CN207006657U - Insertion composite member - Google Patents
Insertion composite member Download PDFInfo
- Publication number
- CN207006657U CN207006657U CN201720946723.XU CN201720946723U CN207006657U CN 207006657 U CN207006657 U CN 207006657U CN 201720946723 U CN201720946723 U CN 201720946723U CN 207006657 U CN207006657 U CN 207006657U
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- Prior art keywords
- radiating
- heat
- composite member
- shell
- mounting surface
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Abstract
A kind of insertion composite member, including radiating shell, heat loss through convection stiffener assembly, and the support component that radiates, offer heat-dissipating cavity in radiating shell, multiple air introduction holes are offered in the side wall of radiating shell；Heat loss through convection stiffener assembly includes radiating block, raised line is strengthened in multiple first radiatings and raised line is strengthened in multiple second radiatings, the end set of radiating block is on the madial wall of radiating shell, and the block that radiates is placed in inside heat-dissipating cavity, the first mounting surface and the second mounting surface are provided with radiating block, each first radiating is strengthened raised line and is respectively arranged on the first mounting surface, and each second radiating is strengthened raised line and is respectively arranged on the second mounting surface；The support component that radiates includes two radiating cylinders, multiple side position heat bulge portions, and two radiating cylinders are respectively arranged on two relative sides of radiating shell.So, the air that can make outside by each air introduction hole is entered in heat-dissipating cavity, it is possible to increase heat loss through convection effect.
Description
Technical field
Technical field of heat dissipation is the utility model is related to, more particularly to a kind of insertion composite member.
Background technology
At present, it is used to reduce caused heat during equipment operation when radiator (Radiator) is the operating of machinery equipment part
Amount, so that mechanical equipment component radiating is freezed to increase the equipment in mechanical action life-span.So direct shadow of the quality of radiator
Ring the life-span of operating mechanical equipment component.
It is common, when needing to improve the heat dispersion of equipment main heat sink part, it will usually in equipment main heat sink portion
The thermal component of one auxiliary, i.e. circumscribed thermal component are installed, to improve overall performance, however, existing be used to pacify on part
The thermal component heat dispersion of auxiliary type is poor on equipment main heat sink part.
Also, the heat loss through convection effect of the thermal component of existing auxiliary type is poor.
Utility model content
Based on this, it is necessary to provide a kind of good heat dispersion performance, and the preferable insertion composite member of heat loss through convection effect.
A kind of insertion composite member, including：
Radiating shell, heat-dissipating cavity is offered in the radiating shell, is offered in the side wall of the radiating shell multiple
Air introduction hole；
Heat loss through convection stiffener assembly, the heat loss through convection stiffener assembly are strengthened convex including radiating block, multiple first radiatings
Raised line is strengthened in bar and multiple second radiatings, the end set of the radiating block on the madial wall of the radiating shell, and
The radiating block is placed in inside the heat-dissipating cavity, and the first mounting surface and the second installation are provided with the radiating block
Face, each first radiating are strengthened raised line and are respectively arranged on first mounting surface, and raised line point is strengthened in each second radiating
It is not arranged on second mounting surface；And
Radiate support component, it is described radiating support component include two radiating cylinder, multiple side position heat bulge portions, two
The radiating cylinder is respectively arranged on two relative sides of the radiating shell, and each side position heat bulge portion interval is set
It is placed on the end of the radiating shell.
In one of the embodiments, the distance between every two neighboring described air introduction hole is equal.
In one of the embodiments, the radiating shell has hollow rectangular parallelepiped structure.
In one of the embodiments, the air introduction hole side of having cavernous structure.
In one of the embodiments, raised line is strengthened in first radiating has polygon prism structure.
In one of the embodiments, the radiating block has rectangular parallelepiped structure.
In one of the embodiments, first mounting surface be arranged in parallel with second mounting surface.
In one of the embodiments, raised line is strengthened in second radiating has polygon prism structure.
In one of the embodiments, the radiating cylinder has rectangular parallelepiped structure.
Above-mentioned insertion composite member can be dissipated by setting radiating shell, heat loss through convection stiffener assembly and radiating support component
Hotlist area, and then improve heat dispersion.And by each air introduction hole the air of outside can be made to enter in heat-dissipating cavity,
Heat loss through convection effect can be improved.
Brief description of the drawings
Fig. 1 is the structural representation of the insertion composite member of the embodiment of the utility model one.
Embodiment
For the ease of understanding the utility model, the utility model is more fully retouched below with reference to relevant drawings
State.Better embodiment of the present utility model is given in accompanying drawing.But the utility model can come in many different forms
Realize, however it is not limited to embodiments described herein.On the contrary, the purpose for providing these embodiments is to make to this practicality newly
The more thorough and comprehensive that the disclosure of type understands.
It should be noted that when element is referred to as " being fixed on " another element, it can be directly on another element
Or there may also be element placed in the middle.When an element is considered as " connection " another element, it can be directly connected to
To another element or it may be simultaneously present centering elements.Term as used herein " vertical ", " horizontal ", " left side ",
For illustrative purposes only, it is unique embodiment to be not offered as " right side " and similar statement.
Unless otherwise defined, all of technologies and scientific terms used here by the article is led with belonging to technology of the present utility model
The implication that the technical staff in domain is generally understood that is identical.It is simply in term used in the description of the present utility model herein
The purpose of description specific embodiment, it is not intended that in limitation the utility model.Term as used herein " and/or " bag
Include the arbitrary and all combination of the Listed Items of one or more correlations.
In one embodiment, a kind of insertion composite member, including：Radiating shell, heat loss through convection stiffener assembly, and radiating support
Component, heat-dissipating cavity is offered in the radiating shell, multiple air introduction holes are offered in the side wall of the radiating shell；Institute
State heat loss through convection stiffener assembly and strengthen raised line and multiple second radiating reinforcement raised lines, institute including radiating block, multiple first radiatings
The end set of radiating block is stated on the madial wall of the radiating shell, and the radiating block is placed in the heat dissipation cavity
Internal portion, the first mounting surface and the second mounting surface is provided with the radiating block, raised line difference is strengthened in each first radiating
It is arranged on first mounting surface, each second radiating is strengthened raised line and is respectively arranged on second mounting surface；It is described
The support component that radiates includes two radiating cylinders, multiple side position heat bulge portions, and two radiating cylinders are respectively arranged at institute
State on two relative sides of radiating shell, each side position heat bulge portion is arranged at intervals at the end of the radiating shell
On, so, above-mentioned insertion composite member can be dissipated by setting radiating shell, heat loss through convection stiffener assembly and radiating support component
Hotlist area, and then improve heat dispersion.And by each air introduction hole the air of outside can be made to enter in heat-dissipating cavity,
Heat loss through convection effect can be improved.
The insertion composite member is illustrated with reference to specific embodiment, to further understand the insertion composite member
Design, referring to Fig. 1, insertion composite member 10 includes：Radiating shell 100, heat loss through convection stiffener assembly 200 and radiating support group
Part 300, heat loss through convection stiffener assembly 200 are arranged on inside radiating shell 100, and radiating support component 300 is arranged at radiating shell
On 100 lateral wall, radiating shell 100, heat loss through convection stiffener assembly 200 and radiating support component 300 are collectively forming one and dissipated
Hot overall structure, for equipment main heat sink part mounted externally, to play collaboration thermolysis, outside improving
The heat dispersion of equipment main heat sink part.For example, the radiating shell 100 is pacified welding, clamping or by way of being spirally connected
On the equipment main heat sink part of outside, the effect of circumscribed is realized.
Referring to Fig. 1, offering heat-dissipating cavity 110 in radiating shell 100, offered in the side wall of the radiating shell more
Individual air introduction hole 120, so, the air that can make outside by each air introduction hole 120 are entered in heat-dissipating cavity 110,
Heat loss through convection effect can be improved, and then improves integrally-built heat dispersion.For example, extraneous air imports from the air
Hole flows into, and the heat-dissipating cavity has opening, is flowed out from the opening of the heat-dissipating cavity, to realize heat loss through convection effect.
Referring to Fig. 1, heat loss through convection stiffener assembly 200 includes radiating block 210, raised line is strengthened in multiple first radiatings and more
Raised line is strengthened in individual second radiating, and the end set of the radiating block described is dissipated on the madial wall of the radiating shell
Hot block is placed in inside the heat-dissipating cavity, and the first mounting surface and the second mounting surface, each institute are provided with the radiating block
State the first radiating reinforcement raised line to be respectively arranged on first mounting surface, each second radiating is strengthened raised line and is respectively arranged at
On second mounting surface, so, heat loss through convection stiffener assembly 200 is by setting radiating block 210, multiple first radiatings to strengthen
Raised line is strengthened in raised line and multiple second radiatings, it is possible to increase cooling surface area, and then improve heat dispersion.
Referring to Fig. 1, radiating support component 300 include two radiating cylinder 310, multiple side position heat bulge portions 320, two
The individual radiating cylinder is respectively arranged on two relative sides of the radiating shell, each side position heat bulge portion interval
It is arranged on the end of the radiating shell, so, radiating support component 300 is by setting two radiating cylinders 310, multiple sides
Position heat bulge portion 320, it is possible to increase cooling surface area, and then improve heat dispersion.
In one embodiment, the distance between every two neighboring described air introduction hole is equal；And for example, the radiating shell
With hollow rectangular parallelepiped structure；And for example, the air introduction hole side of having cavernous structure；And for example, first radiating is strengthened convex
Bar has polygon prism structure；And for example, the radiating block has rectangular parallelepiped structure；And for example, first mounting surface and described the
Two mounting surfaces be arranged in parallel；And for example, raised line is strengthened in second radiating has polygon prism structure；And for example, the radiating cylinder tool
There is rectangular parallelepiped structure, so, overall stability can not only be improved, additionally it is possible to overall heat dispersion.
Above-mentioned insertion composite member 10 is by setting radiating shell 100, heat loss through convection stiffener assembly 200 and radiating support component
300, can cooling surface area, and then improve heat dispersion.It and can enter the air of outside by each air introduction hole 120
To heat-dissipating cavity 110, it is possible to increase heat loss through convection effect.
It should be noted that the radiating shell of the insertion composite member undertakes main radiating load, i.e., it is described to dissipate
Hot housing heat dissipation capacity is maximum, i.e., the true heat gain value that described radiating shell undertakes is maximum, if outside equipment main heat sink portion
The heat increase that part passes over, then will certainly cause the radiating load of insertion composite member to increase, and the auxiliary type of prior art
Thermal component, i.e. the radiating load of insertion composite member is fixed, it is more difficult to be adjusted, in this way, can make outside equipment master
Want thermal component and insertion composite member to be in radiating running overload, so, the normal operation of the equipment of outside can be influenceed, because
This, in order to realize that the radiating load of the insertion composite member can adjust function, for example, the insertion composite member also includes inserting
Heat radiation module is connect, the grafting heat radiation module is used to directly be plugged in the radiating shell, to aid in the insertion composite member
Collaboration thermolysis is played jointly, and inserting on the radiating shell is plugged on according to the heat dissipation capacity actually increased, corresponding adjustment
The quantity of heat radiation module is connect, to realize that the radiating load of the insertion composite member can adjust function, however, the grafting dissipates
The field erected mode of mounting means generally use of thermal module, if the weight of the grafting heat radiation module is excessive, overall knot
Structure is more heavy, is unfavorable for transport and installation operation, it is thus desirable to so that the grafting heat radiation module have it is more light excellent
Point, further, the grafting heat radiation module need to be adjusted according to the radiating load of the equipment main heat sink part of outside,
I.e. when the radiating load increase of the equipment main heat sink part of outside, then correspond to described slotting on the radiating shell
Connecing heat radiation module quantity can also increase, and when the radiating load of the equipment main heat sink part of outside reduces, then correspond to installation
The grafting heat radiation module quantity on the radiating shell can also be reduced, if or even in the insertion composite member and outside
When equipment main heat sink part can meet radiating requirements, then the grafting heat radiation module need not be additionally installed, that is to say, that
The grafting heat radiation module is frequently necessary to remove and install, it is thus desirable to which so that the grafting heat radiation module has is easily installed and tears open
The advantages of unloading, and in unloading process, operating personnel need single-handedly to go to extract the grafting heat radiation module, if the grafting is radiated
The temperature on surface of the module in radiation processes is higher, then operating personnel is easily scalded, in this way, also requiring that the grafting dissipates
For thermal module in radiation processes, the temperature on the grafting heat radiation module surface is relatively low.In order to realize the insertion composite member
Radiating load can adjust function, enable to the grafting heat radiation module that there is the advantages of more light, and enable to
For the grafting heat radiation module in radiation processes, the temperature on the grafting heat radiation module surface is relatively low, preferably protects operator
Member, for example, the insertion composite member also includes grafting heat radiation module, the grafting heat radiation module is plugged in the radiating shell
On, the auxiliary heat dissipation module includes heat-insulation scald-proof shell, heat-insulation scald-proof extension tongue, radiating alloy plug pin, radiating alloy heat-sink
Support nail, the first radiating alloy mounting bar, the second radiating alloy mounting bar and radiating alloy heat-sink piece, the heat-insulation scald-proof shell
With hollow structure, the heat-insulation scald-proof shell is internally formed radiating installation cavity, and one end of the heat-insulation scald-proof shell is opened
Provided with heat dissipation ventilation mouth, for example, the heat-insulation scald-proof shell has the hollow rectangular parallelepiped structure of one end open, the heat dissipation ventilation
Mouth is connected with the radiating installation cavity, and the heat-insulation scald-proof extension tongue is arranged in the radiating installation cavity body, for example, described
The first end of heat-insulation scald-proof extension tongue is connected with the madial wall of the radiating installation cavity, and the second of the heat-insulation scald-proof extension tongue
End is concordant with the heat dissipation ventilation mouth to be set, and the radiating alloy heat-sink piece is arranged on the heat-insulation scald-proof extension tongue, described
The first end that the first end of alloy plug pin that radiates and the radiating alloy heat-sink support nail is respectively arranged at outside the heat-insulation scald-proof
On the lateral wall of shell, the first radiating alloy mounting bar wears the heat-insulation scald-proof shell, and the first radiating alloy
The first end of mounting bar is connected with the radiating alloy plug pin first end, and the second radiating alloy mounting bar wears described heat-insulated
Anti-scald shell, and the first end of the second radiating alloy mounting bar supports nail first end with the radiating alloy heat-sink and connected
Connect, the second end of the second end of the first radiating alloy mounting bar and the second radiating alloy mounting bar dissipates with described respectively
Thermalloy fin connects, and so, the heat absorbed on the radiating alloy plug pin passes through the described first radiating alloy mounting bar
Rapidly it is transferred on the radiating alloy heat-sink piece, and the radiating alloy heat-sink supports and nails on the heat of absorption and pass through institute
State the second radiating alloy mounting bar to be rapidly transferred on the radiating alloy heat-sink piece, so, it is possible so that heat is gathered in
On the radiating alloy heat-sink piece, and the enough heat dissipation ventilation mouths of the heat and can on alloy heat-sink piece that radiates scatter and disappear to outside air
In, and the radiating alloy heat-sink piece is placed in the radiating installation cavity body, it is possible to increase coat the radiating alloy heat-sink
The effect of piece, operating personnel are avoided directly to be contacted with the radiating alloy heat-sink piece, further, since the first radiating alloy peace
Dress bar and the second radiating alloy mounting bar are installed in the heat-insulation scald-proof shell, can also avoid operating personnel directly and institute
Radiating alloy heat-sink piece contact is stated, so, it is possible so that the grafting heat radiation module is in radiation processes, the grafting radiating mould
The temperature on group surface is relatively low, preferably protects operating personnel.Radiating spliced eye is offered on the surface of the radiating shell, it is described
Second end of radiating alloy plug pin is plugged in the radiating spliced eye, and the radiating alloy heat-sink supports the second end and the institute of nail
The surface fitting of radiating shell is stated, i.e., using the mounting means of plug-in type, installing/dismounting is more convenient, can realize the grafting
The radiating load of sub-assembly can adjust function.It so, it is possible so that the alloy heat-sink that radiates supports nail and the radiating alloy plug pin
The heat on the radiating shell is absorbed, to play collaboration thermolysis.So, the grafting heat radiation module passes through setting
Heat-insulation scald-proof shell and heat-insulation scald-proof extension tongue as body supports skeleton, i.e., are heat-insulation scald-proof material as supporting construction, example
Such as, the heat-insulation scald-proof material is organic polymer material, i.e. plastic material, so as to possess the advantages of light quality, is led to
Cross radiating alloy plug pin, radiating alloy heat-sink support nail, first radiating alloy mounting bar and second radiate alloy mounting bar can
Heat on radiating shell is rapidly transferred on radiating alloy heat-sink piece, heat is passed through into radiating by radiating alloy heat-sink piece
Ventilating opening scatters and disappears into outside air, and radiating effect is preferable, can play a part of collaboration radiating.For example, radiating alloy is aluminium
Alloy or copper alloy.
And for example, the grafting heat radiation module also includes heat-insulation scald-proof lid and radiating alloy elastic helical member, the radiating
The first end of alloy elastic helical member is connected with the radiating alloy heat-sink piece, the first end of the radiating alloy elastic helical member
The radiating installation inside cavity is placed in, the radiating alloy elastic helical member passes the heat dissipation ventilation mouth, the radiating
Alloy elastic helical member is used to improve area of dissipation, and to improve heat dispersion, the heat-insulation scald-proof lid rotation is arranged at described
On the edge of heat dissipation ventilation mouth, the heat-insulation scald-proof lid is used to close the heat dissipation ventilation mouth, in this way, working as the radiating alloy
When fin and the radiating alloy elastic helical member need radiating, then the heat-insulation scald-proof lid is opened, make the radiating logical
Air port is opened wide, and is in communication with the outside, and when the grafting heat radiation module need not radiate, then closes the heat-insulation scald-proof lid,
Second end of the radiating alloy elastic helical member supports with the heat-insulation scald-proof lid, at the radiating alloy elastic helical member
In contraction state, so, it is possible preferably to house the radiating alloy elastic helical member.For example, the radiating alloy elastic spiral shell
Rotating part has spring-like structures.
Each technical characteristic of embodiment described above can be combined arbitrarily, to make description succinct, not to above-mentioned reality
Apply all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited
In contradiction, the scope that this specification is recorded all is considered to be.
Embodiment described above only expresses several embodiments of the present utility model, and it describes more specific and detailed
Carefully, but the limitation to the utility model patent scope therefore can not be interpreted as.It should be pointed out that for the general of this area
For logical technical staff, without departing from the concept of the premise utility, various modifications and improvements can be made, these are all
Belong to the scope of protection of the utility model.Therefore, the protection domain of the utility model patent should be determined by the appended claims.
Claims (9)
- A kind of 1. insertion composite member, it is characterised in that including：Radiating shell, heat-dissipating cavity is offered in the radiating shell, multiple air are offered in the side wall of the radiating shell Entrance hole；Heat loss through convection stiffener assembly, the heat loss through convection stiffener assembly include radiating block, it is multiple first radiating strengthen raised line and Raised lines are strengthened in multiple second radiatings, and the end set of the radiating block is and described on the madial wall of the radiating shell Radiating block is placed in inside the heat-dissipating cavity, is provided with the first mounting surface and the second mounting surface on the radiating block, respectively First radiating is strengthened raised line and is respectively arranged on first mounting surface, and each second radiating is strengthened raised line and set respectively In on second mounting surface；AndRadiate support component, and the radiating support component includes two radiating cylinders, multiple side position heat bulge portions, described in two Radiating cylinder is respectively arranged on two relative sides of the radiating shell, and each side position heat bulge portion is arranged at intervals at On the end of the radiating shell.
- 2. insertion composite member according to claim 1, it is characterised in that between per the two neighboring air introduction hole Apart from equal.
- 3. insertion composite member according to claim 1, it is characterised in that the radiating shell has hollow cuboid knot Structure.
- 4. insertion composite member according to claim 1, it is characterised in that the air introduction hole side of having cavernous structure.
- 5. insertion composite member according to claim 1, it is characterised in that raised line is strengthened in first radiating has polygon prism Structure.
- 6. insertion composite member according to claim 1, it is characterised in that the radiating block has rectangular parallelepiped structure.
- 7. insertion composite member according to claim 1, it is characterised in that first mounting surface and second mounting surface It is arranged in parallel.
- 8. insertion composite member according to claim 1, it is characterised in that raised line is strengthened in second radiating has polygon prism Structure.
- 9. insertion composite member according to claim 1, it is characterised in that the radiating cylinder has rectangular parallelepiped structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720946723.XU CN207006657U (en) | 2017-07-31 | 2017-07-31 | Insertion composite member |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720946723.XU CN207006657U (en) | 2017-07-31 | 2017-07-31 | Insertion composite member |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207006657U true CN207006657U (en) | 2018-02-13 |
Family
ID=61457056
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720946723.XU Expired - Fee Related CN207006657U (en) | 2017-07-31 | 2017-07-31 | Insertion composite member |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207006657U (en) |
-
2017
- 2017-07-31 CN CN201720946723.XU patent/CN207006657U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20180213 Termination date: 20180731 |