CN204906509U - High coverage surveillance camera machine - Google Patents
High coverage surveillance camera machine Download PDFInfo
- Publication number
- CN204906509U CN204906509U CN201520480294.2U CN201520480294U CN204906509U CN 204906509 U CN204906509 U CN 204906509U CN 201520480294 U CN201520480294 U CN 201520480294U CN 204906509 U CN204906509 U CN 204906509U
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- CN
- China
- Prior art keywords
- fuselage
- visual field
- camera lens
- large visual
- camera
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses a high coverage surveillance camera machine includes the fuselage that is equipped with the camera lens, wherein the camera lens orientation the top slope of fuselage. Like this, the control visual angle of camera lens be inclination and the fuselage of camera lens T to the pivot angle sum to the monitoring range of camera lens has been improved widely. And the simple structure of this camera, it is convenient to install, convenient to use.
Description
Technical field
The utility model relates to technical field of video monitoring, particularly a kind of large visual field CCTV camera.
Background technology
Often need in the place such as family, office to use video camera to carry out as monitoring such as WiFi connection, the intercommunication of MIC language, infrared night vision, SD storage, network or power-off instructions.
This kind of video camera generally comprises the fuselage that is provided with camera lens and the base two parts for supporting fuselage.At present, the set-up mode of camera lens is, arranges along the axis direction setting of fuselage or the axis direction perpendicular to technology.In use by regulating the angle of fuselage to carry out Multi-azimuth monitoring etc.But when arranging camera lens by the way, the guarded region of camera lens is less.
Therefore, how solving in the less problem of the camera lens guarded region of video camera, is those skilled in the art's technical issues that need to address.
Utility model content
The utility model provides a kind of large visual field CCTV camera, is increased the guarded region of video camera by the angle of inclination arranging camera lens.
The large visual field of the present utility model CCTV camera comprises the fuselage being provided with camera lens, and wherein said camera lens is towards the inclined upward of described fuselage.
In one embodiment, described camera lens is positioned at the head position of described fuselage, and the head of described fuselage bends towards the incline direction of described camera lens.
In one embodiment, described camera lens is fixedly connected with the support on the fixed axis being arranged on described fuselage, and described support is provided with the card ear be embedded in the draw-in groove of described fuselage.
In one embodiment, the T of described fuselage to pivot angle between-60 ° to 60 °.
In one embodiment, described fuselage is connected with the base of magnet with described large visual field CCTV camera by magnetic adsorption plate.
In one embodiment, described magnetic adsorption plate is the hemispherical dome structure of the below being fixed on described fuselage, and described magnetic adsorption plate is arranged in the holding tank of described base.
In one embodiment, in described holding tank, be provided with antislip ring, and the diapire of described base is provided with slipmat.
In one embodiment, the connection jaws of described large visual field CCTV camera is arranged on described fuselage.
In one embodiment, the base of described large visual field CCTV camera is provided with hat-and-coat hook patchhole.
In one embodiment, the upper cover of described base is fixedly connected with by rotary buckle with chassis.
In one embodiment, described fuselage is cylinderical fuselage, and described camera lens is arranged in the head of described cylinderical fuselage.
Relative to prior art, the camera lens of video camera of the present utility model is towards the inclined upward of fuselage.Like this, the monitoring visual angle of camera lens be the angle of inclination of camera lens and the T of fuselage to pivot angle sum, thus greatly increase the monitoring range of camera lens.And the structure of this video camera is simple, it is convenient to install, easy to use.
Accompanying drawing explanation
Also will be described in more detail the utility model with reference to accompanying drawing based on embodiment hereinafter.
Fig. 1 is the structural representation of the video camera of the present embodiment.
Fig. 2 is the internal structure schematic diagram of the video camera of the present embodiment.
Fig. 3 is the structural representation of the support in the present embodiment.
Fig. 4 is the structural representation of the fixed axis of fuselage in the present embodiment.
Fig. 5 is the structural representation of the connection jaws in the present embodiment.
Fig. 6 is the structural representation of the base in the present embodiment.
Fig. 7 is the structural representation of the rotary buckle in the present embodiment.
Fig. 8 is the using state figure of the hat-and-coat hook patchhole of base in the present embodiment.
Fig. 9 is the assembled state schematic diagram one of the video camera of the present embodiment.
Figure 10 is the assembled state schematic diagram two of the video camera of the present embodiment.
Figure 11 is the assembled state schematic diagram three of the video camera of the present embodiment.
In the accompanying drawings, identical parts use identical Reference numeral.Accompanying drawing is not according to the scale of reality.
Fuselage-1, camera lens-2, base-3, support-4, magnetic adsorption plate-5, magnet-6, power line-7, hat-and-coat hook-8, installed surface-9, head-11, connection jaws-12, draw-in groove-13, fixed axis-14, holding tank-31, slipmat-32, balancing weight-33, rotary buckle-34, hat-and-coat hook patchhole-35, chassis-36, upper cover-37, engaging lug-41, Ka Er-42, angle of inclination-a, T are to pivot angle-b.
Embodiment
Below in conjunction with accompanying drawing, the utility model is described in further detail.
As shown in Figure 1, the large visual field CCTV camera of the present embodiment comprises the fuselage 1 being provided with camera lens 2.Camera lens 2 tilts towards the top (side away from the base 3 of video camera) of fuselage 1.Camera lens 2 tilts to refer to, the angle of inclination a (and the angle between the axis of fuselage 1) of camera lens 2 is greater than 0 ° and be less than 90 °.Like this, the monitoring visual angle of camera lens 2 be the angle of inclination of camera lens 2 and the T of fuselage 1 to (direction when swinging in the plane of axis being parallel to fuselage 1) pivot angle b sum, thus greatly increase the monitoring range of camera lens 2.
The angle of inclination a of camera lens 2 can between 30 ° to 60 °.The T of fuselage 1 can select between-60 ° to 60 °, to facilitate setting to pivot angle b.In one example in which, the angle of inclination a of camera lens is 35 °, and the maximum T of fuselage 1 is-45 ° and 45 ° to pivot angle b, and will be arranged at video camera on the high ceiling of distance ground 3m.If when camera lens 2 is arranged along the axis of fuselage 1, fuselage 1 can see when T is 45 ° to pivot angle b the distance that 3m is far away, then arrange by the way, the T being equivalent to camera lens 2 can reach 80 ° to pivot angle b, the distance that 17m is far away can be seen like this, substantially increase monitoring range, corridor monitoring environment can be met better.
The concrete set-up mode of camera lens 2 is, as shown in Figure 2, fuselage 1 can be column construction.Camera lens 2 is positioned at fuselage 1 and is arranged on head 11 position of fuselage 1.Like this, the monitoring visual field of adjustable lens 2 can be carried out by the length arranging fuselage 1, and structure is simple, easy for installation, save trouble and labor.The cylindricality of fuselage 1 can be cylindrical, also can be the cylindricality of prolate.
The head 11 of fuselage 1 also roughly bends corresponding to the incline direction of camera lens 2.That is, when installing camera lens 2, camera lens 2 roughly with the axis being parallel of the head 11 of fuselage 1.Further, camera lens 2 is in communication with the outside by the sight vane on head 11 top being positioned at fuselage 1.Setting like this, structure is simple, save trouble and labor during assembling camera lens 2.
As shown in Figure 2, Figure 3 and Figure 4, camera lens 2 can be fixed in fuselage 1 by support 4.Particularly, fixed axis 14 is provided with in the inner side of fuselage 1.Support 4 is provided with engaging lug 41.By in the hole that fixed axis 14 is located in engaging lug 41, support 4 is fixed.Camera lens 2 is fixedly connected with support 4 by such as screw.Arrange by the way, easy for installation, sound construction, ensures optical property.Engaging lug 41 can and the body of support 4 between bend, to enable the body of support 4 roughly parallel with camera lens 2, to improve installation convenience further.Support 4 can also be provided with card ear 42.Installing, support 4 is good, and card ear 42 is connected in the draw-in groove 13 of fuselage 1, to improve the fastness of support 4 further.The material of support 4 can be panel beating.
As shown in figures 2 and 5, the connection jaws 12 of video camera arranges on the fuselage 1, to facilitate wiring.That is, the USB male joint of video camera is arranged in fuselage 1, and the socket end of USB male joint is positioned at outside fuselage 1, and roughly vertical with fuselage 1.Power line 7 is directly plugged in USB male joint.
In addition, as shown in Figure 2 and Figure 6, fuselage 1 is connected with the base 3 of video camera with magnet 6 by magnetic adsorption plate 5, and structure is simple, and it is convenient to install, and is convenient to the monitoring angle regulating fuselage 1.In one example in which, magnetic adsorption plate 5 is fixed on the below of fuselage 1, as a part for fuselage 1.After on the base 3 fuselage 1 being arranged on video camera, magnetic adsorption plate 5 is arranged in the holding tank 31 of base 3 rotationally, and the shape of magnetic adsorption plate 5 roughly becomes hemisphere, can rotate on the base 3 to make fuselage 1, and it is free-hand namely adjustable, do not need by additional means, save trouble and labor, be applicable to various indoor scenarios.Fuselage 1 is except along T to when swinging, can rotating (as shown in Figure 1, arrow represents along own axis) around himself axis.
Fuselage 1 can comprise Portion and rear shell portion.Now, magnetic adsorption plate 5 also comprises the front magnetic adsorption plate part being fixed on Portion and the rear magnetic adsorption plate part being fixed on rear shell portion.Front magnetic adsorption plate part roughly becomes hemispherical dome structure with after rear magnetic adsorption plate sections fit.
At the middle part of holding tank 31, can through hole be set.After installing magnet 6, magnet 6 is positioned at the lead to the hole site of holding tank 31, to reduce the obstruct between magnet 6 and magnetic adsorption plate 5, thus improves the adhesive effect of magnet 6 and magnetic adsorption plate 5.Holding tank 31 can also arrange antislip ring.When being placed on the base 3 by fuselage 1, magnetic adsorption plate 5 contacts with antislip ring, to improve the steadiness of fuselage 1.
In base 3, balancing weight 33 can also be set, to improve the steadiness of base 3.The diapire of base 3 can also arrange antislip ring, to improve the steadiness of base 3 further.As shown in Figure 7 and Figure 8 (arrow represents the rear rotating base 3 of insertion hat-and-coat hook 8 thus is fixed on hat-and-coat hook 8), hat-and-coat hook patchhole 35 can also be set on the base 3.In use, by hanging camera on hat-and-coat hook 8, to increase the use occasion of video camera.
As shown in Figure 7, the upper cover 37 of base 3 is fixedly connected with by rotary buckle 34 with chassis 36, to improve installation convenience further.As shown in Fig. 9, Figure 10 and Figure 11, when installing video camera, first the chassis 36 of base 3 being fixed on installed surface 9 by such as screw, being then fixed on chassis 36 by the upper cover 37 of rotary buckle 34 by base 3.Finally fuselage 1 is placed in the holding tank 31 of base 3.
When video camera is used for desktop installation, only need base 3 to be put in stably on smooth desktop.Be energized after complete monitoring angle to be regulated and use, convenient succinct, save trouble and labor.Base 3 can also be bonded on installed surface by double faced adhesive tape.
Although be described the utility model with reference to preferred embodiment, when not departing from scope of the present utility model, various improvement can be carried out to it and parts wherein can be replaced with equivalent.Especially, only otherwise there is structural hazard, the every technical characteristic mentioned in each embodiment all can combine in any way.The utility model is not limited to specific embodiment disclosed in literary composition, but comprises all technical schemes fallen in the scope of claim.
Claims (10)
1. a large visual field CCTV camera, is characterized in that, comprises the fuselage being provided with camera lens, wherein said camera lens towards the inclined upward of described fuselage,
Described camera lens is positioned at the head position of described fuselage, and the head of described fuselage bends towards the incline direction of described camera lens.
2. the large visual field according to claim 1 CCTV camera, is characterized in that, described camera lens is fixedly connected with the support on the fixed axis being arranged on described fuselage, and described support is provided with the card ear be embedded in the draw-in groove of described fuselage.
3. the large visual field according to claim 1 CCTV camera, is characterized in that, the T of described fuselage to pivot angle between-60 ° to 60 °.
4. the large visual field according to claim 1 CCTV camera, is characterized in that, described fuselage is connected with the base of magnet with described large visual field CCTV camera by magnetic adsorption plate.
5. the large visual field according to claim 4 CCTV camera, is characterized in that, described magnetic adsorption plate is the hemispherical dome structure of the below being fixed on described fuselage, and described magnetic adsorption plate is arranged in the holding tank of described base.
6. the large visual field according to claim 5 CCTV camera, it is characterized in that, be provided with antislip ring in described holding tank, and the diapire of described base is provided with slipmat.
7. the large visual field CCTV camera according to any one of claim 1-6, is characterized in that, the connection jaws of described large visual field CCTV camera is arranged on described fuselage.
8. the large visual field CCTV camera according to any one of claim 1-6, is characterized in that, the base of described large visual field CCTV camera is provided with hat-and-coat hook patchhole.
9. the large visual field according to claim 8 CCTV camera, it is characterized in that, the upper cover of described base is fixedly connected with by rotary buckle with chassis.
10. the large visual field CCTV camera according to any one of claim 1-6, is characterized in that, described fuselage is cylinderical fuselage, and described camera lens is arranged in the head of described cylinderical fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520480294.2U CN204906509U (en) | 2015-07-01 | 2015-07-01 | High coverage surveillance camera machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520480294.2U CN204906509U (en) | 2015-07-01 | 2015-07-01 | High coverage surveillance camera machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204906509U true CN204906509U (en) | 2015-12-23 |
Family
ID=54928650
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520480294.2U Expired - Fee Related CN204906509U (en) | 2015-07-01 | 2015-07-01 | High coverage surveillance camera machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204906509U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107172333A (en) * | 2017-05-27 | 2017-09-15 | 芜湖星途机器人科技有限公司 | Tilting can dust-proof multi-cam robot recognition of face device |
| CN112017346A (en) * | 2020-08-25 | 2020-12-01 | 杭州海康威视数字技术股份有限公司 | Access control management method, access control terminal, access control system and storage medium |
| CN116753428A (en) * | 2023-08-22 | 2023-09-15 | 杭州海康威视数字技术股份有限公司 | Tripod head camera |
-
2015
- 2015-07-01 CN CN201520480294.2U patent/CN204906509U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107172333A (en) * | 2017-05-27 | 2017-09-15 | 芜湖星途机器人科技有限公司 | Tilting can dust-proof multi-cam robot recognition of face device |
| CN112017346A (en) * | 2020-08-25 | 2020-12-01 | 杭州海康威视数字技术股份有限公司 | Access control management method, access control terminal, access control system and storage medium |
| CN112017346B (en) * | 2020-08-25 | 2023-08-18 | 杭州海康威视数字技术股份有限公司 | Access control method, access control terminal, access control system and storage medium |
| CN116753428A (en) * | 2023-08-22 | 2023-09-15 | 杭州海康威视数字技术股份有限公司 | Tripod head camera |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151223 Termination date: 20200701 |