CN106028766A - Novel cooling fin runner structure - Google Patents

Novel cooling fin runner structure Download PDF

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Publication number
CN106028766A
CN106028766A CN201610622030.5A CN201610622030A CN106028766A CN 106028766 A CN106028766 A CN 106028766A CN 201610622030 A CN201610622030 A CN 201610622030A CN 106028766 A CN106028766 A CN 106028766A
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CN
China
Prior art keywords
fin
path portion
flow passage
flow path
runner
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
CN201610622030.5A
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Chinese (zh)
Inventor
夏辉
吴凤鼎
管玉静
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Chengdu RML Technology Co Ltd
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Chengdu RML Technology Co Ltd
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 Chengdu RML Technology Co Ltd filed Critical Chengdu RML Technology Co Ltd
Priority to CN201610622030.5A priority Critical patent/CN106028766A/en
Publication of CN106028766A publication Critical patent/CN106028766A/en
Pending legal-status Critical Current

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Classifications

    • 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
    • H05K7/2039Modifications to facilitate cooling, ventilating, or heating characterised by the heat transfer by conduction from the heat generating element to a dissipating body
    • H05K7/20409Outer radiating structures on heat dissipating housings, e.g. fins integrated with the housing

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  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention relates to cooling devices, in particular to a novel cooling fin runner structure. The runner structure is divided into at least two runner parts in the length direction, intervals between fins in the runner part close to an air inlet are larger, and therefore the flow resistance of the runner part at the air inlet is reduced, and under the situation that the fan power is not changed, the supply air rate and the air speed in the whole fin runner can be effectively increased relative to an original runner structure; meanwhile, due to the fact that the closer the fins in the runner part are to the air outlet of the runner structure, the smaller the intervals of the fins are, the number of the fins is relatively large, and relative to the runner part at the air inlet, the contact surface of the runner fins with cooling air is increased, and the cooling effect is further enhanced. By means of the structure, under the situation that the fan power is not changed, the highest temperature (generally, a heating device close to the air outlet of the fin runner will have the highest temperature) of the heating device can be effectively reduced.

Description

A kind of Novel fin flow passage structure
Technical field
The present invention relates to heat abstractor, particularly a kind of Novel fin flow passage structure.
Background technology
Restriction due to some equipment (such as phased-array radar) complete machine structure layout, in order to be reached for heater members heat radiation and the demand of complete machine space structure simultaneously, often occur needing applying air inlet, air outlet to carry out situation about dispelling the heat at the rectangular fin runner of both ends of the surface;When specifically applying, rectangular fin runner is arranged with heater members parallel contact, by installing a fan at rectangular fin runner air outlet, cooling air is entered from air inlet, the heat that will be located in thermal conductive contact face heater members from the cooling air of rectangular fin runner process is taken away, but the runner of this rectangle is compared with general runner, have a disadvantage in that cooling air flows through the path of fin longer, flow resistance is bigger, the wind speed causing whole fin runner is difficult to improve, and then cause the closer to outlet cooling air temperature the highest, cooling-down effect near air outlet part is substantially weaker than the partial warm down effect near air inlet, whole fin runner uniform temperature is poor, the best near the heater members radiating effect of radiating fin runner air outlet part, the fin runner having this flow passage structure is caused can not well to realize heat sinking function.
Summary of the invention
The goal of the invention of the present invention is that the path flowing through fin due to air for the rectangular fin runner that length is longer is longer, flow resistance is bigger, cause and be substantially reduced by the cooling air wind speed of fin runner, air quantity, thus cause whole fin runner uniform temperature poor, near the problem that the heater members radiating effect of radiating fin runner air outlet part is the best, there is provided a kind of flow resistance less, the fin flow passage structure that runner uniform temperature is good.
To achieve these goals, the technical solution used in the present invention is:
A kind of Novel fin flow passage structure, described flow passage structure includes flow passage cover plate, runner base plate and the fin multiple parallel to each other between flow passage cover plate and runner base plate, and described fin is vertical with described flow passage cover plate and runner base plate;The two ends of flow passage structure are respectively air inlet and air outlet;Described air inlet or air outlet end are provided with a fan, for being blown into or in suction passage by cooling air;
Described flow passage structure is the most at least divided into two flow path portion, and fin interval difference in each flow path portion, wherein, the closer to the flow path portion of air inlet, the interval between fin is the biggest.Concrete, can as required flow passage structure be divided into 2 flow path portion, 3 flow path portion, even 8 flow path portion of 4 flow path portion, the flow path portion of division is the most, and the uniform temperature of the most whole flow passage structure zones of different is the best.
Preferably, in some embodiments, described flow passage structure is uniformly divided into three flow path portion along its length, and wherein the flow path portion near air inlet is low-temperature zone, and the flow path portion near air outlet is high temperature section, and the flow path portion between low-temperature zone and high temperature section is middle-temperature section;Fin interval in described low-temperature zone is more than the fin interval in middle-temperature section, and the fin interval in described middle-temperature section is more than the fin interval in high temperature section.
Further, described flow passage cover plate and/or runner base plate are the thermal conductive contact face contacted with heater members.
Further, in two adjacent flow path portion, the fin interval in the flow path portion that fin interval is big is 2 times that in the flow path portion that fin interval is little, fin is spaced.
Further, by being initial from air outlet, the fin arranging different length realizes the difference at fin interval in different flow path portion.
nullIn certain embodiments,Compared with prior art,The fin interval that will be closest in the flow path portion (generally high temperature section) at air outlet can be selected to keep constant,The most compared with prior art,Constant near the number of fins in the flow path portion (generally high temperature section) at air outlet,And from one section of flow path portion before high temperature section,(i.e. one section of flow path portion before high temperature section starts to reduce the number of fins in each flow path portion successively to expand the fin interval in follow-up flow path portion successively,Thus realize the increase at fin interval),Advantage of this is that,Achieving,Increase the purpose of fin runner intake,While realizing the more preferable uniform temperature of whole flow passage structure,Along with the expansion at fin interval in some flow path portion along flow channel length,Mean the minimizing of the number of fins arranged wherein,So that the weight of whole fin runner is reduced,In some equipment more sensitive to device weight,Such as phased-array radar,On the premise of the constant even lifting of each device performance,The reduction of complete machine weight has very important meaning,On the premise of i.e. the present invention can realize improving fin runner heat dispersion,Reduce device weight further,Significant.
In sum, owing to have employed technique scheme, the invention has the beneficial effects as follows:
The Novel fin flow passage structure that the present invention provides, compared with prior art, the flow passage structure that the present invention provides is divided at least two flow path portion along its length, fin in the flow path portion of air inlet is spaced at greater, therefore the flow path portion flow resistance of air inlet reduces, in the case of not changing fan power, the intake in whole fin runner and wind speed can be effectively improved relative to original flow passage structure;
Simultaneously, owing in the flow path portion the closer to flow passage structure air outlet, fin interval is the least, so its number of fins is the most, the flow path portion that air inlet goes out relatively, which increase the contact surface of runner fin and cooling air, further enhancing radiating effect, by this structure, same in the case of not changing fan power, can effectively reduce the maximum temperature (typically can have maximum temperature at the heater members at fin runner air outlet) of heater members.
Accompanying drawing explanation
Fig. 1 is typical strip fin flow passage structure schematic diagram.
The structural representation of the Fig. 2 fin flow passage structure specific embodiment for providing in the present invention.
The fin flow passage structure specific embodiment appearance schematic diagram that Fig. 3 provides for the present invention.
Reference: 1-flow passage cover plate, 2-runner base plate, 3-fin, 4-fan, 5-air inlet.
Detailed description of the invention
Below in conjunction with the accompanying drawings, the present invention is described in detail.
In order to make the purpose of the present invention, technical scheme and advantage clearer, below in conjunction with drawings and Examples, the present invention is further elaborated.Should be appreciated that specific embodiment described herein, only in order to explain the present invention, is not intended to limit the present invention.
Embodiment 1:As shown in Figure 2 and Figure 3, the present embodiment provides a kind of Novel fin flow passage structure, described flow passage structure includes flow passage cover plate 1, runner base plate 2 and the fin 3 multiple parallel to each other between flow passage cover plate and runner base plate, and described fin 3 is vertical with described flow passage cover plate 1 and runner base plate 2;The two ends of flow passage structure are respectively air inlet 5 and air outlet;In the present embodiment, described air outlet end is provided with a fan 4, for cooling down in air suction passage (flow passage structure);
In the present embodiment, described flow passage structure is uniformly divided into three flow path portion along its length, and wherein the flow path portion near air inlet is low-temperature zone, and the flow path portion near air outlet is high temperature section, and the flow path portion between low-temperature zone and high temperature section is middle-temperature section;Fin interval in described low-temperature zone is more than the fin interval in middle-temperature section, and the fin interval in described middle-temperature section is more than the fin interval in high temperature section.
In the present embodiment, in two adjacent flow path portion, the fin interval in the flow path portion that fin interval is big is 2 times that in the flow path portion that fin interval is little, fin is spaced.Concrete, as shown in Figure 2, in the present embodiment, all of fin starts to arrange from air outlet, and wherein the first fin 31 length of 1/3rd quantity is identical with high temperature section length, i.e., first fin 31 is positioned only in high temperature section, second fin 32 length of other 1/3rd quantity is equal to high temperature section+middle-temperature section, i.e. the second fin 32 of this 1/3rd quantity is positioned only in high temperature section and middle-temperature section;3rd fin 33 length of last 1/3rd quantity is identical with flow passage structure length, i.e. the 3rd fin 33 of this 1/3rd quantity is simultaneously located in high temperature section, middle-temperature section i.e. low-temperature zone;The fin of different length is initial at air outlet, crosses one another and be arranged in parallel, thus the fin 3 realized in different flow channel section is spaced difference.
In the present embodiment, described runner base plate 2 is the thermal conductive contact face contacted with heater members, heater members transfers heat to each fin 3 by runner base plate 2, and be arranged at the fan 4 of flow passage structure air outlet end face by the air suction passage structure being used for cooling, thus the heat on fin 3 is taken away the effect playing cooling heat radiation.
Embodiment 2:It is with embodiment 2 difference, the Novel fin flow passage structure that the present embodiment provides is divided into two flow path portion along its length, wherein the flow path portion near air inlet 5 is low-temperature zone, flow path portion near air outlet is high temperature section, and the fin interval in described low-temperature zone is more than the fin interval in high temperature section.
And in the present embodiment, described runner base plate 2 is the thermal conductive contact face contacted with heater members with flow passage cover plate 1, it transfers heat to each fin 3 be arrangeding in parallel simultaneously.
The foregoing is only presently preferred embodiments of the present invention, not in order to limit the present invention, all any amendment, equivalent and improvement etc. made within the spirit and principles in the present invention, should be included within the scope of the present invention.

Claims (5)

1. a Novel fin flow passage structure, described flow passage structure includes flow passage cover plate, runner base plate and the fin multiple parallel to each other between flow passage cover plate and runner base plate, and described fin is vertical with described flow passage cover plate and runner base plate;The two ends of flow passage structure are respectively air inlet and air outlet;Described air inlet or air outlet end are provided with a fan, for being blown into or in suction passage by cooling air;
It is characterized in that, described flow passage structure is the most at least divided into two flow path portion, and fin interval difference in each flow path portion, wherein, the closer to the flow path portion of air inlet, the interval between fin is the biggest.
Radiating fin flow passage structure the most according to claim 1, it is characterized in that, described flow passage structure is uniformly divided into three flow path portion along its length, wherein the flow path portion near air inlet is low-temperature zone, flow path portion near air outlet is high temperature section, and the flow path portion between low-temperature zone and high temperature section is middle-temperature section;Fin interval in described low-temperature zone is more than the fin interval in middle-temperature section, and the fin interval in described middle-temperature section is more than the fin interval in high temperature section.
Radiating fin flow passage structure the most according to claim 1, it is characterised in that described flow passage cover plate and/or runner base plate are the thermal conductive contact face contacted with heater members.
Radiating fin flow passage structure the most according to claim 1, it is characterised in that in two adjacent flow path portion, the fin interval in the flow path portion that fin interval is big is 2 times that in the flow path portion that fin interval is little, fin is spaced.
Radiating fin flow passage structure the most according to claim 1, it is characterised in that by being initial from air outlet, the fin arranging different length realizes the difference at fin interval in different flow path portion.
CN201610622030.5A 2016-08-02 2016-08-02 Novel cooling fin runner structure Pending CN106028766A (en)

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106714525A (en) * 2017-02-27 2017-05-24 华为机器有限公司 Heat dissipation device and electronic equipment
CN106993395A (en) * 2017-04-27 2017-07-28 歌尔丹拿音响有限公司 A kind of power amplifier
CN109994442A (en) * 2017-12-29 2019-07-09 鸿富锦精密工业(武汉)有限公司 The electronic device of radiator and the application radiator
CN110313226A (en) * 2018-08-16 2019-10-08 深圳市大疆创新科技有限公司 Radiating subassembly, heat radiation module and unmanned vehicle
CN110313225A (en) * 2018-06-26 2019-10-08 深圳市大疆创新科技有限公司 Radiating subassembly and circuit board assemblies, unmanned vehicle with it
CN110536588A (en) * 2019-08-20 2019-12-03 东软医疗系统股份有限公司 Detector and medical scanning equipment
CN110621138A (en) * 2018-06-20 2019-12-27 鸿富锦精密工业(武汉)有限公司 Liquid cooling heat radiator and electronic device using same
CN111916410A (en) * 2019-05-10 2020-11-10 株洲中车时代电气股份有限公司 Heat radiator
CN112606994A (en) * 2020-12-29 2021-04-06 中国航空工业集团公司西安飞机设计研究所 Integrated thermal control design method for wings of solar unmanned aerial vehicle

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Publication number Priority date Publication date Assignee Title
CN101312632A (en) * 2007-05-25 2008-11-26 富准精密工业(深圳)有限公司 Heat radiating device
CN201440054U (en) * 2009-07-17 2010-04-21 王信懿 Radiating fin structure of radiator
JP2014053442A (en) * 2012-09-07 2014-03-20 Mitsubishi Electric Corp Plate laminated type cooling device
CN103796475A (en) * 2012-10-30 2014-05-14 英业达科技有限公司 Heat radiation module and electronic device
CN104105379A (en) * 2013-04-12 2014-10-15 技嘉科技股份有限公司 Heat radiation assembly and display card module
CN205830253U (en) * 2016-08-02 2016-12-21 成都雷电微力科技有限公司 A kind of Novel fin flow passage structure

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101312632A (en) * 2007-05-25 2008-11-26 富准精密工业(深圳)有限公司 Heat radiating device
CN201440054U (en) * 2009-07-17 2010-04-21 王信懿 Radiating fin structure of radiator
JP2014053442A (en) * 2012-09-07 2014-03-20 Mitsubishi Electric Corp Plate laminated type cooling device
CN103796475A (en) * 2012-10-30 2014-05-14 英业达科技有限公司 Heat radiation module and electronic device
CN104105379A (en) * 2013-04-12 2014-10-15 技嘉科技股份有限公司 Heat radiation assembly and display card module
CN205830253U (en) * 2016-08-02 2016-12-21 成都雷电微力科技有限公司 A kind of Novel fin flow passage structure

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106714525A (en) * 2017-02-27 2017-05-24 华为机器有限公司 Heat dissipation device and electronic equipment
CN106714525B (en) * 2017-02-27 2019-04-19 华为机器有限公司 Radiator and electronic equipment
CN106993395A (en) * 2017-04-27 2017-07-28 歌尔丹拿音响有限公司 A kind of power amplifier
WO2018196141A1 (en) * 2017-04-27 2018-11-01 歌尔丹拿音响有限公司 Power amplifier
CN109994442A (en) * 2017-12-29 2019-07-09 鸿富锦精密工业(武汉)有限公司 The electronic device of radiator and the application radiator
CN110621138A (en) * 2018-06-20 2019-12-27 鸿富锦精密工业(武汉)有限公司 Liquid cooling heat radiator and electronic device using same
CN110313225A (en) * 2018-06-26 2019-10-08 深圳市大疆创新科技有限公司 Radiating subassembly and circuit board assemblies, unmanned vehicle with it
CN110313226A (en) * 2018-08-16 2019-10-08 深圳市大疆创新科技有限公司 Radiating subassembly, heat radiation module and unmanned vehicle
CN110313226B (en) * 2018-08-16 2020-11-20 深圳市大疆创新科技有限公司 Heat dissipation assembly, heat dissipation module and unmanned aerial vehicle
CN111916410A (en) * 2019-05-10 2020-11-10 株洲中车时代电气股份有限公司 Heat radiator
CN110536588A (en) * 2019-08-20 2019-12-03 东软医疗系统股份有限公司 Detector and medical scanning equipment
CN112606994A (en) * 2020-12-29 2021-04-06 中国航空工业集团公司西安飞机设计研究所 Integrated thermal control design method for wings of solar unmanned aerial vehicle

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Application publication date: 20161012

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