CN206524325U - Heat radiation elements for radar battlebus - Google Patents
Heat radiation elements for radar battlebus Download PDFInfo
- Publication number
- CN206524325U CN206524325U CN201720228385.6U CN201720228385U CN206524325U CN 206524325 U CN206524325 U CN 206524325U CN 201720228385 U CN201720228385 U CN 201720228385U CN 206524325 U CN206524325 U CN 206524325U
- Authority
- CN
- China
- Prior art keywords
- heat conducting
- substrate
- groove
- radiating fin
- embedded
- 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.)
- Active
Links
Abstract
The utility model discloses a kind of heat radiation elements for radar battlebus, including radiating fin group, 5 heat conducting pipes and substrate, the radiating fin group is fastened and connected successively by some radiating fins arranged in parallel, the substrate further comprises basic courses department and extension, the radiating fin group upper surface is provided with the slot to make way being embedded in for heat conducting pipe and substrate extension, the upper surface of base plate is provided with the first groove being embedded in for heat conducting pipe, second groove and the 3rd groove, the heat absorbing end of 2 heat conducting pipes in 5 heat conducting pipes is embedded in the first groove of substrate, the heat absorbing end of other 2 heat conducting pipes in 5 heat conducting pipes is embedded in the second groove of substrate, 1 heat conducting pipe of residue in 5 heat conducting pipes is embedded in the 3rd groove of substrate, basic courses department and extension of this 3rd groove through substrate, the extension of substrate is embedded in the slot to make way of radiating fin group, the radiating fin group upper surface and bottom surface are pasted with a polyester film respectively.The utility model Stability Analysis of Structures, it is easily assembled and can effectively prevents hot air reflux, with good radiating efficiency.
Description
Technical field
The utility model is related to a kind of radiating subassembly, more particularly to a kind of heat radiation elements for radar battlebus, belongs to
Heat radiation part field.
Background technology
With the development of electronic industry technology, the transistor density of all kinds of chips increasingly increases, although the speed of data processing
Degree is more and more faster, but the power of consumption and the heat of generation also increasingly increase.Operated in order to which chip can be stablized, high efficiency
Radiator turn into demand inevitable at present.In order to maintain efficient heat sinking function, volume and the weight of radiator also must not
It is more big not heavier therewith, but in the design of military equipment, limited space is always the greatest problem in design.Existing skill
In art, most universal and most efficient method drives air flow using fan, the fin of itself and thermal-arrest is carried out heat exchange,
The purpose of cooling is reached to take away the heat of fin.However, military radiator is because the particularity of its working environment is, it is necessary to enter
The improvement of one step is to adapt to the use environment that its is special.
The content of the invention
The utility model purpose is to provide a kind of heat radiation elements for radar battlebus, and this is used for the radiating of radar battlebus
Component structure is stable, is easily assembled and can effectively prevent hot air reflux, with good radiating efficiency.
To reach above-mentioned purpose, the technical solution adopted in the utility model is：A kind of radiating member device for radar battlebus
Part, including radiating fin group, 5 heat conducting pipes and substrate, the radiating fin group by some radiating fins arranged in parallel successively
It is fastened and connected, the substrate further comprises basic courses department and extension；
The radiating fin group upper surface is provided with the slot to make way being embedded in for heat conducting pipe and substrate extension, radiating fin
2 through holes passed through for heat conducting pipe are provided with so that radiating fin group has 2 passages penetrated for heat conducting pipe, the base
Plate upper surface is provided with 2 in the first groove, the second groove and the 3rd groove being embedded in for heat conducting pipe, 5 heat conducting pipes
The heat absorbing end of heat conducting pipe is embedded in the first groove of substrate, and the radiating end of this 2 heat conducting pipes passes through the passage of radiating fin group, described
The heat absorbing end of other 2 heat conducting pipes in 5 heat conducting pipes is embedded in the second groove of substrate, the radiating end insertion of this 2 heat conducting pipes
1 heat conducting pipe of residue in the slot to make way of radiating fin group, 5 heat conducting pipes is embedded in the 3rd groove of substrate, and this is the 3rd recessed
Basic courses department and extension of the groove through substrate, the extension of substrate are embedded in the slot to make way of radiating fin group；
The radiating fin group upper surface and bottom surface are pasted with a polyester film respectively.
Further improved scheme is as follows in above-mentioned technical proposal：
1. in such scheme, the cross sectional shape of the heat conducting pipe is flat.
2. in such scheme, mutually it is fastened and connected between adjacent heat radiation fin in the radiating fin group.
Because above-mentioned technical proposal is used, the utility model has following advantages and effect compared with prior art：
The utility model is used for the heat radiation elements of radar battlebus, and its substrate further comprises basic courses department and extension, the
Basic courses department and extension of three grooves through substrate, the extension of substrate are embedded in the slot to make way of radiating fin group, substrate extension
Setting, both improved the overall structural strength of radiator, the stability of structure improved again and is easily assembled；Secondly, it dissipates
Hot fins group upper surface and bottom surface are pasted with a polyester film respectively, and the setting of polyester film can both ensure radiation processes
In wind only in radiating fin group internal flow, improve radiating efficiency, the hot air reflux of internal system can be prevented again, it is ensured that dissipate
Thermal effect.
Brief description of the drawings
Accompanying drawing 1 is that the utility model is used for the heat radiation elements structural representation of radar battlebus.
In the figures above：1st, radiating fin group；2nd, heat conducting pipe；201st, heat absorbing end；202nd, radiating end；3rd, substrate；301st, base
Plinth portion；302nd, extension；4th, radiating fin；5th, slot to make way；6th, passage；71st, the first groove；72nd, the second groove；73rd, the 3rd is recessed
Groove；8th, polyester film.
Embodiment
The utility model is further described with reference to embodiment：
Embodiment 1：A kind of heat radiation elements for radar battlebus, including radiating fin group 1,5 heat conducting pipes 2 and substrate
3, the radiating fin group 1 is fastened and connected successively by some radiating fins 4 arranged in parallel, and the substrate 3 further comprises base
Plinth portion 301 and extension 302；
The upper surface of radiating fin group 1 is provided with the slot to make way 5 being embedded in for heat conducting pipe 2 and the extension 302 of substrate 3, dissipates
2 through holes passed through for heat conducting pipe 2 are provided with hot fin 4 so that there are radiating fin group 12 to be penetrated for heat conducting pipe 2
Passage 6, the upper surface of substrate 3 be provided with for heat conducting pipe 2 be embedded in the first groove 71, the second groove 72 and the 3rd groove
73, the heat absorbing end 201 of 2 heat conducting pipes 2 in 5 heat conducting pipes 2 is embedded in the first groove 71 of substrate 3, this 2 heat conducting pipes 2
Radiating end 202 pass through the passage 6 of radiating fin group 1, the heat absorbing end 201 of other 2 heat conducting pipes 2 in 5 heat conducting pipes 2
Second groove 72 of embedded substrate 3, the slot to make way 5 of the insertion radiating fin of radiating end 202 group 1 of this 2 heat conducting pipes 2, described 5
1 heat conducting pipe 2 of residue in heat conducting pipe 2 is embedded in the 3rd groove 73 of substrate 3, and this 3rd groove 73 runs through the basic courses department of substrate 3
301 and extension 302, the slot to make way 5 of the insertion radiating fin of extension 302 group 1 of substrate 3；
The upper surface of radiating fin group 1 and bottom surface are pasted with a polyester film 8 respectively.
The cross sectional shape of above-mentioned heat conducting pipe 2 is flat.
Embodiment 2：A kind of heat radiation elements for radar battlebus, including radiating fin group 1,5 heat conducting pipes 2 and substrate
3, the radiating fin group 1 is fastened and connected successively by some radiating fins 4 arranged in parallel, and the substrate 3 further comprises base
Plinth portion 301 and extension 302；
The upper surface of radiating fin group 1 is provided with the slot to make way 5 being embedded in for heat conducting pipe 2 and the extension 302 of substrate 3, dissipates
2 through holes passed through for heat conducting pipe 2 are provided with hot fin 4 so that there are radiating fin group 12 to be penetrated for heat conducting pipe 2
Passage 6, the upper surface of substrate 3 be provided with for heat conducting pipe 2 be embedded in the first groove 71, the second groove 72 and the 3rd groove
73, the heat absorbing end 201 of 2 heat conducting pipes 2 in 5 heat conducting pipes 2 is embedded in the first groove 71 of substrate 3, this 2 heat conducting pipes 2
Radiating end 202 pass through the passage 6 of radiating fin group 1, the heat absorbing end 201 of other 2 heat conducting pipes 2 in 5 heat conducting pipes 2
Second groove 72 of embedded substrate 3, the slot to make way 5 of the insertion radiating fin of radiating end 202 group 1 of this 2 heat conducting pipes 2, described 5
1 heat conducting pipe 2 of residue in heat conducting pipe 2 is embedded in the 3rd groove 73 of substrate 3, and this 3rd groove 73 runs through the basic courses department of substrate 3
301 and extension 302, the slot to make way 5 of the insertion radiating fin of extension 302 group 1 of substrate 3；
The upper surface of radiating fin group 1 and bottom surface are pasted with a polyester film 8 respectively.
Mutually it is fastened and connected between adjacent heat radiation fin 4 in above-mentioned radiating fin group 1.
During using above-mentioned heat radiation elements for radar battlebus, by the setting of substrate extension, radiating had both been improved
The overall structural strength of device, improves the stability of structure and is easily assembled again；Secondly, the setting of polyester film can both be protected
The wind in radiation processes is demonstrate,proved only in radiating fin group internal flow, radiating efficiency is improved, the hot blast of internal system can be prevented again
Backflow, it is ensured that radiating effect.
Above-described embodiment is only to illustrate technical concepts and features of the present utility model, and its object is to allow be familiar with technique
Personage can understand content of the present utility model and implement according to this, protection domain of the present utility model can not be limited with this.
All equivalent change or modifications made according to the utility model Spirit Essence, should all cover protection domain of the present utility model it
It is interior.
Claims (3)
1. a kind of heat radiation elements for radar battlebus, it is characterised in that：Including radiating fin group（1）, 5 pieces heat conducting pipes（2）
And substrate（3）, the radiating fin group（1）By some radiating fins arranged in parallel（4）It is fastened and connected successively, the substrate
（3）Further comprise basic courses department（301）And extension（302）；
The radiating fin group（1）Upper surface, which is provided with, supplies heat conducting pipe（2）And substrate（3）Extension（302）Embedded slot to make way
（5）, radiating fin（4）On be provided with 2 and supply heat conducting pipe（2）The through hole passed through is so that radiating fin group（1）With 2 confessions
Heat conducting pipe（2）The passage penetrated（6）, the substrate（3）Upper surface, which is provided with, supplies heat conducting pipe（2）The first embedded groove（71）、
Second groove（72）With the 3rd groove（73）, 5 heat conducting pipes（2）In 2 heat conducting pipes（2）Heat absorbing end（201）It is embedded
Substrate（3）The first groove（71）, this 2 heat conducting pipes（2）Radiating end（202）Through radiating fin group（1）Passage（6）,
5 heat conducting pipes（2）In other 2 heat conducting pipes（2）Heat absorbing end（201）Embedded substrate（3）The second groove（72）, this
2 heat conducting pipes（2）Radiating end（202）Embedded radiating fin group（1）Slot to make way（5）, 5 heat conducting pipes（2）In it is surplus
Remaining 1 heat conducting pipe（2）Embedded substrate（3）The 3rd groove（73）, this 3rd groove（73）Through substrate（3）Basic courses department
（301）And extension（302）, substrate（3）Extension（302）Embedded radiating fin group（1）Slot to make way（5）；
The radiating fin group（1）Upper surface and bottom surface are pasted with a polyester film respectively（8）.
2. it is used for the heat radiation elements of radar battlebus according to claim 1, it is characterised in that：The heat conducting pipe（2）Cut
Face is shaped as flat.
3. it is used for the heat radiation elements of radar battlebus according to claim 1, it is characterised in that：The radiating fin group（1）
Middle adjacent heat radiation fin（4）Between be mutually fastened and connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720228385.6U CN206524325U (en) | 2017-03-09 | 2017-03-09 | Heat radiation elements for radar battlebus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720228385.6U CN206524325U (en) | 2017-03-09 | 2017-03-09 | Heat radiation elements for radar battlebus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206524325U true CN206524325U (en) | 2017-09-26 |
Family
ID=59902905
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720228385.6U Active CN206524325U (en) | 2017-03-09 | 2017-03-09 | Heat radiation elements for radar battlebus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206524325U (en) |
-
2017
- 2017-03-09 CN CN201720228385.6U patent/CN206524325U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN108153401A (en) | A kind of computer server radiator | |
| CN201726633U (en) | Hollow laminar type cooling plate unit structure | |
| CN206524325U (en) | Heat radiation elements for radar battlebus | |
| CN205452264U (en) | Heat radiator of chip | |
| CN206525079U (en) | Heat radiation module with water-proof fume-proof mist function | |
| CN201854534U (en) | Ceramic radiation heat dissipating structure | |
| CN204598547U (en) | A kind of liquid cooling plate for electric motor car | |
| CN206430294U (en) | A kind of computer server heat dissipation system for computer room | |
| CN211252247U (en) | Heat dissipation layout structure and printed circuit board | |
| CN204923552U (en) | A semiconductor refrigerator for circulative cooling system | |
| CN206788767U (en) | High-efficiency radiator for all-in-one core component | |
| CN204390151U (en) | A kind of air-cooled heat-pipe radiator | |
| CN206524324U (en) | Military light-duty fast heat radiator | |
| CN206790861U (en) | Synthesis heat radiation module with auxiliary heat dissipation function | |
| US20120227937A1 (en) | Heat dissipation structure for photovoltaic inverter | |
| CN206788765U (en) | Radiator built in all-in-one | |
| CN210129180U (en) | Passive radiating fin for data center | |
| CN208079651U (en) | A kind of dust-protection type communication cartridge with double cooling structure | |
| CN206472412U (en) | A kind of automatically controlled case assembly | |
| CN206531339U (en) | A kind of refrigerator | |
| CN206178631U (en) | High -efficient type CPU radiator | |
| CN219628182U (en) | Phase change material-graphite air-cooled radiator for wind power system | |
| CN108681384A (en) | Military radiator with auxiliary heat dissipation function | |
| CN204482208U (en) | Aluminium alloy heat radiator | |
| CN214676264U (en) | Heat radiator |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |