CN106895922A - A kind of work high above the ground thermal imaging system control device - Google Patents
A kind of work high above the ground thermal imaging system control device Download PDFInfo
- Publication number
- CN106895922A CN106895922A CN201710230929.7A CN201710230929A CN106895922A CN 106895922 A CN106895922 A CN 106895922A CN 201710230929 A CN201710230929 A CN 201710230929A CN 106895922 A CN106895922 A CN 106895922A
- Authority
- CN
- China
- Prior art keywords
- imaging system
- thermal imaging
- control device
- direction controlling
- pinboard
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000001931 thermography Methods 0.000 title claims abstract description 125
- 230000005540 biological transmission Effects 0.000 claims abstract description 49
- 230000008878 coupling Effects 0.000 claims abstract description 47
- 238000010168 coupling process Methods 0.000 claims abstract description 47
- 238000005859 coupling reaction Methods 0.000 claims abstract description 47
- 238000013016 damping Methods 0.000 claims abstract description 42
- 238000005452 bending Methods 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims 1
- 238000007405 data analysis Methods 0.000 abstract description 4
- 238000001514 detection method Methods 0.000 abstract description 3
- 230000001276 controlling effect Effects 0.000 description 54
- 230000000007 visual effect Effects 0.000 description 2
- 239000003086 colorant Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01J—MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
- G01J5/00—Radiation pyrometry, e.g. infrared or optical thermometry
- G01J5/0066—Radiation pyrometry, e.g. infrared or optical thermometry for hot spots detection
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01J—MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
- G01J5/00—Radiation pyrometry, e.g. infrared or optical thermometry
- G01J5/02—Constructional details
- G01J5/0275—Control or determination of height or distance or angle information for sensors or receivers
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D23/00—Control of temperature
- G05D23/19—Control of temperature characterised by the use of electric means
- G05D23/1927—Control of temperature characterised by the use of electric means using a plurality of sensors
- G05D23/193—Control of temperature characterised by the use of electric means using a plurality of sensors sensing the temperaure in different places in thermal relationship with one or more spaces
- G05D23/1931—Control of temperature characterised by the use of electric means using a plurality of sensors sensing the temperaure in different places in thermal relationship with one or more spaces to control the temperature of one space
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01J—MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
- G01J5/00—Radiation pyrometry, e.g. infrared or optical thermometry
- G01J2005/0077—Imaging
Abstract
The invention belongs to power industry unmanned plane testing equipment technical field, specifically related to a kind of work high above the ground thermal imaging system control device, including controller, transmission board, pinboard, damping connects head, balance control module, direction controlling coupling assembly and thermal imaging system, controller and transmission board are connected with pinboard respectively, pinboard is connected with balance control module and thermal imaging system respectively, with unmanned plane be connected the thermal imaging system control device by damping connection head, direction controlling coupling assembly includes 3 direction controlling motors and connector, direction controlling coupling assembly one end is connected head with damping and is connected by balancing control module, the other end connects thermal imaging system.The present invention can quickly carry out data analysis to any shooting point of data and read hot spot data, realize maximum temperature hotspot tracking, coordinate unmanned plane in the comprehensive detection of work high above the ground, reduce personnel's job safety hidden danger, improve operating efficiency.
Description
Technical field
The invention belongs to power industry unmanned plane testing equipment technical field, and in particular to a kind of work high above the ground thermal imaging system
Control device.
Background technology
In power transmission and transformation operational outfit, thermal imaging detector is used in having put into our conventional maintenance detections, due to equipment
Larger, equipment price is expensive, negligible amounts of attaching troops to a unit, and zoom observation effect is poor, and tour personnel's observed bearing also has leak,
Backstage does not pinpoint assigned temperature extraction, not comprehensive without highest hotspot tracking data analysis yet.
The content of the invention
In order to solve the above-mentioned technical problem, the present invention provides a kind of work high above the ground thermal imaging system control device, for detecting
Charging equipment ruuning situation, the current running temperature of testing equipment realizes that temperature, remote control are read in follow-up of hot issues, data analysis
Increase steady.
The present invention is achieved in that a kind of work high above the ground thermal imaging system control device, including controller, transmission board, turns
Fishplate bar, damping connection head, balance control module, direction controlling coupling assembly and thermal imaging system, controller and transmission board point
Be not connected with pinboard, pinboard be connected with balance control module and thermal imaging system respectively, damping connect head by it is described it is hot into
As instrument control device is connected with unmanned plane, direction controlling coupling assembly includes 3 direction controlling motors and connector, direction control
Coupling assembly one end processed is connected head with damping and is connected by balancing control module, other end connection thermal imaging system.
Further, damping connection head includes upper junction plate and shock-absorbing ball, and shock-absorbing ball is arranged on upper junction plate and described
On the extension plate that balance control module two ends are stretched out.
Further, upper junction plate is connected by bolt with unmanned plane.
Further, shock-absorbing ball sets 6 altogether.
Further, shock-absorbing ball is flexible rubber ball.
Further, 3 direction controlling motors of direction controlling coupling assembly are respectively control of sideward roll motor, left-right balance
Controlled motor and pitching control motor.
Further, 3 direction controlling motors constitute bending structure with connector.
Further, thermal imaging system inside sets follow-up of hot issues module and mechanical zoom module, and control thermal imaging system is carried out
Automatic follow-up of hot issues and mechanical zoom.
Further, the temperature range that follow-up of hot issues module is followed the trail of is 50-200 DEG C, and wave-length coverage is 8-600 μm.
Further, transmission board is 5.8G digital transmission system modules.
Further, power module is set on the pinboard.
Compared with prior art, it is an advantage of the current invention that data analysis reading quickly can be carried out to any shooting point of data
Hot spot data is taken, maximum temperature hotspot tracking is realized, coordinates unmanned plane in the comprehensive detection of work high above the ground, reduce personnel's operation peace
Full hidden danger, improves operating efficiency.
Brief description of the drawings
Below in conjunction with the accompanying drawings and implementation method the present invention is further detailed explanation：
Fig. 1 is schematic structural view of the invention；
Fig. 2 is configuration schematic diagram of the present invention.
Specific embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, with reference to the accompanying drawings and examples, it is right
The present invention is further elaborated.It should be appreciated that specific embodiment described herein is used only for explaining the present invention, and
It is not used in the restriction present invention.
Embodiment 1,
With reference to Fig. 1 and Fig. 2, a kind of work high above the ground thermal imaging system control device, including controller 1, transmission board 2, pinboard
3rd, damping connection head 4, balance control module 5, direction controlling coupling assembly and thermal imaging system 7, controller 1 and transmission board 2
It is connected with the data wire of pinboard 3 respectively, pinboard 3 is connected with balance control module 5 and the data wire of thermal imaging system 7 respectively, damping
With unmanned plane be connected thermal imaging system control device by connection head 4, and direction controlling coupling assembly includes 3 direction controlling motors 61
And connector 62, direction controlling coupling assembly one end is connected head 4 with damping and connected by balancing control module 5, the other end
Connection thermal imaging system 7.
When using the present invention carry out high-altitude monitor when, after energization, the original image that thermal imaging system 7 is monitored through pinboard 3,
Transmission board 2 is transferred to ground, and surface personnel as needed, issues an order to controller 1, and controller 1 passes to order
Pinboard 3, pinboard 3 to the direction of thermal imaging system 7 and thermal imaging system 7 by direction controlling coupling assembly so as to be controlled
The new picture for catching is transferred to ground by system, thermal imaging system 7 by transmission board 2 again.
Pinboard 3 can be mixed colours the image that thermal imaging system is exported, electronics amplifies, record and visual 4 kinds of output are whole
Close, with grey, dull gray and colored 3 kinds of forms, electronics amplifies can be expanded to 2-4 times, note by the existing ratio of original image for toning
Record is real-time storage data, is exported with photo form integral data, visual output will data be finally changed into AV outputs
Signal.
Embodiment 2,
With reference to Fig. 1 and Fig. 2, a kind of work high above the ground thermal imaging system control device, including controller 1, transmission board 2, pinboard
3rd, damping connection head 4, balance control module 5, direction controlling coupling assembly and thermal imaging system 7, controller 1 and transmission board 2
It is connected with the data wire of pinboard 3 respectively, pinboard 3 is connected with balance control module 5 and the data wire of thermal imaging system 7 respectively, damping
With unmanned plane be connected thermal imaging system control device by connection head 4, and direction controlling coupling assembly includes 3 direction controlling motors 61
And connector 62, direction controlling coupling assembly one end is connected head 4 with damping and connected by balancing control module 5, the other end
Connection thermal imaging system 7；
Damping connection head 4 includes upper junction plate 41 and shock-absorbing ball 42, and shock-absorbing ball 42 is arranged on upper junction plate 41 and described
On the extension plate that balance control module 5 two ends are stretched out.By the damping vibration of shock-absorbing ball 42, make the picture that thermal imaging system 7 catches more
Plus it is steady and audible.
When using the present invention carry out high-altitude monitor when, after energization, the original image that thermal imaging system 7 is monitored through pinboard 3,
Transmission board 2 is transferred to ground, and surface personnel as needed, issues an order to controller 1, and controller 1 passes to order
Pinboard 3, pinboard 3 to the direction of thermal imaging system 7 and thermal imaging system 7 by direction controlling coupling assembly so as to be controlled
The new picture for catching is transferred to ground by system, thermal imaging system 7 by transmission board 2 again.
Embodiment 3,
With reference to Fig. 1 and Fig. 2, a kind of work high above the ground thermal imaging system control device, including controller 1, transmission board 2, pinboard
3rd, damping connection head 4, balance control module 5, direction controlling coupling assembly and thermal imaging system 7, controller 1 and transmission board 2
It is connected with the data wire of pinboard 3 respectively, pinboard 3 is connected with balance control module 5 and the data wire of thermal imaging system 7 respectively, damping
With unmanned plane be connected thermal imaging system control device by connection head 4, and direction controlling coupling assembly includes 3 direction controlling motors 61
And connector 62, direction controlling coupling assembly one end is connected head 4 with damping and connected by balancing control module 5, the other end
Connection thermal imaging system 7；
Damping connection head 4 includes upper junction plate 41 and shock-absorbing ball 42, and shock-absorbing ball 42 is arranged on upper junction plate 41 and described
On the extension plate that balance control module 5 two ends are stretched out.By the damping vibration of shock-absorbing ball 42, make the picture that thermal imaging system 7 catches more
Plus it is steady and audible.Upper junction plate 41 is connected by bolt with unmanned plane.Shock-absorbing ball 42 sets 6 altogether.Shock-absorbing ball 42 is flexible rubber
Glueballs, can well reduce the vibrations that unmanned plane passes to thermal imaging system.
When using the present invention carry out high-altitude monitor when, after energization, the original image that thermal imaging system 7 is monitored through pinboard 3,
Transmission board 2 is transferred to ground, and surface personnel as needed, issues an order to controller 1, and controller 1 passes to order
Pinboard 3, pinboard 3 to the direction of thermal imaging system 7 and thermal imaging system 7 by direction controlling coupling assembly so as to be controlled
The new picture for catching is transferred to ground by system, thermal imaging system 7 by transmission board 2 again.
Embodiment 4,
With reference to Fig. 1 and Fig. 2, a kind of work high above the ground thermal imaging system control device, including controller 1, transmission board 2, pinboard
3rd, damping connection head 4, balance control module 5, direction controlling coupling assembly and thermal imaging system 7, controller 1 and transmission board 2
It is connected with the data wire of pinboard 3 respectively, pinboard 3 is connected with balance control module 5 and the data wire of thermal imaging system 7 respectively, damping
With unmanned plane be connected thermal imaging system control device by connection head 4, and direction controlling coupling assembly includes 3 direction controlling motors 61
And connector 62, direction controlling coupling assembly one end is connected head 4 with damping and connected by balancing control module 5, the other end
Connection thermal imaging system 7；
In order that thermal imaging system 7 can in all directions carry out picture catching, 3 direction controllings of direction controlling coupling assembly
Motor 61 is respectively control of sideward roll motor 611, left-right balance controlled motor 612 and pitching control motor 613.
When using the present invention carry out high-altitude monitor when, after energization, the original image that thermal imaging system 7 is monitored through pinboard 3,
Transmission board 2 is transferred to ground, and surface personnel as needed, issues an order to controller 1, and controller 1 passes to order
Pinboard 3, pinboard 3 to the direction of thermal imaging system 7 and thermal imaging system 7 by direction controlling coupling assembly so as to be controlled
The new picture for catching is transferred to ground by system, thermal imaging system 7 by transmission board 2 again.
Embodiment 5,
With reference to Fig. 1 and Fig. 2, a kind of work high above the ground thermal imaging system control device, including controller 1, transmission board 2, pinboard
3rd, damping connection head 4, balance control module 5, direction controlling coupling assembly and thermal imaging system 7, controller 1 and transmission board 2
It is connected with the data wire of pinboard 3 respectively, pinboard 3 is connected with balance control module 5 and the data wire of thermal imaging system 7 respectively, damping
With unmanned plane be connected thermal imaging system control device by connection head 4, and direction controlling coupling assembly includes 3 direction controlling motors 61
And connector 62, direction controlling coupling assembly one end is connected head 4 with damping and connected by balancing control module 5, the other end
Connection thermal imaging system 7；3 direction controlling motors 61 constitute bending structure with connector 62, being capable of preferably save space.
When using the present invention carry out high-altitude monitor when, after energization, the original image that thermal imaging system 7 is monitored through pinboard 3,
Transmission board 2 is transferred to ground, and surface personnel as needed, issues an order to controller 1, and controller 1 passes to order
Pinboard 3, pinboard 3 to the direction of thermal imaging system 7 and thermal imaging system 7 by direction controlling coupling assembly so as to be controlled
The new picture for catching is transferred to ground by system, thermal imaging system 7 by transmission board 2 again.
Embodiment 6,
With reference to Fig. 1 and Fig. 2, a kind of work high above the ground thermal imaging system control device, including controller 1, transmission board 2, pinboard
3rd, damping connection head 4, balance control module 5, direction controlling coupling assembly and thermal imaging system 7, controller 1 and transmission board 2
It is connected with the data wire of pinboard 3 respectively, pinboard 3 is connected with balance control module 5 and the data wire of thermal imaging system 7 respectively, damping
With unmanned plane be connected thermal imaging system control device by connection head 4, and direction controlling coupling assembly includes 3 direction controlling motors 61
And connector 62, direction controlling coupling assembly one end is connected head 4 with damping and connected by balancing control module 5, the other end
Connection thermal imaging system 7；In order that during work high above the ground, thermal imaging system can realize follow-up of hot issues and mechanical zoom, thermal imaging system 7
Inside sets follow-up of hot issues module and mechanical zoom module, and control thermal imaging system carries out automatic follow-up of hot issues and mechanical zoom.
When using the present invention carry out high-altitude monitor when, after energization, the original image that thermal imaging system 7 is monitored through pinboard 3,
Transmission board 2 is transferred to ground, and surface personnel as needed, issues an order to controller 1, and controller 1 passes to order
Pinboard 3, pinboard 3 to the direction of thermal imaging system 7 and thermal imaging system 7 by direction controlling coupling assembly so as to be controlled
The new picture for catching is transferred to ground by system, thermal imaging system 7 by transmission board 2 again.
Embodiment 7,
With reference to Fig. 1 and Fig. 2, a kind of work high above the ground thermal imaging system control device, including controller 1, transmission board 2, pinboard
3rd, damping connection head 4, balance control module 5, direction controlling coupling assembly and thermal imaging system 7, controller 1 and transmission board 2
It is connected with the data wire of pinboard 3 respectively, pinboard 3 is connected with balance control module 5 and the data wire of thermal imaging system 7 respectively, damping
With unmanned plane be connected thermal imaging system control device by connection head 4, and direction controlling coupling assembly includes 3 direction controlling motors 61
And connector 62, direction controlling coupling assembly one end is connected head 4 with damping and connected by balancing control module 5, the other end
Connection thermal imaging system 7；In order that during work high above the ground, thermal imaging system can realize follow-up of hot issues and mechanical zoom, thermal imaging system 7
Inside sets follow-up of hot issues module and mechanical zoom module, and control thermal imaging system carries out automatic follow-up of hot issues and mechanical zoom.
The temperature range that follow-up of hot issues module is followed the trail of is 50-200 DEG C, and wave-length coverage is 8-600 μm.
When using the present invention carry out high-altitude monitor when, after energization, the original image that thermal imaging system 7 is monitored through pinboard 3,
Transmission board 2 is transferred to ground, and surface personnel as needed, issues an order to controller 1, and controller 1 passes to order
Pinboard 3, pinboard 3 to the direction of thermal imaging system 7 and thermal imaging system 7 by direction controlling coupling assembly so as to be controlled
The new picture for catching is transferred to ground by system, thermal imaging system 7 by transmission board 2 again.
Embodiment 8,
With reference to Fig. 1 and Fig. 2, a kind of work high above the ground thermal imaging system control device, including controller 1, transmission board 2, pinboard
3rd, damping connection head 4, balance control module 5, direction controlling coupling assembly and thermal imaging system 7, controller 1 and transmission board 2
It is connected with the data wire of pinboard 3 respectively, pinboard 3 is connected with balance control module 5 and the data wire of thermal imaging system 7 respectively, damping
With unmanned plane be connected thermal imaging system control device by connection head 4, and direction controlling coupling assembly includes 3 direction controlling motors 61
And connector 62, direction controlling coupling assembly one end is connected head 4 with damping and connected by balancing control module 5, the other end
Connection thermal imaging system 7；Transmission board is 5.8G digital transmission system modules.
When using the present invention carry out high-altitude monitor when, after energization, the original image that thermal imaging system 7 is monitored through pinboard 3,
Transmission board 2 is transferred to ground, and surface personnel as needed, issues an order to controller 1, and controller 1 passes to order
Pinboard 3, pinboard 3 to the direction of thermal imaging system 7 and thermal imaging system 7 by direction controlling coupling assembly so as to be controlled
The new picture for catching is transferred to ground by system, thermal imaging system 7 by transmission board 2 again.
Embodiment 9,
With reference to Fig. 1 and Fig. 2, a kind of work high above the ground thermal imaging system control device, including controller 1, transmission board 2, pinboard
3rd, damping connection head 4, balance control module 5, direction controlling coupling assembly and thermal imaging system 7, controller 1 and transmission board 2
It is connected with the data wire of pinboard 3 respectively, pinboard 3 is connected with balance control module 5 and the data wire of thermal imaging system 7 respectively, damping
With unmanned plane be connected thermal imaging system control device by connection head 4, and direction controlling coupling assembly includes 3 direction controlling motors 61
And connector 62, direction controlling coupling assembly one end with
Damping connection head 4 is connected by balancing control module 5, other end connection thermal imaging system 7；On the pinboard
Power module is set.
When using the present invention carry out high-altitude monitor when, after energization, the original image that thermal imaging system 7 is monitored through pinboard 3,
Transmission board 2 is transferred to ground, and surface personnel as needed, issues an order to controller 1, and controller 1 passes to order
Pinboard 3, pinboard 3 to the direction of thermal imaging system 7 and thermal imaging system 7 by direction controlling coupling assembly so as to be controlled
The new picture for catching is transferred to ground by system, thermal imaging system 7 by transmission board 2 again.
Claims (11)
1. a kind of work high above the ground thermal imaging system control device, it is characterised in that connect including controller, transmission board, pinboard, damping
Head, balance control module, direction controlling coupling assembly and thermal imaging system are connect, controller and transmission board connect with pinboard respectively
Connect, pinboard is connected with balance control module and thermal imaging system respectively, damping connects head by the thermal imaging system control device
It is connected with unmanned plane, direction controlling coupling assembly includes 3 direction controlling motors and connector, direction controlling coupling assembly one
End is connected head with damping and is connected by balancing control module, other end connection thermal imaging system.
2. work high above the ground thermal imaging system control device as claimed in claim 1, it is characterised in that the damping connects head bag
Upper junction plate and shock-absorbing ball are included, shock-absorbing ball is arranged on the extension plate that upper junction plate and the balance control module two ends are stretched out.
3. work high above the ground thermal imaging system control device as claimed in claim 2, it is characterised in that the upper junction plate passes through spiral shell
Bolt is connected with unmanned plane.
4. work high above the ground thermal imaging system control device as claimed in claim 2, it is characterised in that the shock-absorbing ball sets 6 altogether
It is individual.
5. work high above the ground thermal imaging system control device as claimed in claim 2, it is characterised in that the shock-absorbing ball is flexible rubber
Glueballs.
6. work high above the ground thermal imaging system control device as claimed in claim 1, it is characterised in that the direction controlling connection group
3 direction controlling motors of part are respectively control of sideward roll motor, left-right balance controlled motor and pitching control motor.
7. work high above the ground thermal imaging system control device as claimed in claim 1, it is characterised in that 3 direction controlling electricity
Machine constitutes bending structure with connector.
8. work high above the ground thermal imaging system control device as claimed in claim 1, it is characterised in that set inside the thermal imaging system
Follow-up of hot issues module and mechanical zoom module are put, control thermal imaging system carries out automatic follow-up of hot issues and mechanical zoom.
9. work high above the ground thermal imaging system control device as claimed in claim 7, it is characterised in that the follow-up of hot issues module institute
The temperature range of tracking is 50-200 DEG C, and wave-length coverage is 8-600 μm.
10. work high above the ground thermal imaging system control device as claimed in claim 1, it is characterised in that the transmission board is 5.8G
Digital transmission system module.
11. work high above the ground thermal imaging system control devices as claimed in claim 1, it is characterised in that set on the pinboard
Put power module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710230929.7A CN106895922A (en) | 2017-04-11 | 2017-04-11 | A kind of work high above the ground thermal imaging system control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710230929.7A CN106895922A (en) | 2017-04-11 | 2017-04-11 | A kind of work high above the ground thermal imaging system control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106895922A true CN106895922A (en) | 2017-06-27 |
Family
ID=59196069
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710230929.7A Pending CN106895922A (en) | 2017-04-11 | 2017-04-11 | A kind of work high above the ground thermal imaging system control device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106895922A (en) |
Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2415562Y (en) * | 2000-02-25 | 2001-01-17 | 周国起 | Mine infrared night vision camera apparatus |
| CN103051871A (en) * | 2012-12-10 | 2013-04-17 | 天津中科遥感信息技术有限公司 | Special portable thermal infrared camera system for unmanned aerial vehicle |
| CN103235602A (en) * | 2013-03-25 | 2013-08-07 | 山东电力集团公司电力科学研究院 | Automatic photography control device for power line inspection unmanned aerial vehicle, and control method thereof |
| CN204166392U (en) * | 2014-09-10 | 2015-02-18 | 徐伟佳 | A kind of unmanned plane thermal imaging system |
| CN204258975U (en) * | 2014-12-05 | 2015-04-08 | 锦州联升汽车零部件有限公司 | The night vision applications of a kind of UAV flight |
| CN204462869U (en) * | 2015-04-08 | 2015-07-08 | 王全超 | Unmanned plane zoom The Cloud Terrace |
| CN204473155U (en) * | 2015-02-07 | 2015-07-15 | 赵保安 | Based on the thermal imaging system detecting device of rotor unmanned aircraft |
| CN204515542U (en) * | 2015-03-27 | 2015-07-29 | 深圳市科卫泰实业发展有限公司 | A kind of fast-spliced twin-lens diaxon is from steady cradle head device |
| CN204883296U (en) * | 2015-05-26 | 2015-12-16 | 天津飞腾世纪自动化科技有限公司 | Unattended system of transformer substation based on PLC controlling means |
| CN205071207U (en) * | 2015-10-26 | 2016-03-02 | 广东图谷网络科技有限公司 | Miniature slope image data acquires nacelle |
| CN205537971U (en) * | 2016-02-25 | 2016-08-31 | 南京钟山苑航空技术有限公司 | Infrared thermal imaging nacelle |
| CN206683762U (en) * | 2017-04-11 | 2017-11-28 | 国网辽宁省电力有限公司辽阳供电公司 | A kind of work high above the ground thermal imaging system control device |
-
2017
- 2017-04-11 CN CN201710230929.7A patent/CN106895922A/en active Pending
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2415562Y (en) * | 2000-02-25 | 2001-01-17 | 周国起 | Mine infrared night vision camera apparatus |
| CN103051871A (en) * | 2012-12-10 | 2013-04-17 | 天津中科遥感信息技术有限公司 | Special portable thermal infrared camera system for unmanned aerial vehicle |
| CN103235602A (en) * | 2013-03-25 | 2013-08-07 | 山东电力集团公司电力科学研究院 | Automatic photography control device for power line inspection unmanned aerial vehicle, and control method thereof |
| CN204166392U (en) * | 2014-09-10 | 2015-02-18 | 徐伟佳 | A kind of unmanned plane thermal imaging system |
| CN204258975U (en) * | 2014-12-05 | 2015-04-08 | 锦州联升汽车零部件有限公司 | The night vision applications of a kind of UAV flight |
| CN204473155U (en) * | 2015-02-07 | 2015-07-15 | 赵保安 | Based on the thermal imaging system detecting device of rotor unmanned aircraft |
| CN204515542U (en) * | 2015-03-27 | 2015-07-29 | 深圳市科卫泰实业发展有限公司 | A kind of fast-spliced twin-lens diaxon is from steady cradle head device |
| CN204462869U (en) * | 2015-04-08 | 2015-07-08 | 王全超 | Unmanned plane zoom The Cloud Terrace |
| CN204883296U (en) * | 2015-05-26 | 2015-12-16 | 天津飞腾世纪自动化科技有限公司 | Unattended system of transformer substation based on PLC controlling means |
| CN205071207U (en) * | 2015-10-26 | 2016-03-02 | 广东图谷网络科技有限公司 | Miniature slope image data acquires nacelle |
| CN205537971U (en) * | 2016-02-25 | 2016-08-31 | 南京钟山苑航空技术有限公司 | Infrared thermal imaging nacelle |
| CN206683762U (en) * | 2017-04-11 | 2017-11-28 | 国网辽宁省电力有限公司辽阳供电公司 | A kind of work high above the ground thermal imaging system control device |
Non-Patent Citations (1)
| Title |
|---|
| 张磊: "无人机红外影像技术在配电网巡检中的应用研究", 《中国高新技术企业》 * |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN108033015A (en) | A kind of unmanned plane device and method for the monitoring of coal gangue hill ignition point | |
| CN107147710A (en) | A kind of power network unmanned plane inspection management control device | |
| CN101393246B (en) | Mini robot for detecting internal failure of power transformer | |
| CN201674162U (en) | Electric power maintenance helicopter | |
| CN205176658U (en) | Infrared unmanned aerial vehicle of photovoltaic power plant intelligence fortune dimension device | |
| CN207896741U (en) | A kind of intelligent substation inspection system | |
| CN102097860A (en) | Intelligent robot patrol system for safety detection of substation | |
| CN104122891A (en) | Intelligent robot inspection system for city underground railway detection | |
| CN205918206U (en) | Communication tower safety monitoring system | |
| CN202197057U (en) | UAV (unmanned aerial vehicle) aircraft patrol system for power transmission line | |
| CN106903667A (en) | Relay protection room inspecting robot | |
| CN111857178A (en) | Unmanned aerial vehicle system for safety inspection of construction site of building construction | |
| CN108055003A (en) | A kind of autonomous inspection device of unmanned plane based on double light intelligent loads | |
| CN206683762U (en) | A kind of work high above the ground thermal imaging system control device | |
| CN110267004A (en) | A kind of small drone detection monitoring system | |
| CN106767683A (en) | Measurement apparatus and method of a kind of unmanned plane of electronic information field to ground level | |
| CN106895922A (en) | A kind of work high above the ground thermal imaging system control device | |
| CN206937299U (en) | Relay protection room inspecting robot | |
| CN206594254U (en) | A kind of distribution line failure monitoring device | |
| CN209168187U (en) | A kind of power-line patrolling system | |
| CN207977941U (en) | A kind of autonomous inspection device of unmanned plane based on double light intelligent loads | |
| CN205724666U (en) | Power circuit polling system | |
| CN207751515U (en) | A kind of online environment monitoring system | |
| CN207198323U (en) | A kind of search and rescue positioner based on power transmission tower | |
| CN206060685U (en) | A kind of photovoltaic panel hot spot effect detecting system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170627 |
|
| RJ01 | Rejection of invention patent application after publication |