CN207819918U - A kind of satellite communication terminal with shock-absorbing function - Google Patents
A kind of satellite communication terminal with shock-absorbing function Download PDFInfo
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- CN207819918U CN207819918U CN201820180729.5U CN201820180729U CN207819918U CN 207819918 U CN207819918 U CN 207819918U CN 201820180729 U CN201820180729 U CN 201820180729U CN 207819918 U CN207819918 U CN 207819918U
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- magnet
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- satellite communication
- shock
- electronic component
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Abstract
The utility model is related to technical field of satellite communication,More particularly to a kind of satellite communication terminal with shock-absorbing function,Including shell,Electronic component,Air bump,Air pump,Gas-guide tube,Ventilation duct,Vibrating sensor,Controller,Card slot,Fixture block,Magnet one,Pillar,Magnet two,Block,Damping spring and support plate,Enclosure centre is provided with electronic component,The surrounding of electronic component is respectively arranged with air bump,The both ends of air bump are fixedly connected with electronic component and outer casing inner wall respectively,Air pump is set to enclosure left end bottom,Gas-guide tube and ventilation duct are respectively arranged on air pump,Gas-guide tube is connected with each air bump respectively,The utility model is easily installed and dismantles,Its regulatory function can be adapted for a variety of rugged planes,It is applied widely and easy to use,Shock-absorbing protecting measure with high intensity,Intelligence degree is high,With very strong practicability.
Description
Technical field
The utility model is related to technical field of satellite communication, and in particular to a kind of satellite communication with shock-absorbing function is whole
End.
Background technology
Currently, with the development of the Modern Satellite communication technology, mobile satellite communication device is gradually widely used.So
And existing satellite communication terminal is when in use, suffers from the limitation of landform, when rugged local in use, satellite
Communication terminal put installation then become more more difficult, can not effectively place it is smooth, to affect communication terminal just
Often work.In the course of work, the extraneous vibratory forces transmitted are inevitably encountered, and existing apparatus can not be effectively to the external world
The vibratory forces transmitted are eliminated or are reduced so that the use of communication terminal device is affected, and reduces working efficiency.
Utility model content
In view of the deficiencies of the prior art, the utility model discloses a kind of satellite communication terminals with shock-absorbing function, use
There is limitation in the use for solving existing satellite communication terminal, can not effectively eliminate or reduce extraneous vibratory forces to device
The problem of influence of generation.
Specific technical solution is as follows：
A kind of satellite communication terminal with shock-absorbing function, including shell, electronic component, air bump, air pump, lead
Tracheae, ventilation duct, vibrating sensor, controller, card slot, fixture block, magnet one, pillar, magnet two, block, damping spring and branch
Fagging, the enclosure centre are provided with the electronic component, and the surrounding of the electronic component is respectively set
Air bump is stated, the both ends of the air bump are fixedly connected with the electronic component and the outer casing inner wall respectively,
The air pump is set to enclosure left end bottom, and the gas-guide tube and the ventilation are respectively arranged on the air pump
Pipe, the gas-guide tube are connected with each air bump respectively, and the vibrating sensor is set respectively with the controller
It is placed on the enclosure side wall, the card slot is respectively arranged at left and right sides of the outer casing bottom, is blocked inside the card slot
It connects and the fixture block is installed, the fixture block bottom is provided with the magnet one, and the pillar is set to one lower section of the magnet, institute
It states pillar top and is provided with the magnet two, be provided with the block on the outside of the pillar, the fixture block passes through with the block
The damping spring is fixedly connected, and the pillar bottom end is provided with the support plate, and the controller is passed with the vibration respectively
Sensor and the air pump are electrically connected；
Preferably, the ventilation duct extends to shell exterior through the shell；
Preferably, the pillar is located at immediately below the magnet one, and the magnet one is identical as the magnetic pole of the magnet two；
Preferably, the damping spring is respectively sleeved at the outside of the magnet one and the magnet two；
Preferably, the pillar is rotatablely connected with the support plate by shaft.
Advantageous effect：
When the utility model is used, support plate is positioned over to the position that will be put, since pillar and support plate are by turning
Axis is rotatablely connected, therefore the adjustable angle of support plate so that the support plate after angle adjustment can adapt in a variety of rugged
Plane, to expand the use scope of device；When being influenced by extraneous shaking force, damping spring can be to the present apparatus
Effective damping is carried out, reduces extraneous vibratory forces vibration effect caused by device, and due to the magnetic pole and magnet of magnet one
Two magnetic pole is identical, therefore two magnet are mutually exclusive, further enhance damping dynamics, while reducing the compression of damping spring
Degree has protective effect to damping spring, extends the usage time of damping spring；Since fixture block clamping is mounted on card slot
It is interior, therefore facilitate dismounting and change of the maintenance personal to damping spring；When to detect that vibratory forces reach controller pre- for vibrating sensor
When the value being first arranged, controller controls air pump by gas-guide tube to blasting air inside air bump so that air bump
Expansion ensure that the normal operation of the present apparatus, vibration pass to play good anti-vibration protected measure to internal electronic component
The setting of sensor makes the present apparatus have intelligent anti-vibration protected measure, improves protection efficiency, the setting of ventilation duct ensure that
The normal operation of air pump.
Description of the drawings
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is some embodiments of the utility model, for those of ordinary skill in the art, in the premise not made the creative labor
Under, other drawings may also be obtained based on these drawings.
Fig. 1：Satellite communication terminal overall structure diagram with shock-absorbing function.
Reference numeral is as follows：1, shell, 2, electronic component, 3, air bump, 4, air pump, 5, gas-guide tube, 6, ventilation
Pipe, 7, vibrating sensor, 8, controller, 9, card slot, 10, fixture block, 11, magnet one, 12, pillar, 13, magnet two, 14, block,
15, damping spring, 16, support plate.
Specific implementation mode
It is new below in conjunction with this practicality to keep the purpose, technical scheme and advantage of the utility model embodiment clearer
Attached drawing in type embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that is retouched
The embodiment stated is the utility model a part of the embodiment, instead of all the embodiments.Based on the implementation in the utility model
Example, the every other embodiment that those of ordinary skill in the art are obtained without creative efforts belong to
The range of the utility model protection.
Referring to Fig. 1：A kind of satellite communication terminal with shock-absorbing function, including shell 1 are arranged at 1 center of inside of shell
Have an electronic component 2, the surrounding of electronic component 2 is respectively arranged with air bump 3, the both ends of air bump 3 respectively with
Electronic component 2 is fixedly connected with 1 inner wall of shell, and air pump 4 is set to 1 inside left end bottom of shell, is respectively arranged on air pump 4
Gas-guide tube 5 and ventilation duct 6, gas-guide tube 5 are connected with each air bump 3 respectively, and vibrating sensor 7 is distinguished with controller 8
It is set in 1 internal side wall of shell, card slot 9 is respectively arranged at left and right sides of 1 bottom of shell, 9 inside clamping of card slot is equipped with card
Block 10,10 bottom of fixture block are provided with magnet 1, and pillar 12 is set to one 11 lower section of magnet, and 12 top of pillar is provided with magnet two
13,12 outside of pillar is provided with block 14, and fixture block 10 is fixedly connected with block 14 by damping spring 15, the setting of 12 bottom end of pillar
There are support plate 16, controller 8 to be electrically connected respectively with vibrating sensor 7 and air pump 4.
Specifically, ventilation duct 6 is extended to through shell 1 outside shell 1, pillar 12 is located at immediately below magnet 1, magnet
One 11 is identical as the magnetic pole of magnet 2 13, and damping spring 15 is respectively sleeved at the outside of magnet 1 and magnet 2 13, pillar 12
It is rotatablely connected by shaft with support plate 16.
When the utility model is used, support plate 16 is positioned over to the position that will be put, due to pillar 12 and support plate 16
It is rotatablely connected by shaft, therefore the adjustable angle of support plate 16 so that the support plate 16 after angle adjustment can adapt in a variety of
Rugged plane, to expand the use scope of device；When being influenced by extraneous shaking force, damping spring 15
Effective damping can be carried out to the present apparatus, reduce extraneous vibratory forces vibration effect caused by device, and due to magnet one
11 magnetic pole is identical as the magnetic pole of magnet 2 13, therefore two magnet are mutually exclusive, further enhance damping dynamics, reduce simultaneously
The compression degree of damping spring 15 has protective effect to damping spring 15, extends the usage time of damping spring 15；By
It is mounted in card slot 9 in the clamping of fixture block 10, therefore facilitates dismounting and change of the maintenance personal to damping spring 15；Work as vibrating sensor
7 when detecting that vibratory forces reach 8 pre-set value of controller, and controller 8 controls air pump 4 by gas-guide tube 5 to air damping
Air is blasted inside device 3 so that air bump 3 expands, to play anti-vibration protected well arrange to internal electronic component
It applies, ensure that the normal operation of the present apparatus, the setting of vibrating sensor 7 make the present apparatus have intelligent anti-vibration protected measure,
Protection efficiency is improved, the setting of ventilation duct 6 ensure that the normal operation of air pump 4.
The utility model is easily installed and dismantles, and regulatory function can be adapted for a variety of rugged planes, is applicable in
Range is wide and easy to use, and the shock-absorbing protecting measure with high intensity, intelligence degree is high, has very strong practicability.
Above example is only to illustrate the technical solution of the utility model, rather than its limitations；Although with reference to aforementioned reality
Example is applied the utility model is described in detail, it will be understood by those of ordinary skill in the art that：It still can be to preceding
The technical solution recorded in each embodiment is stated to modify or equivalent replacement of some of the technical features；And these
Modification or replacement, the spirit and model of various embodiments of the utility model technical solution that it does not separate the essence of the corresponding technical solution
It encloses.
Claims (5)
1. a kind of satellite communication terminal with shock-absorbing function, it is characterised in that：Including shell (1), electronic component (2), sky
Gas damper (3), air pump (4), gas-guide tube (5), ventilation duct (6), vibrating sensor (7), controller (8), card slot (9), fixture block
(10), magnet one (11), pillar (12), magnet two (13), block (14), damping spring (15) and support plate (16), it is described outer
It is provided with the electronic component (2) at shell (1) center of inside, the surrounding of the electronic component (2) is respectively arranged with described
Air bump (3), the both ends of the air bump (3) respectively with the electronic component (2) and the shell (1) inner wall
It is fixedly connected, the air pump (4) is set to the shell (1) internal left end bottom, is respectively arranged on the air pump (4) described
Gas-guide tube (5) and the ventilation duct (6), the gas-guide tube (5) is connected with each air bump (3) respectively, described
Vibrating sensor (7) is respectively arranged at the controller (8) in the shell (1) internal side wall, and shell (1) bottom is left
Right both sides are respectively arranged with the card slot (9), are clamped inside the card slot (9) and are equipped with the fixture block (10), the fixture block
(10) bottom is provided with the magnet one (11), and the pillar (12) is set to below the magnet one (11), the pillar
(12) top is provided with the magnet two (13), and the block (14), the fixture block (10) are provided on the outside of the pillar (12)
It is fixedly connected by the damping spring (15) with the block (14), pillar (12) bottom end is provided with the support plate
(16), the controller (8) is electrically connected with the vibrating sensor (7) and the air pump (4) respectively.
2. the satellite communication terminal according to claim 1 with shock-absorbing function, it is characterised in that：The ventilation duct (6)
It is external that shell (1) is extended to through the shell (1).
3. the satellite communication terminal according to claim 1 with shock-absorbing function, it is characterised in that：Pillar (12) position
Immediately below the magnet one (11), the magnet one (11) is identical as the magnetic pole of the magnet two (13).
4. the satellite communication terminal according to claim 1 with shock-absorbing function, it is characterised in that：The damping spring
(15) it is respectively sleeved at the outside of the magnet one (11) and the magnet two (13).
5. the satellite communication terminal according to claim 1 with shock-absorbing function, it is characterised in that：The pillar (12) with
The support plate (16) is rotatablely connected by shaft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820180729.5U CN207819918U (en) | 2018-02-01 | 2018-02-01 | A kind of satellite communication terminal with shock-absorbing function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820180729.5U CN207819918U (en) | 2018-02-01 | 2018-02-01 | A kind of satellite communication terminal with shock-absorbing function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207819918U true CN207819918U (en) | 2018-09-04 |
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ID=63323048
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820180729.5U Active CN207819918U (en) | 2018-02-01 | 2018-02-01 | A kind of satellite communication terminal with shock-absorbing function |
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| CN (1) | CN207819918U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109185608A (en) * | 2018-10-29 | 2019-01-11 | 合肥鸿坤通信工程有限公司 | A kind of onboard satellite communication equipment shock-proof machine frame |
| CN109673118A (en) * | 2018-12-29 | 2019-04-23 | 深圳航星光网空间技术有限公司 | A kind of damping |
| CN109969097A (en) * | 2019-03-12 | 2019-07-05 | 广州小马智行科技有限公司 | Pilotless automobile camera mould group shock-damping structure and automobile |
-
2018
- 2018-02-01 CN CN201820180729.5U patent/CN207819918U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109185608A (en) * | 2018-10-29 | 2019-01-11 | 合肥鸿坤通信工程有限公司 | A kind of onboard satellite communication equipment shock-proof machine frame |
| CN109185608B (en) * | 2018-10-29 | 2020-08-04 | 温州瑞景通科技有限公司 | Shock absorption rack of airborne satellite communication equipment |
| CN109673118A (en) * | 2018-12-29 | 2019-04-23 | 深圳航星光网空间技术有限公司 | A kind of damping |
| CN109969097A (en) * | 2019-03-12 | 2019-07-05 | 广州小马智行科技有限公司 | Pilotless automobile camera mould group shock-damping structure and automobile |
| CN109969097B (en) * | 2019-03-12 | 2024-05-31 | 北京小马慧行科技有限公司 | Unmanned automobile camera module damping structure and automobile |
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