CN202501922U - Flight thermal imager system - Google Patents
Flight thermal imager system Download PDFInfo
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- CN202501922U CN202501922U CN2011205762499U CN201120576249U CN202501922U CN 202501922 U CN202501922 U CN 202501922U CN 2011205762499 U CN2011205762499 U CN 2011205762499U CN 201120576249 U CN201120576249 U CN 201120576249U CN 202501922 U CN202501922 U CN 202501922U
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Abstract
The utility model discloses a flight thermal imager system. The flight thermal imager system comprises a thermal infrared imager arranged on an aircraft. The system further comprises: a signal acquisition and processing unit, which is arranged on the thermal infrared imager and used for acquiring image signals by taking an infrared chart of a monitored object and converting the image signals into communication signals; a communication signal transmission unit, which is used for receiving the communication signals from the signal acquisition and processing unit and sending the communication signals out through a communication channel, and used for receiving communication signals from the outside and sending the communication signals to the thermal infrared imager; and an airborne satellite communication device, which is used for transmitting the communication signals to an international communication satellite through a satellite antenna, and used for receiving communication signals from the international communication satellite and transmitting the communication signals to the communication signal transmission unit. The flight thermal imager system of the utility model can be connected with the international communication satellite, a ground base station or a ground network, and a server system in a ground control center through the airborne satellite communication device, so real-time communication between the thermal infrared imager in the air and the ground control center is realized.
Description
Technical field
The utility model relates to a kind of thermal infrared imager, especially relates to a kind of thermal infrared imager that is used for the high-altitude flight monitoring.
Background technology
Thermal infrared imager has been widely used in fields of society.Traditional thermal imaging system is a kind of handheld device mostly, needs staff's handheld device to operate, with collection and the processing of carrying out associated picture information.Generally speaking; The thermal imaging system that is used for monitoring equipment must link to each other with control system through wired or short-range wireless communication apparatus; The staff comes that through control system thermal imaging system is carried out index and limits and shooting operation, and obtains infrared chart or the infrared video data that thermal imaging system is taken through communication facilities.Wherein, existing radio communication mainly is to carry out short haul connection with thermal imaging system, for example can carry out the exchange of data through bluetooth and thermal infrared imager.
Yet, for some industry, commerce or civil area, be starved of the comprehensive monitoring of implementing monitoring target sometimes aloft.For example when carrying out forest fire protection early warning, forest fire rescue, perhaps when large-area farmland operation and hydraulic and electric engineering facility are monitored, may use investigation with small aircraft, sprinkle water or airborne aircraft such as cropduster in the air.Be not difficult to imagine; If on these aircraft, thermal infrared imager has been installed; Just can take infrared chart or infrared video information to the panorama or the regional area in forest that needs monitoring and farmland etc.; And through the ground control centre captured infrared chart of thermal infrared imager or infrared video information are carried out real-time collecting and in time analyze, this decision-making and enforcement as far as whole monitoring and later stage counter-measure all can be highly beneficial.
But up to now; To how thermal infrared imager being installed in flyer and the image information that thermal infrared imager collects being real-time transmitted to this one side of ground control centre, still the end has design proposal and the product relevant with long distance, wireless (high-altitude) communication technology of the thermal infrared imager that is used for work high above the ground to come out.
Summary of the invention
For overcoming the defective of prior art; The utility model proposes a kind of flight thermal imaging system system; This flight thermal imaging system system links to each other with International Telecommunication Satellite, ground base station and communication network through airborne satellite communication apparatus; Infrared chart or video information that thermal infrared imager is taken convert signal of communication into and are real-time transmitted to the ground control centre; Simultaneously will be from the real-time Transmission such as control signal of ground control centre to this flight thermal imaging system system, thus realize the real-time Communication for Power of aerial thermal infrared imager and ground control centre, be beneficial to the large tracts of land of monitoring target is monitored and the high-speed decision and the enforcement of later stage counter-measure in real time.
Particularly; This flight thermal imaging system system is in order to realize such goal of the invention: the data that adopt infrared eye processing of circuit module to gather infrared image signal; The view data that collects is wirelessly transmitted to airborne satellite communication equipment through the GSM/GPRS module transmits behind compressed encoding, or realize getting online without being tethered to a cable via the Wi-Fi network to communicate signals such as signal or multimedia messages via ground base station.The signal of communication of receiving and sending messages and surfing the Net all can be transferred to International Telecommunication Satellite through airborne satellite communication equipment earlier; International Telecommunication Satellite is connected with ground base station or ground network again; The server system of ground control centre obtains corresponding infrared image signal data further handling from ground base station or ground network, and with control signal etc. through the thermal infrared imager in above-mentioned communications facility and communication network reverse transfer to this flight thermal imaging system system.
For realizing above-mentioned purpose; A kind of flight thermal imaging system system of the utility model comprises and is arranged on carry-on thermal infrared imager; This system also comprises: the signal acquisition process unit; Be arranged on this thermal infrared imager, the infrared chart through the shooting and monitoring object obtains picture signal and is converted into signal of communication; The signal of communication transmission unit; Be arranged on this aircraft and and be connected with this signal acquisition process unit; This signal of communication transmission unit receives and sends through communication port from the signal of communication of signal acquisition process unit and with it, and receives from the signal of communication of outside and send it to this thermal infrared imager; And airborne satellite communication equipment; Be arranged on this aircraft and and communicate by letter with International Telecommunication Satellite with this signal of communication transmission unit; This airborne satellite communication equipment will from the said signal of communication of this signal of communication transmission unit via satellite antenna be emitted to this International Telecommunication Satellite, and receive from the signal of communication of this International Telecommunication Satellite and transmit it to this signal of communication transmission unit.
Embodiment according to the utility model; This signal acquisition process unit comprises: image capture module; Comprise optical lens and coupled infrared eye circuit; This optical lens collection from this detected object infrared radiation signal taking the infrared chart of this monitoring target, this infrared eye circuit collection through this optical lens incident infrared radiation signal and be converted into electric signal, to export as picture signal; Image processing module is connected with the infrared eye circuit of this image capture module, and this image processing module receives said picture signal and is binary code stream with its processed compressed, to export as digital signal; And CPU control module; Be connected with this signal of communication transmission unit with this image processing module; This CPU control module receives said digital signal and stores said digital signal with document form; Is signal of communication according to communication interface standard with institute's stored numbers conversion of signals, through driving and controlling this signal of communication transmission unit said signal of communication is sent to this airborne satellite communication equipment via communication network.
Embodiment according to the utility model; This signal of communication transmission unit comprises: the GSM/GPRS module; Adopt GPRS network to communicate the signal transmission via the GPRS passage; Or adopt short message way to communicate the signal transmission via the SMS passage; This GSM/GPRS module comprises: standard RS232 bidirectional interface, be connected with this signal acquisition process unit, and this standard RS232 bidirectional interface receives said signal of communication and will be sent to this signal acquisition process unit from the signal of communication of this airborne satellite communication equipment from this signal acquisition process unit; SIM is connected with this standard RS232 bidirectional interface, and this SIM has SMS and GPRS function, receive said signal of communication and communicate signal and multimedia messages between bi-directional conversion; And antenna; Be connected with this SIM and communicate by letter with this airborne satellite communication equipment; This antenna emission signal of communication or multimedia messages to this airborne satellite communication equipment are communicating via this International Telecommunication Satellite and ground base station, and reception is from the signal of communication or the multimedia messages of this airborne satellite communication equipment; And WIFI circuit module; Be connected with this signal acquisition process unit and communicate by letter with this airborne satellite communication equipment; This WIFI circuit module carries out the wireless access of WIFI network; Receive said signal of communication from this signal acquisition process unit and be sent to this airborne satellite communication equipment communicating, and will be sent to this signal acquisition process unit with WIFI wireless communication protocol form from the signal of communication of this airborne satellite communication equipment via this International Telecommunication Satellite and ground network with WIFI wireless communication protocol form.
Embodiment according to the utility model; This airborne satellite communication equipment comprises airborne mobile communications device, satellite communication assembly and the satellite antenna that connects successively; This airborne satellite communication equipment is emitted to this International Telecommunication Satellite communicating via this ground base station or ground network with said signal of communication through airborne satellite communication apparatus, and receives from the signal of communication of this International Telecommunication Satellite and transmit it to this signal of communication transmission unit through this satellite antenna.
According to the embodiment of the utility model, this airborne mobile communications device comprises the WIFI mixed-media network modules mixed-media, carries out the transmission of two-way communication signal or multimedia messages between this WIFI mixed-media network modules mixed-media and this WIFI circuit module.
Embodiment according to the utility model; This International Telecommunication Satellite transfers to said signal of communication through ground base station or ground network the server system of this thermal infrared imager; And transfer to this airborne satellite communication equipment via this ground base station or ground network and through this International Telecommunication Satellite from the signal of communication of this server system, wherein this server system is computing machine or the mobile phone that is connected on the communication network.
According to the embodiment of the utility model, this thermal infrared imager can be rotatably set on the fuselage of this aircraft through The Cloud Terrace, and this thermal infrared imager is provided with the transparent shroud of this thermal infrared imager of protection.
The flight thermal imaging system system of the utility model links to each other with International Telecommunication Satellite, ground base station or ground network through airborne satellite communication apparatus; Thereby can the data-signal relevant with infrared chart or video information that thermal infrared imager is taken be real-time transmitted to the ground control centre; Simultaneously will be from the real-time Transmission such as control signal of ground control centre to this flight thermal imaging system system; Thereby realized the real-time Communication for Power of aerial thermal infrared imager and ground control centre, helped the large tracts of land monitoring in real time of monitoring target and the high-speed decision and the enforcement of later stage counter-measure.
Description of drawings
Fig. 1 is the principle of work synoptic diagram according to the flight thermal imaging system system of the embodiment of the utility model
Fig. 2 schematically shows the composition frame chart of flight thermal imaging system shown in Figure 1 system
Fig. 3 schematically shows the instance of the flight thermal imaging system system of the utility model
Fig. 4 is the FB(flow block) that illustrates according to the communication means of the flight thermal imaging system system of the embodiment of the utility model
Wherein, description of reference numerals is following:
The 1-thermal infrared imager
11-signal acquisition process unit
The 111-image capture module
The 112-image processing module
The 113-CPU control module
12-signal of communication transmission unit
The 121-GSM/GPRS module
The 122-WIFI circuit module
The airborne satellite communication equipment of 13-
131 airborne mobile communications devices
132-satellite communication assembly
The 133-satellite antenna
The 2-International Telecommunication Satellite
The 3-ground base station
3 '-ground network
The 4-server system
The 5-aircraft
The 50-aircraft fuselage
The 51-transparent shroud
The 52-The Cloud Terrace
Embodiment
For purpose, technical scheme and the advantage of the embodiment that makes the utility model are clearer,, the embodiment of the utility model is done explanation in further detail below in conjunction with embodiment and accompanying drawing.At this, illustrative examples of the utility model and explanation thereof only are used to explain the utility model, but not as the qualification to the utility model.
Be illustrated in figure 1 as an embodiment of the flight thermal imaging system system of the utility model.This flight thermal imaging system system comprises the thermal infrared imager 1 that is arranged on the aircraft 5.This system also can comprise: signal acquisition process unit 11, be arranged on this thermal infrared imager 1, and the infrared chart through the shooting and monitoring object obtains picture signal and is converted into signal of communication; Signal of communication transmission unit 12 receives and to send through communication port from the signal of communication of signal acquisition process unit 11 and with it, and receives from the signal of communication of outside and send it to this thermal infrared imager 1; And airborne satellite communication equipment 13; Will from the said signal of communication of signal of communication transmission unit 12 via satellite antenna be emitted to International Telecommunication Satellite 2, and receive from the signal of communication of this International Telecommunication Satellite 2 and transmit it to this signal of communication transmission unit 12.
Fig. 2 schematically shows the composition frame chart of flight thermal imaging system shown in Figure 1 system.
As shown in Figure 2; This signal acquisition process unit 11 can comprise: image capture module 111; Comprise optical lens and infrared eye circuit; To take the infrared chart of this monitoring target, this infrared eye circuit will convert electric signal into through the infrared radiation signal of this optical lens incident, to export as picture signal from this detected object infrared radiation signal in this optical lens collection; Image processing module 112 receives said picture signal and is binary code stream with its processed compressed, to export as digital signal; And CPU control module 113; Receive said digital signal and store said digital signal with document form; Is signal of communication according to communication interface standard with institute's stored numbers conversion of signals, through driving and controlling this signal of communication transmission unit 12 said signal of communication is sent to this airborne satellite communication equipment 13 via communication network.
Wherein infrared eye (Infrared Detector) is the device that the infrared radiation signal of incident is transformed into electric signal output.The infrared data that image capture module 111 collects is transferred to image processing module 112.Conversion and processed compressed that this image processing module 112 is accomplished picture signal, picture signal is changed and boil down to binary code stream (digital signal), and system adopts 113 pairs of these binary code streams of CPU control module to manage.
According to the embodiment of the utility model, this signal of communication transmission unit 12 can comprise: GSM/GPRS module 121, adopt GPRS network to communicate the signal transmission via the GPRS passage, or adopt short message way to communicate the signal transmission via the SMS passage; And WIFI circuit module 122, in order to carrying out the wireless access of WIFI network, and communicate with ground network 3 ' via airborne satellite communication equipment 13.
Wherein this GSM/GPRS module 121 can comprise: standard RS232 bidirectional interface, in order to two-way reception with send said signal of communication; SIM is connected with this standard RS232 bidirectional interface, and this SIM has SMS and GPRS function, in order to realize the bi-directional conversion between signal of communication and the multimedia messages; And antenna, being connected with this SIM, communicating via ground base station 3, and reception is from the signal of communication or the multimedia messages of this airborne satellite communication equipment 13 in order to emission signal of communication or multimedia messages to this airborne satellite communication equipment 13 for this antenna.The SIM here is the same with the principle of SIM cards of mobile phones, mainly is used for sending, receives command information or picture.
Wherein, This WIFI circuit module 122 is connected with this signal acquisition process unit 11 and communicates by letter with this airborne satellite communication equipment 13; This WIFI circuit module 122 carries out the wireless access of WIFI network; 11 receive said signals of communication and are sent to this airborne satellite communication equipment 13 communicating with ground network 3 ' via this International Telecommunication Satellite 2 with WIFI wireless communication protocol form from this signal acquisition process unit, and will be sent to this signal acquisition process unit 11 with WIFI wireless communication protocol form from the signal of communication of this airborne satellite communication equipment 13.
These two kinds of communication patterns (SIM communication pattern and WIFI internet communication pattern) the utility model can adopt, and the SIM communication pattern is with better function, and the information of SIM is sent easier.
Embodiment according to the utility model; This airborne satellite communication equipment 13 can comprise airborne mobile communications device 131, satellite communication assembly 132 and the satellite antenna 133 that connects successively; This airborne satellite communication equipment 13 is emitted to this International Telecommunication Satellite 2 communicating via this ground base station 3 or ground network 3 ' with said signal of communication through airborne satellite communication apparatus 131, and receives from the signal of communication of this International Telecommunication Satellite 2 and transmit it to this signal of communication transmission unit 12 through this satellite antenna 133.
Wherein, this airborne mobile communications device 131 can comprise the WIFI mixed-media network modules mixed-media, carries out the transmission of two-way communication signal or multimedia messages between this WIFI mixed-media network modules mixed-media and this WIFI circuit module 122.
Functions such as the control of the driving of the CPU control module 113 main completion GSM/GPRS modules of the utility model, the control of WIFI, peripheral hardware and interface protocol conversion.For the binary code stream after image processing module 112 compressions, CPU control module 113 can be stored with the form of file, and can drive the GSM/GPRS module via GSM network transmission view data; Or utilize the WIFI function via transmitted data on network.
Except that the infrared eye circuit that the collection infrared image is used is fixed, the remaining part of system can take different chips to design according to the development of different times technology.
The GPRS network that the GSM/GPRS module 121 of the utility model both can adopt China Mobile to provide carries out data transmission, also can adopt the mode of short message (SMS) to carry out data transmission.The user can select GPRS passage or SMS passage for use according to actual conditions, and switching channel at any time.The composition of GSM/GPRS module 121 comprises standard RS232 bidirectional interface, antenna for mobile phone and has opened SMS and the SIM of GPRS function that this SIM can be realized sending and receiving multimedia information.And the WIFI circuit module makes that thermal imaging system system that flies to of the utility model possess the WIFI communication function, can carry out the wireless access of network.
The data communication of the flight thermal imaging system of the utility model and the server system of ground control centre has two kinds of forms.Be respectively the note transmission manner of SIM and the mode of WIFI Network Transmission.Said International Telecommunication Satellite will transfer to the server system 4 of this thermal infrared imager 1 from the signal of communication of aircraft through ground base station 3 or ground network 3 '; And will transfer to this airborne satellite communication equipment 13 via this ground base station 3 or ground network 3 ' and through this International Telecommunication Satellite 2 from the signal of communication of this server system 4, wherein this server system 4 is for being connected to computing machine or the mobile phone on the communication network.
Be illustrated in figure 3 as the illustrative example of the flight thermal imaging system system of the utility model.Wherein, the thermal infrared imager 1 of the utility model can be rotatably set on the fuselage 50 of aircraft 5 through The Cloud Terrace 52, and this thermal infrared imager 1 is provided with transparent shroud 51, to protect this thermal infrared imager 1.Said aircraft 5 for example can for investigation with small aircraft, sprinkle water or cropduster etc. in the air.
The flight thermal imaging system system of the utility model is made up of two parts, and a part is airborne satellite communication equipment 13, other be thermal imaging system circuit part (comprising the signal acquisition process unit 11 on the signal of communication transmission unit 12 installation thermal infrared imagers).These two parts can be installed separately.Because be that airborne satellite communication equipment has been installed on some aircraft, at this moment only need to add another part and get final product.Airborne communication satellite equipment 13 generally all is loaded in the cabin.Signal of communication transmission unit 12 (be used for the collection of signal, handle, and pass ground back through airborne satellite communication equipment) can be arranged on the head of aircraft.
Specifically describe communication means below in conjunction with Fig. 4 according to the flight thermal imaging system system of the utility model embodiment.
As shown in Figure 4, this method may further comprise the steps: the picture signal that will obtain through the infrared chart of thermal infrared imager 1 shooting and monitoring object converts signal of communication into; Receive and send signal of communication through communication port, realize the air communication signal communication with aerial roam mode; And with said signal of communication via satellite antenna be emitted to International Telecommunication Satellite 2; And receiving signal of communication from this International Telecommunication Satellite 2, wherein said signal of communication comprises the signal of communication relevant with picture signal infrared chart that obtain through conversion of signals and from the signal of communication of server system 4.
Wherein, said air communication signal communication comprises that adopting GPRS network to communicate signal via the GPRS passage transmits, or adopts short message way to communicate the signal transmission via the SMS passage.Said air communication signal communication comprises that communicating signal through the WIFI network transmits.
Wherein, will transfer to this server system 4 by the airborne satellite communication equipment 13 of this flight thermal imaging system system through this International Telecommunication Satellite 2 and via its ground base station 3 or ground network 3 ' from the signal of communication of this thermal infrared imager 1.
On the other hand; Transfer to the airborne satellite communication equipment 13 of this flight thermal imaging system system via this ground base station 3 or ground network 3 ', through this International Telecommunication Satellite 2 from the signal of communication of this server system 4; And transfer to signal of communication transmission unit 12 by this airborne satellite communication equipment 13, export this thermal infrared imager 1 again to.
Wherein, Signal of communication from this server system 4 comprises thermal imaging system control signal, voice signal and video or the image display signal etc. that send through server system or communication facilities the ground control centre; In order to the shooting action of the thermal infrared imager on the controlling aircraft 1 and angle etc.; So that real-time better purpose monitoring object, and in order to timely transmission and relevant instructions such as post-processed and counter-measure.
Particularly; The control signal to thermal imaging system that server system 4 sends for example can be used for controlling the sequence of operations of thermal imaging system, comprises the focusing (realizing better information acquisition through the camera lens focusing according to actual conditions) of voice and image information collection and transmission, camera lens etc.The signal that server system 4 receives comprises information such as the information that returns on the slave, voice and video.
What the ground communication of the utility model adopted is website formula pattern; For ensureing that high altitude communication can not impact flight safety; What flight thermal imaging system system adopted when aloft communicating by letter is aerial roam mode; SIM combines with GSM/GPRS module 121, is equivalent on flight system, be provided with a mobile site.When the mode that startup GSM/GPRS module 121 is carried out short message (SMS) is carried out data transmission; Module does not directly connect the ground communication network; The note signal can at first be transferred to airborne satellite communication equipment 13; This airborne satellite communication equipment 13 is transferred to International Telecommunication Satellite 2 with signal of communication, and International Telecommunication Satellite 2 transfers signals to ground base station 3 again, accomplishes and the server of ground control centre or the exchanges data between the communication facilities through ground base station 3 then.In this process, be equivalent to GSM mobile handset network of simulation in the cabin of aircraft 5, only need very low emitted energy can realize air communication, thereby it drop in the aircraft security opereating specification.
The same with aerial transmission of messages mode, when launching the WIFI function, because airborne Wi-Fi mixed-media network modules mixed-media in the airborne satellite communication equipment 13, the signal of communication of online links to each other with airborne satellite communication equipment 13.For example through this airborne satellite communication equipment 13 signal of communication is transferred to International Telecommunication Satellite 2, inserts ground network 3 ' then, server system 4 can obtain relevant information through this ground network 3 ', and vice versa.
SIM and WIFI circuit module are two relatively independent parts, are respectively applied for the signal transmission of two kinds of different modes, and this two kinds of communication patterns can freely be selected by the flight thermal imaging system system of the utility model.
A plurality of exemplary embodiments although the front combines accompanying drawing to the utility model specifically describe; But it is understandable that; Within the spirit and scope of the principle of present disclosure, those skilled in the art can derive many other variations and embodiment fully.Especially, can be open at this, multiple variation and improvement are carried out in the combination that is provided with of assembly and/or annex in the scope of accompanying drawing and accompanying claims.Except that the variation and improvement of assembly and/or annex, other selectable application also are conspicuous to those skilled in the art.
Claims (7)
1. a flight thermal imaging system system comprises the thermal infrared imager (1) that is arranged on the aircraft (5), it is characterized in that this system also comprises:
Signal acquisition process unit (11) is arranged on this thermal infrared imager (1), and the infrared chart through the shooting and monitoring object obtains picture signal and is converted into signal of communication;
Signal of communication transmission unit (12); Being arranged on this aircraft (5) upward and with this signal acquisition process unit (11) is connected; This signal of communication transmission unit (12) receives and sends through communication port from the signal of communication of signal acquisition process unit (11) and with it, and receives from the signal of communication of outside and send it to this thermal infrared imager (1); And
Airborne satellite communication equipment (13); Being arranged on this aircraft (5) upward and with this signal of communication transmission unit (12) communicates by letter with International Telecommunication Satellite (2); This airborne satellite communication equipment (13) will from the said signal of communication of this signal of communication transmission unit (12) via satellite antenna be emitted to this International Telecommunication Satellite (2), and receive from the signal of communication of this International Telecommunication Satellite (2) and transmit it to this signal of communication transmission unit (12).
2. flight thermal imaging system according to claim 1 system is characterized in that this signal acquisition process unit (11) comprising:
Image capture module (111); Comprise optical lens and coupled infrared eye circuit; This optical lens collection from this detected object infrared radiation signal to take the infrared chart of this monitoring target; This infrared eye circuit collection through this optical lens incident infrared radiation signal and be converted into electric signal, to export as picture signal;
Image processing module (112) is connected with the infrared eye circuit of this image capture module (111), and this image processing module (112) receives said picture signal and is binary code stream with its processed compressed, to export as digital signal; And
CPU control module (113); Be connected with this signal of communication transmission unit (12) with this image processing module (112); This CPU control module (113) receives said digital signal and stores said digital signal with document form; Is signal of communication according to communication interface standard with institute's stored numbers conversion of signals, through driving and controlling this signal of communication transmission unit (12) said signal of communication is sent to this airborne satellite communication equipment (13) via communication network.
3. flight thermal imaging system according to claim 1 system is characterized in that this signal of communication transmission unit (12) comprising:
GSM/GPRS module (121) adopts GPRS network to communicate the signal transmission via the GPRS passage, or adopts short message way to communicate the signal transmission via the SMS passage, and this GSM/GPRS module (121) comprising:
Standard RS232 bidirectional interface; Be connected with this signal acquisition process unit (11), this standard RS232 bidirectional interface receives said signal of communication and will be sent to this signal acquisition process unit (11) from the signal of communication of this airborne satellite communication equipment (13) from this signal acquisition process unit (11);
SIM is connected with this standard RS232 bidirectional interface, and this SIM has SMS and GPRS function, receive said signal of communication and communicate signal and multimedia messages between bi-directional conversion; And
Antenna; Be connected with this SIM and communicate by letter with this airborne satellite communication equipment (13); This antenna emission signal of communication or multimedia messages to this airborne satellite communication equipment (13) are communicating via this International Telecommunication Satellite (2) and ground base station (3), and reception is from the signal of communication or the multimedia messages of this airborne satellite communication equipment (13); And
WIFI circuit module (122); Be connected with this signal acquisition process unit (11) and communicate by letter with this airborne satellite communication equipment (13); This WIFI circuit module (122) carries out the wireless access of WIFI network; Receive said signal of communication from this signal acquisition process unit (11) and be sent to this airborne satellite communication equipment (13) communicating, and will be sent to this signal acquisition process unit (11) with WIFI wireless communication protocol form from the signal of communication of this airborne satellite communication equipment (13) via this International Telecommunication Satellite (2) and ground network (3 ') with WIFI wireless communication protocol form.
4. flight thermal imaging system according to claim 3 system; It is characterized in that this airborne satellite communication equipment (13) comprises airborne mobile communications device (131), satellite communication assembly (132) and the satellite antenna (133) that connects successively; This airborne satellite communication equipment (13) is emitted to this International Telecommunication Satellite (2) communicating via this ground base station (3) or ground network (3 ') with said signal of communication through airborne satellite communication apparatus (131), and receives from the signal of communication of this International Telecommunication Satellite (2) and transmit it to this signal of communication transmission unit (12) through this satellite antenna (133).
5. flight thermal imaging system according to claim 4 system is characterized in that this airborne mobile communications device (131) comprises the WIFI mixed-media network modules mixed-media, carries out the transmission of two-way communication signal or multimedia messages between this WIFI mixed-media network modules mixed-media and this WIFI circuit module (122).
6. according to any described flight thermal imaging system system of claim 1 to 5; It is characterized in that this International Telecommunication Satellite (2) transfers to said signal of communication through ground base station (3) or ground network (3 ') server system (4) of this thermal infrared imager (1); And from the signal of communication of this server system (4) via this ground base station (3) or ground network (3 ') and transfer to this airborne satellite communication equipment (13) through this International Telecommunication Satellite (2), wherein this server system (4) is to be connected to computing machine or the mobile phone on the communication network.
7. according to any described flight thermal imaging system system of claim 1 to 5; It is characterized in that this thermal infrared imager (1) can be rotatably set on the fuselage (50) of this aircraft (5) through The Cloud Terrace (52), and this thermal infrared imager (1) is provided with the transparent shroud (51) of this thermal infrared imager of protection (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205762499U CN202501922U (en) | 2011-12-30 | 2011-12-30 | Flight thermal imager system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205762499U CN202501922U (en) | 2011-12-30 | 2011-12-30 | Flight thermal imager system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202501922U true CN202501922U (en) | 2012-10-24 |
Family
ID=47038533
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011205762499U Withdrawn - After Issue CN202501922U (en) | 2011-12-30 | 2011-12-30 | Flight thermal imager system |
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| CN (1) | CN202501922U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102519600A (en) * | 2011-12-30 | 2012-06-27 | 广州飒特红外科技有限公司 | Flight thermal imager system and communication method thereof |
| CN109960271A (en) * | 2017-12-14 | 2019-07-02 | 惠州市组合科技有限公司 | A kind of controllable data separating formula UAV Communication equipment and its working method |
-
2011
- 2011-12-30 CN CN2011205762499U patent/CN202501922U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102519600A (en) * | 2011-12-30 | 2012-06-27 | 广州飒特红外科技有限公司 | Flight thermal imager system and communication method thereof |
| CN102519600B (en) * | 2011-12-30 | 2014-12-03 | 广州飒特红外股份有限公司 | Flight thermal imager system and communication method thereof |
| CN109960271A (en) * | 2017-12-14 | 2019-07-02 | 惠州市组合科技有限公司 | A kind of controllable data separating formula UAV Communication equipment and its working method |
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