CN206728144U - A kind of wireless camera - Google Patents
A kind of wireless camera Download PDFInfo
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- CN206728144U CN206728144U CN201720574804.1U CN201720574804U CN206728144U CN 206728144 U CN206728144 U CN 206728144U CN 201720574804 U CN201720574804 U CN 201720574804U CN 206728144 U CN206728144 U CN 206728144U
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Abstract
The utility model discloses a kind of wireless camera, including fuselage and it is arranged on the camera of fuselage side, a mounting seat, the mounting seat is concave structure, the fuselage is arranged in the mounting seat of concave structure, the front end of the camera includes sphere and is arranged on the speculum group of sphere inner surface into the speculum reflection light to camera.In the utility model, because the fixation of whole fuselage, as intermediate buffering band, flexible spring washer is set particularly between firm banking and fuselage, can be caused when high vibration occurs using firm banking, the impact being subject on fuselage body is very small, reduces the influence in itself to video camera；Same camera uses spherical design, and light is reflected with prism, most of light can be reflexed to the porch of camera, timely video camera is shaken in itself, light outside sphere also can normally enter camera, the overlapping phenomenon of image will not occur because of shake.
Description
Technical field
Optical field is the utility model is related to, particularly relates to a kind of intelligent radio camera structure.
Background technology
Video camera includes many kinds, what the general principle of its work was just as：Optical image signal is changed into telecommunications
Number, in order to store or transmit.When we shoot an object, the light reflected on this object is collected by camera lens,
It is set to focus on the smooth surface of picture pick-up device（Such as the target surface of pick-up tube）On, then light is changed into by picture pick-up device by electric energy,
Obtain " vision signal ".Photosignal is very faint, need to be amplified by pre-arcing road, then by various circuits
Reason and adjustment, the standard signal finally obtained can be sent on the recording mediums such as video recorder and record, or pass through broadcasting system
Propagate or be sent on monitor and show.
Conventional video camera is typically all to be powered using battery or power supply, is recorded, saved the video in medium, most
For it is universal be exactly present mobile phone, can substantially realize video record and be wirelessly transferred, but mobile phone is limited by hardware,
It is very undesirable for image definition, and power supply supply is substantially insufficient.And the industry for many specialties is taken the photograph
Camera, although video definition is very high, cost is very high, and belongs to high precision instrument, is not suitable for the use in field,
The region of high vibration is especially related to, because the design of existing camera daylighting, it may appear that the phenomenon of camera lens shake, from
And the picture for causing to photograph is shaken, influence to watch.
As social development needs, many particular surroundings need to be shot, and particular surroundings means that shooting sum
Can not be as being used in home, therefore, for this having specific demand according to transmission, existing video camera can not necessarily expire
Foot its demand is, it is necessary to which new design meets.
The content of the invention
The purpose of this utility model is to provide a kind of intelligent radio camera structure so that it possesses high vibration feelings again
Shooting is not in the phenomenon of excessive jitter under condition.
To achieve the above object, the utility model provides following technical scheme：
A kind of intelligent radio camera structure, including fuselage and the camera for being arranged on fuselage side, including an installation
Base, mounting seat are concave structure, and the top edge of concave structure is clamping mechanism；
Fuselage surface sets fluted；The diameter parallel of groove and fuselage and camera；
Fuselage is arranged in the mounting seat of concave structure, and clamping mechanism is caught in the groove of fuselage；
The front end of camera includes sphere and is arranged on the speculum group of sphere inner surface into, speculum reflection light to taking the photograph
As head；
Fuselage interior is provided with image processing apparatus；Image processing apparatus electrically connects with camera；Image processing apparatus with
Server data connects；Image processing apparatus includes network transmission module, video sending module, video processing module, regulation
Module and video acquisition module；
Video acquisition module electrically connects with video processing module；Video processing module electrically connects with video sending module；Depending on
Frequency transmitter module electrically connects with network transmission module；Network transmission module connects with server signal；Adjustment module respectively with net
Network transport module and video processing module electrical connection；Video processing module includes the interface mould electrically connected respectively with control module
Block, storage module, protection module, power management module, data encryption module and image quality adjustment module；Interface module respectively with regarding
Frequency acquisition module, adjustment module and the electrical connection of video transmission module.
In the above-mentioned technical solutions, it is cavity structure between mounting seat and fuselage.
In the above-mentioned technical solutions, flexible spring washer is provided with the cavity structure.
In the above-mentioned technical solutions, the prismatic minute surface that the speculum is protruded by several forms.
In the above-mentioned technical solutions, it is right angle angle to be formed between the face and face of the prismatic minute surface.
In the above-mentioned technical solutions, it is not provided with speculum on the sphere of camera face position.
Compared with prior art, the beneficial effects of the utility model are：
In the utility model, because the fixation of whole fuselage utilizes firm banking as intermediate buffering band, particularly solid
Determine to set flexible spring washer between base and fuselage, can make it that, when high vibration occurs, the impact being subject on fuselage body is non-
It is often small, reduce the influence in itself to video camera；Same camera uses spherical design, and light is reflected with prism, can
So that most of light to be reflexed to the porch of camera, even if video camera is shaken in itself, the light outside sphere also can be normal
Into camera, the overlapping phenomenon of image will not occur because of shake；This programme uses and sets adjustment module in systems simultaneously,
Vision signal is obtained by network transmission module in real time, and in real time can be transmitted control signal to adjustment module, then passes through tune
Section module control video processing module is adjusted output to image quality, disclosure satisfy that and ensures that video image is clear in the presence of a harsh environment
Reliable transmission display.
Brief description of the drawings
Fig. 1 is overall appearance structural representation of the present utility model；
Fig. 2 is camera structure schematic diagram of the present utility model；
Fig. 3 is the prism structure schematic diagram of camera；
Fig. 4 is system flow block diagram of the present utility model.
Fig. 5 is the structured flowchart of video processing module.
In figure：1 is fuselage, and 2 be groove, and 3 be cavity, and 4 be camera, and 5 be sphere, and 6 be mounting seat, and 5.1 be circular arc
Face, 5.2 be prism, and 7 be image processing apparatus.
Embodiment
Below in conjunction with the accompanying drawing 1-3 in the utility model embodiment, to the technical scheme in the embodiment of the utility model
It is clearly and completely described.
As shown in figure 1, the camera body structure that the utility model uses all is to use one as the structure of routine
Fuselage, the side of fuselage is then provided with camera.Then the utility model is in order to meet special demand, for fuselage
Mounting means and camera take light mode all to make corresponding modification.Main use environment of the present utility model is at nobody
, region that there is sharp pounding, such as in subway tunnel or some railway tunnel, if using conventional camera,
Once there is train by the way that strong vibrations can cause video camera to shake, so that the image appearance in video is overlapping existing
As.
In order to solve these problems, the utility model is carried out in terms of two, is from mounting means first, is reduced fuselage
Vibrations.Therefore, a mounting seat is set on fuselage, mounting seat is fixedly connected with bearing, when outside is shaken,
Vibrations are delivered in mounting seat.And it can not be fixedly connected between mounting seat and fuselage, it is necessary to use the side of flexible connection
Formula, it can so ensure that fuselage reduces shock momentum by free gap when shaking.Therefore, set on fuselage upper surface
A groove is equipped with, groove is parallel with the horizontal axis of fuselage, arcwall face is used in groove, for blocking to mounting seat
Connect.Mounting seat is concave structure, and the top edge of concave structure is clamping mechanism, and clamping mechanism is cylinder, and cylinder is inserted
Enter into groove, cylinder can move in groove along the horizontal axis of fuselage and camera, but can not translate out recessed
Groove, because cylinder is directly direct less than groove arcwall face, but print the bore being open out of groove.Mounting seat with
Fuselage forms a cavity structure between the two after clamping, and when shaking, fuselage is enterprising in mounting seat by groove
Line slip, it can effectively reduce fuselage vibrations.Of course for damping is preferably played a part of, fill and set in cavity structure
Flexible spring washer is equipped with, when fuselage stress, flexible spring washer can reduce the recoil strength of fuselage so that fuselage is given a shock reduction.
Secondly, it is improved for the structure of camera, the camera of traditional industrial camera is using straight barrel type
Structure, that is to say, that the viewfinder range of camera is in the range of 120 °, it is impossible to has bigger scope again.And some commercial are taken the photograph
Sphere cover then use as head, then the mode of progress camera rotation, which can be realized, is up to finding a view for 270 ° of scopes.The former
Structure precision is very high, and scope is small, although and the latter's scope is high, but because camera need rotated, so as to lead
Cause focusing accuracy is not high, and photographic effect is undesirable.
In this programme, using the structure of sphere cover, the visual range that can increase camera reaches 270 °, certainly, in order to
Avoid the blind area of light, and light from projecting on camera, sphere cover inner surface is provided with some prisms, prism is
Raised towards the sphere center of circle.The angle formed between each adjacent minute surface is 90 °, such setting, when light is from sphere
During any position incidence, by continuously reflecting, light can be reflexed on camera.Certainly, camera face
To spherical area without set prism, camera is directly found a view by sphere, and the sphere outside this region
It is interior just to need prism.Such setting, timely fuselage occurs vibrations and causes camera shake, because light is injected from multiple angles
Onto camera, the light so as to ensure in camera viewfinder range can be incident, and because by prism not
Stop reflecting, can reduce because shake and the image fault brought and overlapping.
As shown in Figure 4, Figure 5：The video processing module of this programme receives video acquisition module image signal transmission, and to figure
Transmitted after being handled as signal by video transmission module to network transmission module, finally transmit to server and show, serviced
Device sends control signal to adjustment module, adjustment module by network transmission module and transmits control signal to video processing module
Picture signal is handled.
Video processing module includes the interface module electrically connected respectively with control module, storage module, protection
Module, power management module, data encryption module and image quality adjustment module, the function of each module are：
Interface module：Transmitted for connecting adjustment module, video acquisition module and video transmission module, and by various types of signal
To control module.
Data encryption module：Picture signal is encrypted, prevents picture signal from revealing.
Image quality adjustment module：Processing is adjusted to the parameters of picture signal, makes image clearly reliable.
Power management module：Powered for whole video processing module.
Protection module：The working condition of power management module is monitored, carries out overload protection.
Storage module：Picture signal is stored, prevents loss of data.
Control module：Control signal is received, and controls working condition and the transmission processing of other coupled modules
Picture signal afterwards.
It can effectively have the function that to control image quality in real time using this programme, be easy to use personnel real-time according to demand
Image is adjusted, to meet requirement.
This programme is very suitable for the data acquisition of the like environment such as desert highway, railway tunnel, ensures that data are adopted
The real-time of collection, the influence to video camera and the influence to data acquisition because prolonged sharp pounding is brought are avoided, together
When can overcome influence of the adverse circumstances to image quality, can ensure that operating personnel adjust monitoring image quality in real time, meet all kinds of
Monitoring image quality requirement under environment.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
All any modification, equivalent and improvement made within refreshing and principle etc., should be included in the scope of the protection.
Claims (9)
1. a kind of intelligent radio camera structure, including fuselage and the camera for being arranged on fuselage side, it is characterised in that：Including
One mounting seat, the mounting seat are concave structure, and the top edge of the concave structure is clamping mechanism,
The fuselage surface sets fluted, the diameter parallel of the groove and fuselage and camera,
The fuselage is arranged in the mounting seat of concave structure, and the clamping mechanism is caught in the groove of fuselage；
The front end of the camera includes sphere and is arranged on the speculum group of sphere inner surface into the speculum reflection light
To camera；
The fuselage interior is provided with image processing apparatus；Described image processing unit electrically connects with camera；At described image
Reason device connects with server data；Described image processing unit includes network transmission module, video sending module, at video
Manage module, adjustment module and video acquisition module；
The video acquisition module electrically connects with video processing module；The video processing module is electrically connected with video sending module
Connect；The video transmission module electrically connects with network transmission module；The network transmission module connects with server signal；It is described
Adjustment module electrically connects with network transmission module and video processing module respectively；The video processing module include respectively with control
Interface module, storage module, protection module, power management module, data encryption module and the image quality regulation of molding block electrical connection
Module；The interface module electrically connects with video acquisition module, adjustment module and video transmission module respectively.
2. a kind of intelligent radio camera structure according to claim 1, it is characterised in that the inner surface of the groove is
Arc surface, the clamping mechanism are cylinder.
3. a kind of intelligent radio camera structure according to claim 2, it is characterised in that the cylindrical diameter is small
In the direct of groove inner arc surface, but cylinder directly more than the bore at slot opening.
4. a kind of intelligent radio camera structure according to claim 3, it is characterised in that cylindrical interface arrangment exists
The interior left and right of groove, slide up and down, and interface arrangment is without departing from groove.
5. according to a kind of any described intelligent radio camera structure of Claims 1 to 4, it is characterised in that mounting seat with
It is cavity structure between fuselage.
6. a kind of intelligent radio camera structure according to claim 5, it is characterised in that set in the cavity structure
Flexible spring washer.
7. a kind of intelligent radio camera structure according to claim 1, it is characterised in that the speculum is by several
The prismatic minute surface composition of protrusion.
A kind of 8. intelligent radio camera structure according to claim 7, it is characterised in that the face of the prismatic minute surface with
It is right angle that angle is formed between face.
9. according to a kind of any described intelligent radio camera structure of claim 1,7,8, it is characterised in that camera face
Speculum is not provided with the sphere of position.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720574804.1U CN206728144U (en) | 2017-05-23 | 2017-05-23 | A kind of wireless camera |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720574804.1U CN206728144U (en) | 2017-05-23 | 2017-05-23 | A kind of wireless camera |
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| Publication Number | Publication Date |
|---|---|
| CN206728144U true CN206728144U (en) | 2017-12-08 |
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ID=60513673
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| CN201720574804.1U Active CN206728144U (en) | 2017-05-23 | 2017-05-23 | A kind of wireless camera |
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| CN (1) | CN206728144U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115942073A (en) * | 2021-09-10 | 2023-04-07 | 宁波舜宇光电信息有限公司 | Camera shooting module |
-
2017
- 2017-05-23 CN CN201720574804.1U patent/CN206728144U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115942073A (en) * | 2021-09-10 | 2023-04-07 | 宁波舜宇光电信息有限公司 | Camera shooting module |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20171221 Address after: 621000 Sichuan province Mianyang Branch Innovation Center Building No. 2 room B212 Patentee after: Sichuan Liang Gu Intelligent Technology Co., Ltd. Address before: 621000 Mianyang city of Sichuan Province Branch Campus of Southwest University of Science and Technology National University Science Park Patentee before: Sichuan handsome Technology Group Co., Ltd. |
|
| TR01 | Transfer of patent right |