heat pipe having wire cloth wick and method of fabrication
US6303191B1 (en) * 1997-01-29 2001-10-16 Deutsches Zentrum Fuer Luft -Und Raumfahrt E.V. Process for the production of a heat pipe
US6321452B1 (en) * 2000-03-20 2001-11-27 Liken Lin Method for manufacturing the heat pipe integrated into the heat sink
US6370749B1 (en) * 2000-11-24 2002-04-16 Chaun-Choung Technology Corp. Heat pipe shaping device
US6385044B1 (en) * 2001-07-27 2002-05-07 International Business Machines Corporation Heat pipe heat sink assembly for cooling semiconductor chips
US6410982B1 (en) * 1999-11-12 2002-06-25 Intel Corporation Heatpipesink having integrated heat pipe and heat sink
US20030000689A1 (en) * 2001-06-29 2003-01-02 Dah-Chyi Kuo Heat dissipater
US6679316B1 (en) * 2000-10-02 2004-01-20 The United States Of America As Represented By The Secretary Of The Air Force Passive thermal spreader and method
US6698502B1 (en) * 1999-06-04 2004-03-02 Lee Jung-Hyun Micro cooling device

Family Cites Families (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US492941A (en) * 1893-03-07 Lawn-mower
DE2120475A1 (en) * 1971-04-27 1972-11-02 Brown, Boveri & Cie Ag, 6800 Mannheim Heat pipe
US3993123A (en) * 1975-10-28 1976-11-23 International Business Machines Corporation Gas encapsulated cooling module
CA1066964A (en) * 1976-09-28 1979-11-27 Edna A. Dancy Fabrication of ceramic heat pipes
JPS5512327A (en) * 1978-07-07 1980-01-28 Ngk Spark Plug Co Ltd Method of fabricating heat pipe wick
JPS5936827B2 (en) * 1979-01-12 1984-09-06 日本電信電話株式会社 Integrated circuit device cooling equipment
US4323914A (en) * 1979-02-01 1982-04-06 International Business Machines Corporation Heat transfer structure for integrated circuit package
JPS60251390A (en) * 1984-05-28 1985-12-12 Matsushita Refrig Co Manufacture of heat pipe
JPS618594A (en) * 1984-06-25 1986-01-16 Fujikura Ltd Heat pipe and method of corrosion preventive treatment of inner surface thereof
USH858H (en) * 1988-10-24 1990-12-04 The United States Of America As Represented By The Secretary Of The Air Force Electrical battery cell wicking structure and method
US4885129A (en) * 1988-10-24 1989-12-05 The United States Of America As Represented By The Secretary Of The Air Force Method of manufacturing heat pipe wicks
US5032897A (en) * 1990-02-28 1991-07-16 International Business Machines Corp. Integrated thermoelectric cooling
US5404272A (en) * 1991-10-24 1995-04-04 Transcal Carrier for a card carrying electronic components and of low heat resistance
US5491362A (en) * 1992-04-30 1996-02-13 Vlsi Technology, Inc. Package structure having accessible chip
US5766615A (en) * 1992-11-13 1998-06-16 Isp Investments Inc. Compositions of insoluble film-forming polymers and uses therefor
US5309457A (en) * 1992-12-22 1994-05-03 Minch Richard B Micro-heatpipe cooled laser diode array
GB2278676B (en) * 1993-05-14 1997-05-07 Furukawa Electric Co Ltd Heat pipe type radiator and method for manufacturing same
US5704416A (en) * 1993-09-10 1998-01-06 Aavid Laboratories, Inc. Two phase component cooler
DE19805930A1 (en) * 1997-02-13 1998-08-20 Furukawa Electric Co Ltd Cooling arrangement for electrical component with heat convection line
US6745825B1 (en) * 1997-03-13 2004-06-08 Fujitsu Limited Plate type heat pipe
US5847925A (en) * 1997-08-12 1998-12-08 Compaq Computer Corporation System and method for transferring heat between movable portions of a computer
US6148906A (en) * 1998-04-15 2000-11-21 Scientech Corporation Flat plate heat pipe cooling system for electronic equipment enclosure
JP4177487B2 (en) * 1998-08-14 2008-11-05 株式会社フジクラ Heat pipe manufacturing method
US6118177A (en) * 1998-11-17 2000-09-12 Lucent Technologies, Inc. Heatspreader for a flip chip device, and method for connecting the heatspreader
US6261871B1 (en) * 1999-03-11 2001-07-17 Conexant Systems, Inc. Method and structure for temperature stabilization in flip chip technology
US6302192B1 (en) 1999-05-12 2001-10-16 Thermal Corp. Integrated circuit heat pipe heat spreader with through mounting holes
US6222264B1 (en) * 1999-10-15 2001-04-24 Dell Usa, L.P. Cooling apparatus for an electronic package
KR100497332B1 (en) * 1999-12-22 2005-06-29 한국전자통신연구원 Heat pipe having a sintered wick structure and method for manufacturing the same
EP1187199A2 (en) * 2000-08-28 2002-03-13 Alcan Technology & Management AG Heatsink for Semiconductor Device, Method of Mannufacturing the same, as well as Molding Die therefore
US7027304B2 (en) * 2001-02-15 2006-04-11 Integral Technologies, Inc. Low cost thermal management device or heat sink manufactured from conductive loaded resin-based materials
US6483705B2 (en) * 2001-03-19 2002-11-19 Harris Corporation Electronic module including a cooling substrate and related methods
US6647625B2 (en) * 2001-12-13 2003-11-18 Wei Te Wang Method for fabricating a heat pipe structure in a radiating plate

Patent Citations (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3762011A (en) * 1971-12-16 1973-10-02 Trw Inc Method of fabricating a capillary heat pipe wick
US4106188A (en) * 1976-04-19 1978-08-15 Hughes Aircraft Company Transistor cooling by heat pipes
US4274479A (en) * 1978-09-21 1981-06-23 Thermacore, Inc. Sintered grooved wicks
US4588023A (en) * 1980-06-16 1986-05-13 Showa Aluminum Corporation Device for releasing heat
US4770238A (en) * 1987-06-30 1988-09-13 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Capillary heat transport and fluid management device
US4929414A (en) * 1988-10-24 1990-05-29 The United States Of America As Represented By The Secretary Of The Air Force Method of manufacturing heat pipe wicks and arteries
USH971H (en) * 1988-10-24 1991-10-01 The United States Of America As Represented By The Secretary Of The Air Force Regidized porous material and method
US4880052A (en) * 1989-02-27 1989-11-14 Thermacore, Inc. Heat pipe cooling plate
US4975225A (en) * 1989-03-07 1990-12-04 United Technologies Corporation Manufacture of monolithic, stiff, lightweight ceramic articles
US6194066B1 (en) * 1991-04-24 2001-02-27 The United States Of America As Represented By The Secretary Of The Air Force Microscopic tube devices and method of manufacture
US5355942A (en) * 1991-08-26 1994-10-18 Sun Microsystems, Inc. Cooling multi-chip modules using embedded heat pipes
US5253702A (en) * 1992-01-14 1993-10-19 Sun Microsystems, Inc. Integral heat pipe, heat exchanger, and clamping plate
US5660229A (en) * 1992-04-22 1997-08-26 Sunkyong Industries Co., Ltd. Plate type heat transfer device
US5317805A (en) * 1992-04-28 1994-06-07 Minnesota Mining And Manufacturing Company Method of making microchanneled heat exchangers utilizing sacrificial cores
US5283715A (en) * 1992-09-29 1994-02-01 International Business Machines, Inc. Integrated heat pipe and circuit board structure
US5325913A (en) * 1993-06-25 1994-07-05 The United States Of America As Represented By The Secretary Of The Navy Module cooling system
US5697428A (en) * 1993-08-24 1997-12-16 Actronics Kabushiki Kaisha Tunnel-plate type heat pipe
US6059001A (en) * 1994-04-15 2000-05-09 The United States Of America As Represented By The Secretary Of The Air Force Apparatus for manufacturing microtubes with axially variable geometries
US5598632A (en) * 1994-10-06 1997-02-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method for producing micro heat panels
US6303191B1 (en) * 1997-01-29 2001-10-16 Deutsches Zentrum Fuer Luft -Und Raumfahrt E.V. Process for the production of a heat pipe
US5880524A (en) * 1997-05-05 1999-03-09 Intel Corporation Heat pipe lid for electronic packages
US6133631A (en) * 1997-05-30 2000-10-17 Hewlett-Packard Company Semiconductor package lid with internal heat pipe
US6032726A (en) * 1997-06-30 2000-03-07 Solid State Cooling Systems Low-cost liquid heat transfer plate and method of manufacturing therefor
US6062302A (en) * 1997-09-30 2000-05-16 Lucent Technologies Inc. Composite heat sink
US5933323A (en) * 1997-11-05 1999-08-03 Intel Corporation Electronic component lid that provides improved thermal dissipation
US6178088B1 (en) * 1998-01-27 2001-01-23 Lucent Technologies Inc. Electronic apparatus
US5956229A (en) * 1998-04-01 1999-09-21 Intel Corporation Injection molded thermal interface system
US6070654A (en) * 1998-04-03 2000-06-06 Nissho Iwai Corporation Heat pipe method for making the same and radiating structure
US6230407B1 (en) * 1998-07-02 2001-05-15 Showa Aluminum Corporation Method of checking whether noncondensable gases remain in heat pipe and process for producing heat pipe
US6260613B1 (en) * 1999-01-05 2001-07-17 Intel Corporation Transient cooling augmentation for electronic components
US6698502B1 (en) * 1999-06-04 2004-03-02 Lee Jung-Hyun Micro cooling device
US6282913B1 (en) * 1999-06-11 2001-09-04 Mitsubishi Denki Kabushiki Kaisha Water vaporization type cooling apparatus for heat-generating unit
US6293333B1 (en) * 1999-09-02 2001-09-25 The United States Of America As Represented By The Secretary Of The Air Force Micro channel heat pipe having wire cloth wick and method of fabrication
US6410982B1 (en) * 1999-11-12 2002-06-25 Intel Corporation Heatpipesink having integrated heat pipe and heat sink
US6191946B1 (en) * 2000-01-03 2001-02-20 Thermal Corp. Heat spreader with excess solder basin
US6321452B1 (en) * 2000-03-20 2001-11-27 Liken Lin Method for manufacturing the heat pipe integrated into the heat sink
US6679316B1 (en) * 2000-10-02 2004-01-20 The United States Of America As Represented By The Secretary Of The Air Force Passive thermal spreader and method
US6370749B1 (en) * 2000-11-24 2002-04-16 Chaun-Choung Technology Corp. Heat pipe shaping device
US20030000689A1 (en) * 2001-06-29 2003-01-02 Dah-Chyi Kuo Heat dissipater
US6385044B1 (en) * 2001-07-27 2002-05-07 International Business Machines Corporation Heat pipe heat sink assembly for cooling semiconductor chips

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100139888A1 (en) * 2008-12-08 2010-06-10 Fu Zhun Precision Industry (Shen Zhen) Co., Ltd. Heat spreader and heat dissipation device using same
CN105157460A (en) * 2015-08-24 2015-12-16 东华大学 Pulsating heat pipe heat exchanger with ammonia water as media and stainless steel as materials

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ES2371726T3 (en) 2012-01-09
ATE512462T1 (en) 2011-06-15
EP1296373B1 (en) 2011-06-08
US6935022B2 (en) 2005-08-30
SG152908A1 (en) 2009-06-29
US20030042006A1 (en) 2003-03-06
SG120884A1 (en) 2006-04-26
JP2003193114A (en) 2003-07-09
EP1296373A2 (en) 2003-03-26
EP1296373A3 (en) 2006-10-04
US20060000584A1 (en) 2006-01-05

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