WO2000033628A1 - A fibrous thermal interface adaptor - Google Patents
A fibrous thermal interface adaptor Download PDFInfo
- Publication number
- WO2000033628A1 WO2000033628A1 PCT/US1999/026620 US9926620W WO0033628A1 WO 2000033628 A1 WO2000033628 A1 WO 2000033628A1 US 9926620 W US9926620 W US 9926620W WO 0033628 A1 WO0033628 A1 WO 0033628A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- fibers
- base
- thermal
- interface
- heat
- Prior art date
Links
- 239000000835 fiber Substances 0.000 claims abstract description 64
- 239000004519 grease Substances 0.000 claims description 10
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 9
- 229910052802 copper Inorganic materials 0.000 claims description 9
- 239000010949 copper Substances 0.000 claims description 9
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 8
- 229910002804 graphite Inorganic materials 0.000 claims description 8
- 239000010439 graphite Substances 0.000 claims description 8
- 229910000679 solder Inorganic materials 0.000 claims description 3
- 230000008878 coupling Effects 0.000 description 8
- 238000010168 coupling process Methods 0.000 description 8
- 238000005859 coupling reaction Methods 0.000 description 8
- 239000000463 material Substances 0.000 description 7
- 238000001816 cooling Methods 0.000 description 3
- 239000000758 substrate Substances 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 239000000919 ceramic Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- -1 for example Substances 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 239000012745 toughening agent Substances 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L23/00—Details of semiconductor or other solid state devices
- H01L23/34—Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements
- H01L23/42—Fillings or auxiliary members in containers or encapsulations selected or arranged to facilitate heating or cooling
- H01L23/433—Auxiliary members in containers characterised by their shape, e.g. pistons
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L23/00—Details of semiconductor or other solid state devices
- H01L23/34—Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements
- H01L23/36—Selection of materials, or shaping, to facilitate cooling or heating, e.g. heatsinks
- H01L23/367—Cooling facilitated by shape of device
- H01L23/3677—Wire-like or pin-like cooling fins or heat sinks
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L23/00—Details of semiconductor or other solid state devices
- H01L23/34—Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements
- H01L23/36—Selection of materials, or shaping, to facilitate cooling or heating, e.g. heatsinks
- H01L23/373—Cooling facilitated by selection of materials for the device or materials for thermal expansion adaptation, e.g. carbon
- H01L23/3733—Cooling facilitated by selection of materials for the device or materials for thermal expansion adaptation, e.g. carbon having a heterogeneous or anisotropic structure, e.g. powder or fibres in a matrix, wire mesh, porous structures
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L2224/00—Indexing scheme for arrangements for connecting or disconnecting semiconductor or solid-state bodies and methods related thereto as covered by H01L24/00
- H01L2224/01—Means for bonding being attached to, or being formed on, the surface to be connected, e.g. chip-to-package, die-attach, "first-level" interconnects; Manufacturing methods related thereto
- H01L2224/10—Bump connectors; Manufacturing methods related thereto
- H01L2224/15—Structure, shape, material or disposition of the bump connectors after the connecting process
- H01L2224/16—Structure, shape, material or disposition of the bump connectors after the connecting process of an individual bump connector
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L2224/00—Indexing scheme for arrangements for connecting or disconnecting semiconductor or solid-state bodies and methods related thereto as covered by H01L24/00
- H01L2224/73—Means for bonding being of different types provided for in two or more of groups H01L2224/10, H01L2224/18, H01L2224/26, H01L2224/34, H01L2224/42, H01L2224/50, H01L2224/63, H01L2224/71
- H01L2224/732—Location after the connecting process
- H01L2224/73251—Location after the connecting process on different surfaces
- H01L2224/73253—Bump and layer connectors
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L2924/00—Indexing scheme for arrangements or methods for connecting or disconnecting semiconductor or solid-state bodies as covered by H01L24/00
- H01L2924/0001—Technical content checked by a classifier
- H01L2924/00014—Technical content checked by a classifier the subject-matter covered by the group, the symbol of which is combined with the symbol of this group, being disclosed without further technical details
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L2924/00—Indexing scheme for arrangements or methods for connecting or disconnecting semiconductor or solid-state bodies as covered by H01L24/00
- H01L2924/10—Details of semiconductor or other solid state devices to be connected
- H01L2924/1015—Shape
- H01L2924/10155—Shape being other than a cuboid
- H01L2924/10158—Shape being other than a cuboid at the passive surface
Definitions
- the present invention relates to heat dissipation and more particularly to a thermal interface that efficiently conducts heat from a heat generator to a heat dissipater.
- Computer systems from small handheld electronic devices to medium- sized mobile and desktop systems to large servers and workstations, are becoming increasingly pervasive in our society.
- Computer systems typically include one or more integrated circuits (ICs) such as one or more processors, controllers, or memory devices.
- ICs integrated circuits
- processors processors
- controllers or memory devices.
- an IC tends to generate heat. If this heat is not adequately removed from the IC, the IC may malfunction. In some cases, the heat will cause the IC to fail, causing computer system failure. Thus, to ensure quality and reliability, a computer designer must provide for proper thermal management of the ICs.
- the heat generated by the IC may simply be dissipated directly from the IC to the ambient environment. If this does not provide adequate cooling, a fan may be used to increase the heat dissipative efficiency. If this still does not provide adequate cooling, devices may be thermally coupled to the IC to further increase the heat dissipative efficiency by, for example, increasing the surface area from which the heat is dissipated, converting the thermal energy to an alternate form of energy, or cooling the ambient environment. Such devices are referred to as heat dissipaters.
- thermal grease is typically used at the interface between the IC and the heat dissipater.
- the thermal grease is intended to fill any gaps which may exist at the interface. Such gaps, if not filled, represent locations of high thermal resistivity between the IC and the dissipater, lowering the thermal transport efficiency between the two surfaces.
- One problem with the use of thermal greases is that they tend to separate over time, leaving unfilled gaps behind. This separation occurs because the surface of the IC warps after being packaged at room temperature, then flattens as the IC heats up during operation. The warping may be caused by mismatched thermal constants of materials used in the IC package or the heat dissipater. The constant warping and flattening of the IC has a tendency to pump the thermal grease out of the interface.
- a plurality of flexible, parallel, thermally conductive fibers has a first end that is open and a second end embedded into a thermally conductive base.
- Figure 1 is a thermal interface formed in accordance with an embodiment of the present invention
- Figure 2A is a cross-section of a thermal interface used in a thermal conduction system in accordance with one embodiment of the present invention during a first period of time;
- Figure 2B is the cross-section of Figure 2A during a second period of time
- Figure 3 is a cross-section of a thermal interface used in a thermal conduction system in accordance with another embodiment of the present invention.
- Figure 4A is a thermal conduction system in accordance with another embodiment of the present invention.
- Figure 4B is the thermal conduction system of Figure 4A after thermal coupling has taken place.
- a thermal interface is used to thermally couple an integrated circuit (IC) to a heat dissipater in a computer system.
- the IC may be any of the various different types of ICs typically found in a computer system, such as a processor, chipset, memory device or controller.
- the heat dissipater may include a thermal spreader, fan, heat sink, or heat pipe, and generally includes some type of broad, flat, metallic surface to be bonded to a surface of the thermal interface.
- the thermal interface includes a plurality of flexible, parallel, graphite fibers.
- the first end of the fibers is in direct contact with the IC, and the second end is embedded into a thermally conductive base.
- the first end may have some limited freedom of movement along the surface of the IC or may be embedded into the surface to promote thermal coupling. As the IC heats up and flattens during operation, the fibers flex and bend to accommodate the flattening, maintaining good thermal contact with the IC without forming gaps.
- IC includes not only the semiconductor substrate and circuits formed thereon but also any materials used to package the substrate including, for example, ceramic, plastic, or metal.
- any materials used to package the substrate including, for example, ceramic, plastic, or metal.
- FIG. 1 is a thermal interface 105 formed in accordance with an embodiment of the present invention.
- Thermal interface 105 includes thermally conductive base 100 into which flexible, parallel thermally conductive fibers 101 are embedded at one end. The fibers are open at an opposite end, meaning that they have some freedom of independent movement because they are not embedded into any material.
- base 100 is copper and the fibers are graphite.
- base 100 may comprise other materials in addition to copper or instead of copper, and the fibers may comprise other materials in addition to or instead of graphite. It may be found useful for base 100 to include a material that is the same as the material that is to be thermally coupled to base 100. It may also be found useful to coat the thermal fibers with a flexible covering or adding flexibilizing or toughening agents to the fibrous material.
- length 110 and width 111 of base 100 of interface 105 of Figure 1 are in the range of approximately 0.5 and 5 inches, but may conceivably be any size.
- the length and width of the base are selected to provide a sufficient coupling between the interface and the IC, or other heat generator, to which the interface is to be directly, thermally coupled.
- the edge at the perimeter of base 100 overhangs the boundaries that define the perimeter of fibers 101.
- one of more boundaries of fibers 101 are flush with the edge of the base.
- thickness 113 of base 100 of interface 105 of Figure 1 is in the range of approximately 1 to 250 mils or 1 to 25 mils, but may conceivably be any thickness.
- the base is manufactured to be thick enough to provide a sufficient substrate into which each of fibers 101 may be securely embedded, as demonstrated by fiber 103 in the blowup view, and to provide an adequate surface to which a heat dissipater may be securely bonded.
- the base is also kept thin enough, however, to reduce the thermal resistance between the fibers and the heat dissipater.
- base 100 is formed integrally with the heat dissipater.
- the fibers may be embedded directly into a thermal spreader.
- Fibers 101 are embedded into base 100 by an amount that provides for secure attachment to the base yet reduces thermal resistance between the fibers and the heat dissipater to be bonded to the base.
- the ends of fibers 101 protrude through the upper surface of base 100.
- the ends of the fibers terminate within the bulk of the base.
- length 112 of each of fibers 101 of Figure 1 is less than approximately one inch, but may conceivably be any length.
- Length 112 of fibers 101 are manufactured to be short enough to reduce the thermal resistance of the fibers between the IC and the heat dissipater, yet long enough to provide adequate flexibility of the fibers to accommodate warping of the IC.
- the fibers are manufactured to be thick enough to provide adequate durability and thermal conductance, yet thin enough to provide adequate packing density and flexibility.
- fibers 101 are frayed, as demonstrated by individual fiber 102. Fraying the end of the fiber may be found to improve thermal contact with the IC, reducing thermal resistance.
- FIG. 2A is a cross-section of a thermal interface used in a thermal conduction system in accordance with one embodiment of the present invention.
- IC 202 is coupled to circuit board 200 via solder balls 201.
- the thermal interface comprising thermally conductive, flexible, parallel, graphite fibers 203 embedded into copper base 204 is in direct thermal contact with a surface of IC 202 at one end of the fibers.
- a surface of copper base 203 is bonded to heat dissipater 205.
- Heat dissipater 205 includes a series of fins to increase the surface area of the dissipater, thereby increasing thermal dissipation efficiency.
- Fibers 203 of Figure 2A are not embedded into the surface of IC 202 but rather are slightly compressed onto the surface, allowing for some limited freedom of movement along the surface. Under the compression, fibers 203 bend enough to ensure constant, direct, thermal contact with IC 202 despite warpage of IC 202.
- a thermal grease resides at the interface of fibers 203 and IC 202. This thermal grease is held between fibers 203 of the interface and may improve the thermal coupling between fibers 203 and IC 202.
- the ends of fibers 203 are embedded into the surface of IC 202 to improve the thermal coupling between the IC and the fibers.
- the bond between copper base 204 and the surface of heat dissipater 205 of Figure 2A is a solder bond formed by soldering the dissipater to the surface of the base.
- the bond may be a molecular bond formed by sintering base 204 to dissipater 205 at a temperature high enough to form covalent bonds at the interface.
- the dissipater 205 is thermally coupled to base 203 by simply placing the two surfaces in direct thermal contact with each other with a thermal grease applied at the interface.
- Figure 2B is the cross-section of Figure 2A during operation of the IC.
- IC 202 heats up, its surface flattens as shown.
- fibers 203 are flexible and are compressed against the surface of IC 202, the ends of fibers 203 maintain contact with the surface of IC 202 even though the surface of the IC changes its planarity due to heating.
- a good thermal coupling between fibers 203 and IC 202, exhibiting a low thermal resistance is maintained with IC 202 throughout the operation of the IC.
- a thermal interface such as that described above may be adapted for use in coupling nearly any heat generator to any heat dissipater.
- a thermal interface may be used to connect a thermal block, which generates heat as a result of conducting the heat from an IC, to a heat pipe, which dissipates the heat by transporting it to a remote location.
- a thermal interface such as that described above may be used to connect a first heat pipe to a second heat pipe.
- the thermal interface may be curved to accommodate the curved surfaces of the heat pipes.
- a thermal interface such as that described above may be used to thermally couple virtually any non-planar surface to a relatively planar or smoothly curved surface.
- Figure 3 is a cross-section of a thermal interface used in a thermal conduction system in accordance with another embodiment of the present invention.
- Heat generator 302 has a rough, non-planar surface as shown.
- Thermally conductive, flexible, parallel, graphite fibers 303 flex and bend to conform to the surface of heat generator 302, making highly thermally conductive contact therewith.
- Thermal grease may additionally be used at this interface to improve thermal coupling.
- Fibers 303 conduct heat generated by heat generator 302, and efficiently transport this heat to base 304 into which fibers 303 are embedded, base 304 is bonded to the curved surface of heat dissipater 305, which may be a heat pipe, heat sink, or heat spreader.
- Figure 4A shows a thermal conduction system in which two heat pipes, 400 and 410, include thermal interfaces 405 and 415, respectively. These thermal interfaces are used in conjunction with thermal coupler 420 to form the coupled heat pipes of Figure 4B.
- Thermal interface 405 includes base 407, into which fibers 406 are embedded, entirely wrapped around and soldered to an extended portion of heat pipe 400.
- Thermal interface 415 includes base 417, into which fibers 416 are embedded, entirely wrapped around and soldered to an extended portion of heat pipe 410.
- Heat pipe 400, including thermal interface 405 is inserted into one end of coupler 420, and heat pipe 410, including thermal interface 415, is inserted into the other end of coupler 420.
- heat pipe 400 is thermally coupled to the heat generator of a computer system and heat pipe 410 is thermally coupled to the heat dissipater
- fibers 406 conduct heat from heat pipe 400 and efficiently transport this heat to thermal coupler 420.
- Fibers 416 conduct the heat from coupler 420 and efficiently transport this heat to heat pipe 410.
- Thermal grease may be used at the interface between the fibers and coupler 420.
- the thermal interfaces are bonded to the coupler rather than to the heat pipes.
- the base of the thermal interface may be bonded to the inner surface of coupler 420 with the fibers extending inward from the base to thermally contact the outer surface of the heat pipes or an extended protrusion from the heat pipes.
- coupler 420 is a simple thermally conductive slip or another heat pipe.
- a single thermal interface is used to couple one heat pipe to another either directly or via a removable coupler.
- coupler 420 may be formed integrally with either heat pipe 400 or 410, obviating the need for the thermal interface attached to that heat pipe.
- coupler 420 may be formed having a diameter that is larger than the diameter of heat pipe 400 or 410, eliminating the needed for the extended, narrow protrusions form the heat pipes.
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- General Physics & Mathematics (AREA)
- Computer Hardware Design (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Power Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU16163/00A AU1616300A (en) | 1998-12-02 | 1999-11-10 | A fibrous thermal interface adaptor |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US20610198A | 1998-12-02 | 1998-12-02 | |
US09/206,101 | 1998-12-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2000033628A1 true WO2000033628A1 (en) | 2000-06-08 |
Family
ID=22764995
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US1999/026620 WO2000033628A1 (en) | 1998-12-02 | 1999-11-10 | A fibrous thermal interface adaptor |
Country Status (2)
Country | Link |
---|---|
AU (1) | AU1616300A (en) |
WO (1) | WO2000033628A1 (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2003054958A1 (en) * | 2001-12-20 | 2003-07-03 | Intel Corporation | Carbon nanotube thermal interface structures |
US6617199B2 (en) | 1998-06-24 | 2003-09-09 | Honeywell International Inc. | Electronic device having fibrous interface |
US6676796B2 (en) * | 1998-06-24 | 2004-01-13 | Honeywell International Inc. | Transferrable compliant fibrous thermal interface |
WO2004006330A1 (en) * | 2002-07-02 | 2004-01-15 | Intel Corporation | Method and apparatus using nanotubes for cooling and grounding die |
US6713151B1 (en) | 1998-06-24 | 2004-03-30 | Honeywell International Inc. | Compliant fibrous thermal interface |
US6921462B2 (en) | 2001-12-17 | 2005-07-26 | Intel Corporation | Method and apparatus for producing aligned carbon nanotube thermal interface structure |
WO2006041325A1 (en) * | 2004-10-08 | 2006-04-20 | Verteletsky, Pavel Vasilievich | Multi-filament heat sink |
US7168484B2 (en) | 2003-06-30 | 2007-01-30 | Intel Corporation | Thermal interface apparatus, systems, and methods |
US7180174B2 (en) | 2003-12-30 | 2007-02-20 | Intel Corporation | Nanotube modified solder thermal intermediate structure, systems, and methods |
EP1401641A4 (en) * | 2001-05-30 | 2007-12-12 | Honeywell Int Inc | Interface materials and methods of production and use thereof |
US7456052B2 (en) | 2003-12-30 | 2008-11-25 | Intel Corporation | Thermal intermediate apparatus, systems, and methods |
US7608324B2 (en) | 2001-05-30 | 2009-10-27 | Honeywell International Inc. | Interface materials and methods of production and use thereof |
US7704791B2 (en) | 2003-02-03 | 2010-04-27 | Intel Corporation | Packaging of integrated circuits with carbon nano-tube arrays to enhance heat dissipation through a thermal interface |
DE102012222735B4 (en) * | 2011-12-15 | 2021-06-02 | GM Global Technology Operations, LLC (n.d. Ges. d. Staates Delaware) | Cooling system for a battery cell |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4057101A (en) * | 1976-03-10 | 1977-11-08 | Westinghouse Electric Corporation | Heat sink |
US4446916A (en) * | 1981-08-13 | 1984-05-08 | Hayes Claude Q C | Heat-absorbing heat sink |
US4765139A (en) * | 1987-07-23 | 1988-08-23 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thermocouple for heating and cooling of memory metal actuators |
US5150748A (en) * | 1990-06-18 | 1992-09-29 | Mcdonnell Douglas Corporation | Advanced survivable radiator |
US5224030A (en) * | 1990-03-30 | 1993-06-29 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Semiconductor cooling apparatus |
US5316080A (en) * | 1990-03-30 | 1994-05-31 | The United States Of America As Represented By The Administrator Of The National Aeronautics & Space Administration | Heat transfer device |
US5390734A (en) * | 1993-05-28 | 1995-02-21 | Lytron Incorporated | Heat sink |
US5520976A (en) * | 1993-06-30 | 1996-05-28 | Simmonds Precision Products Inc. | Composite enclosure for electronic hardware |
US5528456A (en) * | 1993-11-15 | 1996-06-18 | Nec Corporation | Package with improved heat transfer structure for semiconductor device |
US5847925A (en) * | 1997-08-12 | 1998-12-08 | Compaq Computer Corporation | System and method for transferring heat between movable portions of a computer |
-
1999
- 1999-11-10 WO PCT/US1999/026620 patent/WO2000033628A1/en active Application Filing
- 1999-11-10 AU AU16163/00A patent/AU1616300A/en not_active Abandoned
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4057101A (en) * | 1976-03-10 | 1977-11-08 | Westinghouse Electric Corporation | Heat sink |
US4446916A (en) * | 1981-08-13 | 1984-05-08 | Hayes Claude Q C | Heat-absorbing heat sink |
US4765139A (en) * | 1987-07-23 | 1988-08-23 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thermocouple for heating and cooling of memory metal actuators |
US5224030A (en) * | 1990-03-30 | 1993-06-29 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Semiconductor cooling apparatus |
US5316080A (en) * | 1990-03-30 | 1994-05-31 | The United States Of America As Represented By The Administrator Of The National Aeronautics & Space Administration | Heat transfer device |
US5150748A (en) * | 1990-06-18 | 1992-09-29 | Mcdonnell Douglas Corporation | Advanced survivable radiator |
US5390734A (en) * | 1993-05-28 | 1995-02-21 | Lytron Incorporated | Heat sink |
US5520976A (en) * | 1993-06-30 | 1996-05-28 | Simmonds Precision Products Inc. | Composite enclosure for electronic hardware |
US5528456A (en) * | 1993-11-15 | 1996-06-18 | Nec Corporation | Package with improved heat transfer structure for semiconductor device |
US5847925A (en) * | 1997-08-12 | 1998-12-08 | Compaq Computer Corporation | System and method for transferring heat between movable portions of a computer |
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6713151B1 (en) | 1998-06-24 | 2004-03-30 | Honeywell International Inc. | Compliant fibrous thermal interface |
US6740972B2 (en) | 1998-06-24 | 2004-05-25 | Honeywell International Inc. | Electronic device having fibrous interface |
US6617199B2 (en) | 1998-06-24 | 2003-09-09 | Honeywell International Inc. | Electronic device having fibrous interface |
US6676796B2 (en) * | 1998-06-24 | 2004-01-13 | Honeywell International Inc. | Transferrable compliant fibrous thermal interface |
US7608324B2 (en) | 2001-05-30 | 2009-10-27 | Honeywell International Inc. | Interface materials and methods of production and use thereof |
EP1401641A4 (en) * | 2001-05-30 | 2007-12-12 | Honeywell Int Inc | Interface materials and methods of production and use thereof |
US6921462B2 (en) | 2001-12-17 | 2005-07-26 | Intel Corporation | Method and apparatus for producing aligned carbon nanotube thermal interface structure |
US7704462B2 (en) | 2001-12-17 | 2010-04-27 | Intel Corporation | Method and apparatus for producing aligned carbon nanotube thermal interface structure |
US6965513B2 (en) | 2001-12-20 | 2005-11-15 | Intel Corporation | Carbon nanotube thermal interface structures |
EP1329953A1 (en) * | 2001-12-20 | 2003-07-23 | Intel Corporation | Carbon nanotube thermal interface structures |
WO2003054958A1 (en) * | 2001-12-20 | 2003-07-03 | Intel Corporation | Carbon nanotube thermal interface structures |
US6856016B2 (en) | 2002-07-02 | 2005-02-15 | Intel Corp | Method and apparatus using nanotubes for cooling and grounding die |
WO2004006330A1 (en) * | 2002-07-02 | 2004-01-15 | Intel Corporation | Method and apparatus using nanotubes for cooling and grounding die |
US7847394B2 (en) | 2003-02-03 | 2010-12-07 | Intel Corporation | Packaging of integrated circuits with carbon nanotube arrays to enhance heat dissipation through a thermal interface |
US7704791B2 (en) | 2003-02-03 | 2010-04-27 | Intel Corporation | Packaging of integrated circuits with carbon nano-tube arrays to enhance heat dissipation through a thermal interface |
US7168484B2 (en) | 2003-06-30 | 2007-01-30 | Intel Corporation | Thermal interface apparatus, systems, and methods |
US7456052B2 (en) | 2003-12-30 | 2008-11-25 | Intel Corporation | Thermal intermediate apparatus, systems, and methods |
US7180174B2 (en) | 2003-12-30 | 2007-02-20 | Intel Corporation | Nanotube modified solder thermal intermediate structure, systems, and methods |
US7985627B2 (en) | 2003-12-30 | 2011-07-26 | Intel Corporation | Thermal intermediate apparatus, systems, and methods |
US8129223B2 (en) | 2003-12-30 | 2012-03-06 | Intel Corporation | Nanotube modified solder thermal intermediate structure, systems, and methods |
WO2006041325A1 (en) * | 2004-10-08 | 2006-04-20 | Verteletsky, Pavel Vasilievich | Multi-filament heat sink |
DE102012222735B4 (en) * | 2011-12-15 | 2021-06-02 | GM Global Technology Operations, LLC (n.d. Ges. d. Staates Delaware) | Cooling system for a battery cell |
Also Published As
Publication number | Publication date |
---|---|
AU1616300A (en) | 2000-06-19 |
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