CN205131672U - Unmanned aerial vehicle with binocular vision structure - Google Patents
Unmanned aerial vehicle with binocular vision structure Download PDFInfo
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- CN205131672U CN205131672U CN201520872642.0U CN201520872642U CN205131672U CN 205131672 U CN205131672 U CN 205131672U CN 201520872642 U CN201520872642 U CN 201520872642U CN 205131672 U CN205131672 U CN 205131672U
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Abstract
The utility model discloses an unmanned aerial vehicle with binocular vision structure, including unmanned aerial vehicle body, mount, detecting device, the mount set up in the lower part of unmanned aerial vehicle body, detecting device is connected with the unmanned aerial vehicle body through the mount, the utility model discloses, set up the binocular vision structure first camera and second camera, first camera is infrared imager, infrared imager is used for gathering infrared image information, the second camera is color video camera, color video camera is used for gathering color image information, detecting device sends infrared image information and color image information for control system through communication module, can solve the unable problem that satisfies based on the detection precision demand of video analysis under the multiple scene through analysis infrared image information and color image information, can satisfy user's user demand.
Description
Technical field
The utility model belongs to fire fighting monitoring technical field, particularly relates to a kind of unmanned plane with binocular vision structure.
Background technology
Robot airplane is called for short " unmanned plane ", and english abbreviation is " UAV ", is the not manned aircraft utilizing radio robot to handle with the process controller provided for oneself.Unmanned plane, by application, can be divided into military and civilian.Unmanned plane is of many uses at civil area, is mainly used in the industries such as police, city management, agricultural, geology, meteorology, electric power, rescue and relief work, video capture.
Along with socioeconomic fast development, detector has been widely applied in the middle of fields such as comprising fire prevention, traffic, Intelligent Recognition.In some cases, detector cannot carry out monitoring effectively and timely, is especially difficult to the place arrived at harsh environment and personnel.Therefore, the unmanned plane with detector is devised out by people.But the detector that unmanned plane of the prior art generally carries comprises single camera, utilize the video image of single camera collection, the accuracy of detection demand based on video analysis cannot be met, great restriction is brought to the application scenarios of detector.
Given this, the utility model provides a kind of unmanned plane with binocular vision structure.
Summary of the invention
The purpose of this utility model is a kind of detector based on binocular vision, to solve the detector that exists in prior art for single camera, its collection video image cannot meet the accuracy of detection demand based on video analysis, the application of detector is brought to the problem of restriction greatly.
For realizing the purpose of this utility model, the utility model provides a kind of unmanned plane with binocular vision structure, comprise unmanned plane body, fixed mount, detector, described fixed mount is arranged at the bottom of described unmanned plane body, described detector is connected with unmanned plane body by fixed mount, described detector comprises the first camera and second camera, power module, communication module, described first camera is infrared thermoviewer, described infrared thermoviewer is for gathering Infrared Image Information, described second camera is colour TV camera, described colour TV camera is for gathering color image information, described power module is used for powering to described infrared thermoviewer and colour TV camera, Infrared Image Information and color image information are sent to control system by communication module by described detector.
Wherein, described detector also comprises shell, and described first camera and second camera, power module, communication module are installed in described shell, and the front end of described shell is provided with transparent window.
Wherein, described unmanned plane body comprises flying platform and power system and automatic control module, and described automatic control module comprises GPS navigation system, attitude control system, altimeter and The Cloud Terrace, and described detector is connected with The Cloud Terrace by fixed mount.
The utility model, compared with prior art, binocular vision structure is set, comprise know clearly the first camera and second camera, first camera is infrared thermoviewer, described infrared thermoviewer is for gathering Infrared Image Information, described second camera is colour TV camera, described colour TV camera is for gathering color image information, Infrared Image Information and color image information are sent to control system by communication module by described detector, the problem that the brilliant image that can be solved under several scenes by analysis Infrared Image Information and color image information is gathered, the user demand of user can be met.
Accompanying drawing explanation
Figure 1 shows that structural representation of the present utility model;
Figure 2 shows that the structural representation of the utility model detector;
In figure: 1. unmanned plane body, 2. fixed mount, 3. detector, 31. shells, 32. transparent windows, 33. first cameras, 34. second cameras, 35. power modules, 36. communication modules.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
Should be noted that, " connection " described in the application and the word for expressing " connection ", as " being connected ", " being connected " etc., both can comprise a certain parts with another parts is directly connected, and also can comprise a certain parts and is connected with another parts by miscellaneous part.
As Fig. 1, shown in Fig. 2, the utility model provides a kind of unmanned plane with binocular vision structure, comprise unmanned plane body 1, fixed mount 2, detector 3, described fixed mount is arranged at the bottom of described unmanned plane body, described detector is connected with unmanned plane body by fixed mount, described detector comprises the first camera and second camera, power module 35, communication module 36, described first camera 33 is infrared thermoviewer front end, described infrared thermoviewer is for gathering Infrared Image Information, described second camera 34 is the front end of colour TV camera, described colour TV camera is for gathering color image information, described power module is used for powering to described infrared thermoviewer and colour TV camera, Infrared Image Information and color image information are sent to control system by communication module by described detector, control system is analyzed the image that detector gathers.Infrared thermoviewer wherein effectively can solve the deficiency of colorful digital video camera monitoring objective under night even pole extreme climate environment condition.
In a preferred embodiment, described detector also comprises shell 31, and described first camera and second camera, power module, communication module are installed in described shell, and the front end of described shell is provided with transparent window 32.
In a preferred embodiment, described unmanned plane body comprises flying platform and power system and automatic control module, described automatic control module comprises GPS navigation system, attitude control system, altimeter and The Cloud Terrace, and described detector is connected with The Cloud Terrace by fixed mount.Described The Cloud Terrace is stable platform, and stable platform can eliminate shake, improves picture quality, meanwhile, can also convert visual angle of taking photo by plane.
The utility model, binocular vision structure is set, comprise know clearly the first camera and second camera, first camera is infrared thermoviewer, described infrared thermoviewer is for gathering Infrared Image Information, described second camera is colour TV camera, described colour TV camera is for gathering color image information, Infrared Image Information and color image information are sent to control system by communication module by described detector, the problem that the brilliant image that can be solved under several scenes by analysis Infrared Image Information and color image information is gathered, the user demand of user can be met.
In a preferred embodiment, convenient, safety is placed in order to make detector, following structure can be set: described unmanned plane body is provided with container cavity, described The Cloud Terrace is arranged in container cavity, described fixed mount is lifting mode fixed mount, particularly, described fixed mount comprises fixing cylinder, snap close, the upper end of described fixing cylinder is connected with The Cloud Terrace, the piston rod of fixing cylinder is fixedly connected with snap close, and described detection device casing upper surface is provided with coupling link, during use, use snap close locking coupling link, thus detector can be connected with fixing cylinder.When not using, cylinder can be utilized in detector retraction container cavity, thus can place detector well, unmanned plane also can comparatively random lifting and parking; When using, cylinder can be utilized to be stretched out outside container cavity by detector.
In a preferred embodiment, in order to make containment structure simple, make easy to process, shell can be divided into upper cover and lower shell structure, one end and the described lower casing of described upper cover are hinged, the other end is connected with lower casing by locking piece, described lower casing comprises protecgulum, centre portion and back cover, described camera lens is arranged on sheet metal component, described buttock line is connected with power supply source through described back cover, the inner side of described upper cover is pasted with sealing EVA foam, described lower casing and the described upper cover place of being tightly connected are provided with sealing rubber strip, described sealing EVA foam surface uniform pastes electrically conductive cloth, and it is seamless between the two after pasting, described sealing rubber strip surface is pasted with electrically conductive cloth completely, and electrically conductive cloth surface smoothing is seamless between the two after pasting.Utilize said structure, the electronic unit in shell can be avoided to be damaged by static electricity.
In a preferred embodiment, in order to ensure the clean of transparent window, shell outside transparent window is provided with air-flow shower nozzle, described air-flow shower nozzle is connected with air pump by pipeline, described air pump is connected with controller, described air-flow shower nozzle can be multiple, and shower nozzle air extractor duct, towards transparent window, arranges injecting time and the interval time of air-flow shower nozzle by controller.
The above is only preferred implementation of the present utility model; it should be noted that; for those skilled in the art; under the prerequisite not departing from the utility model principle; can also make some improvements and modifications, these improvements and modifications also should be considered as protection domain of the present utility model.
Claims (3)
1. the unmanned plane with binocular vision structure, it is characterized in that, comprise unmanned plane body, fixed mount, detector, described fixed mount is arranged at the bottom of described unmanned plane body, described detector is connected with unmanned plane body by fixed mount, described detector comprises the first camera and second camera, power module, communication module, described first camera is infrared thermoviewer, described infrared thermoviewer is for gathering Infrared Image Information, described second camera is colour TV camera, described colour TV camera is for gathering color image information, described power module is used for powering to described infrared thermoviewer and colour TV camera, Infrared Image Information and color image information are sent to control system by communication module by described detector.
2. the unmanned plane with binocular vision structure according to claim 1, it is characterized in that, described detector also comprises shell, and described first camera and second camera, power module, communication module are installed in described shell, and the front end of described shell is provided with transparent window.
3. the unmanned plane with binocular vision structure according to claim 1, it is characterized in that, described unmanned plane body comprises flying platform and power system and automatic control module, described automatic control module comprises GPS navigation system, attitude control system, altimeter and The Cloud Terrace, and described detector is connected with The Cloud Terrace by fixed mount.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201520872642.0U CN205131672U (en) | 2015-11-03 | 2015-11-03 | Unmanned aerial vehicle with binocular vision structure |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520872642.0U CN205131672U (en) | 2015-11-03 | 2015-11-03 | Unmanned aerial vehicle with binocular vision structure |
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| CN205131672U true CN205131672U (en) | 2016-04-06 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105721001A (en) * | 2016-04-14 | 2016-06-29 | 国鹰河北航空科技有限公司 | Unmanned aerial vehicle target positioning system |
| CN106507042A (en) * | 2016-10-27 | 2017-03-15 | 江苏金米智能科技有限责任公司 | A kind of double remaining remotely pilotless machines for fire fighting monitoring |
| WO2020000209A1 (en) * | 2018-06-26 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Sensor assembly and unmanned aerial vehicle |
-
2015
- 2015-11-03 CN CN201520872642.0U patent/CN205131672U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105721001A (en) * | 2016-04-14 | 2016-06-29 | 国鹰河北航空科技有限公司 | Unmanned aerial vehicle target positioning system |
| CN106507042A (en) * | 2016-10-27 | 2017-03-15 | 江苏金米智能科技有限责任公司 | A kind of double remaining remotely pilotless machines for fire fighting monitoring |
| WO2020000209A1 (en) * | 2018-06-26 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Sensor assembly and unmanned aerial vehicle |
| CN110770128A (en) * | 2018-06-26 | 2020-02-07 | 深圳市大疆创新科技有限公司 | Sensor assembly and unmanned aerial vehicle |
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