CN207867032U - A kind of radar and the anti-low slow Small object device of photoelectric linkage - Google Patents
A kind of radar and the anti-low slow Small object device of photoelectric linkage Download PDFInfo
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- CN207867032U CN207867032U CN201820186951.6U CN201820186951U CN207867032U CN 207867032 U CN207867032 U CN 207867032U CN 201820186951 U CN201820186951 U CN 201820186951U CN 207867032 U CN207867032 U CN 207867032U
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Abstract
The utility model discloses a kind of radars and the anti-low slow Small object device of photoelectric linkage, including radar system, electro-optical system, rotary table base and cylinder, electro-optical system is located above radar system, radar system is mounted on by holder on cylinder lateral wall, and rotary table base, cylinder, electro-optical system three are coaxial；Telescopic supporting platform is also set up in the inner cavity of rotary table base, telescopic supporting platform is located at below electro-optical system, and sustainable telescopic platform includes strut and support motor, and support motor is located at rotary table base intracavity bottom, strut is located above support motor, and support motor is connected with strut control；Turntable motor, which is arranged in rotary table base and is controlled with cylinder, to be connected.The utility model has the beneficial effects that the present apparatus integrates radar system and electro-optical system, the miniaturization of realization device, radar system and the respective investigation advantage of electro-optical system are combined together, and become a kind of for the full-featured of low slow Small object investigation, efficiently link Reconnaissance system.
Description
Technical field
The utility model belongs to detection device field, and in particular to a kind of radar and the anti-low slow Small object dress of photoelectric linkage
It sets.
Background technology
As the small-sized rotor wing unmanned aerial vehicle of the growth of unmanned plane explosion type, especially consumer level becomes popular consumer goods, therewith
Also the problem of small-sized slower flight device in this kind of low latitude of unmanned plane is supervised is brought.It is black winged to have there are a lot of unmanned planes, has upset the people
Plane field, the accident for causing flight to ground, brings great security risk.Civil and military airport is always all by shape simultaneously
The threat of bird, it is also desirable to which can airport birds be monitored with the means of investigation.Therefore it is small-sized to low latitude at a slow speed（It is low slow small）Target
Investigation, tracking, monitoring, be current urgent demand.
Radar and photoelectric follow-up are to investigate the effective tool of low slow Small object at present.Radar can large area it is complete at a distance
Weather all the period of time expeditiously implements to investigate, but that there are imaging resolutions is low, cannot carry out imaging identification, determine objective attribute target attribute
Disadvantage；Photoelectric follow-up imaging resolution is high, can be under the conditions of visibility higher weather, by VISIBLE LIGHT SYSTEM or infrared
Electro-optical system carries out continual target imaging identification in 24 hours and tracking.But electro-optical system is small in the presence of search target zone, away from
From remote not as good as radar, investigation search efficiency is low, the shortcomings of cannot achieve round-the-clock investigation.
Utility model content
To overcome technological deficiency of the existing technology, it is anti-low slow that the utility model discloses a kind of radars and photoelectric linkage
Small object device, the structure design of difference of height coaxial by inner and outer ring, by radar system and the respective investigation advantage of electro-optical system
It is combined together, becomes a kind of for the full-featured of low slow Small object investigation, efficiently link Reconnaissance system.
Technical solution adopted by the utility model to solve its technical problems is a kind of radar and photoelectric linkage are anti-low slow small
Destination apparatus, including radar system, electro-optical system, rotary table base and the cylinder being set in rotary table base, electro-optical system are located at
Above radar system, rotary table base is a cavity cylinder, and the radar system is mounted on by holder on cylinder lateral wall, turntable base
Seat, cylinder, electro-optical system three are coaxial；
The telescopic supporting platform for being used to support electro-optical system, and telescopic supporting platform position are also set up in the inner cavity of rotary table base
Below electro-optical system, the sustainable telescopic platform includes strut and support motor, and support motor is located at bottom of chamber in rotary table base
Portion, strut are located above support motor, and support motor is connected with strut control；
Further include turntable motor, the turntable motor, which is arranged in rotary table base and is controlled with cylinder, to be connected.
Preferably, the electro-optical system includes photoelectricity three-axle table and photoelectric follow-up, photoelectricity three-axle table, turntable base
Seat is coaxial with cylinder three, and the photoelectric follow-up includes driving motor group, photocell lens group, and driving motor group includes first
Driving motor and the second driving motor, photocell lens group include the first photocell lens and the second photocell lens, the first driving motor
It controls and connects with the first photocell lens, the second driving motor and the control of the second photocell lens connect.
Preferably, the upper surface of strut is equipped with guide rail sleeve, and described its surrounding of guide rail sleeve and rotary table base inner cavity are tight
Contiguity is touched.
Preferably, further include baffle ring, the baffle ring is located at the top of rotary table base.
Preferably, further include protection cap, the protection cap setting and rotary table base top.
Preferably, the radar system further includes radiating groove, 20 centimetres -30 centimetres of radar system and cylinder distance, described
Radiating groove is located in radar system and close to cylinder one side.
The utility model has the beneficial effects that：
1. the present apparatus integrates radar system and electro-optical system, the miniaturization of realization device, radar system and light
The respective investigation advantage of electric system is combined together, and becomes a kind of for the full-featured of low slow Small object investigation, efficiently
Link Reconnaissance system；
2. same reference axis marker location information, thunder may be used in electro-optical system and radar system coaxial design, i.e. the two
Target position signal is captured without conversion up to system, you can transfers to electro-optical system to use, electro-optical system can accurately find fixed
Position target is gone forward side by side line trace；
3. electro-optical system is located above radar system, the two can be kept when turning to either direction, relative position is all kept
It is constant；On azimuth radially investigation direction, electro-optical system is permanently retained in radar system rear, what radar system to be investigated
Pitch angle and azimuth direction will not be blocked by electro-optical system；In the height direction, electro-optical system is above radar system,
In the level to vertical 90 ° of pitch angles and 360 ° of azimuths to be investigated of electro-optical system, will not equally it block.If Opto-electrical Section
System has the investigation demand of negative angle on pitch angle, can also be realized by raising the difference in height of photoelectric follow-up and radar.
4. electro-optical system can realize the automatic function of packing up or be unfolded, in the feelings without using electro-optical system or harsh weather
Under condition, electro-optical system is received into cylinder bore automatically, covers protection cap, realizes the protection to photoelectric follow-up.
Description of the drawings
Fig. 1 is a kind of specific implementation mode structural schematic diagram of the utility model half sectional view.
Fig. 2 is a kind of specific implementation mode structural schematic diagram of the utility model.
Fig. 3 is a kind of specific implementation mode structural schematic diagram that the utility model carries protection cap.
Reference numeral：1- rotary table bases, 2- cylinders, 3- holders, 4- radar systems, 5- photoelectricity three-axle tables, 6- Opto-electrical Sections
System, the first driving motors of 7-, the second driving motors of 8-, the first photocell lens of 9-, the second photocell lens of 10-, 11- guide rail sleeves,
12- baffle rings, 13- struts, 14- support motor, 15- turntable motors, 16- protection caps.
Specific implementation mode
More detailed description is done to the embodiment of the utility model below in conjunction with attached drawing and reference numeral, makes to be familiar with ability
The technology people in domain can implement according to this after studying this specification carefully.It should be appreciated that specific embodiment described herein is only solving
The utility model is released, is not used to limit the utility model.
In the description of the present invention, it should be noted that the orientation of the instructions such as term "upper", "horizontal", "inner" or
Position relationship is to be based on the orientation or positional relationship shown in the drawings, and is merely for convenience of describing the present invention and simplifying the description,
It does not indicate or imply the indicated device or element must have a particular orientation, with specific azimuth configuration and operation, because
This should not be understood as limiting the present invention.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified
Dress ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
Can also be electrical connection to be mechanical connection；It can be directly connected, can also indirectly connected through an intermediary, Ke Yishi
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood at this with concrete condition
Concrete meaning in utility model.
Embodiment：Referring to attached drawing 1, attached drawing 2, a kind of attached radar shown in Fig. 3 and the anti-low slow Small object device of photoelectric linkage,
Including radar system 4, electro-optical system 6, rotary table base 1 and the cylinder 2 being set in rotary table base 1, electro-optical system 6 is located at radar
4 top of system, rotary table base 1 are a cavity cylinder, and the radar system 4 is mounted on by holder 3 on 2 lateral wall of cylinder, turntable
Pedestal 1, cylinder 2,6 three of electro-optical system are coaxial；
The telescopic supporting platform for being used to support electro-optical system 6, and telescopic supporting platform are also set up in the inner cavity of rotary table base 1
Positioned at 6 lower section of electro-optical system, the sustainable telescopic platform includes strut 13 and support motor 14, and support motor 14 is located at turntable base
1 intracavity bottom of seat, strut 13 are located at 14 top of support motor, and support motor 14 is connected with the control of strut 13；
Further include turntable motor 15, the turntable motor 15, which is arranged in rotary table base 1 and is controlled with cylinder 2, to be connected.
In the present embodiment, cylinder 2 is mounted in rotary table base 1, and turntable motor 15 is mounted on the upper table of 1 bottom plate of rotary table base
Face is connected between turntable motor 15 and cylinder 2 by gear, drives cylinder 2 to rotate horizontally by gear, radar system 4 passes through
Holder 3 be mounted on cylinder 2 on, with cylinder 2 rotate, radar system 4 can 360 ° to surrounding scan monitor, radar battle array as needed
There are certain angles with vertical direction in face；Motor 14 is supported to be mounted on 1 intracavity bottom of rotary table base, support motor can be used linearly
Stepper motor, electro-optical system 6 are located above support telescopic platform, and support motor 14 is by driving strut 13 to move up and down to drive
Electro-optical system 6 moves up and down, and when support motor 14 drives strut 13 upward, jack-up electro-optical system 6 is upward, and electro-optical system 6 is higher than
Rotary table base 1 and radar system 4.
The ceaselessly rotation sweep under the driving of turntable motor 15 of radar system 4, when investigation is to low slow Small object signal,
Azimuth and pitching angle information are generated, and passes it to 6 alignment target region of electro-optical system and carries out target imaging knowledge
Not and track.
Preferably, the electro-optical system 6 includes photoelectricity three-axle table 5 and photoelectric follow-up, and photoelectricity three-axle table 5 turns
Sewing platform base 1 and 2 three of cylinder are coaxial, and the photoelectric follow-up includes driving motor group, photocell lens group, driving motor group packet
The first driving motor 7 and the second driving motor 8 are included, photocell lens group includes the first photocell lens 9 and the second photocell lens 10, the
One driving motor 7 and the control of the first photocell lens 9 connect, and the second driving motor 8 and the control of the second photocell lens 10 connect.
The first driving motor 7 and the second driving motor 8 of electro-optical system 6, which can coordinate, to be used in conjunction with or independently rotates, photoelectricity
System the first driving motor 7, the second driving motor 8 driving under the first photocell lens 9, the second photocell lens 10 can be made total
Same level is rotated by 360 °, can also single camera lens be rotated up and down 360 °, photoelectricity three-axle table 5 can 360 ° of rotations of level, cooperation the
First photocell lens 9 and the second photocell lens 10 can be directed toward any needs and detectd by one driving motor 7 and the second driving motor 8
The field range examined（Illustrate photoelectricity three-axle table）；
Photoelectric follow-up after receiving the target position informations such as azimuth and pitch angle, control photoelectricity three-axle table 5,
First driving motor 7 and the second driving motor 8 by the first photocell lens 9,10 alignment target region of the second photocell lens and carry out
Target imaging identifies and tracking.
Preferably, the upper surface of strut 13 is equipped with guide rail sleeve 11,11 its surrounding of the guide rail sleeve and rotary table base 1
Inner cavity is in close contact.
Guide rail sleeve 11 is the mounting platform for supporting electro-optical system 6, and surrounding is in close contact with 1 inner cavity of rotary table base, both
Cooperation strut 13 plays movement guiding function, and also avoiding the torque of electro-optical system 6 from being transmitted on strut 13 causes suffered by strut 13
The excessive damage for causing strut 13 or supporting motor 14 of moment of flexure.
Preferably, further include baffle ring 12,12 ring of the shelves is located at the top of rotary table base 1.
As shown in Fig. 2,2 side wall of cylinder forms a circular ring structure apart from 1 side wall of rotary table base, and a gear is arranged at the top of it
Ring 12 prevents water and sand dust from entering in the rotating contact face of rotary table base 1 and cylinder 2 and generating corrosion or abrasion.
Preferably, further include protection cap 16, the setting of the protection cap 16 and 1 top of rotary table base.
As shown in Fig. 3, when needing to pack up electro-optical system 6, the first driving motor 7 and the second driving motor 8 difference
First photocell lens 9, the second photocell lens 10 are holded up, then motor 14 are supported to pull down strut 13, drive electro-optical system 6,
It is retracted into the inner cavity of rotary table base 1, then uses protection cap 16, the upper direction of rotary table base 1 is covered, rainwater and sand are prevented
Dirt enters 1 inner cavity of rotary table base, prevents the contact surface that such as sand dust enters 1 inner cavity of guide rail sleeve 11 and rotary table base from generating abrasion
It is even stuck.
Preferably, the radar system further includes radiating groove, 20 centimetres -30 centimetres of radar system and cylinder distance, described
Radiating groove is located in radar system and close to cylinder one side.
Radar system gap certain at a distance from cylinder, when radar being facilitated to rotate, air circulates from the radar back side and band
Walk the heat on radiating groove.
The above content is the further descriptions made to the utility model in conjunction with specific preferred embodiment, cannot recognize
Determine specific embodiment of the present utility model and is confined to these explanations.For the common skill of the utility model technical field
For art personnel, the other embodiment obtained in the case where not departing from the technical solution of the utility model should be included in this practicality
In novel protection domain.
Claims (6)
1. a kind of radar and the anti-low slow Small object device of photoelectric linkage, it is characterised in that：Including radar system（4）, electro-optical system
（6）, rotary table base（1）And it is set in rotary table base（1）On cylinder（2）, electro-optical system（6）Positioned at radar system（4）Top,
Rotary table base（1）For a cavity cylinder, the radar system（4）Pass through holder（3）Mounted on cylinder（2）On lateral wall, turntable base
Seat（1）, cylinder（2）, electro-optical system（6）Three is coaxial；
Rotary table base（1）Inner cavity in also set up and be used to support electro-optical system（6）Telescopic supporting platform, and telescopic supporting platform
Positioned at electro-optical system（6）Lower section, the telescopic supporting platform include strut（13）And support motor（14）, support motor（14）Position
In rotary table base（1）Intracavity bottom, strut（13）Positioned at support motor（14）Top supports motor（14）With strut（13）Control
Connection；
It further include turntable motor（15）, the turntable motor（15）It is arranged in rotary table base（1）Upper and and cylinder（2）Control connects
It connects.
2. radar as described in claim 1 and the anti-low slow Small object device of photoelectric linkage, it is characterised in that：The electro-optical system
（6）Including photoelectricity three-axle table（5）And photoelectric follow-up, photoelectricity three-axle table（5）, rotary table base（1）With cylinder（2）Three
Coaxially, the photoelectric follow-up includes driving motor group, photocell lens group, and driving motor group includes the first driving motor（7）
With the second driving motor（8）, photocell lens group includes the first photocell lens（9）With the second photocell lens（10）, the first driving electricity
Machine（7）With the first photocell lens（9）Control connection, the second driving motor（8）With the second photocell lens（10）Control connection.
3. radar as described in claim 1 and the anti-low slow Small object device of photoelectric linkage, it is characterised in that：Strut（13）It is upper
End face is equipped with guide rail sleeve（11）, the guide rail sleeve（11）Its surrounding and rotary table base（1）Inner cavity is in close contact.
4. radar as described in claim 1 and the anti-low slow Small object device of photoelectric linkage, it is characterised in that：It further include baffle ring
（12）, the baffle ring（12）Positioned at rotary table base（1）Top.
5. radar as described in claim 1 and the anti-low slow Small object device of photoelectric linkage, it is characterised in that：It further include protection cap
（16）, the protection cap（16）Setting and rotary table base（1）Top.
6. radar as described in claim 1 and the anti-low slow Small object device of photoelectric linkage, it is characterised in that：The radar system
（4）Further include radiating groove, radar system（4）With cylinder（2）20 centimetres -30 centimetres of distance, the radiating groove are located at radar system
（4）Upper and close cylinder（2）On one side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820186951.6U CN207867032U (en) | 2018-02-02 | 2018-02-02 | A kind of radar and the anti-low slow Small object device of photoelectric linkage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820186951.6U CN207867032U (en) | 2018-02-02 | 2018-02-02 | A kind of radar and the anti-low slow Small object device of photoelectric linkage |
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| Publication Number | Publication Date |
|---|---|
| CN207867032U true CN207867032U (en) | 2018-09-14 |
Family
ID=63461148
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820186951.6U Active CN207867032U (en) | 2018-02-02 | 2018-02-02 | A kind of radar and the anti-low slow Small object device of photoelectric linkage |
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| CN (1) | CN207867032U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109324631A (en) * | 2018-09-19 | 2019-02-12 | 北京机械设备研究所 | A kind of photoelectronic tracking device auxiliary body having positioning direction-measuring function |
| CN110673133A (en) * | 2019-10-14 | 2020-01-10 | 成都航天科工微电子系统研究院有限公司 | High-precision finger radar system based on search and tracking coaxiality |
| CN111190156A (en) * | 2020-01-08 | 2020-05-22 | 中国船舶重工集团公司第七二四研究所 | Radar and photoelectric based low-slow small target and sea surface small target identification method |
| CN111540999A (en) * | 2020-05-22 | 2020-08-14 | 四川中科成光科技有限公司 | Radar revolving stage |
| CN112162284A (en) * | 2020-08-31 | 2021-01-01 | 河北汉光重工有限责任公司 | Triaxial keeps away and bumps photoelectric device |
| CN114019502A (en) * | 2021-11-08 | 2022-02-08 | 北京环境特性研究所 | Integrated target reconnaissance system |
-
2018
- 2018-02-02 CN CN201820186951.6U patent/CN207867032U/en active Active
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109324631A (en) * | 2018-09-19 | 2019-02-12 | 北京机械设备研究所 | A kind of photoelectronic tracking device auxiliary body having positioning direction-measuring function |
| CN110673133A (en) * | 2019-10-14 | 2020-01-10 | 成都航天科工微电子系统研究院有限公司 | High-precision finger radar system based on search and tracking coaxiality |
| CN111190156A (en) * | 2020-01-08 | 2020-05-22 | 中国船舶重工集团公司第七二四研究所 | Radar and photoelectric based low-slow small target and sea surface small target identification method |
| CN111540999A (en) * | 2020-05-22 | 2020-08-14 | 四川中科成光科技有限公司 | Radar revolving stage |
| CN111540999B (en) * | 2020-05-22 | 2023-02-21 | 四川中科成光科技有限公司 | Radar revolving stage |
| CN112162284A (en) * | 2020-08-31 | 2021-01-01 | 河北汉光重工有限责任公司 | Triaxial keeps away and bumps photoelectric device |
| CN112162284B (en) * | 2020-08-31 | 2023-03-28 | 河北汉光重工有限责任公司 | Triaxial collision-preventing photoelectric device |
| CN114019502A (en) * | 2021-11-08 | 2022-02-08 | 北京环境特性研究所 | Integrated target reconnaissance system |
| CN114019502B (en) * | 2021-11-08 | 2024-10-01 | 北京环境特性研究所 | Integrated target reconnaissance system |
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