CN206629052U - Aviation band transmitter radiator - Google Patents
Aviation band transmitter radiator Download PDFInfo
- Publication number
- CN206629052U CN206629052U CN201720422651.9U CN201720422651U CN206629052U CN 206629052 U CN206629052 U CN 206629052U CN 201720422651 U CN201720422651 U CN 201720422651U CN 206629052 U CN206629052 U CN 206629052U
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- CN
- China
- Prior art keywords
- fin
- heat
- pair
- fan
- heat dissipation
- 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.)
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- Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)
Abstract
The utility model discloses a kind of aviation band transmitter radiator, including pair of radiating fan, the radiation tooth of the pair of fin is oppositely arranged, line plate is crossed in the both sides of the pair of fin provided with parallel with radiation tooth, heat dissipation wind channel is formed among the pair of fin, and one end of the heat dissipation wind channel is provided with fan, the fan is set towards heat dissipation wind channel, the fin is provided with the dividing plate of mounting related components, dividing plate side relative with radiation tooth on fin.The radiator can focus on to heat, heating element is affixed on fin back, heat is poured on fin by way of heat transfer, again by fan, heat is taken away rapidly using cross-ventilation, without allowing heat to disperse, after enclosing cover installation simultaneously, it is completely closed, it is isolated from the outside, electromagnetic shielding capability is strong.
Description
Technical field
Radio compact system field is the utility model is related to, particularly a kind of aviation band transmitter radiator.
Background technology
There is the king-sized module of multiple caloric values inside aviation band transmitter, there is also dry between each other for these modules
Disturb, and easily disturbed by outer signals, and it is also higher to IP class requirements, so common radiating mode can not
Meet demand will be also realized between module and module, module and extraneous electromagnetic screen, it is necessary to heat is put together into processing
Cover.
Utility model content
Based on this, in view of the above-mentioned problems, being necessary to propose a kind of aviation band transmitter radiator, the radiator can be right
Heat is focused on, and heating element is affixed on into fin back, heat is poured into fin by way of heat transfer
On, then by fan, taken away heat rapidly using cross-ventilation, without allowing heat to disperse, while enclosing cover installation
Afterwards, it is completely closed, it is isolated from the outside, electromagnetic shielding capability is strong.
The technical solution of the utility model is：A kind of aviation band transmitter radiator, including pair of radiating fan, described one
The radiation tooth of fin is oppositely arranged, the both sides of the pair of fin be provided with it is parallel with radiation tooth cross line plate, described one
To forming heat dissipation wind channel among fin, and one end of the heat dissipation wind channel is provided with fan, and the fan is set towards heat dissipation wind channel
Put, the fin is provided with the dividing plate of mounting related components, dividing plate side relative with radiation tooth on fin.
Component is installed on dividing plate, and heat conductive silica gel is coated between component and fin, heat caused by component
Conduction distributes on a heat sink, then via radiation tooth, and the fan by heat dissipation wind channel can accelerate air circulation, take away faster
Heat.
Preferably, one end of the heat dissipation wind channel, which is uniformly distributed, is provided with multiple fans.
Multiple fans work simultaneously, can greatly increase radiating efficiency.
Preferably, the material of the fin is silver or copper or aluminium or steel.
The fin made using silver, copper, aluminium or steel, its heat-conducting effect are more preferable.
Preferably, it is additionally provided with enclosing cover on the fin, and described outer is covered on relative with radiation tooth one on fin
Side, the cavity of sealing is formed between the enclosing cover and fin, the dividing plate is in cavity.
The effective dustproof and waterproof of seal cavity energy, dust will not be entered in component with moisture, and IP grades can reach
It is required that.
Preferably, the material of the enclosing cover is copper or aluminium or steel.
Enclosing cover is also made of good heat-conducting copper or aluminium or steel, can auxiliary heat dissipation, use, use as auxiliary heat dissipation
Silver-colored cost of manufacture is too high.
Preferably, the enclosing cover passes through wired earth.
After enclosing cover ground connection, electromagnetic shielding can be played a part of, while prevented also from electrostatic interference.
The beneficial effects of the utility model are：
1st, heat can be focused on, heating module is affixed on to the side of fin, by way of heat transfer
Heat is poured on fin, then the fan by opposite side, taken away heat rapidly using cross-ventilation, without allowing heat
It is scattered；
2nd, it is completely closed after enclosing cover installation, it is isolated from the outside, electromagnetic shielding capability is strong；
3rd, the effective dustproof and waterproof of energy, dust will not be entered in component cavity with moisture, and IP grades can reach will
Ask.
Brief description of the drawings
Fig. 1 is the structural representation of the utility model embodiment；
Reference：10- fin, 20- fans, 30- cross line plate, 40- dividing plates.
Embodiment
Embodiment of the present utility model is described in detail below in conjunction with the accompanying drawings.
Embodiment
As shown in figure 1, a kind of aviation band transmitter radiator, including pair of radiating fan 10, the pair of fin 10
Radiation tooth be oppositely arranged, the both sides of the pair of fin 10 be provided with it is parallel with radiation tooth cross line plate 30, it is the pair of to dissipate
Form heat dissipation wind channel among backing 10, and one end of the heat dissipation wind channel is provided with fan 20, the fan 20 is towards heat dissipation wind channel
Set, the fin 10 is provided with the dividing plate 40 of mounting related components, and the dividing plate 40 is located on fin 10 and radiation tooth phase
To side.
In one of the embodiments, one end of the heat dissipation wind channel, which is uniformly distributed, is provided with multiple fans 20.
In one of the embodiments, the material of the fin 10 is silver or copper or aluminium or steel.
In one of the embodiments, it is additionally provided with enclosing cover on the fin 10, and described outer is covered on fin 10
The side relative with radiation tooth, the cavity of sealing is formed between the enclosing cover and fin 10, the dividing plate 40 is in cavity.
In one of the embodiments, the material of the enclosing cover is copper or aluminium or steel.
In one of the embodiments, the enclosing cover passes through wired earth.
Embodiment described above only expresses specific embodiment of the present utility model, and its description is more specific and detailed,
But therefore it can not be interpreted as the limitation to the utility model patent scope.It should be pointed out that for the common of this area
For technical staff, without departing from the concept of the premise utility, various modifications and improvements can be made, these all belong to
In the scope of protection of the utility model.
Claims (6)
- A kind of 1. aviation band transmitter radiator, it is characterised in that including pair of radiating fan, the radiating of the pair of fin Tooth is oppositely arranged, and line plate, the pair of fin centre shape are crossed in the both sides of the pair of fin provided with parallel with radiation tooth Into heat dissipation wind channel, and one end of the heat dissipation wind channel is provided with fan, and the fan is set towards heat dissipation wind channel, on the fin Dividing plate provided with mounting related components, dividing plate side relative with radiation tooth on fin.
- 2. aviation band transmitter radiator according to claim 1, it is characterised in that one end of the heat dissipation wind channel is equal Even distribution is provided with multiple fans.
- 3. aviation band transmitter radiator according to claim 1 or 2, it is characterised in that the material of the fin For silver or copper or aluminium or steel.
- 4. aviation band transmitter radiator according to claim 1, it is characterised in that be additionally provided with the fin outer Lid, and it is described it is outer be covered on side relative with radiation tooth on fin, the chamber of sealing is formed between the enclosing cover and fin Body, the dividing plate is in cavity.
- 5. aviation band transmitter radiator according to claim 4, it is characterised in that the material of the enclosing cover be copper or Aluminium or steel.
- 6. the aviation band transmitter radiator according to claim 4 or 5, it is characterised in that the enclosing cover passes through wire Ground connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720422651.9U CN206629052U (en) | 2017-04-21 | 2017-04-21 | Aviation band transmitter radiator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720422651.9U CN206629052U (en) | 2017-04-21 | 2017-04-21 | Aviation band transmitter radiator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206629052U true CN206629052U (en) | 2017-11-10 |
Family
ID=60205536
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720422651.9U Active CN206629052U (en) | 2017-04-21 | 2017-04-21 | Aviation band transmitter radiator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206629052U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110446416A (en) * | 2019-09-10 | 2019-11-12 | 山东省产品质量检验研究院 | A kind of electromagnetic compatibility case |
-
2017
- 2017-04-21 CN CN201720422651.9U patent/CN206629052U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110446416A (en) * | 2019-09-10 | 2019-11-12 | 山东省产品质量检验研究院 | A kind of electromagnetic compatibility case |
| CN110446416B (en) * | 2019-09-10 | 2020-04-07 | 山东省产品质量检验研究院 | Electromagnetic compatibility box |
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| GR01 | Patent grant |