CN204669539U - A kind of airborne communication terminal - Google Patents
A kind of airborne communication terminal Download PDFInfo
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- CN204669539U CN204669539U CN201520393559.5U CN201520393559U CN204669539U CN 204669539 U CN204669539 U CN 204669539U CN 201520393559 U CN201520393559 U CN 201520393559U CN 204669539 U CN204669539 U CN 204669539U
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- 238000004891 communication Methods 0.000 title claims abstract description 87
- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical group C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 claims description 3
- 230000005540 biological transmission Effects 0.000 abstract description 7
- 238000007596 consolidation process Methods 0.000 description 1
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- 238000007689 inspection Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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Abstract
The utility model discloses a kind of airborne communication terminal, comprising: codec, satellite communication equipment, microwave transport equipment, Wireless Telecom Equipment and control appliance; The data input pin of codec is connected with the output of image capture device; The data input pin of the data input pin of satellite communication equipment, the data input pin of microwave transport equipment and Wireless Telecom Equipment is all connected with the data output end of codec; Control appliance is connected with the control end of satellite communication equipment, microwave transport equipment and Wireless Telecom Equipment respectively, and control appliance is also connected with the data output end of codec.Disclosed in the utility model, airborne communication terminal has multiple communication equipment, thus improves the available network bandwidth between helicopter and director, when helicopter need take the data compared with large bandwidth to director transmission, can improve the stability of transfer of data.
Description
Technical field
The utility model belongs to communication technical field, particularly relates to a kind of airborne communication terminal.
Background technology
Current helicopter has been widely used in disaster assistance and daily inspection.Be provided with image capture device in helicopter, utilize image capture device to gather ground image, afterwards image is sent to director, staff analyzes the image that helicopter transmits at director, to determine whether to occur extremely.
Present helicopter adopts satellite communication link to communicate with between director usually, but the bandwidth of satellite communication link is less, transfer of data is also unstable, and the data volume of view data is larger, this causes helicopter to there is unstable problem to the process of director transmit image data, cannot meet the data transfer demands of helicopter.
Utility model content
In view of this, the purpose of this utility model is to provide a kind of airborne communication terminal, improves the stability of helicopter to director transmit image data.
For achieving the above object, the utility model provides following technical scheme:
A kind of airborne communication terminal, described airborne communication terminal applies is in helicopter, and described helicopter is provided with image capture device, and described airborne communication terminal comprises: codec, satellite communication equipment, microwave transport equipment, Wireless Telecom Equipment and control appliance;
The data input pin of described codec is connected with the output of described image capture device;
The data input pin of described satellite communication equipment is connected with the data output end of described codec;
The data input pin of described microwave transport equipment is connected with the data output end of described codec;
The data input pin of described Wireless Telecom Equipment is connected with the data output end of described codec;
Described control appliance is connected with the control end of described satellite communication equipment, described microwave transport equipment and described Wireless Telecom Equipment respectively, and described control appliance is also connected with the data output end of described codec.
Optionally, described helicopter is also provided with audio collecting device, and in above-mentioned airborne communication terminal, the data input pin of described codec is connected with the output of described audio collecting device.
Optionally, described helicopter is also provided with operating terminal, and in above-mentioned airborne communication terminal, described helicopter is also provided with operating terminal, and described control appliance is also connected with described operating terminal.
Optionally, above-mentioned airborne communication terminal also comprises a memory device, and described memory device is connected with described control appliance.
Optionally, in above-mentioned airborne communication terminal, described microwave transport equipment is two-way microwave transport equipment.
Optionally, in above-mentioned airborne communication terminal, described Wireless Telecom Equipment is 3G (Third Generation) Moblie Wireless Telecom Equipment.
Optionally, in above-mentioned airborne communication terminal, described satellite communication equipment is Big Dipper two-way satellite device.
Optionally, in above-mentioned airborne communication terminal, described airborne communication terminal also comprises a cabinet, and described codec, described satellite communication equipment, described microwave transport equipment, described Wireless Telecom Equipment, described control appliance and described memory device are all fixed in described cabinet.
As can be seen here, disclosed in the utility model, airborne communication terminal has multiple communication equipment, be respectively satellite communication equipment, microwave transport equipment and Wireless Telecom Equipment, thus the available network bandwidth improved between helicopter and director, when helicopter need take data (as the view data) compared with large bandwidth to director transmission, the stability of transfer of data can be improved.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiment of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to the accompanying drawing provided.
The structural representation of Fig. 1 a kind of airborne communication terminal disclosed in the utility model;
The structural representation of Fig. 2 another kind of airborne communication terminal disclosed in the utility model;
The structural representation of Fig. 3 another kind of airborne communication terminal disclosed in the utility model.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
The utility model discloses a kind of airborne communication terminal, and this airborne communication terminal applies is in helicopter.Utilize this airborne communication terminal, the stability of helicopter to director transmit image data can be improved.
See the structural representation of Fig. 1, Fig. 1 a kind of airborne communication terminal disclosed in the utility model.This airborne communication terminal comprises codec 1, satellite communication equipment 2, microwave transport equipment 3, Wireless Telecom Equipment 4 and control appliance 5.
Wherein:
The data input pin of codec 1 is connected with the output of image capture device in helicopter 001.Codec 1 carries out coded treatment for the image exported image capture device 001, thus improves the fail safe of image.
The data input pin of satellite communication equipment 2 is connected with the data output end of codec 1.Satellite communication equipment 2 after receiving the data, utilizes satellite to complete transfer of data, and its communication range is large, and be not subject to the impact of Land disaster, reliability is high.
The data input pin of microwave transport equipment 3 is connected with the data output end of codec 1.Microwave transport equipment 3 has high, the adaptable advantage of flexibility but its transmission range is shorter.
The data input pin of Wireless Telecom Equipment 4 is connected with the data output end of codec 1.Wireless Telecom Equipment 4 utilizes existing communication network to realize transfer of data.
Control appliance 5 is connected with the control end of satellite communication equipment 2, microwave transport equipment 3 and Wireless Telecom Equipment 4 respectively, and control appliance 5 is also connected with the data output end of codec 1.
Because airborne communication terminal is provided with multiple communication equipment, the available bandwidth therefore between helicopter and director obtains very large lifting.When helicopter needs to director transmission data, control appliance 5 can select wherein one or more to carry out transfer of data in satellite communication equipment 2, microwave transport equipment 3 and Wireless Telecom Equipment 4.
Disclosed in the utility model, airborne communication terminal has multiple communication equipment, be respectively satellite communication equipment, microwave transport equipment and Wireless Telecom Equipment, thus the available network bandwidth improved between helicopter and director, when helicopter need take data (as the view data) compared with large bandwidth to director transmission, the stability of transfer of data can be improved.
In concrete enforcement, when helicopter is also provided with audio collecting device 002 (as microphone), preferably, the output of the data input pin of codec 1 with audio collecting device 002 is connected, as shown in Figure 2.That is, codec 1 both can carry out coded treatment to the image that image capture device 001 exports, and also can carry out coded treatment to the audio frequency having audio collecting device 002 to export, be transmitted afterwards by one or more communication equipment to director.
In addition, when helicopter is also provided with operating terminal 003, preferably, control appliance 5 is connected with operating terminal 003, as shown in Figure 2.Control appliance 5 can communicate with operating terminal 003.
As a kind of preferred version, can also arrange memory device in any one airborne communication terminal above-mentioned, this memory device is connected with control appliance 5.Here composition graphs 3 is described.
See the structural representation of Fig. 3, Fig. 3 another kind of airborne communication terminal disclosed in the utility model.This airborne communication terminal comprises codec 1, satellite communication equipment 2, microwave transport equipment 3, Wireless Telecom Equipment 4, control appliance 5 and memory device 6.
Wherein:
The data input pin of codec 1 is connected with the output of image capture device 001 and audio collecting device 002 respectively.The image that codec 1 pair of image capture device 001 exports and the audio frequency that audio collecting device 002 exports carry out coded treatment.
The data input pin of satellite communication equipment 2 is connected with the data output end of codec 1.The data input pin of microwave transport equipment 3 is connected with the data output end of codec 1.The data input pin of Wireless Telecom Equipment 4 is connected with the data output end of codec 1.
Control appliance 5 is connected with the control end of satellite communication equipment 2, microwave transport equipment 3 and Wireless Telecom Equipment 4 respectively, and control appliance 5 is also connected with the data output end of codec 1, operating terminal 003 and memory device 6.
In embody rule, when helicopter needs to director transmission data, control appliance 5 can calculate the network bandwidth required for data to be transmitted, afterwards according to the real-time available bandwidth of each communication equipment, selects wherein one or more communication equipments to carry out transfer of data.
Such as: (comprise video data and other business datums when needs send data by airborne communication terminal to director, business datum comprises text data) time, determine the network bandwidth required for data to be sent, determine the real-time available bandwidth of satellite communication equipment 2, microwave transport equipment 3 and Wireless Telecom Equipment 4 simultaneously.If the real-time available bandwidth of microwave transport equipment 3 is higher, then transmit data by microwave transport equipment 3 to director.If the real-time available bandwidth of Wireless Telecom Equipment 4 is higher, then transmit data by Wireless Telecom Equipment 4 to director.If the real-time available bandwidth of each communication equipment is all less, be not enough to transmitting video data, then by satellite communication equipment 2 service data transmission, video data be stored to memory device 6, resend video data when the available bandwidth of communication equipment is higher.
In the above-mentioned disclosed airborne communication terminal of the utility model, microwave transport equipment 3 preferably adopts two-way microwave transport equipment, Wireless Telecom Equipment 4 preferably adopts 3G (3G (Third Generation) Moblie) Wireless Telecom Equipment, and satellite communication equipment 5 preferably adopts Big Dipper two-way satellite device.
In addition, on the basis of the above-mentioned disclosed airborne communication terminal of the utility model, can also arrange cabinet further, codec 1, satellite communication equipment 2, microwave transport equipment 3, Wireless Telecom Equipment 4, control appliance 5 and memory device 6 are all fixed in cabinet.Can reduce on the one hand to take up an area space, also be convenient to carry out consolidation process to each equipment on the other hand.
In this specification, each embodiment adopts the mode of going forward one by one to describe, and what each embodiment stressed is the difference with other embodiments, between each embodiment identical similar portion mutually see.
To the above-mentioned explanation of the disclosed embodiments, professional and technical personnel in the field are realized or uses the utility model.To be apparent for those skilled in the art to the multiple amendment of these embodiments, General Principle as defined herein when not departing from spirit or scope of the present utility model, can realize in other embodiments.Therefore, the utility model can not be restricted to these embodiments shown in this article, but will meet the widest scope consistent with principle disclosed herein and features of novelty.
Claims (8)
1. an airborne communication terminal, described airborne communication terminal applies is in helicopter, described helicopter is provided with image capture device, it is characterized in that, described airborne communication terminal comprises: codec, satellite communication equipment, microwave transport equipment, Wireless Telecom Equipment and control appliance;
The data input pin of described codec is connected with the output of described image capture device;
The data input pin of described satellite communication equipment is connected with the data output end of described codec;
The data input pin of described microwave transport equipment is connected with the data output end of described codec;
The data input pin of described Wireless Telecom Equipment is connected with the data output end of described codec;
Described control appliance is connected with the control end of described satellite communication equipment, described microwave transport equipment and described Wireless Telecom Equipment respectively, and described control appliance is also connected with the data output end of described codec.
2. airborne communication terminal according to claim 1, is characterized in that, described helicopter is also provided with audio collecting device, and the data input pin of described codec is connected with the output of described audio collecting device.
3. airborne communication terminal according to claim 1 and 2, is characterized in that, described helicopter is also provided with operating terminal, and described control appliance is also connected with described operating terminal.
4. airborne communication terminal according to claim 3, is characterized in that, described airborne communication terminal also comprises a memory device, and described memory device is connected with described control appliance.
5. the airborne communication terminal according to claim 1,2 or 4, is characterized in that, described microwave transport equipment is two-way microwave transport equipment.
6. the airborne communication terminal according to claim 1,2 or 4, is characterized in that, described Wireless Telecom Equipment is 3G (Third Generation) Moblie Wireless Telecom Equipment.
7. the airborne communication terminal according to claim 1,2 or 4, is characterized in that, described satellite communication equipment is Big Dipper two-way satellite device.
8. airborne communication terminal according to claim 4, it is characterized in that, described airborne communication terminal also comprises a cabinet, and described codec, described satellite communication equipment, described microwave transport equipment, described Wireless Telecom Equipment, described control appliance and described memory device are all fixed in described cabinet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520393559.5U CN204669539U (en) | 2015-06-09 | 2015-06-09 | A kind of airborne communication terminal |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520393559.5U CN204669539U (en) | 2015-06-09 | 2015-06-09 | A kind of airborne communication terminal |
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| Publication Number | Publication Date |
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| CN204669539U true CN204669539U (en) | 2015-09-23 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201520393559.5U Expired - Fee Related CN204669539U (en) | 2015-06-09 | 2015-06-09 | A kind of airborne communication terminal |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105511489A (en) * | 2015-12-07 | 2016-04-20 | 中国电子科技集团公司第十研究所 | Multi-aircraft configuration terminal capable of being quickly accessed to Big Dipper constellation phased-array inter-satellite link |
| CN108234049A (en) * | 2017-12-18 | 2018-06-29 | 深圳市华讯方舟空间信息产业科技有限公司 | Terminal communicating method, device, storage medium and computer equipment |
-
2015
- 2015-06-09 CN CN201520393559.5U patent/CN204669539U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105511489A (en) * | 2015-12-07 | 2016-04-20 | 中国电子科技集团公司第十研究所 | Multi-aircraft configuration terminal capable of being quickly accessed to Big Dipper constellation phased-array inter-satellite link |
| CN105511489B (en) * | 2015-12-07 | 2018-05-22 | 中国电子科技集团公司第十研究所 | Quickly access the multi-aircraft configurating terminal of Big Dipper constellation phased array inter-satellite link |
| CN108234049A (en) * | 2017-12-18 | 2018-06-29 | 深圳市华讯方舟空间信息产业科技有限公司 | Terminal communicating method, device, storage medium and computer equipment |
| CN108234049B (en) * | 2017-12-18 | 2019-03-12 | 深圳市华讯方舟卫星产业科技有限公司 | Terminal communicating method, device, storage medium and computer equipment |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150923 Termination date: 20170609 |
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| CF01 | Termination of patent right due to non-payment of annual fee |