CN206211989U - Satellite communication transceiver machine - Google Patents
Satellite communication transceiver machine Download PDFInfo
- Publication number
- CN206211989U CN206211989U CN201621264650.8U CN201621264650U CN206211989U CN 206211989 U CN206211989 U CN 206211989U CN 201621264650 U CN201621264650 U CN 201621264650U CN 206211989 U CN206211989 U CN 206211989U
- Authority
- CN
- China
- Prior art keywords
- shell body
- satellite communication
- communication transceiver
- orthocoupler
- transceiver machine
- 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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Abstract
The utility model discloses a kind of satellite communication transceiver machine, including shell body, orthocoupler, guide blocks, receiver module and transmitter module, the orthocoupler is arranged on inside the shell body, the orthocoupler has Waveguide interface, input interface and output interface, the guide blocks are arranged at the Waveguide interface, the shell body, orthocoupler and guide blocks are formed in one structure, the receiver module is arranged at the input interface, and the transmitter module is arranged at the output interface.The satellite communication transceiver machine, be fused to shell body to optimize the arrangement space of each module using orthocoupler, it is to avoid split type superposition causes the phenomenon that space increases, and can reduce the machine volume of satellite communication transceiver machine；Also, when being assembled, it is only necessary to which receiver module is arranged at input interface, transmitter module is arranged at output interface can complete assembling, assemble simple and convenient.
Description
Technical field
The utility model is related to technical field of satellite communication, more particularly to a kind of satellite communication transceiver machine.
Background technology
As the quickening of social paces, research and development of products design are most important, integrally-built design will affect enterprise
Benefit.Traditional, when satellite communication transceiver is designed assembling, first debugging index independent to orthocoupler confirms, then
Other structures are designed around orthocoupler, and is accordingly assembled.Because orthocoupler interface has been determined, modules are folded
Added-time arrangement will be limited, cause the volume of satellite communication transceiver larger, and assemble complex.
The content of the invention
Based on this, it is necessary to provide a kind of satellite communication transceiver machine, the satellite communication transceiver machine small volume,
Assembling simple and convenient.
Its technical scheme is as follows：
A kind of satellite communication transceiver machine, including shell body, orthocoupler, guide blocks, receiver module and transmitting mould
Block, the orthocoupler is arranged on inside the shell body, and the orthocoupler has Waveguide interface, input interface and defeated
Outgoing interface, the guide blocks are arranged at the Waveguide interface, and the shell body, orthocoupler and guide blocks are integrated into
Type structure, the receiver module is arranged at the input interface, and the transmitter module is arranged at the output interface.
Wherein in one embodiment, the shell body side relative with the input interface is provided with the first installation cavity
Body, the first installation cavity is communicated with the input interface, and the receiver module is arranged in the described first installation cavity, and
The receiver module is connected with the shell body.
Wherein in one embodiment, the satellite communication transceiver machine also includes being matched with the described first installation cavity
The first cover plate, the first cover plate lid is located at the outside of the receiver module, and first cover plate connects with the shell body
Connect.
Wherein in one embodiment, the cross section of the first installation cavity matches with the receiver module.
Wherein in one embodiment, the shell body side relative with the output interface is provided with the second installation cavity
Body, the second installation cavity is communicated with the output interface, and the transmitter module is arranged in the described second installation cavity, and
The transmitter module is connected with the shell body.
Wherein in one embodiment, the satellite communication transceiver machine also includes being matched with the described second installation cavity
The second cover plate, the second cover plate lid is located at the outside of the transmitter module, and second cover plate connects with the shell body
Connect.
Wherein in one embodiment, the cross section of the second installation cavity matches with the transmitter module.
Wherein in one embodiment, the guide blocks part extend out to the outside of the shell body.
Wherein in one embodiment, the shell body is radiating shell.
Wherein in one embodiment, radiating fin is provided with the outside of the shell body.
The beneficial effects of the utility model are：
The satellite communication transceiver machine, orthocoupler is set within the outer shell, and shell body, orthogonal coupling
Device and guide blocks are formed in one structure, and then orthocoupler is fused in shell body, are merged using orthocoupler
Optimize the arrangement space of each module to shell body, it is to avoid split type superposition causes the phenomenon that space increases, and can reduce satellite
The machine volume of transceiver communication all-in-one；Also, when being assembled, it is only necessary to which receiver module is arranged at input interface, will
Transmitter module is arranged at output interface can complete assembling, and orthocoupler is assembled on shell body without elder generation, then refill
With guide blocks, receiver module and transmitter module, simple and convenient is assembled.
Brief description of the drawings
Fig. 1 is the structural representation one of the satellite communication transceiver machine described in the utility model embodiment；
Fig. 2 is the structural representation two of the satellite communication transceiver machine described in the utility model embodiment；
Fig. 3 is the configuration schematic diagram of the satellite communication transceiver machine described in the utility model embodiment
Description of reference numerals：
100th, shell body, 110, radiating fin, 120, first installs cavity, and 130, second installs cavity, and 200, corss coupling
Clutch, 210, input interface, 220, output interface, 300, guide blocks, 400, receiver module, 500, transmitter module, 600, first
Cover plate, the 700, second cover plate.
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 transceiver machine, including shell body 100, orthocoupler 200,
Guide blocks 300, receiver module 400 and transmitter module 500, the orthocoupler 200 are arranged on inside the shell body 100,
The orthocoupler 200 has Waveguide interface (not shown), input interface 210 and output interface 220, the guide blocks
300 are arranged at the Waveguide interface, and the shell body 100, orthocoupler 200 and guide blocks 300 are formed in one knot
Structure, the receiver module 400 is arranged at the input interface 210, and the transmitter module 500 is arranged on the output interface
At 220.
The satellite communication transceiver machine, orthocoupler 200 is arranged on the inside of shell body 100, and shell body
100th, orthocoupler 200 and guide blocks 300 are formed in one structure, and then orthocoupler 200 is fused into shell body
In 100, it is fused to shell body 100 using orthocoupler 200 to optimize the arrangement space of each module, it is to avoid split type superposition
The phenomenon for causing space to increase, can reduce the machine volume of satellite communication transceiver machine；Also, when being assembled, it is only necessary to
Receiver module 400 is arranged at input interface 210, transmitter module 500 is arranged at output interface 220 can complete dress
Match somebody with somebody, orthocoupler 200 is assembled on shell body 100 without elder generation, then reassemble guide blocks 300, receiver module 400 and transmitting
Module 500, assembles simple and convenient.Satellite communication transceiver machine described in the present embodiment, by by shell body 100, corss coupling
Clutch 200 and guide blocks 300 are set to integrated formed structure, are fused to shell body 100 using orthocoupler 200 to optimize
The arrangement space of modules, it is to avoid split type superposition causes spatial volume to increase and the difficult phenomenon of assembling, can be preferable
Meet appearance and size requirement, reduce the complexity of assembling, it is possible to increase assembling line efficiency, it is cost-effective.
In the present embodiment, the shell body 100 is radiating shell, can play preferable thermolysis.The shell body 100
Outside be provided with radiating fin 110, thermolysis, perfect heat-dissipating can be further functioned as.In the present embodiment, as shown in figure 1, institute
The outside that the part of guide blocks 300 extend out to the shell body 100 is stated, is easy to transmission signal.In the present embodiment, as shown in figure 3, can
With the Waveguide interface direction according to orthocoupler 200, the input interface 210, output interface 220 are arranged, set
Side corresponding with Waveguide interface is first side on shell body 100, and the output interface 220 is arranged in shell body 100 and the
At the relative second side of one side, the input interface 210 is arranged in a side between first side and second side
Place.
In the present embodiment, the side relative with the input interface 210 of the shell body 100 is provided with the first installation cavity
120, the first installation cavity 120 is communicated with the input interface 210, and the receiver module 400 is arranged on the described first peace
It behave affectedly in body 120, and the receiver module 400 is connected with the shell body 100.Using said structure, receiver module 400 can be with
In the first installation cavity 120, and realization is communicated with the input interface 210 of orthocoupler 200, install convenient.This reality
Apply in example, the cross section of the first installation cavity 120 matches with the receiver module 400, and then, first installs cavity 120
Can play guiding and guiding function, receiver module 400 assemble when more facilitate, and the present embodiment satellite communication transceiver
Machine complete machine structure is attractive in appearance.
Further, the satellite communication transceiver machine also includes matched with the described first installation cavity 120 first
Cover plate 600, first cover plate 600 covers the outside for being located at the receiver module 400, and first cover plate 600 is outer with described
Housing 100 is connected.By setting the first cover plate 600, on the one hand, the first cover plate 600 can be played to receiver module 400 and block guarantor
Shield is acted on, and plays water proof and dust proof effect；On the other hand so that the satellite communication transceiver machine good integrity of the present embodiment.
In the present embodiment, the side relative with the output interface 220 of the shell body 100 is provided with the second installation cavity
130, the second installation cavity 130 is communicated with the output interface 220, and the transmitter module 500 is arranged on the described second peace
It behave affectedly in body 130, and the transmitter module 500 is connected with the shell body 100.Using said structure, transmitter module 500 can be with
In the second installation cavity 130, and realization is communicated with the output interface 220 of orthocoupler 200, install convenient.This reality
Apply in example, the cross section of the second installation cavity 130 matches with the transmitter module 500, and then, second installs cavity 130
Can play guiding and guiding function, transmitter module 500 assemble when more facilitate, and the present embodiment satellite communication transceiver
Machine complete machine structure is attractive in appearance.
Further, the satellite communication transceiver machine also includes matched with the described second installation cavity 130 second
Cover plate 700, second cover plate 700 covers the outside for being located at the transmitter module 500, and second cover plate 700 is outer with described
Housing 100 is connected.By setting the second cover plate 700, on the one hand, the second cover plate 700 can be played to transmitter module 500 and block guarantor
Shield is acted on, and plays water proof and dust proof effect；On the other hand so that the satellite communication transceiver machine good integrity of the present embodiment.
Satellite communication transceiver machine described in the present embodiment, orthocoupler 200 is arranged in shell body 100
Portion, and shell body 100, orthocoupler 200 and guide blocks 300 are integrated die sinking molding structure, i.e., in the box of shell body 100
Just orthocoupler 200 and guide blocks 300 are fused in shell body 100 in body design, according to the waveguide of orthocoupler 200
Interface direction correspondence design receiver module 400 and the installation site of transmitter module 500, then correspond to design input interface 210 again
With output interface 220, so as to orthocoupler 200 and guide blocks 300 are merged in shell body 100.By using corss coupling
Clutch 200 is fused to shell body 100 and comes the arrangement space of optimization module, and then ensure that the appearance and size of shell body 100, keeps away
Having exempted from split type superposition causes space to increase and the difficult phenomenon of assembling, can not only meet satellite communication transceiver machine profile chi
Very little requirement, also reduces assembling complexity, improves assembling line efficiency, and saved cost.
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 machine, it is characterised in that including shell body, orthocoupler, guide blocks, receiver module
And transmitter module, the orthocoupler is arranged on inside the shell body, and the orthocoupler has Waveguide interface, input
Interface and output interface, the guide blocks are arranged at the Waveguide interface, the shell body, orthocoupler and guide blocks
Be formed in one structure, and the receiver module is arranged at the input interface, and the transmitter module is arranged on the output and connects
At mouthful.
2. satellite communication transceiver machine according to claim 1, it is characterised in that the shell body connects with the input
The relative side of mouth is provided with the first installation cavity, and the first installation cavity is communicated with the input interface, the reception mould
Block is arranged in the described first installation cavity, and the receiver module is connected with the shell body.
3. satellite communication transceiver machine according to claim 2, it is characterised in that also including with first installation cavity
First cover plate of body matching, the first cover plate lid is located at the outside of the receiver module, and first cover plate is outer with described
Housing is connected.
4. satellite communication transceiver machine according to claim 2, it is characterised in that described first installs the transversal of cavity
Face matches with the receiver module.
5. satellite communication transceiver machine according to claim 1, it is characterised in that the shell body connects with the output
The relative side of mouth is provided with the second installation cavity, and the second installation cavity is communicated with the output interface, the transmitting mould
Block is arranged in the described second installation cavity, and the transmitter module is connected with the shell body.
6. satellite communication transceiver machine according to claim 5, it is characterised in that also including with second installation cavity
Second cover plate of body matching, the second cover plate lid is located at the outside of the transmitter module, and second cover plate is outer with described
Housing is connected.
7. satellite communication transceiver machine according to claim 5, it is characterised in that described second installs the transversal of cavity
Face matches with the transmitter module.
8. the satellite communication transceiver machine according to claim any one of 1-7, it is characterised in that the guide blocks part
It extend out to the outside of the shell body.
9. the satellite communication transceiver machine according to claim any one of 1-7, it is characterised in that the shell body is scattered
Hot housing.
10. satellite communication transceiver machine according to claim 9, it is characterised in that be provided with the outside of the shell body
Radiating fin.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621264650.8U CN206211989U (en) | 2016-11-21 | 2016-11-21 | Satellite communication transceiver machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621264650.8U CN206211989U (en) | 2016-11-21 | 2016-11-21 | Satellite communication transceiver machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206211989U true CN206211989U (en) | 2017-05-31 |
Family
ID=58746974
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621264650.8U Expired - Fee Related CN206211989U (en) | 2016-11-21 | 2016-11-21 | Satellite communication transceiver machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206211989U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109412681A (en) * | 2018-12-17 | 2019-03-01 | 南京天际易达通信技术有限公司 | A kind of enhanced satellite communication portable station all-in-one machine |
-
2016
- 2016-11-21 CN CN201621264650.8U patent/CN206211989U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109412681A (en) * | 2018-12-17 | 2019-03-01 | 南京天际易达通信技术有限公司 | A kind of enhanced satellite communication portable station all-in-one machine |
| CN109412681B (en) * | 2018-12-17 | 2023-12-22 | 南京天际易达通信技术有限公司 | Portable station all-in-one of enhancement mode satellite communication |
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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: 20181121 |