CN205131673U - Unmanned aerial vehicle with window protection architecture detector - Google Patents
Unmanned aerial vehicle with window protection architecture detector Download PDFInfo
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- CN205131673U CN205131673U CN201520881780.5U CN201520881780U CN205131673U CN 205131673 U CN205131673 U CN 205131673U CN 201520881780 U CN201520881780 U CN 201520881780U CN 205131673 U CN205131673 U CN 205131673U
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Abstract
The utility model discloses an unmanned aerial vehicle with window protection architecture detector, 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, detecting device sends infrared image information and color image information for control system through communication module, can solve the clear image acquisition's under the multiple scene problem through analysis infrared image information and color image information, can satisfy user's user demand, simultaneously, the utility model provides a transparent window fixed structure to making the transparent window effectively fixed, having avoided prior art, the transparent window is fixed not good, and is easy to be damaged, thereby influence product life's problem emergence, satisfied customer'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 windows be protected feature detector.
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 existing panel detector structure arranges not too reasonable, and the transparent window being arranged on its front end is easily damaged, and has had a strong impact on the service life of product, has added the use cost of user.Given this, the utility model provides a kind of unmanned plane with windows be protected feature detector.
Summary of the invention
The purpose of this utility model is a kind of unmanned plane with windows be protected feature detector; the purpose of this utility model is to propose a kind of detector being provided with transparent window; the transparent window being arranged on its front end to solve detector of the prior art is easily damaged; have a strong impact on the service life of product, add the problem of the use cost of user.
For realizing the purpose of this utility model, the utility model provides a kind of unmanned plane with windows be protected feature detector, 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 shell, upper cover, sheet metal component, circuit card, camera lens, buttock line, wherein, one end of described upper cover and described housing hinge, described circuit card is fixedly mounted on sheet metal component, described sheet metal component is fixedly mounted in described shell, described shell comprises protecgulum, centre portion and bonnet, described camera lens is arranged on described sheet metal component, described buttock line is connected with described circuit card through described bonnet, described protecgulum offers form, transparent window is coated with inside described form, the edge of described transparent window is pushed down by protecgulum pressing plate, and be fixed on protecgulum, described protecgulum pressing plate is U-type groove structure, its bottom face is provided with tapped bore, described protecgulum pressing plate is connected with described upper cover by screw.
Wherein, described detector comprises the first camera and second camera, power module, communication module, first camera is infrared thermoviewer, described infrared thermoviewer is for gathering Infrared Image Information, second camera is colour TV camera, described colour TV camera is for gathering color image information, and described power module is used for powering to described infrared thermoviewer and colour TV camera, and Infrared Image Information and color image information are sent to control system by communication module by described detector.
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.
Wherein, described protecgulum pressing plate is two, fixes the two ends up and down of transparent window respectively.
The utility model, compared with prior art, binocular vision structure is set, comprise know clearly the first camera and second camera, first camera is arranged on infrared thermoviewer front end, described infrared thermoviewer is for gathering Infrared Image Information, 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, simultaneously, the utility model provides a kind of transparent window fixed sturcture, thus make transparent window effectively fixing, avoid in prior art, transparent window is fixed bad, easy breakage, thus affect the problem generation in product service life, meet the user demand of client.
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 windows be protected feature detector, comprise unmanned plane body 1, fixed mount 2, detector 3, described fixed mount 2 is arranged at the bottom of described unmanned plane body 1, described detector 3 is connected with unmanned plane body 1 by fixed mount 2, described detector 3 comprises shell 31, upper cover, sheet metal component, circuit card, camera lens, buttock line, wherein, one end and the described shell 31 of described upper cover are hinged, described circuit card is fixedly mounted on sheet metal component, described sheet metal component is fixedly mounted in described shell 31, described shell 31 comprises protecgulum, centre portion and bonnet, described camera lens is arranged on described sheet metal component, described buttock line is connected with described circuit card through described bonnet, described protecgulum offers form, transparent window 32 is coated with inside described form, the edge of described transparent window 32 is pushed down by protecgulum pressing plate, and be fixed on protecgulum, described protecgulum pressing plate is U-type groove structure, its bottom face is provided with tapped bore, described protecgulum pressing plate is connected with described upper cover by screw.Infrared thermoviewer wherein effectively can solve the deficiency of colorful digital video camera monitoring objective under night even pole extreme climate environment condition.Described control system is front-end control or Background control.
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.
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 (4)
1. the unmanned plane with windows be protected feature detector, 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 shell, upper cover, sheet metal component, circuit card, camera lens, buttock line, wherein, one end of described upper cover and described housing hinge, described circuit card is fixedly mounted on sheet metal component, described sheet metal component is fixedly mounted in described shell, described shell comprises protecgulum, centre portion and bonnet, described camera lens is arranged on described sheet metal component, described buttock line is connected with described circuit card through described bonnet, described protecgulum offers form, transparent window is coated with inside described form, the edge of described transparent window is pushed down by protecgulum pressing plate, and be fixed on protecgulum, described protecgulum pressing plate is U-type groove structure, its bottom face is provided with tapped bore, described protecgulum pressing plate is connected with described upper cover by screw.
2. the unmanned plane with windows be protected feature detector according to claim 1, it is characterized in that, described detector comprises the first camera and second camera, power module, communication module, first camera is infrared thermoviewer, described infrared thermoviewer is for gathering Infrared Image Information, 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.
3. the unmanned plane with windows be protected feature detector 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.
4. the unmanned plane with windows be protected feature detector according to claim 1, is characterized in that, wherein, described protecgulum pressing plate is two, fixes the two ends up and down of transparent window respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520881780.5U CN205131673U (en) | 2015-11-03 | 2015-11-03 | Unmanned aerial vehicle with window protection architecture detector |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520881780.5U CN205131673U (en) | 2015-11-03 | 2015-11-03 | Unmanned aerial vehicle with window protection architecture detector |
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| Publication Number | Publication Date |
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| CN205131673U true CN205131673U (en) | 2016-04-06 |
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| CN201520881780.5U Active CN205131673U (en) | 2015-11-03 | 2015-11-03 | Unmanned aerial vehicle with window protection architecture detector |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105763841A (en) * | 2015-11-03 | 2016-07-13 | 天津艾思科尔科技有限公司 | Aircraft provided with detector with protector |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105763841A (en) * | 2015-11-03 | 2016-07-13 | 天津艾思科尔科技有限公司 | Aircraft provided with detector with protector |
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| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20201229 Address after: Room 105, building 1, Hongrun Huaxia Hotel, 96 fengle Road, Jinshui District, Zhengzhou City, Henan Province, 450053 Patentee after: Henan aiseker Information Technology Co.,Ltd. Address before: No.20, 6th Street, Binhai New Area Economic Development Zone, Tianjin 300457 Patentee before: TIANJIN ISECURE TECHNOLOGY Co.,Ltd. |