CN201647126U - Suspended cabin for helicopter power inspection - Google Patents
Suspended cabin for helicopter power inspection Download PDFInfo
- Publication number
- CN201647126U CN201647126U CN2010201560347U CN201020156034U CN201647126U CN 201647126 U CN201647126 U CN 201647126U CN 2010201560347 U CN2010201560347 U CN 2010201560347U CN 201020156034 U CN201020156034 U CN 201020156034U CN 201647126 U CN201647126 U CN 201647126U
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- gondola
- camera
- helicopter
- support
- servomotor
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- Expired - Lifetime
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- 238000007689 inspection Methods 0.000 title claims abstract description 30
- 238000000034 method Methods 0.000 claims description 25
- 238000010521 absorption reaction Methods 0.000 claims description 11
- 230000035939 shock Effects 0.000 claims description 11
- 230000008878 coupling Effects 0.000 claims description 4
- 238000010168 coupling process Methods 0.000 claims description 4
- 238000005859 coupling reaction Methods 0.000 claims description 4
- 239000000725 suspension Substances 0.000 abstract 2
- 230000036544 posture Effects 0.000 abstract 1
- 230000002950 deficient Effects 0.000 description 6
- 230000003287 optical effect Effects 0.000 description 6
- 230000007547 defect Effects 0.000 description 4
- 125000004122 cyclic group Chemical group 0.000 description 2
- 238000001514 detection method Methods 0.000 description 2
- 238000010835 comparative analysis Methods 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 208000024891 symptom Diseases 0.000 description 1
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Abstract
The utility model discloses a suspended cabin for helicopter power inspection, which comprises a cabin body, a cabin support and a mounting rack. A suspension structure connected with an external suspension joint of a helicopter is arranged on the upper portion of the mounting rack, the cabin support is mounted below the mounting rack through a rotating device controlled by a servomotor, two ends of the cabin body are respectively pivotally mounted at two ends of the cabin support through pivot structures, a rotating mechanism controlled by the servomotor is arranged between the cabin body and the cabin support, and an infrared camera, a visible light camera and an ultraviolet camera are mounted inside the cabin body. The cameras for power inspection are integrated into one suspended cabin, thereby facilitating centralized management and control, and preventing the cameras in working from being affected by flying postures of the helicopter and external wind speed.
Description
Technical field
The utility model relates to a kind of gondola, particularly a kind of gondola of the time shooting usefulness that is used for helicopter in electric inspection process.
Background technology
Electric inspection process adopts the mode of manual inspection hand-kept more, and work capacity is huge, inefficiency, and the cyclic in-position measuring rate is low, and omission, false retrieval phenomenon are often arranged, and adopts paper notes record accident defect, and subjective factor is many, and fault report is described and is differed, can't the Fast Classification arrangement.Electric power enterprise is strengthened informatization in order to cut operating costs, improve effectiveness of operation, adopts modern patrolling and checking management system imperative.
The situation that puts in place and defect statistics also are that defective is maked an inspection tour a main difficult problem that exists in the management work.Become increasingly conspicuous circuit and substation periodical inspection of cyclic in-position measuring rate that power network development, unattended operation transformer station increase bring and the problem of patrolling and examining quality monitoring lacks important line section and the substation that emphasis, particularly commute wreck.Track walker's know-how is uneven, only judges not standard reference at the scene easily at the scene by rule of thumb.The equipment of need patrolling and examining is large in number and widely distributed, and it is poor that track walker's sense of responsibility has." does track walker put in place? whether fault grading accurate? how does Symptom quantize? " the tour report content is multifarious, to the description disunity with a kind of defective, makes the higher level operating personal can't judge the classification of defective, more can't arrange to handle.Defect report quantity is very big in the mensal tour cycle, with repeating to report defective, at all can't taxonomic revision by manpower, and the foundation of science also just can not be provided for the elimination defective.Manually transcribe fault report and make work capacity huge, the efficient that defective is maked an inspection tour reduces, and the defect report book is difficult for preserving.The mode of hand-made paper record in numerous and diverse data statistics, also also is unfavorable for real work because efficient is low, loaded down with trivial details.Existing production management system class is numerous, multifarious, but lacking the actv. means integrates all data.
In view of the foregoing, electric inspection process is just having the trend of marching toward and patrolling and examining automatically with helicopter, it all is the support that the pick up camera that is used for electric inspection process is directly installed on helicopter that but existing helicopter is patrolled and examined, and can not live very much when this method is used, and is difficult to adjust image pickup scope and the angle wanted; In addition, use a kind of pick up camera incessantly usually during electric inspection process, the angle of field of each camera photography, image pickup scope and camera angle all are used, so pick up camera is directly installed on unified control and the management that is unfavorable for pick up camera on the support of helicopter.
The utility model content
Task of the present utility model is: a kind of gondola that is used for helicopter in electric inspection process is provided, and this gondola is installed in a plurality of pick up cameras that are used for electric inspection process in the gondola, is convenient to unified management and control, follows the trail of photographic subjects automatically by the angle of control gondola.
The technical solution of the utility model is as follows:
A kind of gondola that is used for helicopter in electric inspection process, it is characterized in that: this gondola comprises gondola body, gondola support and erecting frame, the top of erecting frame is provided with and helicopter hard disk bonded assembly hanging structure, the gondola support is installed in the erecting frame below by the slewing arrangement by servomotor control, the two ends of gondola body articulate by pin-jointed structure respectively and are installed on the two ends of gondola support, be provided with rotating mechanism between gondola body and the gondola support, noctovisor, visible light camera and ultraviolet pick up camera are installed in the gondola body by servomotor control.
Described slewing arrangement by servomotor control comprises servomotor, driving gear and driven gear, servomotor is installed in the erecting frame, the turning cylinder of driving gear and servomotor is coupling, and driven gear is horizontally set on the top of gondola support, and driving gear is meshed with driven gear.
The camera lens of described noctovisor, visible light camera and ultraviolet pick up camera is towards the same side of gondola body, noctovisor is arranged on the left upper portion of gondola body, visible light camera is arranged on the bottom, left side of gondola body, and the ultraviolet pick up camera is arranged on the right side of gondola body.
The angle of field and the camera angle of described noctovisor, visible light camera and ultraviolet pick up camera are consistent.
Described erecting frame comprises stay bearing plate and shock absorption device, and shock absorption device is arranged on the stay bearing plate bottom, and described slewing arrangement by servomotor control is arranged between shock absorption device and the gondola support.
Described gondola support comprises a biside plate and a transverse slat, the upper end of biside plate vertically is arranged on the two ends, the left and right sides of transverse slat, the middle part of transverse slat is connected with described slewing arrangement by servomotor control, and the two ends, the left and right sides of gondola body articulate the bottom that is installed in biside plate by pin-jointed structure.
Also be provided with laser rangefinder in the gondola body.
The utility model has the advantages that: the pick up camera that is used for electric inspection process is arranged in the gondola body, and the pick up camera that is used in electric inspection process obtains certain protection, and shock absorption device is set on erecting frame, and the protection pick up camera is avoided the influence of helicopter vibrations; Noctovisor, visible light camera and ultraviolet pick up camera that electric inspection process is commonly used are installed concentratedly in the gondola body, helped unified control and management; Can adjust the angle and the camera angle of gondola easily by servomotor and airborne control program, to realize following the trail of automatically photographic subjects.
Description of drawings
The utility model is described in more detail below in conjunction with accompanying drawing,
Fig. 1 is a kind of front view scheme drawing that is used for the gondola of helicopter in electric inspection process of the utility model;
Fig. 2 is a kind of lateral plan scheme drawing that is used for the gondola of helicopter in electric inspection process of the utility model;
Fig. 3 is a kind of inner structure scheme drawing that is used for the gondola of helicopter in electric inspection process of the utility model.
The specific embodiment
A kind of gondola that is used for helicopter in electric inspection process, as Figure 1-3, comprise gondola body 3, gondola support 2 and erecting frame 1, the top of erecting frame 1 is provided with and helicopter hard disk bonded assembly hanging structure 101, gondola support 2 is installed in erecting frame 1 below by the slewing arrangement 4 by servomotor control, control gondola support 2 left-right rotation in the horizontal direction by servomotor, accurately adjust the angle of gondola support 2, the two ends of gondola body 3 articulate by pin-jointed structure respectively and are installed on the two ends of gondola support 2, be provided with rotating mechanism 5 between gondola body 3 and the gondola support 2 by servomotor control, rotating mechanism 5 control gondola bodies 3 by servomotor control rotate up and down in vertical direction, accurately control the rotational angle of gondola body 3, noctovisor 6 is installed in the gondola body 3, visible light camera 7 and ultraviolet pick up camera 8 are controlled noctovisor 6 in the gondola body 3 by the angle of adjusting gondola support 2 and gondola body 3, the camera angle of visible light camera 7 and ultraviolet pick up camera 8.
Above-mentioned pin-jointed structure specifically comprises rotating shaft, and an end of rotating shaft is connected with an end of gondola support 2, and the other end of rotating shaft extend in the axle sleeve on the gondola body 3, in the axle sleeve bearing can be set, and gondola body 3 can rotate around the axis.
The camera lens of noctovisor 6, visible light camera 7 and ultraviolet pick up camera 8 is towards the same side of gondola body 3, noctovisor 6 is arranged on the left upper portion of gondola body 3, visible light camera 7 is arranged on the bottom, left side of gondola body 3, and ultraviolet pick up camera 8 is arranged on the right side of gondola body 3.With noctovisor 6 detection electric wireline and electric wireline shaft tower whether overheated place is arranged, whether the thermal map that detects electric wireline and electric wireline shaft tower is normal; Tangible physical imperfection whether occurs or do not hang with foreign matter etc. with visible light camera 7 detection electric wireline and electric wireline shaft tower; Detect corona and flashover situation with ultraviolet pick up camera 8.
The angle of field and the camera angle of noctovisor 6, visible light camera 7 and ultraviolet pick up camera 8 are consistent, and the graphicinformation that noctovisor 6, visible light camera 7 and ultraviolet pick up camera 8 are obtained conveniently is used for comparative analysis.
Erecting frame comprises stay bearing plate 102 and shock absorption device 103, and shock absorption device 103 is arranged on stay bearing plate 102 bottoms, and described slewing arrangement 4 by servomotor control is arranged between shock absorption device 103 and the gondola support 2.Installing damping device 103 can be avoided the influence that helicopter shakes by actv. protection gondola body 3 interior pick up cameras, and the actv. of doing has been protected the safety of pick up camera.
In the gondola body 3 laser rangefinder can also be set, measure the distance of helicopter distance objective with laser rangefinder.
The utility model is concentrated noctovisor 6, visible light camera 7 and ultraviolet pick up camera 8 and is arranged in the gondola body 3, can eliminate the interference of helicopter vibration and swing, guarantee optical axis spatial stability, and enough big search, tracking field is provided, realize variation and control that the optical axis points to.
Gondola is during with helicopter flight, causes except being subjected to helicopter flight attitude angle variable effect the optical axis orientation stability descends, and also will be subjected to Influences on Wind Velocity.The helicopter high-speed flight, make be exposed to outside the fuselage gondola body 3 be subjected to constantly that numerical value is bigger, the moment of wind resistance disturbing influence of random variation, also cause and stablize the optical axis orientation stability and reduce.This method of designing of the utility model makes the air draught that acts on gondola body 3 can directly not affact input axis and fastens, guarantee that noctovisor 6, visible light camera 7 and ultraviolet pick up camera 8 are not subjected to the influence of extraneous air draught, its optical axis has the advantages of higher stability precision.The utility model can guarantee that noctovisor 6, visible light camera 7 and ultraviolet pick up camera 8 neither are subjected to the influence of resisting moment, can isolate helicopter driftage, pitching and roll motion again, makes platform have high optical axis stable precision and bigger search coverage.
Claims (7)
1. gondola that is used for helicopter in electric inspection process, it is characterized in that: this gondola comprises gondola body, gondola support and erecting frame, the top of erecting frame is provided with and helicopter hard disk bonded assembly hanging structure, the gondola support is installed in the erecting frame below by the slewing arrangement by servomotor control, the two ends of gondola body articulate by pin-jointed structure respectively and are installed on the two ends of gondola support, be provided with rotating mechanism between gondola body and the gondola support, noctovisor, visible light camera and ultraviolet pick up camera are installed in the gondola body by servomotor control.
2. the gondola that is used for helicopter in electric inspection process according to claim 1, it is characterized in that: described slewing arrangement by servomotor control comprises servomotor, driving gear and driven gear, servomotor is installed in the erecting frame, the turning cylinder of driving gear and servomotor is coupling, driven gear is horizontally set on the top of gondola support, and driving gear is meshed with driven gear.
3. the gondola that is used for helicopter in electric inspection process according to claim 1, it is characterized in that: the camera lens of described noctovisor, visible light camera and ultraviolet pick up camera is towards the same side of gondola body, noctovisor is arranged on the left upper portion of gondola body, visible light camera is arranged on the bottom, left side of gondola body, and the ultraviolet pick up camera is arranged on the right side of gondola body.
4. the gondola that is used for helicopter in electric inspection process according to claim 3 is characterized in that: the angle of field and the camera angle of described noctovisor, visible light camera and ultraviolet pick up camera are consistent.
5. be used for the gondola of helicopter in electric inspection process according to described any one of claim 1-4, it is characterized in that: described erecting frame comprises stay bearing plate and shock absorption device, shock absorption device is arranged on the stay bearing plate bottom, and described slewing arrangement by servomotor control is arranged between shock absorption device and the gondola support.
6. be used for the gondola of helicopter in electric inspection process according to described any one of claim 1-4, it is characterized in that: described gondola support comprises a biside plate and a transverse slat, the upper end of biside plate vertically is arranged on the two ends, the left and right sides of transverse slat, the middle part of transverse slat is connected with described slewing arrangement by servomotor control, and the two ends, the left and right sides of gondola body articulate the bottom that is installed in biside plate by pin-jointed structure.
7. be used for the gondola of helicopter in electric inspection process according to described any one of claim 1-4, it is characterized in that: also be provided with laser rangefinder in the described gondola body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010201560347U CN201647126U (en) | 2010-04-12 | 2010-04-12 | Suspended cabin for helicopter power inspection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010201560347U CN201647126U (en) | 2010-04-12 | 2010-04-12 | Suspended cabin for helicopter power inspection |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201647126U true CN201647126U (en) | 2010-11-24 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010201560347U Expired - Lifetime CN201647126U (en) | 2010-04-12 | 2010-04-12 | Suspended cabin for helicopter power inspection |
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| CN (1) | CN201647126U (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102679114A (en) * | 2011-12-13 | 2012-09-19 | 河南科技大学 | Hoisting chamber |
| CN102856840A (en) * | 2012-09-29 | 2013-01-02 | 江苏省电力公司徐州供电公司 | Auxiliary suspension device of power inspection aircraft |
| CN102874413A (en) * | 2012-10-12 | 2013-01-16 | 北京航空航天大学 | Method and tail fin for improving flight stability of hung object of helicopter |
| CN104571140A (en) * | 2014-11-20 | 2015-04-29 | 中国建材检验认证集团股份有限公司 | Photovoltaic module routing inspection photographing control system |
| CN105607639A (en) * | 2015-12-21 | 2016-05-25 | 河北汉光重工有限责任公司 | Posture solving and compensating method for triaxial stable servo platform |
| CN106043721A (en) * | 2016-05-26 | 2016-10-26 | 北京北科天绘科技有限公司 | Helicopter laser radar nacelle |
| CN106428590A (en) * | 2016-08-03 | 2017-02-22 | 国网山东省电力公司青岛供电公司 | Aerial photography line patrol cradle head and aerial photography line patrol device |
| CN106471358A (en) * | 2014-04-22 | 2017-03-01 | 高空遥控器股份有限公司 | The fault detection detection system of solar panel |
| CN108438244A (en) * | 2018-04-27 | 2018-08-24 | 南京拓威航空科技有限公司 | A kind of airborne aerial device and the unmanned plane containing it |
| CN115196031A (en) * | 2022-09-15 | 2022-10-18 | 国网电力空间技术有限公司 | Power grid equipment shooting device for helicopter |
-
2010
- 2010-04-12 CN CN2010201560347U patent/CN201647126U/en not_active Expired - Lifetime
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102679114B (en) * | 2011-12-13 | 2014-04-16 | 河南科技大学 | Hoisting chamber |
| CN102679114A (en) * | 2011-12-13 | 2012-09-19 | 河南科技大学 | Hoisting chamber |
| CN102856840B (en) * | 2012-09-29 | 2016-03-23 | 江苏省电力公司徐州供电公司 | A kind of auxiliary suspension device of power inspection aircraft |
| CN102856840A (en) * | 2012-09-29 | 2013-01-02 | 江苏省电力公司徐州供电公司 | Auxiliary suspension device of power inspection aircraft |
| CN102874413A (en) * | 2012-10-12 | 2013-01-16 | 北京航空航天大学 | Method and tail fin for improving flight stability of hung object of helicopter |
| CN106471358A (en) * | 2014-04-22 | 2017-03-01 | 高空遥控器股份有限公司 | The fault detection detection system of solar panel |
| CN104571140A (en) * | 2014-11-20 | 2015-04-29 | 中国建材检验认证集团股份有限公司 | Photovoltaic module routing inspection photographing control system |
| CN104571140B (en) * | 2014-11-20 | 2017-10-27 | 中国建材检验认证集团股份有限公司 | A kind of photovoltaic module inspection is taken pictures control system |
| CN105607639A (en) * | 2015-12-21 | 2016-05-25 | 河北汉光重工有限责任公司 | Posture solving and compensating method for triaxial stable servo platform |
| CN106043721A (en) * | 2016-05-26 | 2016-10-26 | 北京北科天绘科技有限公司 | Helicopter laser radar nacelle |
| CN106043721B (en) * | 2016-05-26 | 2019-04-23 | 北京北科天绘科技有限公司 | A helicopter lidar pod |
| CN106428590A (en) * | 2016-08-03 | 2017-02-22 | 国网山东省电力公司青岛供电公司 | Aerial photography line patrol cradle head and aerial photography line patrol device |
| CN108438244A (en) * | 2018-04-27 | 2018-08-24 | 南京拓威航空科技有限公司 | A kind of airborne aerial device and the unmanned plane containing it |
| CN115196031A (en) * | 2022-09-15 | 2022-10-18 | 国网电力空间技术有限公司 | Power grid equipment shooting device for helicopter |
| CN115196031B (en) * | 2022-09-15 | 2022-12-20 | 国网电力空间技术有限公司 | Power grid equipment shooting device for helicopter |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20101124 |
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| CX01 | Expiry of patent term |