CN204718445U - The multiple aluminium profiles radiator of a kind of plane cylinder wing - Google Patents
The multiple aluminium profiles radiator of a kind of plane cylinder wing Download PDFInfo
- Publication number
- CN204718445U CN204718445U CN201520414617.8U CN201520414617U CN204718445U CN 204718445 U CN204718445 U CN 204718445U CN 201520414617 U CN201520414617 U CN 201520414617U CN 204718445 U CN204718445 U CN 204718445U
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- heat
- conduction tube
- heat conduction
- dissipation aluminum
- sectional material
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Abstract
The utility model relates to the multiple aluminium profiles radiator of a kind of plane cylinder wing, the interpolation head for installing compound heat conduction tube are equipped with at the upper/lower terminal of heat-dissipation aluminum sectional material, in heat-dissipation aluminum sectional material circular hole part sidewall on be provided with the protruding gap bar be consistent with the extension direction of heat-dissipation aluminum sectional material, be provided with melting gap between the end face of one end of compound heat conduction tube and the bottom of interpolation head.The utility model main innovate point is the improvement of partial structurtes and the mode of connection, by protruding gap bar solve metal material and composite heat-conducting tubing due to reason of expanding with heat and contract with cold often occur de-, sliding, rising causes product quality degradation problem, this programme takes upper and lower head and compound heat conduction tube to adopt interior spigot-and-socket double heat staking connection, the another wall thickness weak location of compound heat conduction tube of giving at least has thickeied the intensity that 2mm ~ 3mm then ensure that this place completely, improves security reliability.
Description
Technical field
The utility model relates to the multiple aluminium profiles radiator of a kind of plane cylinder wing.
Background technology
Current domestic heating radiator material classification is made up of following substantially: 1, the metal material such as various iron, steel, copper aluminium make 2, metal material combine with pure plastic material make (as PE-RT aluminium plastic radiator) 3, radiator that a kind of mineral-base composite material is made or made with corrupt split, due to China's many regional water quality inclement condition, cause metal radiator short seriously corroded in service life, thus result in national resources and waste greatly and produce contaminated environment.Also occurred that each metalloid was combined the radiator made with nonmetallic phase in recent years, mainly solve the interior Anticorrosion of radiator, achieve very large success, but because some problems have in use appearred in technological reason, cause security and radiating efficiency to decline, have impact on Total Product quality.Therefore the technology improving this series products is improved just necessary.
Utility model content
The technical problems to be solved in the utility model is: overcome the problems referred to above, provides a kind of plane cylinder wing multiple aluminium profiles radiator, by heat-dissipation aluminum sectional material together with compound heat conduction tube effective integration, can improve the effect of structural strength and heat radiation.
The utility model solves the technical scheme that its technical problem adopts: the multiple aluminium profiles radiator of a kind of plane cylinder wing, comprise heat-dissipation aluminum sectional material, upper at described heat-dissipation aluminum sectional material, lower two ends are equipped with the interpolation head for installing compound heat conduction tube, in described heat-dissipation aluminum sectional material circular hole part sidewall on be provided with the protruding gap bar be consistent with the extension direction of heat-dissipation aluminum sectional material, the cross section of described protruding gap bar is semicircular arc outwardly convex shape, described interpolation head are inserted in the port of one end of compound heat conduction tube, and be provided with hot melt layer between, and be provided with melting gap between the bottom of the end face of one end of described compound heat conduction tube and interpolation head.
Further, as a kind of concrete embodiment, the radius of the cross section of the bar of protruding gap described in the utility model is 1 ~ 2.5mm.
Further, as a kind of concrete embodiment, the head of interpolation described in the utility model are at least inserted in 20mm in compound heat conduction tube.
Further, in order to strengthen partial structurtes intensity, the length in melting gap described in the utility model is not less than 2mm.
Further, as a kind of concrete embodiment, each heat-dissipation aluminum sectional material of the utility model all has two left and right symmetrically arranged protruding gap bars.
The beneficial effects of the utility model are: in the utility model, heat-dissipation aluminum sectional material is made into connection box support and sink body by the metal aluminum alloy section bar of traditional excellent radiation performance, and internal water channel is made up of high-heat-conductive composite material, main innovate point is the improvement of partial structurtes and the mode of connection, by protruding gap bar solve metal material and composite heat-conducting tubing due to reason of expanding with heat and contract with cold often occur de-, sliding, rise and cause product quality degradation problem, and compound heat conduction tube ordinary circumstance lower wall thickness thinner (2mm-3mm), fitted by aluminium section bar interference in outside, but there is no aluminium section bar protection with sweat soldering place of upper and lower head, therefore intensity is not high, because pressure height in water channel very easily occurs that fracture cracking causes major safety risks of leaking, therefore this programme is taked, lower head and compound heat conduction tube adopt interior spigot-and-socket double heat staking connection, the another wall thickness weak location of compound heat conduction tube of giving at least has thickeied the intensity that 2mm ~ 3mm then ensure that this place completely, improve security reliability.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the utility model is further illustrated.
Fig. 1 is the cross-sectional structure schematic diagram of heat-dissipation aluminum sectional material in the utility model;
Fig. 2 is the structural representation at interpolation head place in the utility model;
In figure: 1. heat-dissipation aluminum sectional material, 2. compound heat conduction tube, 3. interpolation head, 4. protruding gap bar, 5. hot melt layer.
Detailed description of the invention
By reference to the accompanying drawings the utility model is described in further detail now.These accompanying drawings are the schematic diagram of simplification, only basic structure of the present utility model are described in a schematic way, and therefore it only shows the formation relevant with the utility model.
The preferred embodiment of the multiple aluminium profiles radiator of a kind of plane cylinder wing of the utility model as depicted in figs. 1 and 2, comprise heat-dissipation aluminum sectional material 1, upper at heat-dissipation aluminum sectional material 1, lower two ends are equipped with the interpolation head 3 for installing compound heat conduction tube 2, in heat-dissipation aluminum sectional material 1 circular hole part sidewall on be provided with the protruding gap bar 4 be consistent with the extension direction of heat-dissipation aluminum sectional material 1, the cross section of described protruding gap bar 4 is semicircular arc outwardly convex shape, the radius of the cross section of described protruding gap bar 4 is 1 ~ 2.5mm, each heat-dissipation aluminum sectional material 1 all has two left sides, right symmetrically arranged protruding gap bar 4, protruding gap bar 4 has anti-expansive force, contraction elasticity is had in certain pressure limit, when heat conduction composite pipe is moved in aluminium section bar hole by interference pressure, inherently define one to coordinate more closely, because compound heat conduction tube 2 has certain elastic force that rises, one can be formed in the place of protruding gap bar 4 and fill angle, an irregular micro-oval angle is become by 360 DEG C of wholecircle angles, actually define the version that one is similar to little deck, protruding gap bar 4 can be made to coordinate tightr with heat-dissipation aluminum sectional material 1, be not easy to loosen by temperature reason,
Described interpolation head 3 are inserted in the port of one end of compound heat conduction tube 2, and be provided with hot melt layer 5 between, and be provided with melting gap between the bottom of the end face of one end of compound heat conduction tube 2 and interpolation head 3, described interpolation head 3 are at least inserted in 20mm in compound heat conduction tube 2, the length in described melting gap is not less than 2mm, concrete implementing process adopts special hot melt spigot-and-socket butt welding machine equipment, hot melt die head design temperature reaches 210 DEG C ~ 270 DEG C, the internal diameter of the male of interpolation head 3 and compound heat conduction tube 2 is melted 0.2mm ~ 0.3mm by automatic average rate, die head is withdrawn, the male of interpolation head 3 and compound heat conduction tube 2 are inserted presetting position and are formed one by bonding machine equipment automatically.
With above-mentioned according to desirable embodiment of the present utility model for enlightenment, by above-mentioned description, relevant staff in the scope not departing from this utility model technological thought, can carry out various change and amendment completely.The technical scope of this utility model is not limited to the content on description, must determine its technical scope according to right.
Claims (5)
1. the multiple aluminium profiles radiator of the plane cylinder wing, comprise heat-dissipation aluminum sectional material (1), upper at described heat-dissipation aluminum sectional material (1), lower two ends are equipped with the interpolation head (3) for installing compound heat conduction tube (2), it is characterized in that: on the sidewall of the middle circular hole part of described heat-dissipation aluminum sectional material (1), be provided with protruding gap bar (4) be consistent with the extension direction of heat-dissipation aluminum sectional material (1), the cross section of described protruding gap bar (4) is semicircular arc outwardly convex shape, described interpolation head (3) are inserted in the port of one end of compound heat conduction tube (2), and be provided with hot melt layer (5) between, and be provided with melting gap between the bottom of the end face of one end of described compound heat conduction tube (2) and interpolation head (3).
2. the multiple aluminium profiles radiator of a kind of plane cylinder wing as claimed in claim 1, is characterized in that: the radius of the cross section of described protruding gap bar (4) is 1 ~ 2.5mm.
3. the multiple aluminium profiles radiator of a kind of plane cylinder wing as claimed in claim 1, is characterized in that: described interpolation head (3) are at least inserted in compound heat conduction tube (2) interior 20mm.
4. the multiple aluminium profiles radiator of a kind of plane cylinder wing as claimed in claim 1, is characterized in that: the length in described melting gap is not less than 2mm.
5. the multiple aluminium profiles radiator of a kind of plane cylinder wing as claimed in claim 1, is characterized in that: each heat-dissipation aluminum sectional material (1) all has two left and right symmetrically arranged protruding gaps bar (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520414617.8U CN204718445U (en) | 2015-06-17 | 2015-06-17 | The multiple aluminium profiles radiator of a kind of plane cylinder wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520414617.8U CN204718445U (en) | 2015-06-17 | 2015-06-17 | The multiple aluminium profiles radiator of a kind of plane cylinder wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204718445U true CN204718445U (en) | 2015-10-21 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520414617.8U Expired - Fee Related CN204718445U (en) | 2015-06-17 | 2015-06-17 | The multiple aluminium profiles radiator of a kind of plane cylinder wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204718445U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109028683A (en) * | 2018-08-30 | 2018-12-18 | 广州金抡电器有限公司 | A kind of aluminum steel compound heat conduction tube |
| CN110715563A (en) * | 2019-10-29 | 2020-01-21 | 广东吉荣核电设备暖通技术有限公司 | Finned heat exchanger with higher heat exchange efficiency |
-
2015
- 2015-06-17 CN CN201520414617.8U patent/CN204718445U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109028683A (en) * | 2018-08-30 | 2018-12-18 | 广州金抡电器有限公司 | A kind of aluminum steel compound heat conduction tube |
| CN110715563A (en) * | 2019-10-29 | 2020-01-21 | 广东吉荣核电设备暖通技术有限公司 | Finned heat exchanger with higher heat exchange efficiency |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| DD01 | Delivery of document by public notice | ||
| DD01 | Delivery of document by public notice |
Addressee: Ni Jinlong Document name: payment instructions |
|
| DD01 | Delivery of document by public notice | ||
| DD01 | Delivery of document by public notice |
Addressee: Ni Jinlong Document name: Notice of termination of patent |
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151021 Termination date: 20200617 |