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GB1526160A - Cooling system - Google Patents

Cooling system

Info

Publication number
GB1526160A
GB1526160A GB28187/77A GB2818777A GB1526160A GB 1526160 A GB1526160 A GB 1526160A GB 28187/77 A GB28187/77 A GB 28187/77A GB 2818777 A GB2818777 A GB 2818777A GB 1526160 A GB1526160 A GB 1526160A
Authority
GB
United Kingdom
Prior art keywords
equipment
liquid
heat
july
thermally connected
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB28187/77A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Telefonaktiebolaget LM Ericsson AB
Original Assignee
Telefonaktiebolaget LM Ericsson AB
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 Telefonaktiebolaget LM Ericsson AB filed Critical Telefonaktiebolaget LM Ericsson AB
Publication of GB1526160A publication Critical patent/GB1526160A/en
Expired legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K7/00—Constructional details common to different types of electric apparatus
    • H05K7/20—Modifications to facilitate cooling, ventilating, or heating
    • H05K7/2029—Modifications to facilitate cooling, ventilating, or heating using a liquid coolant with phase change in electronic enclosures
    • H05K7/20336—Heat pipes, e.g. wicks or capillary pumps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D15/00—Heat-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
    • F28D15/02—Heat-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
    • F28D15/0233—Heat-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 the conduits having a particular shape, e.g. non-circular cross-section, annular
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D15/00—Heat-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
    • F28D15/02—Heat-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
    • F28D15/0266—Heat-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 with separate evaporating and condensing chambers connected by at least one conduit; Loop-type heat pipes; with multiple or common evaporating or condensing chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D5/00—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, using the cooling effect of natural or forced evaporation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2265/00—Safety or protection arrangements; Arrangements for preventing malfunction
    • F28F2265/26—Safety or protection arrangements; Arrangements for preventing malfunction for allowing differential expansion between elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2265/00—Safety or protection arrangements; Arrangements for preventing malfunction
    • F28F2265/30—Safety or protection arrangements; Arrangements for preventing malfunction for preventing vibrations

Landscapes

  • Engineering & Computer Science (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

1526160 Heat pipes TELEFONAKTIE BOLAGET L M ERICSSON 5 July 1977 [9 July 1976] 28187/77 Heading F4U A cooling system for dissipating to the surroundings heat generated in equipment 20, e.g. transmitter or computer equipment in an aircraft, comprises a heat pipe 18 having an evaporator portion 19, thermally connected to the equipment, and a condenser portion 22 thermally connected to a porous heat conducting body 13, an evaporable liquid being supplied to the body 13 in use of the system. As shown, the body 13 comprises a sheet of sintered copper located in an aperture 12 in an aircraft fuselage 11 and secured to a plate 16 forming one end of the heat pipe. A liquid, e.g. water, is fed through an inlet tube 15 to channels 14 provided in the body 13. Alternatively, if the body 13 is located adjacent to the inlet of a jet engine, an inflammable liquid, e.g. methyl alcohol, light petrol or jet fuel may be used instead of water.
GB28187/77A 1976-07-09 1977-07-05 Cooling system Expired GB1526160A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE7607878A SE411949B (en) 1976-07-09 1976-07-09 cooling device

Publications (1)

Publication Number Publication Date
GB1526160A true GB1526160A (en) 1978-09-27

Family

ID=20328438

Family Applications (1)

Application Number Title Priority Date Filing Date
GB28187/77A Expired GB1526160A (en) 1976-07-09 1977-07-05 Cooling system

Country Status (4)

Country Link
FR (1) FR2357986A1 (en)
GB (1) GB1526160A (en)
IT (1) IT1081523B (en)
SE (1) SE411949B (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2393330A (en) * 2002-09-18 2004-03-24 Hewlett Packard Development Co Circuit cooling apparatus
WO2005063566A3 (en) * 2003-12-30 2005-09-22 Airbus Gmbh Cooling system and method for expelling heat from a heat source located in the interior of an aircraft
EP1524190A3 (en) * 2003-10-14 2006-08-30 ROLLS-ROYCE plc Engine cooling
WO2007072027A3 (en) * 2005-12-22 2008-03-06 Hal Errikos Calamvokis Aircraft fuselage heating
EP2567894A1 (en) * 2011-09-07 2013-03-13 Bell Helicopter Textron Inc. System for heat dissipation from an internal actuator in a rotor blade
US10124894B2 (en) 2012-03-30 2018-11-13 B/E Aerospace, Inc. Aircraft galley chilled air distribution system
EP3524529A1 (en) * 2018-02-09 2019-08-14 General Electric Company Additively manufactured structures for thermal and/or mechanical systems, and methods for manufacturing the structures
US11220340B2 (en) 2013-03-28 2022-01-11 Rockwell Collins, Inc. Galley cart bay rub strip assembly with enhanced airflow

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2449794A1 (en) * 1979-02-23 1980-09-19 Renault Combustion gas preheater for IC-engine - has gas inlet passage adjacent to exhaust gases with corrugated capsule between two manifolds
DE3832005C1 (en) * 1988-09-21 1990-05-17 Erno Raumfahrttechnik Gmbh, 2800 Bremen, De
US5894887A (en) * 1995-11-30 1999-04-20 Applied Materials, Inc. Ceramic dome temperature control using heat pipe structure and method
FR2957053B1 (en) * 2010-03-03 2016-09-09 Aircelle Sa COOLING ASSEMBLY FOR A COMPONENT OF A NACELLE FOR A TURBOJET ENGINE

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1244917A (en) * 1959-06-29 1960-11-04 Chausson Usines Sa evaporative heat exchanger
JPS5433710B2 (en) * 1973-02-12 1979-10-22

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2393330A (en) * 2002-09-18 2004-03-24 Hewlett Packard Development Co Circuit cooling apparatus
GB2393330B (en) * 2002-09-18 2005-11-16 Hewlett Packard Development Co Circuit cooling apparatus
US7019973B2 (en) 2002-09-18 2006-03-28 Hewlett-Packard Development Company, L.P. Circuit cooling apparatus
EP1524190A3 (en) * 2003-10-14 2006-08-30 ROLLS-ROYCE plc Engine cooling
CN100510604C (en) * 2003-12-30 2009-07-08 空中客车德国有限公司 Cooling system and method for expelling heat from a heat source located in the interior of an aircraft
JP2007519555A (en) * 2003-12-30 2007-07-19 エアバス ドイチェランド ゲゼルシャフト ミット ベシュレンクテル ハフツング Cooling system and method for exhausting heat from a heat source located inside an aircraft
DE10361653B4 (en) * 2003-12-30 2008-08-07 Airbus Deutschland Gmbh Cooling device for removing heat from an arranged in the interior of an aircraft heat source
WO2005063566A3 (en) * 2003-12-30 2005-09-22 Airbus Gmbh Cooling system and method for expelling heat from a heat source located in the interior of an aircraft
RU2378596C2 (en) * 2003-12-30 2010-01-10 Эйрбас Дойчланд Гмбх Cooling system and method of heat removal from thermal sources located inside aircraft
US7967249B2 (en) 2003-12-30 2011-06-28 Airbus Deutschland Gmbh Cooling system and method for expelling heat from a heat source located in the interior of an aircraft
WO2007072027A3 (en) * 2005-12-22 2008-03-06 Hal Errikos Calamvokis Aircraft fuselage heating
EP2567894A1 (en) * 2011-09-07 2013-03-13 Bell Helicopter Textron Inc. System for heat dissipation from an internal actuator in a rotor blade
US8926272B2 (en) 2011-09-07 2015-01-06 Textron Innovations Inc. System for heat dissipation from an internal actuator in a rotor blade
US10124894B2 (en) 2012-03-30 2018-11-13 B/E Aerospace, Inc. Aircraft galley chilled air distribution system
US11220340B2 (en) 2013-03-28 2022-01-11 Rockwell Collins, Inc. Galley cart bay rub strip assembly with enhanced airflow
EP3524529A1 (en) * 2018-02-09 2019-08-14 General Electric Company Additively manufactured structures for thermal and/or mechanical systems, and methods for manufacturing the structures
CN110132039A (en) * 2018-02-09 2019-08-16 通用电气公司 The structure of the increasing material manufacturing of heat and/or mechanical system and the method for manufacturing the structure

Also Published As

Publication number Publication date
IT1081523B (en) 1985-05-21
FR2357986B1 (en) 1984-07-20
SE411949B (en) 1980-02-11
FR2357986A1 (en) 1978-02-03
SE7607878L (en) 1978-01-10

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Legal Events

Date Code Title Description
PS Patent sealed
PE20 Patent expired after termination of 20 years

Effective date: 19970704