CN203968569U - Body heat abstractor - Google Patents
Body heat abstractor Download PDFInfo
- Publication number
- CN203968569U CN203968569U CN201420427300.3U CN201420427300U CN203968569U CN 203968569 U CN203968569 U CN 203968569U CN 201420427300 U CN201420427300 U CN 201420427300U CN 203968569 U CN203968569 U CN 203968569U
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- China
- Prior art keywords
- opening
- heat abstractor
- accommodation space
- section
- lamellar body
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Abstract
A kind of body heat abstractor, comprise a body fuselage, at least one lamellar body and at least one drivening piece, described body fuselage has at least one the first opening and at least one the second opening and an accommodation space, and this lamellar body is arranged in described accommodation space and see through described drivening piece, drive displacement in described accommodation space, so that arround its body fuselage inside and housing exterior can produce cross-ventilation effect, and then reach and in the body of limited space, can effectively improve cross-ventilation the effect person of the improving heat radiation efficiency significantly.
Description
[technical field]
A heat abstractor, espespecially a kind ofly can effectively improve the interior cross-ventilation of body, and reaches in the body of limited space the significantly body heat abstractor of improving heat radiation efficiency.
[background technology]
In recent years with the development of showing electronic industry, the performance of electronic component promotes rapidly, calculation process speed is more and more faster, and the arithmetic speed of its internal wafer group constantly promotes, number of wafers also constantly increases, and the also corresponding increase of heat that aforementioned wafer distributes when work, if these thermals source are not distributed immediately, the performance of electronic component will greatly be affected, make the calculation process Speed Reduction of electronic component, and constantly accumulating with work heat, also may burn electronic component, therefore heat radiation has become one of important topic of electronic component, and utilize radiator fan, as heat abstractor, be to be common method.
Electronic equipment development trend is gradually toward microminiaturized future development now, as notebook computer, panel computer, mobile phone etc., and in the situation of microminiaturization development, the space of its electronic equipment body inside is significantly reduction also, therefore in its space, reduce and need be provided with in the situation of many electronic components and circuit board, in this electronic equipment body, just without vacant space, can supply radiator fan setting, again or in the situation of the thickness attenuation of its electronic equipment, what the flabellum of radiator fan and bearing must have highly also cannot be arranged in electronic equipment, therefore, in the situation that cannot arrange at radiator fan in its electronic equipment body, its meeting as easy as rolling off a log normal operation that affects electronic equipment of thermal source that electronic component produced, the also relative increase of the maintenance cost of its relative electronic equipment.
Therefore, how to solve the above-mentioned problem of commonly using and disappearance, the utility model people who is this case desires most ardently to the relevant manufacturer that is engaged in the industry the direction place person who studies improvement.
[utility model content]
The object of the utility model is to provide a kind of body heat abstractor that can effectively improve cross-ventilation.
Another object of the utility model is providing in a kind of body at limited space the significantly body heat abstractor of improving heat radiation efficiency.
For reaching above-mentioned purpose, the utility model provides a kind of body heat abstractor, comprises: a body fuselage, and this body fuselage has at least one the first opening and at least one the second opening and an accommodation space, and this accommodation space is communicated with described the first opening and the second opening; At least one lamellar body, is arranged in described accommodation space, and this lamellar body has one first section and one second section, and this first section and the second section are relatively arranged on respectively described the first opening and the second opening; At least one drivening piece, be arranged on described body fuselage and drive described brake component in described accommodation space, to produce displacement and make the first opening and the second opening between cross-ventilation.
Described lamellar body is in the intersegmental centre portion that has more of the first section and Second Region.
The first end upper and lower displacement that described drivening piece drives described lamellar body is in accommodation space and compress the gas in its accommodation space, and drives its centre portion and the second section upper and lower displacement by its gas.
Described body fuselage has a first side and a second side, and described the first opening and the second opening are formed at respectively described first side and second side.
In described body fuselage, be provided with at least one keeper, this keeper is extended toward top from the bottom of body fuselage.
Described lamellar body relative positioning part position has a hole and wears for described keeper, and this lamellar body keeper described in upper and lower displacement simultaneously while producing displacement in described accommodation space.
Described drivening piece is a magnetic part and makes its lamellar body produce displacement in described accommodation space to lamellar body generation magnetic field.
Described drivening piece is a cam.
Have more a driver element, drivening piece rotates and makes its lamellar body produce displacement described in this drive unit drives.
Described lamellar body is a bendable lamellar body.
Drivening piece is arranged on body fuselage and sees through drivening piece and drives displacement in accommodation space, and when displacement produces, makes the cross-ventilation between the first opening and the second opening, and then reaches in the body of limited space the significantly effect of improving heat radiation efficiency.
[accompanying drawing explanation]
Fig. 1 is the decomposing schematic representation of the utility model the first preferred embodiment;
Fig. 2 is the three-dimensional combination figure of the utility model the first preferred embodiment;
Fig. 3 a is the enforcement schematic diagram one of the utility model the first preferred embodiment;
Fig. 3 b is the enforcement schematic diagram two of the utility model the first preferred embodiment;
Fig. 3 c is the enforcement schematic diagram three of the utility model the first preferred embodiment;
Fig. 4 a is the enforcement schematic diagram one of the utility model the second preferred embodiment;
Fig. 4 b is the enforcement schematic diagram two of the utility model the second preferred embodiment;
Fig. 4 c is the enforcement schematic diagram three of the utility model the second preferred embodiment;
Fig. 5 is the enforcement schematic diagram of the utility model the 3rd preferred embodiment;
Fig. 6 is the enforcement schematic diagram of the utility model the 4th preferred embodiment.
The member name that in figure, each Reference numeral is corresponding is called:
Body heat abstractor 1
Body fuselage 2
First side 21
The first opening 211
Second side 22
The second opening 221
Accommodation space 23
Keeper 24
Bottom 25
Top 26
Lamellar body 3
Hole 31
The first section 32
The second section 33
Centre portion 34
Drivening piece 4
[embodiment]
Characteristic in the above-mentioned purpose of the utility model and structure thereof and function, will be explained according to appended graphic preferred embodiment.
As Fig. 1, shown in 2, decomposing schematic representation and three-dimensional combination figure for the first preferred embodiment of the utility model body heat abstractor, as shown in the figure, the body heat abstractor 1 of the utility model comprises a body fuselage 2 and at least one lamellar body 3 and at least one drivening piece 4, wherein this body fuselage 2 has a 21Ji Yi second side, first side 22, on this first side 21, there is at least one the first opening 211, and on this second side 22, there is at least one the second opening 221, and to take one first opening 211 be embodiment in its first side 21 in the present embodiment, and its first opening 211 is equivalent to the air inlet of this body heat abstractor 1, and to take one second opening 221 be embodiment in its second side 22, and its second opening 221 is equivalent to the air outlet of this body heat abstractor 1, but be not limited to this, its first opening 211 also can be defined as air outlet and the second opening 221 also can be defined as air inlet, and in the first opening 211 and 221 of the second openings, there is an accommodation space 23 in this body fuselage 2, this accommodation space 23 is communicated with described the first opening 211 and the second opening 221, in another this body fuselage 2, be provided with at least one keeper 24,26 extensions from one of body fuselage 2 bottom 25 toward one of body fuselage 2 top of this keeper 24, these keepers 24 are arranged at bottom 25 26 extensions toward top of body fuselage 2 in the present embodiment with cylinder.
And this lamellar body 3 is arranged in the accommodation space 23 of described body fuselage 2, this lamellar body 3 has at least one hole 31, the position of these hole 31 settings is equivalent to the position of this keeper 24, and its lamellar body 3 in the present embodiment, to take a bendable lamellar body 3 be execution mode, another these lamellar body 3 two ends have respectively one first section 32 and one second section 33, this first section 32 and the second section 33 are oppositely arranged respectively and are adjacent to described the first opening 211 and the second opening 221 positions, and this first section 32 and 33 of the second sections have more a centre portion 34, in the present embodiment, the setting position of its hole 31 is in its centre portion 34 positions, and its keeper 24 wears described hole 31 and extends toward body fuselage 2 tops 26.
And this drivening piece 4 is arranged on described body fuselage 2, in the present embodiment, its drivening piece 4 is 26 positions, top that are arranged at this body fuselage 2, but is not limited to this, and its drivening piece 4 also can be arranged at 25 positions, bottom of this body fuselage 2.
As Fig. 3 a, 3b, shown in 3c, enforcement schematic diagram one for the utility model the first embodiment, two, three, as shown in the figure, in the present embodiment, wherein said lamellar body 3 is the bendable lamellar body 3 of a metal material, and its lamellar body 3 is positioned in accommodation space 23 by this keeper 24, and its drivening piece 4 is magnetic part, and this drivening piece 4 is arranged at this first section 32 positions, after these drivening piece 4 conductions, can produce an effect of inhaling magnetic to the first section 32 of its lamellar body 3, and make its first section 32 toward top 26 displacements of body fuselage 2, then its drivening piece 4 stops after conduction, 25 displacements push the interior air of its accommodation space 23 and produce air-flow toward bottom of this first section 32, its centre portion 34 is moved and is pushed in its air-flow change from its first section 32 toward centre portion 34, centre portion 34 depends on 26 displacements and simultaneously drive 26 displacements toward top of its second section 33 toward top of its keeper 24, until its air-flow is sent toward the second opening 221.
When then its drivening piece 4 conducts electricity again, its first section 32 is top 26 displacements of past body fuselage 2 again, and when its first section 32 is moved to top 26 completely, the variation that its body fuselage 2 outer air are stressed simultaneously and being entered in its accommodation space 23 by the first opening 211, and then stop its drivening piece 4 conductions, 25 displacements push the interior air of its accommodation space 23 and produce air-flow toward bottom of this first section 32, its air-flow is just moved and is pushed its centre portion 34 from its first section 32 toward centre portion 34, centre portion 34 depends on 26 displacements and simultaneously drive 26 displacements toward top of its second section 33 toward top of its keeper 24, until its air-flow is sent toward the second opening 221, make by this inside and outside cross-ventilation effect that produces of its body fuselage 2 also can dispel the heat for the interior pyrotoxin of its body fuselage 2, and then reach and in the body of limited space, can effectively improve cross-ventilation the effect person of the improving heat radiation efficiency significantly.
As Fig. 4 a, 4b, shown in 4c, enforcement schematic diagram one for 1 second preferred embodiment of the utility model body heat abstractor, two, three, as shown in the figure, the present embodiment part-structure is identical with aforementioned the first embodiment, therefore will repeat no more at this, only the present embodiment and aforementioned the first embodiment's does not exist together for described drivening piece 4 is for producing the application mode of swing, described drivening piece 4 is cam, this drivening piece 4 connects a driver element and is driven so that the conversion of an angle of 90 degrees degree is lower by this driver element, and this drivening piece 4 attaches described lamellar body 3, 3 of the lamellar bodies that a side is attached when this drivening piece 4 rotates produce upper and lower displacement according to the eccentric situation of its drivening piece 4, the top of its drivening piece 4 peaks at the first section 32 of its lamellar body 3 at the top 26 of body fuselage 2, and if the top of its drivening piece 4 is when swung by driver element, its lamellar body 3 moments are toward bottom 25 displacements of body fuselage 2, 25 displacements push the interior air of its accommodation space 23 and produce air-flow toward bottom of this first section 32, its air-flow is moved and is pushed its centre portion 34 from this first section 32 toward centre portion 34, centre portion 34 depends on 26 displacements and simultaneously drive 26 displacements toward top of its second section 33 toward top of its keeper 24, until its air-flow is sent toward the second opening 221.
Then the top of its drivening piece 4 peaks at the first section 32 of its lamellar body 3 at the top 26 of body fuselage 2, and when its first section 32 is moved to top 26 completely, the variation that its body fuselage 2 outer air are stressed simultaneously and being entered in its accommodation space 23 by the first opening 211, and then swing its drivening piece 4, 25 displacements push the interior air of its accommodation space 23 and produce air-flow toward bottom of this first section 32, its centre portion 34 is moved and is pushed in its air-flow change from its first section 32 toward centre portion 34, centre portion 34 depends on 26 displacements and simultaneously drive 26 displacements toward top of its second section 33 toward top of its keeper 24, until its air-flow is sent toward the second opening 221, make by this inside and outside cross-ventilation effect that produces of its body fuselage 2 also can dispel the heat for the interior pyrotoxin of its body fuselage 2, and then reach and in the body of limited space, can effectively improve cross-ventilation the effect person of the improving heat radiation efficiency significantly.
For another Fig. 5, shown in 6, enforcement schematic diagram for the 3rd preferred embodiment of the utility model body heat abstractor 1 and the 4th preferred embodiment, as shown in the figure, the present embodiment part-structure is identical with aforementioned the first embodiment, therefore will repeat no more at this, only not existing together of the present embodiment and aforementioned the first embodiment can be set to two or four for the interior lamellar body 3 of described body fuselage 2, and its lamellar body 3 has respectively affiliated drivening piece 4, make the lamellar body 3 of its difference via drivening piece 4 drives of difference, make by this inside and outside cross-ventilation effect that produces of its body fuselage 2 also can dispel the heat for the interior pyrotoxin of its body fuselage 2, and then reach and in the body of limited space, can effectively improve cross-ventilation the effect person of the improving heat radiation efficiency significantly.
In sum, the body heat abstractor of the utility model is when being used, for really reaching its effect and object, therefore the utility model is really the invention of a practicality excellence, for meeting the application important document of utility model patent, file an application in accordance with the law, expect that examining committee grants accurate this case early, to ensure inventor's arduous invention, if Patent Office examine committee have any check doubtful, the indication of please writing to us without sparing, settled the doing one's utmost of inventor coordinates, and true feeling moral is just.
Claims (10)
1. a body heat abstractor, is characterized in that, comprises:
One body fuselage, this body fuselage has at least one the first opening and at least one the second opening and an accommodation space, and this accommodation space is communicated with described the first opening and the second opening;
At least one lamellar body, is arranged in described accommodation space, and this lamellar body has one first section and one second section, and this first section and the second section are relatively arranged on respectively described the first opening and the second opening;
At least one drivening piece, be arranged on described body fuselage and drive described brake component in described accommodation space, to produce displacement and make the first opening and the second opening between cross-ventilation.
2. body heat abstractor according to claim 1, is characterized in that, described lamellar body is in the intersegmental centre portion that has more of the first section and Second Region.
3. body heat abstractor according to claim 1, it is characterized in that, the first end upper and lower displacement that described drivening piece drives described lamellar body is in accommodation space and compress the gas in its accommodation space, and drives its centre portion and the second section upper and lower displacement by its gas.
4. body heat abstractor according to claim 1, is characterized in that, described body fuselage has a first side and a second side, and described the first opening and the second opening are formed at respectively described first side and second side.
5. body heat abstractor according to claim 1, is characterized in that, is provided with at least one keeper in described body fuselage, and this keeper is extended toward top from the bottom of body fuselage.
6. body heat abstractor according to claim 1, is characterized in that, described lamellar body relative positioning part position has a hole and wears for described keeper, and this lamellar body keeper described in upper and lower displacement simultaneously while producing displacement in described accommodation space.
7. body heat abstractor according to claim 1, is characterized in that, described drivening piece is a magnetic part and makes its lamellar body produce displacement in described accommodation space to lamellar body generation magnetic field.
8. body heat abstractor according to claim 1, is characterized in that, described drivening piece is a cam.
9. body heat abstractor according to claim 8, is characterized in that, has more a driver element, and drivening piece rotates and makes its lamellar body produce displacement described in this drive unit drives.
10. body heat abstractor according to claim 1, is characterized in that, described lamellar body is a bendable lamellar body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420427300.3U CN203968569U (en) | 2014-07-30 | 2014-07-30 | Body heat abstractor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420427300.3U CN203968569U (en) | 2014-07-30 | 2014-07-30 | Body heat abstractor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203968569U true CN203968569U (en) | 2014-11-26 |
Family
ID=51929102
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420427300.3U Expired - Fee Related CN203968569U (en) | 2014-07-30 | 2014-07-30 | Body heat abstractor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203968569U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105324006A (en) * | 2014-07-30 | 2016-02-10 | 奇鋐科技股份有限公司 | Machine body heat dissipation device |
-
2014
- 2014-07-30 CN CN201420427300.3U patent/CN203968569U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105324006A (en) * | 2014-07-30 | 2016-02-10 | 奇鋐科技股份有限公司 | Machine body heat dissipation device |
| CN105324006B (en) * | 2014-07-30 | 2017-09-15 | 奇鋐科技股份有限公司 | Body heat abstractor |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| 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: 20141126 Termination date: 20190730 |