CN108872943A - Building block system radar front system and installation method - Google Patents
Building block system radar front system and installation method Download PDFInfo
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- CN108872943A CN108872943A CN201810721689.5A CN201810721689A CN108872943A CN 108872943 A CN108872943 A CN 108872943A CN 201810721689 A CN201810721689 A CN 201810721689A CN 108872943 A CN108872943 A CN 108872943A
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- radar
- radar module
- oblique angle
- braced frame
- building block
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- 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
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- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Radar Systems Or Details Thereof (AREA)
- Support Of Aerials (AREA)
Abstract
The present invention relates to Radar Technology fields, more particularly to building block system radar front system and installation method, including several grounds, the support frame, the oblique angle radar module that are made of several braced frames, several braced frames are fixed on the supporting surface being made of several grounds, and oblique angle radar module is fixed on the support frame.Installation method is：Definitely radix amount, scribing line, mounting foundation, installation braced frame, installation oblique angle radar module etc..The advantage of the invention is that：Radar front system is subjected to modularization decomposition, to keep building for radar front system relatively simple, and its front precision can be adjusted step by step during building, and the extension of radar front system can be carried out as needed, simultaneously when recycling radar front system, modules can be removed rapidly, be transported, therefore its mobility is stronger.
Description
Technical field
The present invention relates to Radar Technology fields, and in particular to building block system radar front system and installation method.
Background technique
Radar front system is the chief component of radar system, has enormous size, required precision height, sets up difficulty
The features such as big.Currently, traditional radar front main structure body is mainly that steel skeleton components grade is spliced, when erection, is not only consumed
When, effort, and be difficult to skeleton structure level once build meet front installation high-precision requirement structure, it is still necessary in front
On the basis of skeleton, carries out single layer even multilayer and adjust, to be spliced into the multistage skeleton of suitable radar front installation requirement, no
Extensive work only is brought to erected on site and the time wastes, and does not have ability that is expansible, can moving.
Summary of the invention
The technical problem to be solved by the present invention is to：Radar front system accuracy is low in the prior art, it is difficult to set up, can not expand
The problem of exhibition.
In order to solve the above technical problems, the technical solution adopted by the present invention is that：Building block system radar front system, if including
Dry ground, support frame, the oblique angle radar module being made of several braced frames, several braced frames are fixed on by several
On the supporting surface of ground composition, oblique angle radar module is fixed on the support frame.
Optimization, the ground includes at least three supporting legs, cabinet, mounting blocks, and supporting leg is distributed in the bottom of cabinet,
And cabinet is adjustable relative to supporting leg height, the upper surface of cabinet is arranged in mounting blocks.
Optimization, the supporting leg includes the rod-shaped adjusting support leg of screw thread, adjusts and is screwed with nut in support leg；
It is vertically arranged with sleeve in the cabinet, is adjusted in the upper end insertion sleeve of support leg, nut withstands on the following table of cabinet
Face.
Optimization, the supporting leg further includes Anti-off bolt, and mounting blocks are located at the top for adjusting support leg, and Anti-off bolt passes through
Mounting blocks, which are screwed in, to be adjusted in support leg.
Optimization, be provided with counterweight part in the cabinet, counterweight part by reinforcing bar and coagulation local soil type at.
Optimization, the braced frame is cuboid framework, and is equipped with support seat board on each surface of braced frame, is supported
Seat board is connected in braced frame, and support seat board is equipped with support rim, and support rim end face is higher than the surface of braced frame, branch
Connecting hole is offered on support boss, and the end face of all support rims on the same surface of braced frame is coplanar, braced frame
Roll adjustment component is installed on the support seat board of upper surface.
Optimization, the four corners on each surface of braced frame are arranged in the support seat board.
Optimization, two adjacent sides are also equipped with roll adjustment component in the braced frame.
Optimization, the oblique angle radar module includes radar module skeleton, radar front unit, radar corollary equipment, radar battle array
Face unit and radar corollary equipment are installed on radar module skeleton, and radar corollary equipment is connected on radar front unit.
Optimization, the radar module skeleton is two relatively parallel faces quadrangular shape in a rectangular trapezoid, and normal
When putting, the plane where two right-angled trapezium bottom edges is the bottom surface of radar module skeleton, flat where two right-angled trapezium bevel edges
Face is the inclined-plane of radar module skeleton, and radar front unit is mounted on the inclined-plane of radar module skeleton, and radar corollary equipment is mounted on
The inside of radar module skeleton.
Optimization, the position on the top surface of the radar module skeleton close to radar module skeleton inclined-plane is provided with guide-localization
Part is provided with guide-localization corresponding with guide-localization part hole, guide-localization part, guide-localization hole on the bottom surface of radar module skeleton
Inclination direction and inclination angle size it is identical as the inclination direction on radar module skeleton inclined-plane and inclination angle size.
Optimization, the length of the top and bottom of the radar module skeleton, width be braced frame top and bottom length,
The integral multiple of width, and the height of radar module skeleton is the integral multiple of the height of braced frame.
Optimization, radar module seat is respectively provided on other each faces in face where removing radar front unit on the radar module skeleton
Plate, radar module seat board are equipped with connection boss, and the outer end face for connecting boss is higher than the surface of radar module skeleton, connect and open on boss
Equipped with radar module connecting hole, and the outer end face of all connection boss on radar module skeleton on the same face is coplanar.
Optimization, the radar front unit includes reflecting plate, transmitting bar, antenna, and reflecting plate is mounted on radar module skeleton
On, transmitting bar, antenna are mounted on reflecting plate, and reflecting plate, transmitting bar, antenna are connect with radar corollary equipment.
Optimization, the radar corollary equipment includes the electronic equipment controlled radar front unit, sets to electronics
The liquid cooling system of standby and oblique angle radar module internal environment control, liquid cooling system leads to inside oblique angle radar module and electronic equipment.
Invention additionally discloses a kind of installation methods applied to above-mentioned building block system radar front system, include the following steps：
A. according to the scale of building block system radar front system, the quantity of ground is determined；
B. it crosses in the location chosen in advance according to the placement position of ground；
C., ground is placed into the region of scribing line；
D. the height of each ground top surface is measured, the height of adjustment ground top surface flushes the top surface of all grounds, this is the
One layer；
E. braced frame is installed on ground, and adjacent braced frame is linked together, this is the second layer；
F. oblique angle radar module is installed in braced frame, and adjusts the position of oblique angle radar module, comply with default position
Requirement is set, adjacent oblique angle radar module is linked together, and support frame is installed in the position that this layer does not install oblique angle radar module
Frame, and braced frame is connect with oblique angle radar module, adjacent braced frame also links together, and adjusts this layer of braced frame
Position flushes this layer of oblique angle radar module with braced frame, this is third layer.
G. oblique angle radar module is mounted on the oblique angle radar module of third layer, adjusts the position of oblique angle radar module, guarantee this
The front of layer oblique angle radar module is flushed with the oblique angle radar module front of third layer, will be adjacent to constitute the front met the requirements
Oblique angle radar module links together, and installs braced frame in the position that this layer does not install oblique angle radar module, and by braced frame
It is connect with oblique angle radar module, adjacent braced frame also links together, and adjusts the position of this layer of braced frame, makes this layer of oblique angle
Radar module is flushed with braced frame, this is the 4th layer.
H. and so on, step G is repeated, until building block system radar front system is installed.
The beneficial effects of the present invention are：
1. radar front system is subjected to modularization decomposition, thus keep building for radar front system relatively simple, and
Its front precision can be adjusted during building step by step, and the extension of radar front system can be carried out as needed, while
When recycling radar front system, modules can be removed rapidly, be transported, therefore its mobility is stronger；
It, can be according to the big of radar system scale in practical build process 2. Foundation Part is divided into several independent grounds
The small laying for carrying out ground can carry out random permutation and combination to several grounds, build demand, and the height of ground to meet
It can be adjusted according to actual needs, building for ground is made to be influenced by surface state smaller, therefore the adaptability of ground is stronger,
It can guarantee requirement of the radar front to precision；
3. braced frame is to play the role of the component of main support in radar system, braced frame is pre- in advance using factory
System, the mode installed of scene set up radar more convenient, rapid, and each braced frame is generally applicable, the scope of application compared with
Extensively, and in braced frame it is provided with roll adjustment component, can be adjusted according to actual needs in the build process of radar, to protect
Demonstrate,prove the precision of radar front；
4. the setting of oblique angle radar module is divided into multiple identical components for entire radar front is modular, by radar front
Front end component be integrated into each cabin, convenient for set up, remove, while be convenient for daily maintenance, the guide-localization part being arranged thereon
And guide-localization hole, when the oblique angle radar module on upper layer can be made to be installed to the oblique angle radar module of lower layer, oblique angle radar module is fixed according to guiding
The inclined direction of position part is fallen, so that the components such as the antenna destroyed on lower layer oblique angle radar module inclined-plane because falling vertically are avoided,
Oblique angle radar module can also be positioned simultaneously, to guarantee the precision of radar front；
5. the length of the top and bottom of radar module skeleton, width be braced frame top and bottom length, width it is whole
Several times, and the height of radar module skeleton is the integral multiple of the height of braced frame, it is ensured that when progress radar system is built,
It is fitted close between oblique angle radar module and braced frame, to build the shape of rule, guarantees the precision of radar system.
Detailed description of the invention
Fig. 1 is the schematic diagram of building block system radar front system in the embodiment of the present invention；
Fig. 2 is the schematic diagram of ground in the embodiment of the present invention；
Fig. 3 is the main view of ground in the embodiment of the present invention；
Fig. 4 is the top view of ground in the embodiment of the present invention；
Fig. 5 is the permutation and combination schematic diagram of ground in the embodiment of the present invention；
Fig. 6 is the schematic diagram of braced frame in the embodiment of the present invention；
Fig. 7 is that braced frame is installed to the schematic diagram on ground in the embodiment of the present invention；
Fig. 8 is the side view of oblique angle radar module in the embodiment of the present invention；
Fig. 9 is the axonometric drawing of oblique angle radar module in the embodiment of the present invention；
Figure 10 is the schematic diagram of radar module skeleton in the embodiment of the present invention；
Figure 11 is the schematic diagram (removing radar module skeleton) of oblique angle radar module in the embodiment of the present invention；
Figure 12 is the schematic diagram of guide-localization part in the embodiment of the present invention；
Wherein, ground -11, braced frame -12, oblique angle radar module -13；
Supporting leg -111, cabinet -112, mounting blocks -113, support seat board -121, radar module skeleton -131, radar front list
First -132, radar corollary equipment -133；
Adjust support leg -1111, nut -1112, Anti-off bolt -1113, gasket -1114, sleeve -1121, reinforcing bar -1122,
Concrete -1123, cushion block -1131, pressing plate -1132, support rim -1211, roll adjustment component -1212, radar module seat board -1311,
Guide-localization part -1312, guide-localization hole -1313, reflecting plate -1321, transmitting bar -1322, antenna -1323, electronic equipment -
1331, liquid cooling system -1332；
Connecting hole -12111, radar module connecting hole -13112, guide-localization bolt -13121, is led at connection boss -13111
To positioning screw cap -13122.
Specific embodiment
The present invention is described in detail below in conjunction with attached drawing.
In the description of the present invention, it should be noted that the orientation of the instructions such as term " on ", "lower", "inner" or position are closed
System is merely for convenience of description of the present invention and simplification of the description to be based on the orientation or positional relationship shown in the drawings, rather than indicates
Or imply that signified device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore cannot understand
For limitation of the present invention.
As shown in Figure 1, building block system radar front system, including several grounds 11, it is made of several braced frames 12
Support frame, oblique angle radar module 13, several braced frames 12 are fixed on the supporting surface being made of several grounds 11, oblique angle
Radar module 13 is fixed on the support frame, and the ground 11 in the present embodiment is arranged 12, and braced frame 12 is arranged 68 altogether, oblique angle thunder
Be arranged 16 up to cabin 13, in practical build process, first according to design by 12 grounds 11 be laid with on ground, such as Fig. 5 institute
Show, is the permutation and combination schematic diagram of ground 11 in the embodiment of the present invention, this is first layer, then installs 30 braced frames 12
Onto ground 11, braced frame 12 is the second layer, and 4 oblique angle radar modules 13 are then installed to the braced frame 12 of the second layer
On, and 17 braced frames 12 of this layer are installed in the braced frame 12 of the second layer, this is third layer, and third layer installs
The 4th layer of installation is carried out after finishing, a part of the 4th layer of 4 oblique angle radar modules 13 is installed to the oblique angle radar module of third layer
On 13, another part is then installed in the braced frame 12 of third layer, and so on carry out the installation of other layers, until be mounted to
Radar front system as shown in Figure 1.
As shown in Fig. 2, the ground 11 includes at least three supporting legs 111, cabinet 112, mounting blocks 113, supporting leg 111
It is distributed in the bottom of cabinet 112, and cabinet 112 is adjustable relative to 111 height of supporting leg, cabinet 112 is arranged in mounting blocks 113
Upper surface.
As shown in figure 3, the supporting leg 111 includes the rod-shaped adjusting support leg 1111 of screw thread, adjusts and be screwed in support leg 1111
Nut 1112.
It is vertically arranged with sleeve 1121 in the cabinet 112, adjusts in the upper end insertion sleeve 1121 of support leg 1111, nut
1112 withstand on the lower surface of cabinet 112, further, are additionally provided with gasket between 112 lower surface of nut 1112 and cabinet
1114, nut 1112 is turned, nut 1112 is moved up and down along support leg 1111 is adjusted, to realize the mesh of adjustment 11 height of ground
's.
Further, the supporting leg 111 further includes Anti-off bolt 1113, and mounting blocks 113, which are located at, adjusts support leg 1111
Top, Anti-off bolt 1113 pass through mounting blocks 113 and are screwed in adjusting support leg 1111, to prevent from adjusting support leg 1111 from sleeve 1121
In fall off.
As shown in Figure 3-4, it is provided with counterweight part in the cabinet 112, counterweight part is by reinforcing bar 1122 and concrete
1123 compositions, to prevent ground 11 from moving because of the extraneous external force such as strong wind, to guarantee the whole of radar front system
Body intensity and stability.
It is then the arrangement mode of ground 11 in the embodiment of the present invention shown in Fig. 5.
As shown in fig. 6, the braced frame 12 is cuboid framework, and support base is equipped on each surface of braced frame 12
Plate 121, support seat board 121 are connected in braced frame 12, and support seat board 121 is equipped with support rim 1211, support rim
1211 end faces are higher than the surface of braced frame 12, offer connecting hole 12111 on support rim 1211, and braced frame 12 is same
The end face of all support rims 1211 on surface is coplanar, is equipped with tune on the support seat board 121 of the upper surface of braced frame 12
Away from component 1212.
Further, the four corners on each surface of braced frame 12 are arranged in the support seat board 121.
Further, two sides adjacent in the braced frame 12 are also equipped with roll adjustment component 1212, the present embodiment
In roll adjustment component 1212 be the bolt being arranged on support seat board 121, head withstands on the other component contacted, spiral shell
Bolt turns in support seat board 121, to realize the adjusting of distance.
Connection type between the braced frame 12 adjacent thereto of braced frame 12 is：The connecting hole of the two corresponding position
12111 pairs its, adjusting roll adjustment component 1212 makes spacing between the two reach requirement, and bolt is then passed through opposite two connections
Hole 12111 is simultaneously tightened with nut, and the connection of two neighboring braced frame 12 can be realized.
As shown in fig. 7, the schematic diagram on ground 11 is installed to for braced frame 12 in the embodiment of the present invention, by braced frame
12 are placed on mounting blocks 113, and then cushion block 1131 is put on mounting blocks 113, and the intermediate pressing plate 1132 for being equipped with long hole is put
Onto support seat board 121 and cushion block 1131, bolt is then passed through into the long hole of pressing plate 1132 and is screwed into setting in mounting blocks 113
On threaded hole in, thus by braced frame 12 be fixed to ground 11 on.
As illustrated in figs. 8-11, the oblique angle radar module 13 is matched including radar module skeleton 131, radar front unit 132, radar
Equipment 133 is covered, radar front unit 132 and radar corollary equipment 133 are installed on radar module skeleton 131, and radar is mating
Equipment 133 is connected on radar front unit 132.
Emphasis refering to fig. 10, the radar module skeleton 131 are two relatively parallel faces four prism type in a rectangular trapezoid
Shape, and normally when putting, the plane where two right-angled trapezium bottom edges is the bottom surface of radar module skeleton 131, two right-angled trapeziums
Plane where bevel edge is the inclined-plane of radar module skeleton 131, and radar front unit 132 is mounted on the inclined-plane of radar module skeleton 131
On, radar corollary equipment 133 is mounted on the inside of radar module skeleton 131.
As seen in figs. 8-10, the position on the top surface of the radar module skeleton 131 close to 131 inclined-plane of radar module skeleton is arranged
There is guide-localization part 1312, as shown in figure 12, guide-localization part 1312 includes guide-localization bolt 13121, guide-localization nut
13122, as seen in figs. 8-10, when another oblique angle radar module 13 is not installed on the upper layer of oblique angle radar module 13, guide-localization nut
13122 are screwed on guide-localization bolt 13121, and emphasis is provided with and is led on the bottom surface of radar module skeleton 131 refering to Fig. 9
To the corresponding guide-localization hole 1313 of locating piece 1312, guide-localization part 1312, guide-localization hole 1313 inclination direction and incline
Angle size is identical as the inclination direction on 131 inclined-plane of radar module skeleton and inclination angle size, therefore it can play the role of guide-localization,
When the guide-localization hole 1313 of oblique angle radar module 13 above it is oliquely downward slided along guide-localization part 1312, Ji Keyin
It leads upper layer oblique angle radar module 13 accurately to fall on the top surface of lower layer's oblique angle radar module 13, to guarantee the whole essence of radar front
Degree, at the same can also avoid because when upper layer oblique angle radar module 13 is vertically fallen with the radar front unit of lower layer oblique angle radar module 13
The problem of 132 interference.
Further, the length of the top and bottom of the radar module skeleton 131, width are 12 top surface of braced frame and bottom
The integral multiple of face length, width, and the height of radar module skeleton 131 is the integral multiple of the height of braced frame 12, to guarantee
It can be spliced into complete structure when carrying out radar front system building, increase its overall stability and precision.
As shown in Figure 10, it removes on the radar module skeleton 131 and is all provided on other each faces in 132 place face of radar front unit
Radar module seat board 1311 is set, radar module seat board 1311 is equipped with connection boss 13111, and the outer end face of connection boss 13111 is higher than
The surface of radar module skeleton 131 connects and offers radar module connecting hole 13112 on boss 13111, and on radar module skeleton 131
The outer end face of all connection boss 13111 on the same face is coplanar, the connection boss 13111 between adjacent oblique angle radar module 13
Alignment, bolt are threaded together after passing through two radar module connecting holes 13112 with nut, and two neighboring oblique angle radar module can be realized
13 connection further for the adjusting for realizing two neighboring 13 distance of oblique angle radar module, is arranged on radar module seat board 1311
Distance adjustor (not shown) identical with roll adjustment component 1212 on support seat board 121.
As shown in figure 8, the radar front unit 132 includes reflecting plate 1321, transmitting bar 1322, antenna 1323, reflection
Plate 1321 is mounted on radar module skeleton 131, and transmitting bar 1322, antenna 1323 are mounted on reflecting plate 1321, and reflecting plate
1321, transmitting bar 1322, antenna 1323 are connect with radar corollary equipment 133.
The radar corollary equipment 133 includes the electronic equipment 1331 controlled radar front unit 132, to electronics
Equipment 1331 and the liquid cooling system 1332 of 13 internal environment of oblique angle radar module control, liquid cooling system 1332 lead to oblique angle radar module 13
Internal and electronic equipment 1331, liquid cooling system 1332 carry out environmental Kuznets Curves to 13 inside of oblique angle radar module and electronic equipment 1331.
Liquid cooling system 1332 includes liquid cooling unit, pipeline, liquid cooling allocation set and fan coil, and liquid cooling pipeline is embedded in radar
Skeleton 131 bottom in cabin is connect with liquid cooling unit, liquid cooling allocation set and fan coil, is realized to 13 inside of oblique angle radar module and electricity
The environmental Kuznets Curves of sub- equipment 1331.
Invention additionally discloses a kind of installation methods applied to above-mentioned building block system radar front system, include the following steps：
A. according to the scale of building block system radar front system, the quantity of ground 11, as shown in Figure 1,5, the present embodiment are determined
In ground 11 be arranged 12；
B. it crosses in the location chosen in advance according to the placement position of ground 11；
C., ground 11 is placed into the region of scribing line, as shown in Figure 5 is the disposing way of ground 11 in the present embodiment,
It arranges and arranges by 4 rows 3；
D. the height of each 11 top surface of ground is measured, the height of adjustment 11 top surface of ground flushes the top surface of all grounds 11,
This is first layer, and specific regulative mode is：Rotating nut 1112, nut 1112 are moved up and down along support leg 1111 is adjusted, and work as peace
When the top surface of dress block 113 is relatively low relative to other faces, nut 1112 is adjusted up, cabinet 112 is then in the promotion of nut 1112
Under move upwards, after mounting blocks 113 rise to suitable position, stop adjust, when the top surface of mounting blocks 113 relative to
When other faces are higher, nut 1112 is adjusted downwards, cabinet 112 then moves downward under gravity, when under mounting blocks 113
After dropping to suitable position, stop adjusting；
E. as shown in Figure 1,30 braced frames 12 are installed on the supporting surface that ground 11 forms, and by adjacent support
Frame 12 links together, this is the second layer, and the specific mounting means that braced frame 12 is installed to ground 11 is：As shown in fig. 7,
It is installed to the schematic diagram on ground 11 for braced frame 12 in the embodiment of the present invention, braced frame 12 is placed into mounting blocks 113
On, then cushion block 1131 is put on mounting blocks 113, the intermediate pressing plate 1132 for being equipped with long hole is put into support seat board 121 and pad
On block 1131, bolt is then passed through into the long hole of pressing plate 1132 and is screwed into the threaded hole being arranged on mounting blocks 113, thus
Braced frame 12 is fixed on ground 11；Connection type between two neighboring braced frame 12 is：The support rim of the two
1211 alignment, then adjust distance between the two by roll adjustment component 1212, then by two support frames of screw bolt passes
The connecting hole 12111 of frame 12, and be threaded together with nut, that is, complete the installation of two neighboring braced frame 12；
F. oblique angle radar module 13 is installed in braced frame 12, and adjusts the position of oblique angle radar module 13, complied with
Predeterminated position requirement, adjacent oblique angle radar module 13 is linked together, and do not install the position of oblique angle radar module 13 in this layer
Braced frame 12 to be installed, and braced frame 12 is connect with oblique angle radar module 13, adjacent braced frame 12 also links together,
The position for adjusting this layer of braced frame 12 flushes this layer of oblique angle radar module 13 with braced frame 12, this is third layer, wherein tiltedly
Connection type between angle radar module 13 and braced frame 12 is identical as the connection type between two neighboring braced frame 12, phase
The connection type between connection type and two neighboring braced frame 12 between adjacent two oblique angle radar modules 13 is also identical.
G. oblique angle radar module 13 is mounted on the oblique angle radar module 13 of third layer, adjusts the position of oblique angle radar module 13,
The front for guaranteeing this layer of oblique angle radar module 13 is flushed with 13 front of oblique angle radar module of third layer, to constitute the battle array met the requirements
Face links together adjacent oblique angle radar module 13, and installs support frame in the position that this layer does not install oblique angle radar module 13
Frame 12, and braced frame 12 is connect with oblique angle radar module 13, adjacent braced frame 12 also links together, and adjusts this layer of branch
The position of support frame frame 12 flushes this layer of oblique angle radar module 13 with braced frame 12, this is the 4th layer, when the 4th layer of oblique angle thunder
When being mounted on the oblique angle radar module 13 of third layer up to cabin 13, first by the guide-localization hole 1313 of the 4th layer of oblique angle radar module 13
It is directed at the guide-localization part 1312 of third layer oblique angle radar module 13, and makes the 4th layer of oblique angle radar module 13 along guide-localization part
1312 slidings are fallen, and then back out guide-localization nut 13122, are put washer and are tightened later with nut, are then carried out adjacent
The installation of two oblique angle radar modules 13, oblique angle radar module 13 and braced frame 12, two neighboring braced frame 12.
H. and so on, step G is repeated, until building block system radar front system is installed.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention
Made any modifications, equivalent replacements, and improvements etc., should all be included in the protection scope of the present invention within mind and principle.
Claims (16)
1. building block system radar front system, it is characterised in that：Including several grounds (11), by several braced frame (12) groups
At support frame, oblique angle radar module (13), several braced frames (12) are fixed on the support being made of several grounds (11)
On face, oblique angle radar module (13) is fixed on the support frame.
2. building block system radar front system according to claim 1, it is characterised in that：The ground (11) includes at least three
A supporting leg (111), cabinet (112), mounting blocks (113), supporting leg (111) are distributed in the bottom of cabinet (112), and cabinet
(112) adjustable relative to supporting leg (111) height, mounting blocks (113) are arranged in the upper surface of cabinet (112).
3. building block system radar front system according to claim 2, it is characterised in that：The supporting leg (111) includes spiral shell
The adjusting support leg (1111) of rasp bar shape adjusts and is screwed with nut (1112) on support leg (1111)；
It is vertically arranged with sleeve (1121), is adjusted in upper end insertion sleeve (1121) of support leg (1111) in the cabinet (112),
Nut (1112) withstands on the lower surface of cabinet (112).
4. building block system radar front system according to claim 3, it is characterised in that：The supporting leg (111) further includes
Anti-off bolt (1113), mounting blocks (113) are located at the top for adjusting support leg (1111), and Anti-off bolt (1113) passes through mounting blocks
(113) it is screwed in and adjusts on support leg (1111).
5. building block system radar front system according to claim 2, it is characterised in that：It is provided in the cabinet (112)
Counterweight part, counterweight part are made of reinforcing bar (1122) and concrete (1123).
6. building block system radar front system according to claim 1, it is characterised in that：The braced frame (12) is rectangular
Body frame, and support seat board (121) is equipped on braced frame (12) each surface, support seat board (121) is connected to braced frame
(12) on, support seat board (121) is equipped with support rim (1211), and support rim (1211) end face is higher than braced frame (12)
Surface offers connecting hole (12111) on support rim (1211), and all supports on braced frame (12) same surface are convex
The end face of platform (1211) is coplanar, is equipped with roll adjustment component (1212) on the support seat board (121) of the upper surface of braced frame (12).
7. building block system radar front system according to claim 6, it is characterised in that：Support seat board (121) setting
Four corners on braced frame (12) each surface.
8. building block system radar front system according to claim 6, it is characterised in that：It is adjacent on the braced frame (12)
Two sides be also equipped with roll adjustment component (1212).
9. building block system radar front system according to claim 1, it is characterised in that：The oblique angle radar module (13) includes
Radar module skeleton (131), radar front unit (132), radar corollary equipment (133), radar front unit (132) and radar are matched
Set equipment (133) is installed on radar module skeleton (131), and radar corollary equipment (133) is connected to radar front unit
(132) on.
10. building block system radar front system according to claim 9, it is characterised in that：The radar module skeleton (131) is
Two relatively parallel faces quadrangular shape in a rectangular trapezoid, and normally when putting, it is flat where two right-angled trapezium bottom edges
Face is the bottom surface of radar module skeleton (131), and the plane where two right-angled trapezium bevel edges is the inclined-plane of radar module skeleton (131),
Radar front unit (132) is mounted on the inclined-plane of radar module skeleton (131), and radar corollary equipment (133) is mounted on radar module
The inside of skeleton (131).
11. building block system radar front system according to claim 10, it is characterised in that：The radar module skeleton (131)
Top surface on be provided with guide-localization part (1312) close to the position on radar module skeleton (131) inclined-plane, radar module skeleton (131)
Guide-localization corresponding with guide-localization part (1312) hole (1313) is provided on bottom surface, guide-localization part (1312), guiding are fixed
The inclination direction and inclination angle size in position hole (1313) are identical as the inclination direction on radar module skeleton (131) inclined-plane and inclination angle size.
12. building block system radar front system according to claim 9, it is characterised in that：The radar module skeleton (131)
The length of top and bottom, the integral multiple that width is braced frame (12) top and bottom length, width, and radar module skeleton
(131) height is the integral multiple of the height of braced frame (12).
13. building block system radar front system according to claim 9, it is characterised in that：On the radar module skeleton (131)
Except being respectively provided with radar module seat board (1311) on other each faces in face where radar front unit (132), radar module seat board (1311)
It is equipped with connection boss (13111), the outer end face of connection boss (13111) is higher than the surface of radar module skeleton (131), connects convex
It is offered on platform (13111) radar module connecting hole (13112), and all connections on radar module skeleton (131) on the same face are convex
The outer end face of platform (13111) is coplanar.
14. building block system radar front system according to claim 9, it is characterised in that：The radar front unit (132)
Including reflecting plate (1321), transmitting bar (1322), antenna (1323), reflecting plate (1321) is mounted on radar module skeleton (131),
Transmitting bar (1322), antenna (1323) are mounted on reflecting plate (1321), and reflecting plate (1321), transmitting bar (1322), antenna
(1323) it is connect with radar corollary equipment (133).
15. building block system radar front system according to claim 9, it is characterised in that：The radar corollary equipment (133)
Including radar front unit (132) is controlled electronic equipment (1331), to electronic equipment (1331) and oblique angle radar module
(13) liquid cooling system (1332) of internal environment control, liquid cooling system (1332) leads to oblique angle radar module (13) inside and electronics is set
Standby (1331).
16. a kind of installation method applied to the building block system radar front system as described in claim any one of 1-9, feature exist
In：Include the following steps：
A. according to the scale of building block system radar front system, the quantity of ground (11) is determined；
B. it crosses in the location chosen in advance according to the placement position of ground (11)；
C., ground (11) is placed into the region of scribing line；
D. the height of each ground (11) top surface is measured, the height of adjustment ground (11) top surface keeps the top surface of all grounds (11) neat
Flat, this is first layer；
E. braced frame (12) is installed on ground (11), and adjacent braced frame (12) is linked together, this is
Two layers；
F. oblique angle radar module (13) is installed on braced frame (12), and adjusts the position of oblique angle radar module (13), make its symbol
Predeterminated position requirement is closed, adjacent oblique angle radar module (13) is linked together, and in this layer oblique angle radar module (13) are not installed
Position braced frame (12) are installed, and braced frame (12) is connect with oblique angle radar module (13), adjacent braced frame
(12) it also links together, adjusts the position of this layer of braced frame (12), make this layer of oblique angle radar module (13) and braced frame
(12) it flushes, this is third layer.
G. oblique angle radar module (13) is mounted on the oblique angle radar module (13) of third layer, adjusts the position of oblique angle radar module (13)
It sets, the front for guaranteeing this layer of oblique angle radar module (13) is flushed with oblique angle radar module (13) front of third layer, is wanted with constituting to meet
Adjacent oblique angle radar module (13) is linked together, and does not install the position of oblique angle radar module (13) in this layer by the front asked
It installs braced frame (12), and braced frame (12) is connect with oblique angle radar module (13), adjacent braced frame (12) also connects
It is connected together, adjusts the position of this layer of braced frame (12), flush this layer of oblique angle radar module (13) with braced frame (12), this
It is the 4th layer.
H. and so on, step G is repeated, until building block system radar front system is installed.
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| CN201810721689.5A CN108872943B (en) | 2018-07-04 | 2018-07-04 | Building block type radar array system and installation method |
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| CN201810721689.5A CN108872943B (en) | 2018-07-04 | 2018-07-04 | Building block type radar array system and installation method |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111596265A (en) * | 2020-06-08 | 2020-08-28 | 中国人民解放军32181部队 | Target indication radar field construction method |
Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030193442A1 (en) * | 2002-04-10 | 2003-10-16 | Lockheed Martin Corporation | Rolling radar array |
| US20040257261A1 (en) * | 2003-06-23 | 2004-12-23 | Agler Robert Cordell | Rf shielding elimination for linear array sar radar systems |
| CN201130708Y (en) * | 2007-12-24 | 2008-10-08 | 中国兵器工业第二○六研究所 | High bearing closed type radar transmission-receive square cabin |
| US20090267835A1 (en) * | 2008-04-25 | 2009-10-29 | Lockheed Martin Corporation | Foldable antenna for reconfigurable radar system |
| US20140140002A1 (en) * | 2012-11-22 | 2014-05-22 | Furuno Electric Co., Ltd. | Radar antenna and radar apparatus |
| US9070964B1 (en) * | 2011-12-19 | 2015-06-30 | Raytheon Company | Methods and apparatus for volumetric coverage with image beam super-elements |
| CN105043284A (en) * | 2015-08-06 | 2015-11-11 | 中国电子科技集团公司第三十八研究所 | System and method for large-scale radar antenna deformation real time measurement |
| CN106374236A (en) * | 2016-10-28 | 2017-02-01 | 安徽四创电子股份有限公司 | Large-array surface phased array radar antenna |
| CN106646393A (en) * | 2016-09-29 | 2017-05-10 | 上海航天测控通信研究所 | Modular and building block type digital array radar system |
| CN106646404A (en) * | 2016-11-23 | 2017-05-10 | 北京无线电测量研究所 | Error correction method and system for double-strip-shaped array plane phased array radar |
| CN106895811A (en) * | 2017-05-04 | 2017-06-27 | 中国电子科技集团公司第三十八研究所 | A kind of antenna arrays of radar automatic Mosaic guides system |
| CN207183510U (en) * | 2017-09-25 | 2018-04-03 | 广西路桥工程集团有限公司 | Geological radar antenna support base |
-
2018
- 2018-07-04 CN CN201810721689.5A patent/CN108872943B/en active Active
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030193442A1 (en) * | 2002-04-10 | 2003-10-16 | Lockheed Martin Corporation | Rolling radar array |
| US20040257261A1 (en) * | 2003-06-23 | 2004-12-23 | Agler Robert Cordell | Rf shielding elimination for linear array sar radar systems |
| CN201130708Y (en) * | 2007-12-24 | 2008-10-08 | 中国兵器工业第二○六研究所 | High bearing closed type radar transmission-receive square cabin |
| US20090267835A1 (en) * | 2008-04-25 | 2009-10-29 | Lockheed Martin Corporation | Foldable antenna for reconfigurable radar system |
| US9070964B1 (en) * | 2011-12-19 | 2015-06-30 | Raytheon Company | Methods and apparatus for volumetric coverage with image beam super-elements |
| US20140140002A1 (en) * | 2012-11-22 | 2014-05-22 | Furuno Electric Co., Ltd. | Radar antenna and radar apparatus |
| CN105043284A (en) * | 2015-08-06 | 2015-11-11 | 中国电子科技集团公司第三十八研究所 | System and method for large-scale radar antenna deformation real time measurement |
| CN106646393A (en) * | 2016-09-29 | 2017-05-10 | 上海航天测控通信研究所 | Modular and building block type digital array radar system |
| CN106374236A (en) * | 2016-10-28 | 2017-02-01 | 安徽四创电子股份有限公司 | Large-array surface phased array radar antenna |
| CN106646404A (en) * | 2016-11-23 | 2017-05-10 | 北京无线电测量研究所 | Error correction method and system for double-strip-shaped array plane phased array radar |
| CN106895811A (en) * | 2017-05-04 | 2017-06-27 | 中国电子科技集团公司第三十八研究所 | A kind of antenna arrays of radar automatic Mosaic guides system |
| CN207183510U (en) * | 2017-09-25 | 2018-04-03 | 广西路桥工程集团有限公司 | Geological radar antenna support base |
Non-Patent Citations (2)
| Title |
|---|
| 张根烜 等: "大型相控阵雷达阵面结构设计研究", 《雷达科学与技术》 * |
| 王小贞 等: "卫星微型雷达中刚柔耦合运动分析", 《实验科学与技术》 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111596265A (en) * | 2020-06-08 | 2020-08-28 | 中国人民解放军32181部队 | Target indication radar field construction method |
| CN111596265B (en) * | 2020-06-08 | 2024-05-17 | 中国人民解放军32181部队 | Method for field construction of target indication radar |
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| Publication number | Publication date |
|---|---|
| CN108872943B (en) | 2022-09-02 |
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