CN206211988U - Satellite communication transceiver and satellite communication equipment - Google Patents
Satellite communication transceiver and satellite communication equipment Download PDFInfo
- Publication number
- CN206211988U CN206211988U CN201621254886.3U CN201621254886U CN206211988U CN 206211988 U CN206211988 U CN 206211988U CN 201621254886 U CN201621254886 U CN 201621254886U CN 206211988 U CN206211988 U CN 206211988U
- Authority
- CN
- China
- Prior art keywords
- satellite communication
- heat dissipation
- dissipation base
- communication transceiver
- installation panel
- 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.)
- Expired - Fee Related
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- Details Of Aerials (AREA)
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Abstract
The utility model discloses a kind of satellite communication transceiver and satellite communication equipment, the satellite communication transceiver includes heat dissipation base and heating module, the heating module is arranged in the first side of the heat dissipation base, the heat dissipation base is used for the installation panel installed in dual-mode antenna, the face relative with the first side is second side on the heat dissipation base, and the second side is used for the mounting surface installed in the installation panel.The satellite communication transceiver and satellite communication equipment, the heat that heating module is distributed can be transferred on the installation panel of dual-mode antenna by heat dissipation base, and then using the big area of dissipation of dual-mode antenna, heat fully is carried out into free convection to realize good radiating, good heat dissipation effect, and, because itself is without being radiated, without setting radiation tooth, small volume, lighter in weight on housing.
Description
Technical field
The utility model is related to technical field of satellite communication, more particularly to a kind of satellite communication transceiver and satellite communication
Equipment.
Background technology
With continuing to develop for electronic technology, the miniaturization of communication equipment seems further important, and small product size requirement is more next
It is smaller, performance requirement more and more higher.Traditional, satellite communication transceiver is larger due to power consumption, generally by its own box
Body or lid carry more radiation tooth, and are thus radiated, and cause the volume of product larger, heavier-weight.Also, satellite
When communication transceiver and dual-mode antenna are supported the use, can also increase to a certain extent the overall volume of satellite communication device and
Weight.
The content of the invention
Based on this, it is necessary to provide a kind of satellite communication transceiver and satellite communication equipment, satellite communication transmitting-receiving letter
The perfect heat-dissipating of machine and satellite communication equipment, small volume, lighter in weight.
Its technical scheme is as follows：
A kind of satellite communication transceiver, including heat dissipation base and heating module, the heating module are arranged on described dissipating
In the first side of hot base, the heat dissipation base is used for the installation panel installed in dual-mode antenna, on the heat dissipation base
The face relative with the first side is second side, and the second side is used for the mounting surface installed in the installation panel
On.
Wherein in one embodiment, the satellite communication transceiver also includes lid, and the lid is located at described
The outside of heating module, and the lid is connected with the heat dissipation base.
Wherein in one embodiment, the lid includes the first fixture, cover body and the openend along the cover body
The connecting plate that edge is set, the outward flange of the connecting plate matches with the outward flange of the heat dissipation base, the connecting plate and institute
Heat dissipation base is stated to be connected by first fixture.
Wherein in one embodiment, the lid also includes the second fixture, the connecting plate, the heat dissipation base one
Rise and be connected with the installation panel by second fixture.
Wherein in one embodiment, the lid is provided with multiple perforates.
Wherein in one embodiment, the first signal communication hole is offered on the heat dissipation base, first signal leads to
Letter hole is used to be connected with the secondary signal communicating hole on the installation panel.
Wherein in one embodiment, the heat dissipation base is heat radiating metal material.
Wherein in one embodiment, the second side of the heat dissipation base is precision-machined surface, the installation panel
Mounting surface is precision-machined surface.
A kind of satellite communication equipment, including dual-mode antenna and described satellite communication transceiver, the dual-mode antenna bag
Include radiating pot and be arranged on it is described radiating pot lateral surface on installation panel, the radiating pot be parabolic shape or
Plane pot.
Wherein in one embodiment, the medial surface of the radiating pot is provided with signal transmitting tube.
It is appreciated that term " first ", " second " used in it etc. is used to distinguish object herein, but these are right
As should not be limited by these terms.
The beneficial effects of the utility model are：
The satellite communication transceiver, is arranged in the first side of heat dissipation base by by heating module, will radiate
The second side of base is arranged on the installation panel of dual-mode antenna, and the heat that heating module is distributed can be turned by heat dissipation base
Move on the installation panel of dual-mode antenna, so using dual-mode antenna big area of dissipation, fully by heat carry out free convection with
Realize good radiating, good heat dissipation effect, also, because itself is without being radiated, without setting radiation tooth, energy on housing
Enough reduce the volume and weight of product.The satellite communication transceiver, transmitting-receiving day is transferred to by the area of dissipation required for it
On line, while perfect heat-dissipating is met, small volume, lighter in weight.
The satellite communication equipment, including satellite communication transceiver described above, possess the satellite communication transmitting-receiving
The technique effect of letter machine, perfect heat-dissipating, small volume, lighter in weight.
Brief description of the drawings
Fig. 1 is the structural representation of the satellite communication equipment described in the utility model embodiment；
Fig. 2 is the configuration schematic diagram one of the satellite communication equipment described in the utility model embodiment；
Fig. 3 is the configuration schematic diagram two of the satellite communication equipment described in the utility model embodiment；
Fig. 4 is the structural representation of the satellite communication transceiver described in the utility model embodiment.
Description of reference numerals：
100th, satellite communication transceiver, 110, heat dissipation base, the 111, first signal communication hole, 120, heating module,
130th, lid, 131, perforate, 132, cover body, 133, connecting plate, the 134, first fixture, the 135, second fixture, 200, transmitting-receiving
Antenna, 210, panel is installed, 211, secondary signal communicating hole, 220, radiating pot, 230, signal transmitting tube.
Specific embodiment
In order that the purpose of this utility model, technical scheme and advantage become more apparent, below in conjunction with accompanying drawing and implementation
Example, is further elaborated to the utility model.It should be appreciated that specific embodiment described herein is only used to explain
The utility model, is not used to limit the utility model.
As shown in Figure 1, Figure 2, Figure 3 shows, a kind of satellite communication equipment, including satellite communication transceiver 100 and dual-mode antenna
200。
As shown in Figure 2, Figure 3, Figure 4, the satellite communication transceiver 100 includes heat dissipation base 110 and heating module
120, the heating module 120 is arranged in the first side of the heat dissipation base 110, and the heat dissipation base 110 is used to install
On the installation panel 210 of dual-mode antenna 200, the face relative with the first side is the second side on the heat dissipation base 110
Face, the second side is used for the mounting surface installed in the installation panel 210.During actual design, for the ease of installing, can
The part heating module larger to choose the internal heat generation amount of the satellite communication transceiver 100, by the heating module 120 of this part
It is arranged on the heat dissipation base 110.In the present embodiment, the heat dissipation base 110 can be using heat conductivilitys such as aluminium sheet, copper coins
Preferable heat radiating metal material, heat conduction and perfect heat-dissipating, effectively can conduct to transmitting-receiving the heat that heating module 120 is distributed
On antenna 200.
The satellite communication transceiver 100, by the first side that heating module 120 is arranged on heat dissipation base 110
On, the second side of heat dissipation base 110 is arranged on the installation panel 210 of dual-mode antenna 200, what heating module 120 was distributed
Heat can be transferred on the installation panel 210 of dual-mode antenna 200 by heat dissipation base 110, and then using dual-mode antenna 200
Big area of dissipation, fully carries out free convection to realize good radiating, good heat dissipation effect by heat, also, because the satellite is logical
Transceiver 100 itself is believed without being radiated, without setting radiation tooth, and then the satellite communication transceiver on its housing
100 volume and weight can be made thin small, can reduce the volume and weight of product.The satellite communication transceiver
100, the area of dissipation required for it is transferred on dual-mode antenna 200, while perfect heat-dissipating is met, small volume,
Lighter in weight.
Further, as shown in figure 4, the satellite communication transceiver 100 also includes lid 130, the lid 130 covers
The outside of the heating module 120 is located at, and the lid 130 is connected with the heat dissipation base 110.Using said structure, box
Lid 130 can be protected to the internal part of the satellite communication transceiver 100, play sealing role.In the present embodiment,
The lid 130 is provided with multiple perforates 131.By setting perforate 131, on the one hand, cross-ventilated effect can be played, entered
One step improves the heat dispersion of the satellite communication transceiver 100 of the present embodiment；On the other hand, it is also possible to reduce lid 130
Weight, further reduces the weight of the whole machine of satellite communication transceiver 100 of the present embodiment.Specifically, the perforate 131 is set
On following cover bodies 132, and the perforate 131 is multiple, the circumferentially spaced setting of multiple perforates 131.The present embodiment
In, as shown in Figure 2 and Figure 3, the first signal communication hole 111, the first signal communication hole are offered on the heat dissipation base 110
111 are used to be connected with the secondary signal communicating hole 211 on the installation panel 210.By setting the first signal communication hole 111,
And secondary signal communicating hole 211 is set on the installation panel 210 of dual-mode antenna 200, it is easy to signal transmission.
In the present embodiment, the lid 130 includes the first fixture 134, cover body 132 and opening along the cover body 132
The connecting plate 133 that mouth end margin is set, the outward flange of the connecting plate 133 matches with the outward flange of the heat dissipation base 110, institute
Connecting plate 133 is stated to be connected by first fixture 134 with the heat dissipation base 110.Using said structure, the lid
130 can realize being connected with heat dissipation base 110, also, the outward flange of the connecting plate 133 is outer with the heat dissipation base 110
Edge matching, after the lid 130 is connected with the heat dissipation base 110, good integrity, structure is attractive in appearance.It is described in the present embodiment
First fixture 134 is fixing bolt, and first fixture 134 is multiple, multiple first fixtures 134 circumferentially between
Every setting.Using above-mentioned setting, the lid 130 is easy to connect with heat dissipation base 110, reliable.
In the present embodiment, the lid 130 also includes the second fixture 135, the connecting plate 133, the heat dissipation base
110 are connected by second fixture 135 with the installation panel 210 together.Likewise, by setting the second fixture
135, the satellite communication transceiver 100 of the present embodiment can realize the connection with dual-mode antenna 200.It is described in the present embodiment
Second fixture 135 is fixing bolt, and second fixture 135 is multiple, multiple second fixtures 135 circumferentially between
Every setting.Using above-mentioned setting, the satellite communication transceiver 100 is easy to connect with dual-mode antenna 200, reliable.
In the present embodiment, the second side of the heat dissipation base 110 is precision-machined surface, the peace of the installation panel 210
Dress face is precision-machined surface.The second side of the heat dissipation base 110 is fabricated to precision-machined surface using finishing, it is ensured that the
The finish and flatness of two side faces, meanwhile, the mounting surface of the installation panel 210 of dual-mode antenna 200 is also adopted by finishing manufacture
It is precision-machined surface, it is ensured that the finish and flatness of mounting surface, after second side and mounting surface coordinate to be installed, its is mutual
Between can be brought into close contact, and then, can fully by the heat that heating module 120 sends conduct to install panel 210 on, fully
The huge area of dissipation of dual-mode antenna 200 is played, high cooling efficiency is realized, radiating effect is improved.
In the present embodiment, the dual-mode antenna 200 includes radiating pot 220 and is arranged on the radiating pot 220
Installation panel 210 on lateral surface, the radiating pot 220 is parabolic shape or plane pot.By by the radiating pot
Body 220 is set to parabolic shape or plane, and area of dissipation is big, the satellite communication equipment described in the present embodiment, including described above
Satellite communication transceiver 100, possess the technique effect of the satellite communication transceiver 100, perfect heat-dissipating, volume compared with
Small, lighter in weight is conducive to entirety to be adjusted motion.
In the present embodiment, the installation panel 210 is formed in one structure with the radiating pot 220, installs panel 210
On heat can effectively be transferred to radiating pot 220 on, realize big area of dissipation.Further, the radiating pot 220
Medial surface be provided with signal transmitting tube 230, for transmission signal.Specifically, one end of the signal transmitting tube 230 with it is described
The secondary signal communicating hole 211 installed on panel 210 is docked, for the signal for sending the satellite communication transceiver 100
Launch.
Satellite communication transceiver 100 and satellite communication equipment described in the present embodiment, are believed by the way that satellite communication is received and dispatched
Area of dissipation required for machine 100 is transferred on dual-mode antenna 200, and satellite communication transceiver 100 is carried out with dual-mode antenna 200
Coordinate after installing, satellite communication transceiver 100 can utilize the huge area of dissipation of dual-mode antenna 200, fully enter heat
Row Natural Heat Convection, realizes the good heat radiating requirement of satellite communication transceiver 100, also, meeting the same of cooling requirements
When, the volume and weight of satellite communication transceiver 100 can be reduced, be conducive to the integrated regulation of satellite communication equipment to move.
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 of this specification record is all considered to be.
Embodiment described above only expresses several embodiments of the present utility model, and its description is more specific and detailed,
But therefore can not be interpreted as the limitation to utility model patent scope.It should be pointed out that for the common skill of this area
For art personnel, without departing from the concept of the premise utility, various modifications and improvements can be made, these are belonged to
Protection domain of the present utility model.Therefore, the protection domain of the utility model patent should be determined by the appended claims.
Claims (10)
1. a kind of satellite communication transceiver, it is characterised in that including heat dissipation base and heating module, the heating module is set
In the first side of the heat dissipation base, the heat dissipation base is used for the installation panel installed in dual-mode antenna, described to dissipate
The face relative with the first side is second side on hot base, and the second side is used for installed in the installation panel
On mounting surface.
2. satellite communication transceiver according to claim 1, it is characterised in that also including lid, the lid cover sets
It is connected with the heat dissipation base in the outside of the heating module, and the lid.
3. satellite communication transceiver according to claim 2, it is characterised in that the lid include the first fixture,
Cover body and the connecting plate of the open end edge setting along the cover body, the outward flange of the connecting plate and the heat dissipation base
Outward flange is matched, and the connecting plate is connected with the heat dissipation base by first fixture.
4. satellite communication transceiver according to claim 3, it is characterised in that the lid also includes that second fixes
Part, the connecting plate, the heat dissipation base are connected by second fixture with the installation panel together.
5. satellite communication transceiver according to claim 2, it is characterised in that the lid is provided with multiple perforates.
6. the satellite communication transceiver according to claim any one of 1-5, it is characterised in that opened on the heat dissipation base
The first signal communication hole is provided with, the first signal communication hole is used to connect with the secondary signal communicating hole on the installation panel
It is logical.
7. the satellite communication transceiver according to claim any one of 1-5, it is characterised in that the heat dissipation base is scattered
Thermometal material.
8. the satellite communication transceiver according to claim any one of 1-5, it is characterised in that the of the heat dissipation base
Two side faces are precision-machined surface, and the mounting surface of the installation panel is precision-machined surface.
9. a kind of satellite communication equipment, it is characterised in that lead to including the satellite described in dual-mode antenna and claim any one of 1-8
Letter transceiver, the dual-mode antenna includes radiating pot and the mounting surface being arranged on the lateral surface of the radiating pot
Plate, the radiating pot is parabolic shape or plane pot.
10. satellite communication equipment according to claim 9, it is characterised in that the medial surface of the radiating pot is provided with
Signal transmitting tube.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621254886.3U CN206211988U (en) | 2016-11-16 | 2016-11-16 | Satellite communication transceiver and satellite communication equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621254886.3U CN206211988U (en) | 2016-11-16 | 2016-11-16 | Satellite communication transceiver and satellite communication equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206211988U true CN206211988U (en) | 2017-05-31 |
Family
ID=58749171
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621254886.3U Expired - Fee Related CN206211988U (en) | 2016-11-16 | 2016-11-16 | Satellite communication transceiver and satellite communication equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206211988U (en) |
-
2016
- 2016-11-16 CN CN201621254886.3U patent/CN206211988U/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: 20170531 Termination date: 20181116 |