CN209105337U - Video monitoring instrument based on 4G communication - Google Patents
Video monitoring instrument based on 4G communication Download PDFInfo
- Publication number
- CN209105337U CN209105337U CN201822185156.8U CN201822185156U CN209105337U CN 209105337 U CN209105337 U CN 209105337U CN 201822185156 U CN201822185156 U CN 201822185156U CN 209105337 U CN209105337 U CN 209105337U
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- fuselage
- video monitoring
- monitoring instrument
- end outer
- fixedly installed
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Abstract
The utility model discloses the video monitoring instruments communicated based on 4G, including fuselage, fixed frame side is fixedly mounted in the lower end outer surface of the fuselage, the two sides inner surface of the fixed frame side is connected with working panel, the leading exterior surface of the working panel is fixedly installed with radar installations, photo resistance, dot matrix infrared lamp, LED white light and high-definition camera, the photo resistance is located at the upper end of high-definition camera, and the radar installations is located at the lower end of high-definition camera.Video monitoring instrument described in the utility model based on 4G communication; equipped with Surge Protector, lifting slide wall and fuselage thermovent; the safety of instrument can be protected well when machine is struck by lightning; and instrument can be declined the case where ensuring personal safety and removed; it repairs and clears up convenient for people, facilitate the heat dispersal situations of instrument fuselage, protect the working condition and service life of instrument; people can also be facilitated to repair internal, bring better prospect of the application.
Description
Technical field
The video monitoring instrument field that the utility model relates to be communicated based on 4G, in particular to based on the video prison of 4G communication
Control instrument.
Background technique
Video monitoring instrument based on 4G communication is the monitor that a kind of pair of Image Acquisition is transferred to another equipment by 4G
Device, its appearance can be very good to bring safety and supervisory role, it is not only easy to operate, and widely used;It is existing
There are certain drawbacks when in use based on the video monitoring instrument that 4G is communicated in some, firstly, in use, it cannot be very light
Pine arbitrarily removes camera, has certain inconvenience, secondly, cannot have good cooling system, to the longevity of instrument itself
Life and working condition cause deleterious effect, in addition, the damage caused by being struck by lightning cannot ought be prevented well in use
It loses, is unfavorable for the property safety of people, certain adverse effect is brought to the use process of people, for this purpose, it is proposed that base
In the video monitoring instrument of 4G communication.
Utility model content
The main purpose of the utility model is to provide the video monitoring instruments communicated based on 4G, can effectively solve background
The problems in technology.
To achieve the above object, the technical solution that the utility model is taken are as follows: the video based on G communication of the utility model
Fixed frame side, table in the two sides of the fixed frame side is fixedly mounted in monitoring instrument, including fuselage, the lower end outer surface of the fuselage
Face is connected with working panel, and the leading exterior surface of the working panel is fixedly installed with radar installations, photo resistance, point
Battle array infrared lamp, LED white light and high-definition camera, the photo resistance are located at the upper end of high-definition camera, the radar installations
Positioned at the lower end of high-definition camera, the dot matrix infrared lamp is located at the two sides of high-definition camera, and the LED white light is located at dot matrix
The lower end of infrared lamp, the back end outer surface of the fuselage are fixedly installed with fuselage thermovent, and the upper end outer surface of the fuselage is living
Dynamic to be connected with rotation top, the surrounding outer surface on the rotation top is movably installed with antenna, and the upper end outer surface on the rotation top is solid
Dingan County is equipped with connecting rod, and the upper end outer surface of the connecting rod is fixedly connected with radiating motor device, the radiating motor device
Upper end outer surface be fixedly connected with bracket, a side external surface of the bracket is fixedly connected with lifting slide wall, and the lifting is slided
One side external surface of wall is connected with fixation wall, and a side external surface of the fixation wall is movably installed with lifting button, described
The inside of fixation wall is fixedly installed with lifting motor and swingle, and the swingle is located at the upper end outer surface of lifting motor, institute
The inside for stating bracket is fixedly installed with Surge Protector, and the inside of the radiating motor device is fixedly installed with radiating motor, tooth
Wheel, toothed disc and drive rod, the radiating motor are located at the side of gear, and the toothed disc is located at the lower end outer surface of gear,
The drive rod is located at the lower end outer surface of toothed disc, and the inside of the fuselage thermovent is fixedly installed with radiator fan.
Preferably, the swingle is provided with screw thread, the rotation through lifting slide wall, and between swingle and lifting slide wall
The surrounding outer surface of bull stick is flexibly connected by screw thread with the inner surface for going up and down slide wall.
Preferably, sliding slot is provided between lifting slide wall and the fixation wall, and two side external surfaces for going up and down slide wall are logical
The inner surface for crossing sliding slot and fixation wall is slidably connected.
Preferably, the drive rod runs through connecting rod, and ball bearing is provided between drive rod and connecting rod, the biography
The surrounding outer surface of lever is flexibly connected by ball bearing with the inner surface of connecting rod.
Preferably, power supply line, and the input terminal and power supply line of radiating motor are provided between the radiating motor and fuselage
Output end be electrically connected.
Preferably, the quantity of the dot matrix infrared lamp is four groups, and the quantity of the LED white light is two groups.
Compared with prior art, the utility model has the following beneficial effects: being somebody's turn to do the video monitoring instrument that communicated based on 4G,
By the Surge Protector of setting, when each video monitoring instrument is struck by lightning, protection video monitoring instrument can be very good
Safety guarantees the normal work of video monitoring instrument, by the lifting slide wall of setting, can safety easily by monitoring instrument
It removes and is safeguarded and cleared up, the setting of fuselage thermovent, work of the heat for preventing instrument from generating in work process to instrument
It is impacted as effect, also protects the service life of instrument well, the video monitoring instrument structure entirely based on 4G communication
Simply, easy to operate, the effect used is more preferable relative to traditional approach.
Detailed description of the invention
Fig. 1 is overall structure diagram of the utility model based on the 4G video monitoring instrument communicated.
Fig. 2 is partial view of the utility model based on the 4G video monitoring instrument communicated.
Fig. 3 is radiator enlarged drawing of the utility model based on the 4G video monitoring instrument communicated.
Fig. 4 is fixation wall partial view of the utility model based on the 4G video monitoring instrument communicated.
Fig. 5 is the enlarged drawing of A in the Fig. 2 of the utility model based on the 4G video monitoring instrument communicated.
Fig. 6 is the enlarged drawing of B in the Fig. 4 of the utility model based on the 4G video monitoring instrument communicated.
In figure: 1, fuselage;2, fixed frame side;3, radar installations;4, rotation top;5, fixation wall;6, slide wall is gone up and down;7, it props up
Frame;8, radiating motor device;9, antenna;10, connecting rod;11, photo resistance;12, dot matrix infrared lamp;13, LED white light;14,
High-definition camera;15, working panel;16, swingle;17, fuselage thermovent;18, lifting button;19, drive rod;20, it goes up and down
Motor;21, radiating motor;22, gear;23, toothed disc;24, radiator fan;25, Surge Protector.
Specific embodiment
To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below
In conjunction with specific embodiment, the utility model is further described.
As shown in figures 1 to 6, the video monitoring instrument based on 4G communication of the utility model, including fuselage 1, under fuselage 1
Hold outer surface that fixed frame side 2 is fixedly mounted, the two sides inner surface of fixed frame side 2 is connected with working panel 15, working face
The leading exterior surface of plate 15 is fixedly installed with radar installations 3, photo resistance 11, dot matrix infrared lamp 12, LED white light 13 and high definition
Camera 14, photo resistance 11 are located at the upper end of high-definition camera 14, and radar installations 3 is located at the lower end of high-definition camera 14, point
Battle array infrared lamp 12 is located at the two sides of high-definition camera 14, and LED white light 13 is located at the lower end of dot matrix infrared lamp 12, after fuselage 1
End outer surface is fixedly installed with fuselage thermovent 17, and the upper end outer surface of fuselage 1 is connected with rotation top 4, and the four of 4 are pushed up in rotation
All outer surfaces are movably installed with antenna 9, and the upper end outer surface on rotation top 4 is fixedly installed with connecting rod 10, the upper end of connecting rod 10
Outer surface is fixedly connected with radiating motor device 8, and the upper end outer surface of radiating motor device 8 is fixedly connected with bracket 7, bracket 7
A side external surface be fixedly connected with lifting slide wall 6, lifting slide wall 6 a side external surface be connected with fixation wall 5, fixation wall
5 side external surface is movably installed with lifting button 18, and the inside of fixation wall 5 is fixedly installed with lifting motor 20 and swingle
16, swingle 16 is located at the upper end outer surface of lifting motor 20, and the inside of bracket 7 is fixedly installed with Surge Protector 25, heat dissipation
The inside of electric machine 8 is fixedly installed with radiating motor 21, gear 22, toothed disc 23 and drive rod 19, and radiating motor 21 is located at
The side of gear 22, toothed disc 23 are located at the lower end outer surface of gear 22, and drive rod 19 is located at the lower end outer surface of toothed disc 23,
The inside of fuselage thermovent 17 is fixedly installed with radiator fan 24.
Swingle 16 is provided with screw thread through lifting slide wall 6, and between swingle 16 and lifting slide wall 6, swingle 16
Surrounding outer surface is flexibly connected by screw thread with the inner surface for going up and down slide wall 6, the oscilaltion of easy of rise slide wall 6;Lifting is slided
Sliding slot is provided between wall 6 and fixation wall 5, and two side external surfaces for going up and down slide wall 6 pass through the inner surface of sliding slot Yu fixation wall 5
It is slidably connected, is conducive to the stable lifting for going up and down slide wall 6;Drive rod 19 runs through connecting rod 10, and drive rod 19 and connecting rod 10
Between be provided with ball bearing, the surrounding outer surface of drive rod 19 is connected by the inner surface activity of ball bearing and connecting rod 10
It connects, when rotating fuselage 1, the position of radiator fan 24 is unaffected;It is provided with power supply line between radiating motor 21 and fuselage 1,
And the input terminal of radiating motor 21 and the output end of power supply line are electrically connected, and are conducive to the heat dissipation of fuselage 1;Dot matrix infrared lamp 12
Quantity is four groups, and the quantity of LED white light 13 is two groups, keeps monitor video apparent.
It should be noted that the utility model is the video monitoring instrument communicated based on 4G, when in use, we can be incited somebody to action
Fixed frame side 2 is mounted on wall, then monitoring instrument is loaded onto, then monitoring instrument is raised to us by lifting button 18 and is monitored
Position, we again connect some data lines such as the power supply line of monitoring instrument, so that monitoring instrument is worked, in monitoring instrument work
Inside can generate heat when making, and will affect the monitoring effect of instrument and the service life of monitoring instrument in this way, our used settings
The work of some radiating motors 21 drives the rotation of internal gear 22, drives toothed disc 23 to rotate, makes 24 turns of radiator fan
It is dynamic, internal heat is distributed, we are such as hit by thunder and lightning in thunderstorm weather in monitoring instrument work, we
Monitoring instrument can be protected by the Surge Protector 25 of setting, whether instrument is started by the induction of photo resistance 11
Infrared lamp source, the evening draws on, and dot matrix infrared lamp 12 and LED white light 13 is just opened, and so that monitoring effect is achieved the effect that daytime, makes
Monitoring effect is apparent, radio wave and monitors echo by the constantly transmitting of radar installations 3, carrys out the movement of detecting object, then by
Internal smart host processing, working panel 15 are followed object mobile and rotates, and fuselage 1 and rotation are pushed up and rotated between 4, at any time with
The mobile monitor of track object, we can also be put down monitoring instrument by going up and down slide wall 6, we tie up monitoring instrument
Repair and clear up, do not need people go to remove again ladder or it is padded take, it is safer in this way and humanized, it is more practical.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above.Current row
The technical staff of industry is described in above embodiments and description it should be appreciated that the present utility model is not limited to the above embodiments
Only illustrate the principles of the present invention, on the premise of not departing from the spirit and scope of the utility model, the utility model is also
It will have various changes and improvements, these various changes and improvements fall within the scope of the claimed invention.The utility model
Claimed range is defined by the appending claims and its equivalent thereof.
Claims (6)
1. based on the video monitoring instrument of 4G communication, including fuselage (1), it is characterised in that: the lower end outer surface of the fuselage (1)
Fixed frame side (2) are fixedly mounted, the two sides inner surface of the fixed frame side (2) is connected with working panel (15), described
The leading exterior surface of working panel (15) is fixedly installed with radar installations (3), photo resistance (11), dot matrix infrared lamp (12), LED
White light (13) and high-definition camera (14), the photo resistance (11) are located at the upper end of high-definition camera (14), the radar
Device (3) is located at the lower end of high-definition camera (14), and the dot matrix infrared lamp (12) is located at the two sides of high-definition camera (14), institute
The lower end that LED white light (13) is located at dot matrix infrared lamp (12) is stated, the back end outer surface of the fuselage (1) is fixedly installed with fuselage
Thermovent (17), the upper end outer surface of the fuselage (1) are connected with rotation top (4), the surrounding appearance of the rotation top (4)
Face is movably installed with antenna (9), and the upper end outer surface of the rotation top (4) is fixedly installed with connecting rod (10), the connecting rod
(10) upper end outer surface is fixedly connected with radiating motor device (8), and the upper end outer surface of the radiating motor device (8) is fixed
It is connected with bracket (7), a side external surface of the bracket (7) is fixedly connected with lifting slide wall (6), lifting slide wall (6)
One side external surface is connected with fixation wall (5), and a side external surface of the fixation wall (5) is movably installed with lifting button
(18), the inside of the fixation wall (5) is fixedly installed with lifting motor (20) and swingle (16), and the swingle (16) is located at
The inside of the upper end outer surface of lifting motor (20), the bracket (7) is fixedly installed with Surge Protector (25), the heat dissipation electricity
The inside of machine device (8) is fixedly installed with radiating motor (21), gear (22), toothed disc (23) and drive rod (19), described to dissipate
Thermoelectric perpetual motion machine (21) is located at the side of gear (22), and the toothed disc (23) is located at the lower end outer surface of gear (22), the transmission
Bar (19) is located at the lower end outer surface of toothed disc (23), and the inside of the fuselage thermovent (17) is fixedly installed with radiator fan
(24).
2. the video monitoring instrument according to claim 1 based on 4G communication, it is characterised in that: the swingle (16) is passed through
Lifting slide wall (6) is worn, and is provided with screw thread between swingle (16) and lifting slide wall (6), outside the surrounding of the swingle (16)
Surface is flexibly connected by screw thread with the inner surface for going up and down slide wall (6).
3. the video monitoring instrument according to claim 1 based on 4G communication, it is characterised in that: the lifting slide wall (6)
Two side external surfaces for being provided with sliding slot between fixation wall (5), and going up and down slide wall (6) pass through the interior of sliding slot and fixation wall (5)
Surface is slidably connected.
4. the video monitoring instrument according to claim 1 based on 4G communication, it is characterised in that: the drive rod (19) is passed through
It wears connecting rod (10), and is provided with ball bearing between drive rod (19) and connecting rod (10), the surrounding of the drive rod (19)
Outer surface is flexibly connected by ball bearing with the inner surface of connecting rod (10).
5. the video monitoring instrument according to claim 1 based on 4G communication, it is characterised in that: the radiating motor (21)
Power supply line is provided between fuselage (1), and the output end of the input terminal of radiating motor (21) and power supply line is electrically connected.
6. the video monitoring instrument according to claim 1 based on 4G communication, it is characterised in that: the dot matrix infrared lamp
(12) quantity is four groups, and the quantity of the LED white light (13) is two groups.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201822185156.8U CN209105337U (en) | 2018-12-25 | 2018-12-25 | Video monitoring instrument based on 4G communication |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201822185156.8U CN209105337U (en) | 2018-12-25 | 2018-12-25 | Video monitoring instrument based on 4G communication |
Publications (1)
Publication Number | Publication Date |
---|---|
CN209105337U true CN209105337U (en) | 2019-07-12 |
Family
ID=67163343
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201822185156.8U Active CN209105337U (en) | 2018-12-25 | 2018-12-25 | Video monitoring instrument based on 4G communication |
Country Status (1)
Country | Link |
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CN (1) | CN209105337U (en) |
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2018
- 2018-12-25 CN CN201822185156.8U patent/CN209105337U/en active Active
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