WO1998003997A1 - Closed loop liquid cooling within rf modules - Google Patents

Closed loop liquid cooling within rf modules Download PDF

Info

Publication number
WO1998003997A1
WO1998003997A1 PCT/US1997/013326 US9713326W WO9803997A1 WO 1998003997 A1 WO1998003997 A1 WO 1998003997A1 US 9713326 W US9713326 W US 9713326W WO 9803997 A1 WO9803997 A1 WO 9803997A1
Authority
WO
WIPO (PCT)
Prior art keywords
assembly according
heat
heat exchanger
pump
microchannels
Prior art date
Application number
PCT/US1997/013326
Other languages
French (fr)
Inventor
Robin E. Hamilton
Paul G. Kennedy
Original Assignee
Northrop Grumman Corporation
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Northrop Grumman Corporation filed Critical Northrop Grumman Corporation
Publication of WO1998003997A1 publication Critical patent/WO1998003997A1/en

Links

Classifications

    • 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
    • H01L23/46Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements involving the transfer of heat by flowing fluids
    • H01L23/473Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements involving the transfer of heat by flowing fluids by flowing liquids
    • 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

Definitions

  • the present invention relates to convection cooling of high power semiconductor devices and more particularly to a module including a self-contained coolant loop having a microchannel heat sink for cooling relatively high power semiconductive devices, such as RF power transistors.
  • the number of transistors and related peripheral circuits that are required in such a solid state transmitter is a function of the thermal capacitance of the transistor device packaging and their associated air cooled heat sinks.
  • the packaging approach utilized by the ARSR-4 solid state transmitter has been embraced by the industry for several years due to its simplicity, low cost and customer acceptance.
  • FIG. 1 is illustrative of an air cooled RF module 10 for an ARSR-4 transmitter.
  • the module 10 is shown including a heat generating transistor chip 12; a ceramic substrate 14; a metallic mounting flange 16; a multilayer soft aluminum clad substrate 18 ; a metallic ground plane 20; and a cold plate 22 which is a bonded sandwich of aluminum finstock 24 and sheet metal 26.
  • a flow of cooling air directed to the finstock 24 is shown by reference numeral 28.
  • the flange 16 is mounted on the ground plane 20 where it is bolted to the substrate 18.
  • the groundplane 20 is in turn bolted to the air cooled coldplate 22.
  • the maximum device junction temperature of the transistor devices, not shown, located on the chip 12, as dictated by system reliability studies, is typically between 125 and 135°C.
  • a conventional packaging and realizable air flow delivery limit the maximum heat dissipation of a silicon RF transistor packet such as shown in Figure 1, to about 10 watts.
  • Four design features typically drive the temperature gradient occurring in such a structure. These are the mass of air flow 28, the efficiency of the coldplate 22, the device to substrate interface, i.e. elements 16, 18 and 20, and the internal temperature rise of the chip 12.
  • an ARSR-4 transmitter generates over 12 kilowatts average heat dissipation.
  • a blower, not shown, used to cool this very large system is a 20 HP piece of apparatus rated to deliver approximately 10,000 cubic feet per minute of air at 8 inches of water pressure drop.
  • Such a blower is excessively large, expensive and noisy. In fact, such a blower typically requires that it to be housed in its own cabinet.
  • a closed loop liquid cooling arrangement in conjunction with an air-to-liquid heat exchanger integrated into a module which is easily installed and removed as a self-contained unit and furthermore includes a microchannel heat sink which is directly integrated into the chip containing the heat- generating components.
  • Fluid coolant is forced through a plurality of microchannels formed in the heat sink by a micropump located on a substrate formed on a ground plane/heat exchanger which includes coolant input and output ducts coupled to the microchannels.
  • the ground plane/heat exchanger additionally includes a set of heat exchanger fins which receive air flow from an external blower or fan.
  • Figure 1 is an exploded parts diagram depicting a semiconductor component cooling system according to the known prior art
  • FIG 2 is a mechanical schematic diagram broadly illustrative of a modular liquid cooling system in accordance with the present invention
  • Figure 3 an exploded parts diagram illustrative of the preferred embodiment of the invention.
  • Figure 4 is a perspective view of the unit shown in Figure 3 mounted on the ground plane and including a microchannel heat sink utilized for convection cooling of a plurality of semiconductor devices mounted thereon.
  • reference numeral 30 denotes a module 30 which includes a load/heat sink 32, a heat exchanger 34 and a fluid coolant pump 36. These elements are shown interconnected by coolant fluid flow paths 38, 40 and 42. In addition, a fan 44 is depicted for forcing air past the heat exchanger 34.
  • the load/heat sink 32 as shown in Figures 3 and 4 , is comprised of a body of material having high thermal conductivity which is attached to a ceramic substrate 48. The ceramic substrate 48 is in turn attached to a metal flange member 50.
  • the flange 50 as shown in Figure 4, includes a pair of open-ended U-shaped slots 52 which are used for being bolted to the soft substrate portion 35 of a circuit board or groundplane member 54 which doubles as an air-to-liquid heat exchanger.
  • the groundplane 54 also has a set of heat exchanger fins 56 depending from the bottom portion thereof; however, now the groundplane 54 also includes fluid flow paths or conduits 40 and 42 leading to and from a liquid coolant feed pump 36 located on the soft substrate 35.
  • the ceramic substrate 48 seals the microchannels 62 and serves as a mechanical fluid manifold together with the metal flange 50 and serves to supply a liquid coolant 63 from the pump 36 in and out of the microchannel grooves 62 via pairs of openings 47, 49, and 50, 53.
  • 0-ring seals 55 and 57 seal coolant being delivered from and to the pump 36 via the fluid flow paths 40 and 42.
  • a coolant 63 such as FC-43 "Fluorinert" brand liquid manufactured by the 3M Company, comprises an optimum type of coolant liquid because of its high boiling point temperature (174 °C) and its non-corrosive nature.
  • the pump 36 typically comprises a microminiature piezoelectric diaphragm pump such as shown and described in U.S.
  • the pump 36 may comprise a non-mechanical magnetic micropump such as shown and described in the above-referenced copending application Serial No. 08/681,345 (WE58,812), entitled “Non-Mechanical Magnetic Pump For Liquid Cooling", filed in the name of Robin E. Hamilton et al. on July 22, 1996.
  • the body 46 of the heat sink 32 is shown including a semiconductor chip 58 having integrated therewith a plurality of semiconductor devices 60 which may be, for example, high powered RF bipolar transistors.
  • Beneath semiconductor chip 58 and the semiconductor devices 60 is a plurality of mutually parallel close-ended microchannels 62 of rectangular cross section formed in the material from which the heat sink body 46 is formed.
  • Each microchannel 62 comprises an elongated linear groove ranging in width between 0.001 in. and 0.004 in., a depth ranging between 0.004 in. and 0.01 in. , with the spacing therebetween ranging between 0.001 in. and 0.003 in.
  • the rectangular spacing sections 64 separating the microchannels 62 act as fins for conducting heat generated by the semiconductor devices 60 to the coolant 63 which is pumped through the microchannel 62 by the micropump 36.
  • the heat generating semiconductors e.g. transistors
  • the microchannels 62 can be inexpensively etched, using standard photolithographic processes, in the body of silicon, for example.
  • Microchannel cooling may be integrated into different electrical components and even with integrated circuits up to wafer scale level of integration. It can also be used with various semiconductors such as silicon, silicon carbide, germanium and gallium arsenide which in turn are bonded to substrates such as, but not constrained to, beryllium oxide and aluminum nitride.
  • a microchannel heat sink 32 is far more efficient than conventional liquid heat sinks, for example, as shown in Figure 1.
  • the fundamental difference between a microchannel heat sink and a conventional heat sink is the dimensions of the channels 62 ( Figure 4) .
  • the use of very narrow microchannels enhances heat transfers in two ways. First, narrow channels can be closely spaced, providing a large number of fins 64, with a combined surface area much greater than the "foot print" of the heat sink body 46. In addition, the small hydraulic diameters of the narrow passages result in relatively high convection heat transfer coefficients.
  • the microchannels 62 provide an increase in the maximum power density for a given operating temperature and thus are ideal for direct cooling of hot components.
  • a self- contained coolant loop with a microchannel heat sink coupled to a micropump and an air-to-liquid heat exchanger built right into a module which provides the thermal cooling efficiency of a liquid system while offering the simplicity of an air-cooled package.
  • a structure is provided which can cool electronic devices with twice the heat dissipation than previously practical with air-cooled designs. Integration of higher power components into the electronics thus minimizes parts count, and reduces the quantity of peripheral circuits.

Abstract

A self-contained coolant loop for semiconductor devices such as high power transistors. The coolant loop includes a microchannel heat sink (32), a micropump (36), and an air-to-liquid heat exchanger (34) incorporated into a replaceable module (30).

Description

CLOSED LOOP LIQUID COOLING WITHIN RF MODULES
Cross Reference to Related Application
This application is related to copending U.S. application Serial No. 08/681,345 (WE58,812) entitled,
"Non-Mechanical Magnetic Pump For Liquid Cooling", Robin E. Hamilton et al, filed on July 22, 1996; and
U.S. patent application Serial No. 08/681,207
(WE58,813) entitled, "Microchannel Cooling Of High
Power Semiconductor Devices", Robin Hamilton et al , filed on July 22, 1996. Both of these application are assigned to the assignee of the present invention and are meant to be incorporated herein by reference.
Background of the Invention
Field of the Invention The present invention relates to convection cooling of high power semiconductor devices and more particularly to a module including a self-contained coolant loop having a microchannel heat sink for cooling relatively high power semiconductive devices, such as RF power transistors.
Description of the Prior Art
State of the art electronic packaging frequently utilizes redundant components in order to compensate for the limited capacity of the means utilized for cooling. This results in greater system cost, size and weight. For example, in a well known air cooled solid state transmitter such as the ARSR-4 developed by the Westinghouse Electric Corporation, RF power transistors are designed to operate below their power output capability and are spaced relatively far apart from one another in order to meet prescribed operating standards.
The number of transistors and related peripheral circuits that are required in such a solid state transmitter is a function of the thermal capacitance of the transistor device packaging and their associated air cooled heat sinks. The packaging approach utilized by the ARSR-4 solid state transmitter has been embraced by the industry for several years due to its simplicity, low cost and customer acceptance.
Figure 1 is illustrative of an air cooled RF module 10 for an ARSR-4 transmitter. The module 10 is shown including a heat generating transistor chip 12; a ceramic substrate 14; a metallic mounting flange 16; a multilayer soft aluminum clad substrate 18 ; a metallic ground plane 20; and a cold plate 22 which is a bonded sandwich of aluminum finstock 24 and sheet metal 26. A flow of cooling air directed to the finstock 24 is shown by reference numeral 28.
In accordance with prior art practice, the flange 16 is mounted on the ground plane 20 where it is bolted to the substrate 18. The groundplane 20 is in turn bolted to the air cooled coldplate 22. Advancement in high power device designs, however, has pushed the requirement for efficient thermal designs beyond conventional packaging schemes.
With respect to cooling the structure shown in Figure 1, the maximum device junction temperature of the transistor devices, not shown, located on the chip 12, as dictated by system reliability studies, is typically between 125 and 135°C. A conventional packaging and realizable air flow delivery limit the maximum heat dissipation of a silicon RF transistor packet such as shown in Figure 1, to about 10 watts. Four design features typically drive the temperature gradient occurring in such a structure. These are the mass of air flow 28, the efficiency of the coldplate 22, the device to substrate interface, i.e. elements 16, 18 and 20, and the internal temperature rise of the chip 12.
Increasing the mass flow rate of air to save in air temperature rise through the electronics is often an almost impossible task. For example, an ARSR-4 transmitter generates over 12 kilowatts average heat dissipation. A blower, not shown, used to cool this very large system is a 20 HP piece of apparatus rated to deliver approximately 10,000 cubic feet per minute of air at 8 inches of water pressure drop. Such a blower is excessively large, expensive and noisy. In fact, such a blower typically requires that it to be housed in its own cabinet.
Alternatively, dramatic improvement in a finstock type air-cooled coldplate 22, without further pushing air flow and pressure drop, is at this time unrealizable. However, the thermal interface between the flange 16, the substrate 18 and the ground plane 20 may be improved with solder. Unfortunately, this adds considerable system cost in module rework. Furthermore, great thermal or electrical efficiency improvements in the device has up to the present eluded transistor vendors.
Although it is known that heat dissipating components may be successfully cooled with liquid, many end-users have strong objections to liquid cooling because it is perceived to be expensive and heavy, with low reliability and excessive maintenance problems due to leaks, fouling and corrosion. The Federal Aviation Administration (FAA) , for example, require that their ground-based radars be cooled with air. Furthermore, many applications simply do not have liquid cooling available. Summary Accordingly, it is a primary object of the invention to provide an improvement in the extraction of heat from electronic components.
It is another object of the invention to provide an improvement in the cooling of high power semiconductor devices.
It is yet another object of the invention to provide an improvement in the cooling of densely packaged semiconductor devices by convection cooling.
It is a further object of the invention to provide an improvement in the cooling of high power RF semiconductor devices, such as bipolar transistors, which are utilized in densely packaged configurations.
Briefly, the foregoing and other objects are fulfilled by providing a closed loop liquid cooling arrangement in conjunction with an air-to-liquid heat exchanger integrated into a module which is easily installed and removed as a self-contained unit and furthermore includes a microchannel heat sink which is directly integrated into the chip containing the heat- generating components. Fluid coolant is forced through a plurality of microchannels formed in the heat sink by a micropump located on a substrate formed on a ground plane/heat exchanger which includes coolant input and output ducts coupled to the microchannels. The ground plane/heat exchanger additionally includes a set of heat exchanger fins which receive air flow from an external blower or fan. Further scope of applicability of the present invention will become apparent from the detailed description given hereinafter. However, it should be understood that the detailed description and specific examples, while indicating preferred embodiments of the invention, are given by way of illustration only, since various changes and modifications within the spirit and scope of the invention will become apparent to those skilled in the art from this detailed description. Brief Description of the Drawings
The present invention will become more fully understood from the detailed description given hereinbelow and the accompanying drawings which are given by way of illustration only, and thus are not limitative of the present invention, and wherein:
Figure 1 is an exploded parts diagram depicting a semiconductor component cooling system according to the known prior art;
Figure 2 is a mechanical schematic diagram broadly illustrative of a modular liquid cooling system in accordance with the present invention; Figure 3 an exploded parts diagram illustrative of the preferred embodiment of the invention; and
Figure 4 is a perspective view of the unit shown in Figure 3 mounted on the ground plane and including a microchannel heat sink utilized for convection cooling of a plurality of semiconductor devices mounted thereon. Detailed Description of the Preferred Embodiment
Referring now to the figures and more particularly to Figure 2, shown thereat is a schematic broadly illustrative of the inventive concept of this invention. In Figure 2, reference numeral 30 denotes a module 30 which includes a load/heat sink 32, a heat exchanger 34 and a fluid coolant pump 36. These elements are shown interconnected by coolant fluid flow paths 38, 40 and 42. In addition, a fan 44 is depicted for forcing air past the heat exchanger 34. In accordance with the preferred embodiment of the invention, the load/heat sink 32, as shown in Figures 3 and 4 , is comprised of a body of material having high thermal conductivity which is attached to a ceramic substrate 48. The ceramic substrate 48 is in turn attached to a metal flange member 50. The flange 50, as shown in Figure 4, includes a pair of open-ended U-shaped slots 52 which are used for being bolted to the soft substrate portion 35 of a circuit board or groundplane member 54 which doubles as an air-to-liquid heat exchanger. As in Figure 1, the groundplane 54 also has a set of heat exchanger fins 56 depending from the bottom portion thereof; however, now the groundplane 54 also includes fluid flow paths or conduits 40 and 42 leading to and from a liquid coolant feed pump 36 located on the soft substrate 35. The ceramic substrate 48 seals the microchannels 62 and serves as a mechanical fluid manifold together with the metal flange 50 and serves to supply a liquid coolant 63 from the pump 36 in and out of the microchannel grooves 62 via pairs of openings 47, 49, and 50, 53. 0-ring seals 55 and 57 seal coolant being delivered from and to the pump 36 via the fluid flow paths 40 and 42. A coolant 63, such as FC-43 "Fluorinert" brand liquid manufactured by the 3M Company, comprises an optimum type of coolant liquid because of its high boiling point temperature (174 °C) and its non-corrosive nature. The pump 36 typically comprises a microminiature piezoelectric diaphragm pump such as shown and described in U.S. patent application Serial No. 08/320,614 entitled, "Micro-Miniature Piezoelectric Diaphragm Pump For The Low Pressure Pumping Of Gases", filed in the names of Robert Young et al on October 7, 1994 , and which is meant to be incorporated herein by reference. Alternatively, the pump 36 may comprise a non-mechanical magnetic micropump such as shown and described in the above-referenced copending application Serial No. 08/681,345 (WE58,812), entitled "Non-Mechanical Magnetic Pump For Liquid Cooling", filed in the name of Robin E. Hamilton et al. on July 22, 1996.
Further as shown in Figure 4, the body 46 of the heat sink 32 is shown including a semiconductor chip 58 having integrated therewith a plurality of semiconductor devices 60 which may be, for example, high powered RF bipolar transistors. Beneath semiconductor chip 58 and the semiconductor devices 60, is a plurality of mutually parallel close-ended microchannels 62 of rectangular cross section formed in the material from which the heat sink body 46 is formed.
Each microchannel 62 comprises an elongated linear groove ranging in width between 0.001 in. and 0.004 in., a depth ranging between 0.004 in. and 0.01 in. , with the spacing therebetween ranging between 0.001 in. and 0.003 in. The rectangular spacing sections 64 separating the microchannels 62 act as fins for conducting heat generated by the semiconductor devices 60 to the coolant 63 which is pumped through the microchannel 62 by the micropump 36.
For maximum effectiveness in cooling, the heat generating semiconductors, e.g. transistors, can be formed directly on the microchannel heat sink 32. This eliminates the numerous thermal resistances between the heat source and the heat sink. The microchannels 62 can be inexpensively etched, using standard photolithographic processes, in the body of silicon, for example.
The subject inventive concept is not limited to power transistors. Microchannel cooling may be integrated into different electrical components and even with integrated circuits up to wafer scale level of integration. It can also be used with various semiconductors such as silicon, silicon carbide, germanium and gallium arsenide which in turn are bonded to substrates such as, but not constrained to, beryllium oxide and aluminum nitride.
It can be shown that a microchannel heat sink 32, as depicted in Figure 4 , is far more efficient than conventional liquid heat sinks, for example, as shown in Figure 1. The fundamental difference between a microchannel heat sink and a conventional heat sink is the dimensions of the channels 62 (Figure 4) . The use of very narrow microchannels enhances heat transfers in two ways. First, narrow channels can be closely spaced, providing a large number of fins 64, with a combined surface area much greater than the "foot print" of the heat sink body 46. In addition, the small hydraulic diameters of the narrow passages result in relatively high convection heat transfer coefficients. Since the thermal conductance of a heat sink is proportional to the product of the convective heat transfer coefficient and the surface area, the microchannels 62 provide an increase in the maximum power density for a given operating temperature and thus are ideal for direct cooling of hot components. Thus what has been shown and described is a self- contained coolant loop with a microchannel heat sink coupled to a micropump and an air-to-liquid heat exchanger built right into a module which provides the thermal cooling efficiency of a liquid system while offering the simplicity of an air-cooled package. A structure is provided which can cool electronic devices with twice the heat dissipation than previously practical with air-cooled designs. Integration of higher power components into the electronics thus minimizes parts count, and reduces the quantity of peripheral circuits. Less hardware correlates to less complexity, cost, volume and weight. Most importantly, a self-contained coolant loop eliminates end user's basic objections to liquid systems. Furthermore, there is no cabinet level plumbing to fail or fluid couplings to leak when replacing a unit in the field.
The invention being thus disclosed, it will be obvious that the same may be varied in many ways. Such variations are not to be regarded as a departure from the spirit and scope of the invention, and all such modifications that would be obvious to one skilled in the art are intended to be included within the scope of the following claims.

Claims

1. A modular type closed loop liquid coolant assembly for supporting and dissipating heat generated by at least one electronics device, comprising: air-to-liquid heat exchanger means; heat sink means mounted on said heat exchanger means and including at least one heat generating electronics device thereon and a plurality of convection cooling channels; and a pump fluidly connected to said cooling channels for circulating a fluid coolant through said cooling channels for providing convection cooling of said electronics device.
2. An assembly according to claim 1 wherein said pump comprises a pump assembly mounted on said heat exchanger means.
3. An assembly according to claim 2 wherein said fluid coolant comprises a liquid coolant.
4. An assembly according to claim 3 wherein said heat exchanger means includes a groundplane.
5. An assembly according to claim 4 wherein said pump is fluidly connected to said cooling channels through said groundplane.
6. An assembly according to claim 5 wherein said heat exchanger means additionally includes a set of air cooled heat dissipating elements extending from said groundplane.
7. An assembly according to claim 6 wherein said set of heat dissipating elements comprises a set of air cooled fins.
8. An assembly according to claim 1 wherein said cooling channels comprise microchannels having a width ranging between about 0.001 in. and about 0.004 in., a depth ranging between about 0.004 in. and about 0.01 in. , and a spacing therebetween ranging between about 0.001 in. and about 0.005 in.
9. An assembly according to claim 8 wherein said at least one electronics device comprises at least one semiconductor device.
10. An assembly according to claim 9 wherein said at least one semiconductor device comprises a plurality of semiconductor devices.
11. An assembly according to claim 10 wherein said heat sink means comprises a body of material having relatively high thermal conductivity.
12. An assembly according to claim 11 wherein said plurality of semiconductor devices are integrated in a semiconductor chip located on said body.
13. An assembly according to claim 12 wherein and said plurality of semiconductor devices are located adjacent said microchannels.
14. An assembly according to claim 11 and additionally including a mounting flange for mounting said body on said groundplane.
15. An assembly according to claim 14 wherein said mounting flange includes means for coupling said fluid coolant therethrough between said microchannels and said pump.
16. An assembly according to claim 15 and additionally including a ceramic substrate located between said body of said heat sink means and said mounting flange.
17. An assembly according to claim 16 wherein said ceramic substrate includes means for coupling said fluid coolant therethrough between said microchannels and said pump.
18. A closed loop liquid coolant assembly for supporting and dissipating heat generated by semiconductor devices, comprising: an air-to-liquid heat exchanger; a heat sink for electronic devices mounted on said heat exchanger means and including at least one semiconductor device thereon and a plurality of convection cooling microchannels, said microchannels having a width ranging between about 0.001 in. and about 0.004 in., a depth ranging between 0.004 in. and about 0.01 in., and a spacing therebetween ranging between about 0.001 in. and about 0.005 in.; and a pump located on said heat exchanger, said heat exchanger including a fluid connection from said pump to said microchannels for circulating a liquid coolant therethrough for providing convection cooling of said semiconductor device.
19. An assembly according to claim 18 wherein said heat exchanger includes a groundplane for supporting said heat sink and a set of heat dissipating elements for dissipating heat coupled thereto from said liquid coolant flowing in said fluid connection.
20. An assembly according to claim 19 wherein said heat sink includes a semiconductor chip.
PCT/US1997/013326 1996-07-22 1997-07-22 Closed loop liquid cooling within rf modules WO1998003997A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US68134496A 1996-07-22 1996-07-22
US08/681,344 1996-07-22

Publications (1)

Publication Number Publication Date
WO1998003997A1 true WO1998003997A1 (en) 1998-01-29

Family

ID=24734879

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1997/013326 WO1998003997A1 (en) 1996-07-22 1997-07-22 Closed loop liquid cooling within rf modules

Country Status (1)

Country Link
WO (1) WO1998003997A1 (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002028160A2 (en) * 2000-09-29 2002-04-04 Nanostream, Inc. Microfluidic devices for heat transfer
WO2002039241A2 (en) * 2000-11-13 2002-05-16 P21 - Power For The 21St Century Gmbh Electrical component
US6629425B2 (en) 2000-07-24 2003-10-07 Micron Technology, Inc. MEMS heat pumps for integrated circuit heat dissipation
EP1576320A2 (en) * 2001-09-28 2005-09-21 The Board Of Trustees Of The Leland Stanford Junior University Electroosmotic microchannel cooling system
EP1622198A2 (en) 2004-07-28 2006-02-01 Brother Kogyo Kabushiki Kaisha Substrate mounted with electronic element thereon and liquid ejection head including the substrate
US7018917B2 (en) 2003-11-20 2006-03-28 Asm International N.V. Multilayer metallization
WO2007002766A2 (en) * 2005-06-27 2007-01-04 Intel Corporation Optical transponder module with active heat transfer
DE102007044754A1 (en) * 2007-09-19 2009-04-09 Robert Bosch Gmbh Method for producing an electronic assembly and electronic assembly
WO2010086282A1 (en) * 2009-01-30 2010-08-05 Robert Bosch Gmbh Composite component and method for producing a composite component
WO2014182380A1 (en) * 2013-05-10 2014-11-13 Raytheon Company Method for creating a selective solder seal interface for an integrated circuit cooling system
US9012278B2 (en) 2013-10-03 2015-04-21 Asm Ip Holding B.V. Method of making a wire-based semiconductor device

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4894709A (en) * 1988-03-09 1990-01-16 Massachusetts Institute Of Technology Forced-convection, liquid-cooled, microchannel heat sinks
US5316077A (en) * 1992-12-09 1994-05-31 Eaton Corporation Heat sink for electrical circuit components
WO1995008844A1 (en) * 1993-09-21 1995-03-30 Siemens Aktiengesellschaft Cooling device for a power semiconductor module
EP0709885A2 (en) * 1994-10-31 1996-05-01 AT&T Corp. Circuit pack with integrated closed-loop cooling system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4894709A (en) * 1988-03-09 1990-01-16 Massachusetts Institute Of Technology Forced-convection, liquid-cooled, microchannel heat sinks
US5316077A (en) * 1992-12-09 1994-05-31 Eaton Corporation Heat sink for electrical circuit components
WO1995008844A1 (en) * 1993-09-21 1995-03-30 Siemens Aktiengesellschaft Cooling device for a power semiconductor module
EP0709885A2 (en) * 1994-10-31 1996-05-01 AT&T Corp. Circuit pack with integrated closed-loop cooling system

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
"HERMETICALLY SEALED, FIELD REMOVABLE MODULE HAVING AN INTEGRAL PUMP AND COOLANT HEAT EXCHANGER FOR FORCED CONVECTION IMMERSION COOLING OF ELECTRONIC CIRCUIT MODULES", IBM TECHNICAL DISCLOSURE BULLETIN., vol. 35, no. 4B, September 1992 (1992-09-01), NEW YORK US, pages 443 - 444, XP002046249 *

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7107777B2 (en) 2000-07-24 2006-09-19 Micro Technology, Inc. MEMS heat pumps for integrated circuit heat dissipation
US7084004B2 (en) 2000-07-24 2006-08-01 Micron Technology, Inc. MEMS heat pumps for integrated circuit heat dissipation
US6629425B2 (en) 2000-07-24 2003-10-07 Micron Technology, Inc. MEMS heat pumps for integrated circuit heat dissipation
SG105459A1 (en) * 2000-07-24 2004-08-27 Micron Technology Inc Mems heat pumps for integrated circuit heat dissipation
WO2002028160A2 (en) * 2000-09-29 2002-04-04 Nanostream, Inc. Microfluidic devices for heat transfer
US6501654B2 (en) 2000-09-29 2002-12-31 Nanostream, Inc. Microfluidic devices for heat transfer
WO2002028160A3 (en) * 2000-09-29 2002-06-27 Nanostream Inc Microfluidic devices for heat transfer
WO2002039241A3 (en) * 2000-11-13 2003-02-27 P21 Gmbh Electrical component
WO2002039241A2 (en) * 2000-11-13 2002-05-16 P21 - Power For The 21St Century Gmbh Electrical component
EP1576320A2 (en) * 2001-09-28 2005-09-21 The Board Of Trustees Of The Leland Stanford Junior University Electroosmotic microchannel cooling system
EP1576320A4 (en) * 2001-09-28 2005-10-05 Univ Leland Stanford Junior Electroosmotic microchannel cooling system
US7018917B2 (en) 2003-11-20 2006-03-28 Asm International N.V. Multilayer metallization
US7558071B2 (en) 2004-07-28 2009-07-07 Brother Kogyo Kabushiki Kaisha Substrate mounted with electronic element thereon
EP1622198A2 (en) 2004-07-28 2006-02-01 Brother Kogyo Kabushiki Kaisha Substrate mounted with electronic element thereon and liquid ejection head including the substrate
EP1622198A3 (en) * 2004-07-28 2007-04-11 Brother Kogyo Kabushiki Kaisha Substrate mounted with electronic element thereon and liquid ejection head including the substrate
US7352591B2 (en) 2004-07-28 2008-04-01 Brother Kogyo Kabushiki Kaisha Substrate mounted with electronic element thereon and liquid ejection head including the substrate
WO2007002766A2 (en) * 2005-06-27 2007-01-04 Intel Corporation Optical transponder module with active heat transfer
WO2007002766A3 (en) * 2005-06-27 2007-04-26 Intel Corp Optical transponder module with active heat transfer
US7457126B2 (en) 2005-06-27 2008-11-25 Intel Corporation Optical transponder with active heat transfer
DE102007044754A1 (en) * 2007-09-19 2009-04-09 Robert Bosch Gmbh Method for producing an electronic assembly and electronic assembly
WO2010086282A1 (en) * 2009-01-30 2010-08-05 Robert Bosch Gmbh Composite component and method for producing a composite component
US8730676B2 (en) 2009-01-30 2014-05-20 Robert Bosch Gmbh Composite component and method for producing a composite component
WO2014182380A1 (en) * 2013-05-10 2014-11-13 Raytheon Company Method for creating a selective solder seal interface for an integrated circuit cooling system
US8987892B2 (en) 2013-05-10 2015-03-24 Raytheon Company Method for creating a selective solder seal interface for an integrated circuit cooling system
US9012278B2 (en) 2013-10-03 2015-04-21 Asm Ip Holding B.V. Method of making a wire-based semiconductor device
US9553148B2 (en) 2013-10-03 2017-01-24 Asm Ip Holding B.V. Method of making a wire-based semiconductor device

Similar Documents

Publication Publication Date Title
US5692558A (en) Microchannel cooling using aviation fuels for airborne electronics
US5763951A (en) Non-mechanical magnetic pump for liquid cooling
US7327570B2 (en) Fluid cooled integrated circuit module
US6972365B2 (en) Thermal management system and method for electronics system
US6411512B1 (en) High performance cold plate
US6421240B1 (en) Cooling arrangement for high performance electronic components
US5801442A (en) Microchannel cooling of high power semiconductor devices
US6705089B2 (en) Two stage cooling system employing thermoelectric modules
US5036384A (en) Cooling system for IC package
US7492594B2 (en) Electronic circuit modules cooling
US6970358B2 (en) Stack up assembly
US5001548A (en) Multi-chip module cooling
US6496367B2 (en) Apparatus for liquid cooling of specific computer components
TWI243011B (en) Cooling system or electronic apparatus, and electronic apparatus using the same
US20050174735A1 (en) High performance cooling systems
US20120087088A1 (en) Microscale heat transfer systems
US20120106083A1 (en) Liquid cooling system for an electronic system
US20150047809A1 (en) Fabricating thermal transfer structure(s) and attachment mechanism(s) for cooling electronics card(s)
JPH10215094A (en) Device for eliminating heat from pc card array
WO1998003997A1 (en) Closed loop liquid cooling within rf modules
US7187550B1 (en) Gasketed field-replaceable active integrated liquid pump heat sink module for thermal management of electronic components
US20220007551A1 (en) Impinging jet coldplate for power electronics with enhanced heat transfer
JPH08213526A (en) Circuit pack
US20050047085A1 (en) High performance cooling systems
TWI403883B (en) Methodology of cooling multiple heat sources in a personal computer through the use of multiple fluid-based heat exchanging loops coupled via modular bus-type heat exchangers

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): JP

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LU MC NL PT SE

DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
121 Ep: the epo has been informed by wipo that ep was designated in this application
NENP Non-entry into the national phase

Ref country code: JP

Ref document number: 1998507253

Format of ref document f/p: F

122 Ep: pct application non-entry in european phase