CN104125004A - Satellite communication box - Google Patents
Satellite communication box Download PDFInfo
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- CN104125004A CN104125004A CN201410317918.9A CN201410317918A CN104125004A CN 104125004 A CN104125004 A CN 104125004A CN 201410317918 A CN201410317918 A CN 201410317918A CN 104125004 A CN104125004 A CN 104125004A
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- module
- satellite communication
- heater
- usb interface
- satellite
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Abstract
The invention discloses a satellite communication box. The satellite communication box comprises a box body, a power supply module, a satellite communication module, a GPS positioning module, a USB interface, a camera shooting module, a display module, a switchover module, an illumination module, a temperature control module, a heater and a temperature inductor, wherein the temperature inductor and the heater are arranged on the satellite communication module; the satellite module communicates with the outside through a satellite link; the temperature control module is used for controlling the heater to heat the satellite communication module when a temperature is lower than a set threshold value; the switchover module is used for switching information in the camera shooting module, the satellite communication module and the equipment connected through the USB interface in the display module. The satellite communication box disclosed by the invention is capable of intuitively sending various kinds of information out, and guaranteeing normal working in a low-temperature condition.
Description
Technical field
The present invention relates to satellite communication field, relate in particular to a kind of satellite communication case.
Background technology
Satellite communication be exactly briefly between the radio communication station that (comprises that ground is with in lower atmosphere layer) on the earth, utilize satellite as in then carry out communicate by letter.Satellite communication system is made up of satellite and earth station two parts.The feature of satellite communication is that communication range is large; As long as in the scope covering at the electric wave of satellite launch, all can communicate between any 2; Be not subject to the impact (reliability is high) of Land disaster; As long as being set, earth station circuit can open (opening circuit rapid); Can receive in many places, can realize economically broadcast, multiple access communication (multiple access feature) simultaneously; Circuit arranges very flexible, can disperse at any time the telephone traffic of too concentrating; Same channel can be used for different directions or different interval (multiple access).
Satellite communication case can produce very large effect in running into emergency, especially in snow disaster, big flood, earthquake, can rapidly the situation at the condition of a disaster scene be passed, make outside command centre grasp rapidly situation, make correct deployment.
Existing satellite communication case often, still by audio communication, can not reflect situation intuitively, and meanwhile, in some severe cold areas, serious low temperature environment has affected the application of satellite communication significantly.
Summary of the invention
Technical problem to be solved by this invention is the defect for background technology, and a kind of satellite communication case is provided, and can under low temperature environment, normally use, and can reflect intuitively field condition.
The present invention is for solving the problems of the technologies described above by the following technical solutions:
A kind of satellite communication case, comprises casing, power module, satellite communication module, GPS locating module, USB interface, photographing module, display module, handover module, lighting module, temperature control modules, heater and temperature inductor, wherein:
Described power module, satellite communication module, GPS locating module, USB interface, photographing module, display module, handover module, lighting module, temperature control modules, heater, temperature inductor are all arranged in described casing, and described temperature inductor and heater are arranged on satellite communication module;
Described power module is connected with satellite communication module, GPS locating module, USB interface, photographing module, display module, handover module, lighting module, temperature control modules, heater, temperature inductor respectively, described satellite communication module respectively GPS locating module, USB interface, photographing module is connected, described handover module is connected with USB interface, photographing module, display module, satellite communication module respectively, and described temperature control modules is connected with heater, temperature inductor respectively;
Described satellite modules via satellite link is communicated by letter with extraneous;
Described temperature control modules temperature during lower than setting threshold control heater heat to satellite communication module;
Described handover module is for the data in the equipment that switches the data that show photographing module and take, data that satellite communication module receives and USB interface at described display module and connect.
As the further prioritization scheme of a kind of satellite communication case of the present invention, described power module adopts rechargeable battery.
As the further prioritization scheme of a kind of satellite communication case of the present invention, the outer surface of described casing is also provided with solar panels, and described solar panels are connected with described rechargeable battery.
The ambient temperature of temperature inductor induction satellite communication module, in the time that ambient temperature is less than the threshold value of setting, temperature control modules control heater heats satellite communication module, guarantees that it can work under cryogenic conditions.
Photographing module is used for directly taking, and user can be switched by handover module, the data in the equipment that the information that makes display module show photographing module to take, the information that satellite communication module receives or USB interface connect.
GPS locating module by the position of communication box via satellite communication module launch, make extraneous command centre grasp rapidly accident spot.
The present invention adopts above technical scheme compared with prior art, has following technique effect:
1. guarantee that communication box can normally use at low temperatures;
2. can pass through solar recharging, improve the flying power under mal-condition;
3. can intuitively various information be passed.
Brief description of the drawings
Fig. 1 is structural representation of the present invention.
Embodiment
Below in conjunction with accompanying drawing, technical scheme of the present invention is described in further detail:
As shown in Figure 1, the invention discloses a kind of satellite communication case, comprise casing, power module, satellite communication module, GPS locating module, USB interface, photographing module, display module, handover module, lighting module, temperature control modules, heater and temperature inductor, wherein:
Described power module, satellite communication module, GPS locating module, USB interface, photographing module, display module, handover module, lighting module, temperature control modules, heater, temperature inductor are all arranged in described casing, and described temperature inductor and heater are arranged on satellite communication module;
Described power module is connected with satellite communication module, GPS locating module, USB interface, photographing module, display module, handover module, lighting module, temperature control modules, heater, temperature inductor respectively, described satellite communication module respectively GPS locating module, USB interface, photographing module is connected, described handover module is connected with USB interface, photographing module, display module, satellite communication module respectively, and described temperature control modules is connected with heater, temperature inductor respectively;
Described satellite modules via satellite link is communicated by letter with extraneous;
Described temperature control modules temperature during lower than setting threshold control heater heat to satellite communication module;
Described handover module is for the data in the equipment that switches the data that show photographing module and take, data that satellite communication module receives and USB interface at described display module and connect.
Described power module adopts rechargeable battery.
The outer surface of described casing is also provided with solar panels, and described solar panels are connected with described rechargeable battery.
The ambient temperature of temperature inductor induction satellite communication module, in the time that ambient temperature is less than the threshold value of setting, temperature control modules control heater heats satellite communication module, guarantees that it can work under cryogenic conditions.
Photographing module is used for directly taking, and user can be switched by handover module, the data in the equipment that the information that makes display module show photographing module to take, the information that satellite communication module receives or USB interface connect.
GPS locating module by the position of communication box via satellite communication module launch, make extraneous command centre grasp rapidly accident spot.
Above-described embodiment; object of the present invention, technical scheme and beneficial effect are further described; institute is understood that; the foregoing is only the specific embodiment of the present invention; be not limited to the present invention; within the spirit and principles in the present invention all, any amendment of making, be equal to replacement, improvement etc., within all should being included in protection scope of the present invention.
Claims (3)
1. a satellite communication case, it is characterized in that, comprise casing, power module, satellite communication module, GPS locating module, USB interface, photographing module, display module, handover module, lighting module, temperature control modules, heater and temperature inductor, wherein:
Described power module, satellite communication module, GPS locating module, USB interface, photographing module, display module, handover module, lighting module, temperature control modules, heater, temperature inductor are all arranged in described casing, and described temperature inductor and heater are arranged on satellite communication module;
Described power module is connected with satellite communication module, GPS locating module, USB interface, photographing module, display module, handover module, lighting module, temperature control modules, heater, temperature inductor respectively, described satellite communication module respectively GPS locating module, USB interface, photographing module is connected, described handover module is connected with USB interface, photographing module, display module, satellite communication module respectively, and described temperature control modules is connected with heater, temperature inductor respectively;
Described satellite modules via satellite link is communicated by letter with extraneous;
Described temperature control modules temperature during lower than setting threshold control heater heat to satellite communication module;
Described handover module is for the data in the equipment that switches the data that show photographing module and take, data that satellite communication module receives and USB interface at described display module and connect.
2. satellite communication case according to claim 1, is characterized in that, described power module adopts rechargeable battery.
3. satellite communication case according to claim 2, is characterized in that, the outer surface of described casing is also provided with solar panels, and described solar panels are connected with described rechargeable battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410317918.9A CN104125004A (en) | 2014-07-07 | 2014-07-07 | Satellite communication box |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410317918.9A CN104125004A (en) | 2014-07-07 | 2014-07-07 | Satellite communication box |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104125004A true CN104125004A (en) | 2014-10-29 |
Family
ID=51770280
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410317918.9A Pending CN104125004A (en) | 2014-07-07 | 2014-07-07 | Satellite communication box |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104125004A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102092481A (en) * | 2009-12-11 | 2011-06-15 | 上海卫星工程研究所 | Blocking device for loop heat pipe of satellite borne equipment |
| CN201893777U (en) * | 2010-12-06 | 2011-07-06 | 北京中交通信科技有限公司 | Emergency satellite communication box |
| CN203136414U (en) * | 2013-01-24 | 2013-08-14 | 南京中网卫星通信股份有限公司 | Outdoor satellite communication cabinet |
| CN103448925A (en) * | 2013-08-08 | 2013-12-18 | 上海卫星工程研究所 | High-precision temperature control device for star sensors for satellites |
| CN203951473U (en) * | 2014-07-07 | 2014-11-19 | 江苏中寰卫星导航通信有限公司 | A kind of satellite communication case |
-
2014
- 2014-07-07 CN CN201410317918.9A patent/CN104125004A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102092481A (en) * | 2009-12-11 | 2011-06-15 | 上海卫星工程研究所 | Blocking device for loop heat pipe of satellite borne equipment |
| CN201893777U (en) * | 2010-12-06 | 2011-07-06 | 北京中交通信科技有限公司 | Emergency satellite communication box |
| CN203136414U (en) * | 2013-01-24 | 2013-08-14 | 南京中网卫星通信股份有限公司 | Outdoor satellite communication cabinet |
| CN103448925A (en) * | 2013-08-08 | 2013-12-18 | 上海卫星工程研究所 | High-precision temperature control device for star sensors for satellites |
| CN203951473U (en) * | 2014-07-07 | 2014-11-19 | 江苏中寰卫星导航通信有限公司 | A kind of satellite communication case |
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20141029 |
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| WD01 | Invention patent application deemed withdrawn after publication |