CN106405544A - Low altitude surveillance radar system - Google Patents
Low altitude surveillance radar system Download PDFInfo
- Publication number
- CN106405544A CN106405544A CN201610975351.3A CN201610975351A CN106405544A CN 106405544 A CN106405544 A CN 106405544A CN 201610975351 A CN201610975351 A CN 201610975351A CN 106405544 A CN106405544 A CN 106405544A
- Authority
- CN
- China
- Prior art keywords
- radar system
- low altitude
- antenna
- driving means
- altitude coverage
- 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.)
- Pending
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
- G01S13/886—Radar or analogous systems specially adapted for specific applications for alarm systems
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- General Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
- Aerials With Secondary Devices (AREA)
Abstract
The invention discloses a low altitude surveillance radar system, which comprises an antenna, a transmitting and receiving device, a driving device and a supporting device, wherein the driving device is connected with an electronic cabin and a display device; the driving mechanism is provided with a cooling device; the antenna is connected onto the driving device through a transfer structure; and the transfer structure comprises an angle adjustment piece. The cooling performance is good, and the radar operation is stable.
Description
Technical field
A kind of the present invention relates to radar system field, in particular it relates to low altitude coverage radar system.
Background technology
Low altitude airspace administrative reform instruction》Require " all the time guaranteeing air defence safety, the important mesh of flight safety and ground
Mark safety is put in the first place.Forbidden zone, airspace danger area, border area, national emphasis air defense objective area and emphasis air defense mesh in the air
Mark around the region such as certain area overhead and flight City Regions, airport control area, do not draw in principle set supervision spatial domain and
Report spatial domain." it means that low latitude " control zone " needs search, early warning and disposes the target of super spatial domain scope flight.Low latitude
Warning, air traffic control system etc. will welcome comprehensive outburst in interior whole General Aviation industrial chain.
Current air control, air-defence critical area are mainly detected by Large Radar, and mini-plant mainly includes antenna, transmitting-receiving
The structures such as device, driving means and support meanss, but, its shortage radiator structure of existing mini-plant, affect it stable
Property.
Content of the invention
The present invention provides a kind of low altitude coverage radar system to solve above-mentioned technical problem, and its perfect heat-dissipating ensures thunder
Reach stable.
The present invention solves the above problems and be employed technical scheme comprise that：
A kind of low altitude coverage radar system, including antenna, R-T unit, driving means and support meanss, described driving means with
Electronic compartment is connected with display device, and described drive mechanism is provided with heat abstractor, and described antenna is connected to by exchanging structure
In driving means, described exchanging structure includes angle adjusting piece.Drive mechanism arranges radiator structure, is easy to heat extraction, favorably
In the stability improving radar operation.The angle of antenna is adjusted fix using angle regulator, is easy to antenna
Adjust.
Preferably, described heat abstractor includes multiple louvres, the top of described louvre is provided with screening dirt cap.
Further, described screening dirt cap section becomes " L " type, and its formation with driving means Open Side Down.
Heat abstractor adopts the structure of louvre, and it can effectively realize heat extraction purpose, but, using poroid structure,
It can lead to dust to enter in driving means simultaneously, effectively dust is protected using hiding dirt cap.
Preferably, described angle adjustment mechanism includes being arranged on the groove of antenna and setting on the drive means logical
Hole, described angle regulator is arranged in groove and through hole.
Further, described angle regulator is bolt.
To sum up, the invention has the beneficial effects as follows：
1st, this programme arranges radiator structure in drive mechanism, is easy to heat extraction, is conducive to improving the stability that radar runs.
2nd, this programme is adjusted to the angle of antenna fixing using angle regulator, is easy to the regulation to antenna.
Specific embodiment
With reference to embodiment, the technical scheme in the embodiment of the present invention is clearly and completely described it is clear that institute
The embodiment of description is only a part of embodiment of the present invention, rather than whole embodiments.Based on the embodiment in the present invention, this
The every other embodiment that field those of ordinary skill is obtained under the premise of not making creative work, broadly falls into the present invention
The scope of protection.
Embodiment 1：
A kind of low altitude coverage radar system, including antenna, R-T unit, driving means and support meanss, described driving means with
Electronic compartment is connected with display device, and described drive mechanism is provided with heat abstractor, and described antenna is connected to by exchanging structure
In driving means, described exchanging structure includes angle adjusting piece.
Embodiment 2：
The present embodiment refines on the basis of above-described embodiment, and that is, described heat abstractor includes multiple louvres, described scattered
The top of hot hole is provided with screening dirt cap.
The structure hiding dirt cap may be configured as various structures it is preferred that described screening dirt cap section becomes " L " type, and itself and driving
Open Side Down for the formation of device.
Embodiment 3：
The present embodiment refines on the basis of above-described embodiment, and that is, described angle adjustment mechanism includes being arranged on the recessed of antenna
Groove and setting through hole on the drive means, described angle regulator is arranged in groove and through hole.
Described angle regulator is bolt.
Not only can achieve the fixation to antenna using bolt, and it can achieve the regulation to aerial angle, its structure is simple.
As described above, the present invention can preferably be realized.
Claims (5)
1. a kind of low altitude coverage radar system, including antenna, R-T unit, driving means and support meanss, described driving means
Be connected with electronic compartment and display device it is characterised in that：It is provided with heat abstractor, described antenna passes through to turn in described drive mechanism
Access node structure connects on the drive means, and described exchanging structure includes angle adjusting piece.
2. a kind of low altitude coverage radar system according to claim 1 it is characterised in that：Described heat abstractor includes multiple
Louvre, the top of described louvre is provided with screening dirt cap.
3. a kind of low altitude coverage radar system according to claim 2 it is characterised in that：Described screening dirt cap section becomes " L "
Type, and its formation with driving means Open Side Down.
4. a kind of low altitude coverage radar system according to claim 1 it is characterised in that：Described angle adjustment mechanism includes
It is arranged on the groove of antenna and the through hole arranging on the drive means, described angle regulator is arranged in groove and through hole.
5. a kind of low altitude coverage radar system according to claim 4 it is characterised in that：Described angle regulator is spiral shell
Bolt.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610975351.3A CN106405544A (en) | 2016-11-07 | 2016-11-07 | Low altitude surveillance radar system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610975351.3A CN106405544A (en) | 2016-11-07 | 2016-11-07 | Low altitude surveillance radar system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106405544A true CN106405544A (en) | 2017-02-15 |
Family
ID=58014898
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610975351.3A Pending CN106405544A (en) | 2016-11-07 | 2016-11-07 | Low altitude surveillance radar system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106405544A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20080086714A (en) * | 2007-03-23 | 2008-09-26 | (주)하이게인안테나 | Low altitude radar antenna |
| CN103353590A (en) * | 2013-07-06 | 2013-10-16 | 西安雷通科技有限责任公司 | Hermetically-sealed integrated radar |
| CN104280730A (en) * | 2013-07-09 | 2015-01-14 | 北京瑞达恩科技股份有限公司 | Low-altitude search radar |
| CN204720539U (en) * | 2015-06-02 | 2015-10-21 | 上海无线电设备研究所 | A kind of secured adjusted device |
| CN205248414U (en) * | 2015-11-20 | 2016-05-18 | 天津昶兴科技有限公司 | Antenna receiving device |
| CN105738957A (en) * | 2016-04-15 | 2016-07-06 | 北京市政路桥股份有限公司 | Radar detection vehicle for tunnel lining |
-
2016
- 2016-11-07 CN CN201610975351.3A patent/CN106405544A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20080086714A (en) * | 2007-03-23 | 2008-09-26 | (주)하이게인안테나 | Low altitude radar antenna |
| CN103353590A (en) * | 2013-07-06 | 2013-10-16 | 西安雷通科技有限责任公司 | Hermetically-sealed integrated radar |
| CN104280730A (en) * | 2013-07-09 | 2015-01-14 | 北京瑞达恩科技股份有限公司 | Low-altitude search radar |
| CN204720539U (en) * | 2015-06-02 | 2015-10-21 | 上海无线电设备研究所 | A kind of secured adjusted device |
| CN205248414U (en) * | 2015-11-20 | 2016-05-18 | 天津昶兴科技有限公司 | Antenna receiving device |
| CN105738957A (en) * | 2016-04-15 | 2016-07-06 | 北京市政路桥股份有限公司 | Radar detection vehicle for tunnel lining |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170215 |
|
| WD01 | Invention patent application deemed withdrawn after publication |