CN202481324U - Wireless remote control flying monitoring thermal imager device - Google Patents
Wireless remote control flying monitoring thermal imager device Download PDFInfo
- Publication number
- CN202481324U CN202481324U CN2012200370768U CN201220037076U CN202481324U CN 202481324 U CN202481324 U CN 202481324U CN 2012200370768 U CN2012200370768 U CN 2012200370768U CN 201220037076 U CN201220037076 U CN 201220037076U CN 202481324 U CN202481324 U CN 202481324U
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- remote control
- aircraft
- thermal imager
- wireless
- wireless remote
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Abstract
The utility model relates to a monitoring thermal imager device, and in particular relates to a wireless remote control flying monitoring thermal imager device. The wireless remote control flying monitoring thermal imager device mainly comprises a flying machine, a circuit board and an infrared thermal imager, wherein the circuit board and the infrared thermal imager are arranged on the flying machine; the infrared thermal imager is electrically connected with the circuit board; and the circuit board comprises a central processing unit for processing a video signal and a wireless transceiver unit for transmitting data to external wireless receiving equipment. A monitor remotely controls the flying machine to fly; acquired video data is subjected to data transmission through a wireless signal transceiver and external equipment such as a computer with a wireless receiving function under the action of shooting of the infrared thermal imager; and the monitor can monitor the flying machine in real time.
Description
Technical field
The utility model relates to a kind of monitoring thermal imaging system device, especially relates to a kind of wireless remote control flight monitoring thermal imaging system device.
Background technology
DV and pick up camera are through the development of decades at present, and technical level increases substantially, and function is gradually improved, and scale is gradually improved from small to large.Pick up camera its as a kind of video input apparatus, need extensively to be applied to the office of safety facilities in the past, the inside of hospital, bank, public building etc. or outside are carried out ground and are taken.Along with the development of society, increasing pick up camera is installed on the aircraft, mainly is positioned alert to use the field, satisfies the fields such as aerial investigation and patrol, especially anti-terrorism, fire alarm, patrol police of sudden, zonule property, locality; Can satisfy simultaneously the needs in fields such as the anti-dangerous disaster relief.Like one Chinese patent application number is 200820108389 the small aircraft with the function of taking photo by plane, and it is in an aircraft bottom high energy battery group to be housed, and the below of this high energy battery group is provided with pick up camera; Be provided with rotating mechanism in the said pick up camera, also be provided with video transmission equipment on the pick up camera; This aircraft below also is provided with support, and this aircraft mainly is the emergent monitoring to the scene of the accident.
But the monitor that flies at present all can only carry out common video to be taken and monitoring function; When the generation sudden accident, like dark forest fires calamity, market fire, building fire; On-the-spot often with a large amount of dense smoke and noxious gas; Thereby on-the-spot visiblity is reduced greatly, and traditional like this pick up camera just can not meet requirements; Simultaneously because the scope of scene of fire is bigger, the investigation that the fire fighter need not stop the scene is being sued and laboured to find trapped personnel, has increased the time of rescuing so greatly, thereby has caused bigger injures and deaths.Therefore be badly in need of a kind of device can let the rescue group accurately, fast speed knows scene of the accident personnel's situation, thereby carry out autotelic rescue, to reach the purpose of reducing the loss or averting a calamity as far as possible.
The utility model content
The purpose of the utility model is to overcome the defective and the deficiency of prior art; A kind of wireless remote control flight monitoring thermal imaging system device is provided; When unexpected incidents take place when the monitor staff through this device can be exactly, the situation with the scene feeds back to the rescue group apace, thereby carry out autotelic rescue.
A kind of wireless remote control flight monitoring thermal imaging system device mainly comprises aircraft, circuit card, thermal infrared imager, and said circuit card, thermal infrared imager are installed on the said aircraft, and said thermal infrared imager and the electric connection of said circuit card.
Further, said circuit card comprises the center processing unit that is used to handle vision signal, is used for the wireless signal control module of carrying out the wireless transmit/receive units of data transmission and being used for controlling aircraft flight with the external wireless reception facilities.
As optimal way, said circuit card is arranged on the inside of said aircraft; Said thermal infrared imager is arranged on the bottom of said aircraft.
As optimal way, the detachable battery group is installed also on the said aircraft.
As optimal way, the bottom of said aircraft is provided with USB interface.
Above-mentioned wireless remote control flight monitoring thermal imaging system device is arranged on thermal infrared imager on the aircraft of remote-controlled control.Said thermal infrared imager can be exactly, apace important informations such as personnel's situation of the scene of the accident, personnel positions are fed back to the rescue group through the wireless signal transceiver on the circuit card; Thereby the rescue group can be rescued targetedly; Lowered rescue time greatly, thereby be reduced to injures and deaths and loss minimum.
Description of drawings
Through below in conjunction with accompanying drawing is exemplary embodiment being described, above-mentioned and other characteristics and the advantage of the utility model will become apparent, wherein:
Fig. 1 is the integral structure scheme drawing of the utility model.
The specific embodiment
Below through concrete embodiment and combine accompanying drawing that the utility model is done further detailed description.
Thermal infrared imager is to utilize infrared detector and optical imagery object lens to accept the infrared energy distributed image of measured target and be reflected on the infrared detector photosensitive assembly; Thereby the acquisition Infrared Thermogram, this thermal image is corresponding with the heat distribution field of body surface.The popular thermal infrared imager of saying is exactly to change the black light energy that object sends into the appreciiable heat picture.The top different colours of heat picture is represented the different temperatures of testee.
But the utility model provides a kind of wireless remote control flight monitoring thermal imaging system device, and this device comprises the aircraft 1 of remote-controlled control, thermal infrared imager 2 and circuit card 3.As shown in Figure 1; Said thermal infrared imager 2 is arranged on the fuselage of aircraft 1; Said circuit card 3 is arranged in the inner chamber of aircraft 1, and said circuit card 3 is provided with the center processing unit that is used to handle vision signal, wireless signal transceiver 3a, wireless signal control module 3b.The mouth of said thermal infrared imager 2 connects the input end of said circuit card 3.
The detachable battery group also is installed on the aircraft 1, is used for to equipment and components and parts power supplies such as aircraft 1, thermal infrared imager 2, circuit cards 3.This aircraft can drive through the circuit supply of battery pack, also can drive through alternate manners such as engines.
Also be provided with USB interface 4 on the aircraft 1, be used for being connected, give batteries charging with external power supply.
As shown in Figure 1, the input end of the wireless signal transceiver 3a on the mouth of thermal infrared imager 2 and the circuit card 3 is connected; When aircraft 1 through remote control control flight during to the high-altitude, thermal infrared imager 2 can be comprehensive, the taking of multi-angle, and realizes the monitoring to the scene; Simultaneously; The video data that thermal infrared imager 2 collects is through the vision signal center processing unit on the circuit card; Carry out data transmission through wireless signal transceiver 3a with outside external devices such as computing machine then with wireless receiving function; Supply the monitor staff to monitor in real time, forms such as that said transmission of wireless signals mode comprises is infrared, bluetooth, radio frequency, WIFI, Zigbee.Wireless signal control module 3b on the said circuit card 3 is used for the flight of controlling aircraft.The monitor staff can pass through the wireless signal control module 3b sending controling instruction of external device on circuit card 3, thus the scope and the angle of controlling aircraft 1 flight.
Claims (6)
1. a wireless remote control flight monitoring thermal imaging system device mainly comprises aircraft, circuit card, thermal infrared imager; It is characterized in that said circuit card, thermal infrared imager are installed on the said aircraft, and said thermal infrared imager and the electric connection of said circuit card.
2. wireless remote control according to claim 1 flight monitoring thermal imaging system device is characterized in that: said circuit card comprises the center processing unit that is used to handle vision signal, be used for the wireless signal control module of carrying out the wireless transmit/receive units of data transmission and being used for controlling aircraft flight with the external wireless reception facilities.
3. wireless remote control flight monitoring thermal imaging system device according to claim 2, it is characterized in that: said circuit card is arranged on the inside of said aircraft.
4. wireless remote control flight monitoring thermal imaging system device according to claim 3, it is characterized in that: said thermal infrared imager is arranged on the bottom of said aircraft.
5. wireless remote control flight monitoring thermal imaging system device according to claim 4 is characterized in that: row detachable battery group also is installed on the said aircraft.
6. wireless remote control flight monitoring thermal imaging system device according to claim 5, it is characterized in that: the base of said mobile vehicle is provided with USB interface.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012200370768U CN202481324U (en) | 2012-02-06 | 2012-02-06 | Wireless remote control flying monitoring thermal imager device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012200370768U CN202481324U (en) | 2012-02-06 | 2012-02-06 | Wireless remote control flying monitoring thermal imager device |
Publications (1)
Publication Number | Publication Date |
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CN202481324U true CN202481324U (en) | 2012-10-10 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN2012200370768U Expired - Fee Related CN202481324U (en) | 2012-02-06 | 2012-02-06 | Wireless remote control flying monitoring thermal imager device |
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CN (1) | CN202481324U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104565876A (en) * | 2015-01-05 | 2015-04-29 | 惠州市加迈电器有限公司 | Portable lighting device |
GB2547416A (en) * | 2016-02-10 | 2017-08-23 | Tyco Fire & Security Gmbh | A fire detection system |
-
2012
- 2012-02-06 CN CN2012200370768U patent/CN202481324U/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104565876A (en) * | 2015-01-05 | 2015-04-29 | 惠州市加迈电器有限公司 | Portable lighting device |
GB2547416A (en) * | 2016-02-10 | 2017-08-23 | Tyco Fire & Security Gmbh | A fire detection system |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
DD01 | Delivery of document by public notice |
Addressee: Liao Zhihua Document name: Notice of termination of patent |
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DD01 | Delivery of document by public notice | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20121010 Termination date: 20200206 |
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CF01 | Termination of patent right due to non-payment of annual fee |