SE411949B - cooling device - Google Patents

cooling device

Info

Publication number
SE411949B
SE411949B SE7607878A SE7607878A SE411949B SE 411949 B SE411949 B SE 411949B SE 7607878 A SE7607878 A SE 7607878A SE 7607878 A SE7607878 A SE 7607878A SE 411949 B SE411949 B SE 411949B
Authority
SE
Sweden
Prior art keywords
cooling device
cooling
Prior art date
Application number
SE7607878A
Other languages
Swedish (sv)
Other versions
SE7607878L (en
Inventor
N A Persson
Original Assignee
Ericsson Telefon Ab L M
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 Ericsson Telefon Ab L M filed Critical Ericsson Telefon Ab L M
Priority to SE7607878A priority Critical patent/SE411949B/en
Priority to FR7720506A priority patent/FR2357986A1/en
Priority to GB28187/77A priority patent/GB1526160A/en
Priority to IT25490/77A priority patent/IT1081523B/en
Publication of SE7607878L publication Critical patent/SE7607878L/en
Publication of SE411949B publication Critical patent/SE411949B/en

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, or structural parts of the aircraft
    • 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)
  • Pulmonology (AREA)
  • General Health & Medical Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
SE7607878A 1976-07-09 1976-07-09 cooling device SE411949B (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
SE7607878A SE411949B (en) 1976-07-09 1976-07-09 cooling device
FR7720506A FR2357986A1 (en) 1976-07-09 1977-07-04 COOLING DEVICE TO DISSIPATE THE HEAT EMITTED BY AN APPLIANCE
GB28187/77A GB1526160A (en) 1976-07-09 1977-07-05 Cooling system
IT25490/77A IT1081523B (en) 1976-07-09 1977-07-07 HEAT TUBE COOLING SYSTEM

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
SE7607878L SE7607878L (en) 1978-01-10
SE411949B true SE411949B (en) 1980-02-11

Family

ID=20328438

Family Applications (1)

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

Country Status (4)

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

Families Citing this family (12)

* 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
US20040052052A1 (en) * 2002-09-18 2004-03-18 Rivera Rudy A. Circuit cooling apparatus
GB0323993D0 (en) * 2003-10-14 2003-11-19 Rolls Royce Plc Engine cooling
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
GB0526190D0 (en) * 2005-12-22 2006-02-01 Calamvokis Hal E Aircraft fuselage heating
FR2957053B1 (en) * 2010-03-03 2016-09-09 Aircelle Sa COOLING ASSEMBLY FOR A COMPONENT OF A NACELLE FOR A TURBOJET ENGINE
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
US10746479B2 (en) * 2018-02-09 2020-08-18 General Electric Company Additively manufactured structures for thermal and/or mechanical systems, and methods for manufacturing the structures

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

Also Published As

Publication number Publication date
FR2357986B1 (en) 1984-07-20
FR2357986A1 (en) 1978-02-03
GB1526160A (en) 1978-09-27
IT1081523B (en) 1985-05-21
SE7607878L (en) 1978-01-10

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