CN204096095U - A kind of unmanned plane full angle image aerial device - Google Patents
A kind of unmanned plane full angle image aerial device Download PDFInfo
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- CN204096095U CN204096095U CN201420496319.3U CN201420496319U CN204096095U CN 204096095 U CN204096095 U CN 204096095U CN 201420496319 U CN201420496319 U CN 201420496319U CN 204096095 U CN204096095 U CN 204096095U
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Abstract
The utility model discloses a kind of unmanned plane full angle image aerial device, it comprises unmanned plane body, this unmanned plane full angle image aerial device comprises a full angle image instrument further, described full angle image instrument is fixedly installed in the downside of unmanned plane body fuselage, described full angle image instrument comprises pick-up head mounting structure and multiple camera, and described multiple camera is installed and is uniformly distributed in the side of pick-up head mounting structure.The utility model adopts the structure of taking photo by plane of annular shooting head group, can realize carrying out full angle image collection to region of taking photo by plane, without the need to the unmanned plane that hovers, provide work efficiency, and need not configure motor and cradle head structure, alleviates unmanned plane burden, cost-saving.
Description
Technical field
The utility model relates to unmanned air vehicle technique field, is specifically related to a kind of unmanned plane full angle image aerial device.
Background technology
Unmanned plane, because of its have maneuverability, reaction fast, unmanned flight and the advantage such as operation requirements is low, it can realize the image real-time Transmission under the conditions such as high-risk areas by carrying multiclass sensor, is that satellite remote sensing and the strong of traditional air remote sensing supplement.At present, unmanned plane of taking photo by plane all is widely used in fields such as electric power, communication, meteorology, agricultural, oceans.
For power industry, unmanned plane, by the aerial device that it is arranged, can be patrolled and examined overhead transmission line and shaft tower etc.Existing unmanned plane aerial device mostly comprises visible ray digital camera head and whether to occur disconnected stock, circuit physical imperfection to circuit or whether to hang with foreign matter etc. monitors, usually, visible ray digital camera head is installed on a The Cloud Terrace, when certain region is patrolled and examined, after needing unmanned plane to hover, controlled by the direction of motor to The Cloud Terrace, thus realize the full angle image collection of patrolling and examining region.Although this mode can carry out comprehensive monitoring to patrolling and examining region to a certain extent, but its hovering needs time of overspending, and the motor controlled The Cloud Terrace adds the weight of unmanned plane, while causing the alerting ability of unmanned plane to reduce, also make the expense of patrolling and examining too high.
Utility model content
For above deficiency, the purpose of this utility model is to provide a kind of unmanned plane full angle image aerial device, and it, by the fit structure of annular shooting head group, can realize carrying out full angle image collection to region of taking photo by plane, cost-saving, raises the efficiency.
For realizing above object, the technical scheme that the utility model is taked is:
A kind of unmanned plane full angle image aerial device, it comprises unmanned plane body, this unmanned plane full angle image aerial device comprises a full angle image instrument further, described full angle image instrument is fixedly installed in the downside of unmanned plane body fuselage, described full angle image instrument comprises pick-up head mounting structure and multiple camera, and described multiple camera is installed and is uniformly distributed in the side of pick-up head mounting structure.
Described pick-up head mounting structure is hemispherical dome structure.
Described full angle image instrument is installed on unmanned plane body by a fixed support.
Described fixed support comprises integrated pipe link and goalpost, is provided with the ball groove matched with goalpost in described pick-up head mounting structure, and described goalpost is installed in this ball groove to realize pick-up head mounting structure and fixed support is rotatably connected.
Described multiple camera is 4 ~ 8, is preferably 8.
Described unmanned plane body is depopulated helicopter or rotor wing unmanned aerial vehicle.
This unmanned plane full angle image aerial device comprises a ultrasonic range finder further, and described ultrasonic range finder is installed on the downside of unmanned plane body fuselage, and compared with the head of full angle image instrument near unmanned plane body.
Compared with prior art, its beneficial effect is the utility model:
1, adopt the structure of taking photo by plane of annular shooting head group, can realize carrying out full angle image collection to region of taking photo by plane, without the need to the unmanned plane that hovers, provide work efficiency, and motor and cradle head structure need not be configured, alleviate unmanned plane burden, cost-saving.
2, fixed support and full angle image instrument adopt the fit structure of trough for used balls and goalpost, 360 ° of rotations can be realized, when unmanned plane nonlevel flight, full angle image instrument relies on self gravitation to realize and support bracket fastened rotation, ensure that the full angle image instrument moment is horizontal and takes photo by plane.
3, on front side of unmanned plane, ultrasonic range finder is set, whether has obstacle with sensorcraft front, ensure that the safety of unmanned plane during flying.
Accompanying drawing explanation
Fig. 1 is the structural representation of a kind of unmanned plane full angle of the utility model image aerial device.
Fig. 2 is the structural representation of full angle image instrument;
Fig. 3 is full angle image instrument and support bracket fastened fit structure schematic diagram.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, content of the present utility model is described in further details.
Embodiment
Please refer to shown in Fig. 1-2, a kind of unmanned plane full angle image aerial device, it comprises unmanned plane body 1, full angle image instrument 2 and ultrasonic range finder 5, wherein, unmanned plane body 1 can adopt depopulated helicopter or rotor wing unmanned aerial vehicle, full angle image instrument 2 and ultrasonic range finder 5 are all fixedly installed in the downside of unmanned plane body 1 fuselage, and ultrasonic range finder 5 is positioned at the front side of full angle apomecometer 2, and namely ultrasonic range finder is closer to the Handpiece Location of unmanned plane body 1.Full angle image instrument 2 comprises pick-up head mounting structure 22 and multiple camera 21, and multiple camera 21 is installed and is uniformly distributed in the side of pick-up head mounting structure 22.Camera 21 adopts 4-8 can realize full angle image collection.Be preferably 8, each like this angle has at least 2 cameras to take it, and namely each angle can form perspective view.Coordinate between camera 21 and form full angle intersection image, thus produce degree of depth image effect, obtain full angle image, by this kind of style of shooting, each angle can be taken, avoid the difficult problem that the shooting of traditional unmanned plane exists dead angle, simultaneously because each angle can be taken, operator only needs the control of carrying out taking path to unmanned plane, without the need to controlling camera angle, simplify human users, improve operating efficiency, reduce operational risk.Camera 21 can adopt Multiple Type, and such as adopt sports type camera, it has 1,200 ten thousand pixels, resolution Fps fps 4K/4K, can carry out impact shooting, carry Protune pattern in high-speed motion, instruments weight is no more than 1 kilogram, and power is no more than 100 watts.Pick-up head mounting structure 22 can adopt the hemispherical dome structure shown in Fig. 2, also can adopt rectangular structure.Each angle has at least 2 cameras to take it, and namely each angle can form perspective view.Whether ultrasonic range finder 5 has obstacle as effective distance measuring device sensorcraft front the most directly perceived, for the flight safety of unmanned plane body 1 provides guarantee.Ultrasonic range finder 5 can adopt multiplex ultrasonic sensor combined action to hinder and path planning to complete keeping away of whole unmanned plane body 1, ultrasonic transduter can select Multiple Type, such as select MINI-AE type ultrasonic transduter, it is measuring distance 10 meters farthest, frequency of operation 10HZ to 50HZ, weight is no more than 2 kilograms, and power is no more than 5 watts.
In order to prevent unmanned plane body 1 nonlevel flight (such as turn or side fly time) time, the angle of taking photo by plane of full angle image instrument 2 changes, in the utility model preferred embodiment, balling-up access node structure being set by connecting full angle image instrument 2 and the fixed support of unmanned plane body 1 fuselage and the fit structure of full angle image instrument 2,360 ° of rotations can being realized to realize fixed support on full angle image instrument 2.Particularly, please refer to shown in Fig. 3, fixed support comprises integrated pipe link 4 and goalpost 3, is provided with the ball groove matched with goalpost 3 in pick-up head mounting structure 22, and goalpost 3 is installed in this ball groove and is rotatably connected with fixed support to realize pick-up head mounting structure 22.Like this, when 1 nonlevel flight of unmanned plane body, full angle image instrument 2 is still in horizontality after relying on self gravitation to make to rotate between itself and fixed support, thus does not affect the effect of taking photo by plane.
Above-listed detailed description is illustrating for the utility model possible embodiments, and this embodiment is also not used to limit the scope of the claims of the present utility model, does not allly depart from the equivalence that the utility model does and implements or change, and all should be contained in the scope of the claims of this case.
Claims (7)
1. a unmanned plane full angle image aerial device, it comprises unmanned plane body (1), it is characterized in that, this unmanned plane full angle image aerial device comprises a full angle image instrument (2) further, described full angle image instrument (2) is fixedly installed in the downside of unmanned plane body (1) fuselage, described full angle image instrument (2) comprises pick-up head mounting structure (22) and multiple camera (21), and described multiple camera (21) is installed and is uniformly distributed in the side of pick-up head mounting structure (22).
2. unmanned plane full angle image aerial device according to claim 1, it is characterized in that, described pick-up head mounting structure (22) is hemispherical dome structure.
3. unmanned plane full angle image aerial device according to claim 2, is characterized in that, described full angle image instrument (2) is installed on unmanned plane body (1) by a fixed support.
4. unmanned plane full angle image aerial device according to claim 3, it is characterized in that, described fixed support comprises integrated pipe link (4) and goalpost (3), be provided with the ball groove matched with goalpost (3) in described pick-up head mounting structure (22), described goalpost (3) is installed in this ball groove and is rotatably connected with fixed support to realize pick-up head mounting structure (22).
5. unmanned plane full angle image aerial device according to claim 1, is characterized in that, described multiple camera (21) is 4 ~ 8.
6. unmanned plane full angle image aerial device according to claim 1, is characterized in that, described unmanned plane body (1) is depopulated helicopter or rotor wing unmanned aerial vehicle.
7. unmanned plane full angle image aerial device according to claim 1, it is characterized in that, this unmanned plane full angle image aerial device comprises a ultrasonic range finder (5) further, described ultrasonic range finder (5) is installed on the downside of unmanned plane body (1) fuselage, and comparatively full angle image instrument (2) near the head of unmanned plane body (1).
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| Application Number | Priority Date | Filing Date | Title |
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| CN201420496319.3U CN204096095U (en) | 2014-09-01 | 2014-09-01 | A kind of unmanned plane full angle image aerial device |
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| CN201420496319.3U CN204096095U (en) | 2014-09-01 | 2014-09-01 | A kind of unmanned plane full angle image aerial device |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105277177A (en) * | 2015-10-17 | 2016-01-27 | 佛山市安尔康姆航空科技有限公司 | Oblique photography system adopting multi-rotor unmanned aerial vehicle |
| CN105292379A (en) * | 2015-11-19 | 2016-02-03 | 中国船舶工业系统工程研究院 | Visual display testing method for ship air flow field |
| CN105391950A (en) * | 2015-12-23 | 2016-03-09 | 北京观著信息技术有限公司 | Miniature inclined photographing camera system |
| CN106428545A (en) * | 2016-10-31 | 2017-02-22 | 朱建萍 | Three-dimensional geographic information collecting system and collecting method thereof |
| CN106851127A (en) * | 2016-12-25 | 2017-06-13 | 重庆警蜂科技有限公司 | Circuit court shoots with video-corder terminal with multi-angle |
| CN107168005A (en) * | 2017-06-12 | 2017-09-15 | 上海微小卫星工程中心 | Big breadth optical imaging method based on rotation |
| CN107168006A (en) * | 2017-06-12 | 2017-09-15 | 上海微小卫星工程中心 | Big breadth optical imaging system based on rotation |
| CN110091991A (en) * | 2019-04-15 | 2019-08-06 | 中国建筑第八工程局有限公司 | Gravity self-balancing laser range finder for small drone |
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2014
- 2014-09-01 CN CN201420496319.3U patent/CN204096095U/en active Active
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105277177A (en) * | 2015-10-17 | 2016-01-27 | 佛山市安尔康姆航空科技有限公司 | Oblique photography system adopting multi-rotor unmanned aerial vehicle |
| CN105292379A (en) * | 2015-11-19 | 2016-02-03 | 中国船舶工业系统工程研究院 | Visual display testing method for ship air flow field |
| CN105391950A (en) * | 2015-12-23 | 2016-03-09 | 北京观著信息技术有限公司 | Miniature inclined photographing camera system |
| CN105391950B (en) * | 2015-12-23 | 2019-02-19 | 北京观著信息技术有限公司 | Miniature oblique photograph camera system |
| CN106428545A (en) * | 2016-10-31 | 2017-02-22 | 朱建萍 | Three-dimensional geographic information collecting system and collecting method thereof |
| CN106851127A (en) * | 2016-12-25 | 2017-06-13 | 重庆警蜂科技有限公司 | Circuit court shoots with video-corder terminal with multi-angle |
| CN106851127B (en) * | 2016-12-25 | 2019-06-21 | 重庆警蜂科技有限公司 | Circuit court shoots with video-corder terminal with multi-angle |
| CN107168005A (en) * | 2017-06-12 | 2017-09-15 | 上海微小卫星工程中心 | Big breadth optical imaging method based on rotation |
| CN107168006A (en) * | 2017-06-12 | 2017-09-15 | 上海微小卫星工程中心 | Big breadth optical imaging system based on rotation |
| CN107168006B (en) * | 2017-06-12 | 2019-06-04 | 上海微小卫星工程中心 | Big breadth optical imaging system based on rotation |
| CN107168005B (en) * | 2017-06-12 | 2019-10-01 | 上海微小卫星工程中心 | Big breadth optical imaging method based on rotation |
| CN110091991A (en) * | 2019-04-15 | 2019-08-06 | 中国建筑第八工程局有限公司 | Gravity self-balancing laser range finder for small drone |
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