CN106352725A - Heat dissipation device capable of achieving integrated structural thermal control and processing method - Google Patents

Heat dissipation device capable of achieving integrated structural thermal control and processing method Download PDF

Info

Publication number
CN106352725A
CN106352725A CN201610919770.5A CN201610919770A CN106352725A CN 106352725 A CN106352725 A CN 106352725A CN 201610919770 A CN201610919770 A CN 201610919770A CN 106352725 A CN106352725 A CN 106352725A
Authority
CN
China
Prior art keywords
heat dissipation
thermal control
dissipation device
shell body
inner housing
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.)
Pending
Application number
CN201610919770.5A
Other languages
Chinese (zh)
Inventor
励精图治
李磊
黄金印
满广龙
张红星
孙萌
杨沪宁
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.)
Beijing Institute of Spacecraft System Engineering
Original Assignee
Beijing Institute of Spacecraft System Engineering
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 Beijing Institute of Spacecraft System Engineering filed Critical Beijing Institute of Spacecraft System Engineering
Priority to CN201610919770.5A priority Critical patent/CN106352725A/en
Publication of CN106352725A publication Critical patent/CN106352725A/en
Pending legal-status Critical Current

Links

Classifications

    • 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
    • F28D15/04Heat-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 tubes having a capillary structure
    • F28D15/046Heat-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 tubes having a capillary structure characterised by the material or the construction of the capillary structure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F21/00Constructions of heat-exchange apparatus characterised by the selection of particular materials
    • F28F21/08Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K7/00Constructional details common to different types of electric apparatus
    • H05K7/20Modifications to facilitate cooling, ventilating, or heating
    • H05K7/2029Modifications to facilitate cooling, ventilating, or heating using a liquid coolant with phase change in electronic enclosures
    • H05K7/20336Heat pipes, e.g. wicks or capillary pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)

Abstract

The invention discloses a heat dissipation device capable of achieving integrated structural thermal control and a processing method. Through the adoption of the heat dissipation device, the continuous heat transfer in a three-dimensional direction can be achieved; the heat transfer efficiency can be improved; the device is high in structural stability and can achieve a certain support effect.

Description

A kind of structure thermal control integral heat dissipation device and processing method
Technical field
The present invention relates to thermal control technical field is and in particular to a kind of structure thermal control integral heat dissipation device and processing method.
Background technology
With the continuous development of electronic technology, the integrated level of all kinds of chips and module and power consumption are all greatly improved, a side Face leads to heat flow density to increase, and brings risk for the reliability that it is used safely, on the other hand then can cause difference in functionality chip Or dense layout in same system for the module, it is to realize effectively radiating in small space to bring bigger difficulty.
For the heater element of high-power high heat flux, particularly the signal-data processing unit of board form, generally Using soaking plate provide radiating, this is the flat plate heat spreading apparatus that a kind of inwall has capillary structure, when heat by heat source extremely During evaporating area, the working medium in cavity starts to gasify, and absorbs heat, and the gas-phase working medium relatively low region condensation of temperature internally is put Heat, the liquid phase working fluid after condensation returns at thermal source in the presence of capillary force or other driving forces, thus realizing the diffusion of heat And transmission.
The requirement to thermal control for the whole machine improves constantly, in the middle of the higher system of the integrated level not possessing liquid cool condition, as The cabinet of structural support or framework are it is also desirable to possess heat sinking function.Traditional soaking plate only can expand heat in two dimensional surface direction, needs Three-dimensional heat transfer just be can achieve by connecting method, but larger interface resistance can be produced in stitching portion, and due to steam The blocking-up of passage and overheated gas cannot be delivered directly to the relatively low cold end of temperature, therefore heat dissipation capacity is extremely limited.Additionally, for , not in conplane application scenario, traditional soaking plate then cannot realize break-in spatially or bending for heating face and cooling surface. To sum up, for adapting to more and more harsh thermal control condition, need a kind of steam cavity configuration of three-dimensional communication, this kind of heat abstractor is realized Structure thermal control integration, has a biphase heat-transfer capability on three-dimensional, on the basis of ensureing high efficiency and heat radiation level, has Simplifying further beneficial to system.
Content of the invention
In view of this, the invention provides a kind of structure thermal control integral heat dissipation device, can more efficiently radiate Simultaneously moreover it is possible to play the effect of structural support.
The present invention is a kind of structure thermal control integral heat dissipation device, and described heat abstractor is cuboid or the cylinder of hollow For the cavity structure of closing inside body, this cuboid or cylinder, in cavity structure, there are the support column in array distribution, support column Two ends are contacted with cuboid or cylindrical cavity wall respectively, and the central axis upright supporting in cuboid wall or with Cylinder is radially consistent;There is capillary structure on the wall of cavity structure and support column surface;There is liquid medium in capillary structure.
Further, described projection is cylinder or cube.
Further, described capillary structure is metal dust, multiple layer metal silk screen or the metal felt of sintering.
The processing method that the present invention also designs described structure thermal control integral heat dissipation device, specifically includes following steps:
Step 1, the respectively bossed inner housing of the outer surface belt (1) of machining molding heat abstractor and corresponding shell Body (2), in addition to the two contact surface, each face is both needed to leave enough allowance;
Step 2, capillary structure is sintered on shell body (4) and the inner surface of inner housing (1);
Step 3, by inner housing (1) and shell body (4) cooperation be bolted together, adopt agitating friction in the junction at edge Weld inner housing (1) and shell body (4) seam;
Step 4, using agitating friction weldering by the support column (2) of (1) on inner housing and shell body (4) joint face seam.
Step 5, on housing arrange filling exit;
Step 6, liquid medium is filled by filling exit and filling aperture is sealed;
Step 7, polish molding.
Beneficial effect:
1st, this heat abstractor reaches without hindrance stealpass heat on three-dimensional, and steam channel all connects on three-dimensional, keeps away Exempt from the use of interface Heat Conduction Material, heat transfer resistance reduces by more than 80%, heat transfer temperature difference reduces by more than 5 DEG C, and integral heat sink amount carries High more than 2 times;
2nd, this heat abstractor is three-dimensional integratedization space structure, and plane at an angle to each other is continuous structure in intersection, There is not the blocking-up being formed because of assembly processes such as splicings, improve structural stability and the bulk strength of heat abstractor.
Brief description
Fig. 1 (a) is inner housing schematic diagram.
Fig. 1 (b) is shell body schematic diagram.
Fig. 1 (c) is the assembling schematic diagram of inner housing and shell body.
Fig. 2 integrated radiating schematic diagram.
Wherein, 1- inner housing, 2- support column, 3- steam channel, 4- shell body.
Specific embodiment
Develop simultaneously embodiment below in conjunction with the accompanying drawings, describes the present invention.
The invention provides a kind of structure thermal control integral heat dissipation device and processing method.
Structure thermal control integral heat dissipation device should include at least 2 soaking plate that are at an angle to each other and having splicing relation, herein Taking comprise the framework of 4 face soaking versions as a example explanation.
As shown in figure 1, being the processing method of this device, specifically comprise the following steps that
The inner housing with support column 2 as shown in Fig. 1 (a) of step 1, respectively machining molding heat abstractor, and Corresponding shell body as shown in Fig. 1 (a), in addition to the two contact surface, each face is both needed to leave enough allowance.
Step 2, capillary structure is sintered on the inner surface of shell and the outer surface of inner shell;
Step 3, by inner housing 1 and shell body 4 cooperation be bolted together, edge junction adopt agitating friction weldering will Inner housing 1 and shell body 4 seam, such as shown in Fig. 1 (c).
Step 4, using agitating friction weldering by inner housing 1 support column 4 and shell body 4 joint face seam.
Step 5, according to practical situation select liquid medium filling exit position carry out punching, fill, seal.
Step 6, polish molding.
The heat abstractor machining is as shown in Fig. 2 be for closing inside the rectangular structure of hollow, rectangular structure Cavity, has the support column in array distribution in cavity, support two ends contact with the cavity wall of this rectangular structure respectively and Place along perpendicular to wall direction, cavity wall and support surface and have capillary structure, in capillary structure, have liquid medium.
Double Shell can be copper, copper alloy, aluminum, aluminium alloy, stainless steel and other metal materials, and liquid medium 15 can be The heat-exchange working mediums such as water, ethanol, fluoride, acetone, ammonia.Support column 2 as supporting construction, can be cylinder table can also be rectangle Platform is it is therefore an objective to ensure that this heat abstractor is born interior pressure or external pressure all the time within overall tolerance yield strength.Capillary Structure is attached to the inner surface of metal rectangular structure, and this capillary structure can be sintering metal powder, multiple layer metal silk screen or Person's metal felt etc..Cavity within rectangular structure is steam channel 3.Liquid medium in capillary structure be subject to thermal evaporation after, Carry heat and enter steam channel 3, liquefy to the cold in temperature lower region, reenter capillary structure, carried in capillary structure Return to heat affected zone under the driving of capillary force.This device can not only complete to radiate in the either side of rectangular structure, also Can be conducted heat on three-dimensional by the no steam channel of blocking-up and capillary structure, enter into adjacent or even phase from a side Is radiated in side, concrete mode is: liquid medium in a side of rectangular structure be subject to thermal evaporation after, can pass through Liquefy to the cold in the temperature lower region that steam channel 3 enters into an adjacent side, the capillary structure through connecting the two also may be used To return to the heat affected zone of this device, realize quick transmission on three dimensions for the heat.
In sum, these are only presently preferred embodiments of the present invention, be not intended to limit protection scope of the present invention. All any modification, equivalent substitution and improvement within the spirit and principles in the present invention, made etc., should be included in the present invention's Within protection domain.

Claims (4)

1. a kind of structure thermal control integral heat dissipation device is it is characterised in that described heat abstractor is cuboid or the cylinder of hollow For the cavity structure of closing inside body, this cuboid or cylinder, in cavity structure, there are the support column in array distribution, support column Two ends are contacted with cuboid or cylindrical cavity wall respectively, and the central axis upright supporting in cuboid wall or with Cylinder is radially consistent;There is capillary structure on the wall of cavity structure and support column surface;There is liquid medium in capillary structure.
2. structure thermal control integral heat dissipation device as claimed in claim 1 is it is characterised in that described projection is cylinder or side Body.
3. structure thermal control integral heat dissipation device as claimed in claim 1 is it is characterised in that described capillary structure is sintering Metal dust, multiple layer metal silk screen or metal felt.
4. a kind of processing method for the structure thermal control integral heat dissipation device described in claim 1 was it is characterised in that should add Work method comprises the following steps:
Step 1, the respectively bossed inner housing of the outer surface belt (1) of machining molding heat abstractor and corresponding shell body (2), in addition to the two contact surface, each face is both needed to leave enough allowance;
Step 2, capillary structure is sintered on shell body (4) and the inner surface of inner housing (1);
Step 3, by inner housing (1) and shell body (4) cooperation be bolted together, edge junction adopt agitating friction weldering will Inner housing (1) and shell body (4) seam;
Step 4, using agitating friction weldering by the support column (2) of (1) on inner housing and shell body (4) joint face seam.
Step 5, on housing arrange filling exit;
Step 6, liquid medium is filled by filling exit and filling aperture is sealed;
Step 7, polish molding.
CN201610919770.5A 2016-10-21 2016-10-21 Heat dissipation device capable of achieving integrated structural thermal control and processing method Pending CN106352725A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610919770.5A CN106352725A (en) 2016-10-21 2016-10-21 Heat dissipation device capable of achieving integrated structural thermal control and processing method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610919770.5A CN106352725A (en) 2016-10-21 2016-10-21 Heat dissipation device capable of achieving integrated structural thermal control and processing method

Publications (1)

Publication Number Publication Date
CN106352725A true CN106352725A (en) 2017-01-25

Family

ID=57863542

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610919770.5A Pending CN106352725A (en) 2016-10-21 2016-10-21 Heat dissipation device capable of achieving integrated structural thermal control and processing method

Country Status (1)

Country Link
CN (1) CN106352725A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107771017A (en) * 2017-12-05 2018-03-06 匀加速科技有限公司 Handset shell
CN107846827A (en) * 2017-12-05 2018-03-27 匀加速科技有限公司 capillary radiating mobile phone

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2479467Y (en) * 2001-04-16 2002-02-27 李嘉豪 Cylinder radiator
JP2007317876A (en) * 2006-05-25 2007-12-06 Fujitsu Ltd Heat sink
CN101272674A (en) * 2008-05-15 2008-09-24 中山大学 Three-dimensional uniform temperature heat transfer device
CN201812811U (en) * 2010-10-15 2011-04-27 游明郎 Temperature equalizing plate
CN102149266A (en) * 2010-02-04 2011-08-10 台烨科技股份有限公司 Temperature equalizing plate
CN202354010U (en) * 2011-11-23 2012-07-25 燿佳科技股份有限公司 Heat radiation device
CN206310966U (en) * 2016-10-21 2017-07-07 北京空间飞行器总体设计部 A kind of structure thermal control integral heat dissipation device

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2479467Y (en) * 2001-04-16 2002-02-27 李嘉豪 Cylinder radiator
JP2007317876A (en) * 2006-05-25 2007-12-06 Fujitsu Ltd Heat sink
CN101272674A (en) * 2008-05-15 2008-09-24 中山大学 Three-dimensional uniform temperature heat transfer device
CN102149266A (en) * 2010-02-04 2011-08-10 台烨科技股份有限公司 Temperature equalizing plate
CN201812811U (en) * 2010-10-15 2011-04-27 游明郎 Temperature equalizing plate
CN202354010U (en) * 2011-11-23 2012-07-25 燿佳科技股份有限公司 Heat radiation device
CN206310966U (en) * 2016-10-21 2017-07-07 北京空间飞行器总体设计部 A kind of structure thermal control integral heat dissipation device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107771017A (en) * 2017-12-05 2018-03-06 匀加速科技有限公司 Handset shell
CN107846827A (en) * 2017-12-05 2018-03-27 匀加速科技有限公司 capillary radiating mobile phone
CN107846827B (en) * 2017-12-05 2019-10-29 南通沃特光电科技有限公司 Capillary heat dissipation mobile phone

Similar Documents

Publication Publication Date Title
CN100565074C (en) Plate type heat exchanger and manufacture method thereof
CN100470773C (en) Heat pipe radiating device
KR950014044B1 (en) Integral heat pipe heat exchanger and clamping plate
US7215547B2 (en) Integrated cooling system for electronic devices
US10462932B2 (en) Memory module cooler with vapor chamber device connected to heat pipes
JP2006503436A (en) Plate heat transfer device and manufacturing method thereof
CN213426737U (en) Liquid cooling heat abstractor and have this liquid cooling heat abstractor's liquid cooling system
EP2687319B1 (en) Gravity circuit heat pipe radiator, condenser and preparation process
CN111863746B (en) Heat abstractor, circuit board and electronic equipment
US10240873B2 (en) Joint assembly of vapor chambers
JP5094045B2 (en) Electronic circuit device having cooling function and manufacturing method thereof
WO2022257963A1 (en) Heat dissipation member and electronic device
CN101101180A (en) Compound heat-exchanger
CN104662656A (en) Cooling device, heat reception unit and boiling unit used therein, and method for manufacturing same
CN103327792A (en) Passive-driven micro-channel heat-sink cooling device
CN106352725A (en) Heat dissipation device capable of achieving integrated structural thermal control and processing method
CN107801351B (en) Evaporator and manufacturing method thereof
CN206310966U (en) A kind of structure thermal control integral heat dissipation device
JP2016021474A (en) Laminate structure having intercommunication space therein and manufacturing method for the same
WO2012161002A1 (en) Flat plate cooling device, and method for using same
CN104080313A (en) Heat dissipation module
CN108106473A (en) The hot transmission module of phase stream
CN107195603A (en) A kind of preparation method of the encapsulating structure based on high heat conduction phase-change material phase-change heat technology
JP5546280B2 (en) Connection part of heat pipe heat receiving part and connection method of heat pipe heat receiving part
CN108601286B (en) Electronic device

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20170125

RJ01 Rejection of invention patent application after publication