CN205749877U - A kind of radar test frock - Google Patents
A kind of radar test frock Download PDFInfo
- Publication number
- CN205749877U CN205749877U CN201620541711.4U CN201620541711U CN205749877U CN 205749877 U CN205749877 U CN 205749877U CN 201620541711 U CN201620541711 U CN 201620541711U CN 205749877 U CN205749877 U CN 205749877U
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- China
- Prior art keywords
- support
- square box
- frame
- party
- fixed flange
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- 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.)
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Abstract
This utility model belongs to radar equipment technical field, is specifically related to a kind of radar test frock.This utility model includes the first support, the second support and for installing the fixed flange of radar equipment to be tested, described first support is provided with installing rack, described fixed flange is bolted on described installing rack, described first support is positioned at above the second support and is attached by rotating pin therebetween, and described first support realizes between described fixed flange card and horizontal plane angle in the adjustment of 0 90 ° of scopes around the axial rotation of rotating pin.First support described in the utility model rotates the upset that radar equipment to be tested can be made to carry out 0 90 ° around rotating pin, when fixed flange card is positioned at horizontal plane or vertical guide, can implement the test process of radar equipment to be tested.This test fixture simple in construction, cheap, the substantial amounts of time has been saved in the test job of radar equipment, substantially reduces the lead time.
Description
Technical field
This utility model belongs to radar equipment technical field, is specifically related to a kind of radar test frock.
Background technology
In radar equipment production process, test is a critically important link.The restriction of source-under-test, logical in test process
Often radar is overturn 90 °, so a lot of Large Radar needs to be equipped with special test fixture, to ensure feasibility and the standard of test
Really property.Currently used more test fixture is test table, its cost about 400,000, and installing/dismounting bothers, so assembling number
Amount is few, and a lot of radars are queued up and used, and leverage the lead time of radar equipment.
Utility model content
In order to solve above-mentioned technical problem, this utility model provides a kind of radar test frock.
In order to realize the purpose of this utility model, this utility model have employed techniques below scheme:
A kind of radar test frock, including the first support, the second support and for installing consolidating of radar equipment to be tested
Determining ring flange, described first support is provided with installing rack, and described fixed flange is bolted on described installing rack, institute
Stating the first support be positioned at above the second support and be attached by rotating pin therebetween, described first support is around rotational pin
The axial rotation of axle realizes between described fixed flange card and horizontal plane angle in the adjustment of 0-90 ° of scope.
Further technical scheme, described first support includes being arranged vertically constituted by the first square box, the second square box
L-shaped bracing frame and for strengthening the support bar of described L-shaped support frame structure intensity, described support bar two ends are fixed respectively
On described first square box, the second square box, described installing rack is positioned at inside L-shaped bracing frame, and described installing rack is provided with confession
The installing hole that bolt passes through, described fixed flange card is parallel with the frame face of described first square box, described first square box
It is provided with the gimbal lever and the first installed part passed through for described rotating pin back to the side of described installing rack, wherein said
First installed part is arranged near the junction of described first square box, the second square box, and the described gimbal lever is away from described first party
Shape frame, the junction of the second square box are arranged, by the described gimbal lever when described fixed flange card turns to be positioned at horizontal plane
First square box is supported.
Further technical scheme, described second support includes that third party's shape frame, the frame face of described third party's shape frame are positioned at
Horizontal direction, is provided with bracing piece, on one group of relative edge of described third party's shape frame between adjacent frame limit in described third party's shape frame
Side is connected to the second installed part passed through for described rotating pin.
Further technical scheme, this radar test frock also includes the 3rd support being made up of straight-bar, described fixation
Being supported the first support fixing by described 3rd support when blue dish card turns to be positioned at vertical guide, described 3rd support one end is solid
Due to described first square box its back to the side of described installing rack, the described 3rd support other end is fixed on described third party's shape
On frame.
Further technical scheme, described third party's shape frame bottom is connected with pedestal by connecting bolt.
Further technical scheme, is provided with described angle away from the frame limit of the first square box in described second square box
The trimming bolt that degree is finely adjusted.
Further technical scheme, in described first square box, the frame limit away from the second square box is provided with and crane gear
The lifting part being connected, described lifting part is provided with hole for hoist.
Further technical scheme, described first support, the second support, the 3rd support, fixed flange are all through surface
Spray paint process.
Further technical scheme is long between the mounting hole that fixing hole is mounting hole and two ends at described 3rd support two ends
Degree direction is vertical, and the length direction of the mounting hole that described 3rd support is connected with described first square box is positioned at vertical.
The beneficial effects of the utility model are:
(1) this utility model is in use, is installed on described fixed flange by radar equipment to be tested, described first
Support rotates the upset that radar equipment to be tested can be made to carry out 0-90 ° around rotating pin, when fixed flange card is positioned at
In horizontal plane or vertical guide, the test process of radar equipment to be tested can be implemented.Described installing rack can be used for and different structure
Fixed flange connect, with the test request of satisfied different radar equipments, reach the purpose that many equipment shares.Described fixation
Blue dish is connected with installing rack bolt, install, dismantle the most very convenient.This test fixture simple in construction, cheap, for radar equipment
Test job saved the substantial amounts of time, substantially reduce the lead time.
(2) when fixed flange card described in the utility model is positioned at horizontal plane, the frame face of described first square box with
The frame face of third party's shape frame is parallel, and the frame face of described second square box is vertical with the frame face of third party's shape frame, described first square
Frame is supported in above third party's shape frame by the described gimbal lever；When described fixed flange card is positioned at vertical guide, described
The frame face of one square box is vertical with the frame face of third party's shape frame, and the frame face of described second square box is flat with the frame face of third party's shape frame
OK, described third party's shape frame directly supports described second square box, enters described first support additionally by described 3rd support
Row supports, it is ensured that structural stability, prevents the first support in test process from back overturning.
(3) connecting bolt described in the utility model is for connecting the second support and pedestal, and the height of described pedestal can root
Being customized according to needs, the distance between the most described second support and pedestal slightly can also be adjusted by connecting bolt
Whole.
(4) fixed flange card described in the utility model is overturn 90 ° by being positioned at horizontal plane state, is then adjusted to position
When vertical guide, in order to improve Adjustment precision further, can be adjusted by described trimming bolt, described trimming bolt is twisted
Dynamic, the first support can be realized around micro-turn of described rotating pin so that described fixed flange card is strictly positioned at vertical guide
In, improve the test result reliability of radar equipment to be tested further.
(5) after radar equipment to be tested being installed on the first support described in the utility model, when needing to overturn, Ke Yitong
Cross described hole for hoist to be attached with crane gear, by the assosting effect of crane gear so that above-mentioned switching process is more
Easily.Surface lacquer processing procedure described in this utility model can improve the corrosion resistance of Surface of profile further.
(6) mounting hole at the 3rd support two ends described in the utility model can facilitate when the first support is supported right
Installing rack perpendicularity is adjusted, to reach radar test purpose.
Accompanying drawing explanation
Fig. 1 is this utility model the first supporting structure schematic diagram；
Fig. 2 is this utility model the second supporting structure schematic diagram；
Fig. 3 is this utility model the 3rd supporting structure schematic diagram；
Fig. 4 is that this utility model the first support assembles structural representation with fixed flange；
Fig. 5 is fixed flange card horizontal positioned schematic diagram after this utility model assembling；
Fig. 6 is that after this utility model assembles, fixed flange card is disposed vertically schematic diagram.
In accompanying drawing, the implication of labelling is as follows:
10-the first support 11-installing rack 111-installing hole 12-the first square box
13-the second square box 14-support bar 15-the first installed part 16-gimbal lever 17-hole for hoist
20-the second support 21-third party's shape frame 22-bracing piece 23-the second installed part
30-fixed flange 40-rotating pin 50-the 3rd support 51-mounting hole
60-connecting bolt 70-trimming bolt
Detailed description of the invention
Below in conjunction with embodiment technical solutions of the utility model are made more specific detail:
A kind of radar test frock, including first support the 10, second support 20 and for installing radar equipment to be tested
Fixed flange 30, described first support 10 is provided with installing rack 11, and described fixed flange 30 is bolted on institute
Stating on installing rack 11, described first support 10 is positioned at above the second support 20 and therebetween by rotating pin 40 and carries out even
Connecing, described first support 10 realizes between card and the horizontal plane of described fixed flange 30 around the axial rotation of rotating pin 40
Angle is in the adjustment of 0-90 ° of scope.Radar equipment to be tested in use, is installed on described fixed flange by this utility model
On 30, described first support 10 rotates the upset that radar equipment to be tested can be made to carry out 0-90 ° around rotating pin 40, when solid
Determine ring flange 30 card and be positioned at horizontal plane or vertical guide, the test process of radar equipment to be tested can be implemented.Described installation
The fixed flange 30 that frame 11 can be used for different structure is connected, with the test request of satisfied different radar equipments, for reaching many
The purpose that equipment shares.Described fixed flange 30 is connected with installing rack 11 bolt, install, dismantle the most very convenient.This test work
Assembling structure is simple, and cheap, the substantial amounts of time has been saved in the test job of radar equipment, substantially reduces the lead time.
As it is shown in figure 1, described first support 10 includes being arranged vertically by first square box the 12, second square box 13 and constitutes
L-shaped bracing frame and for strengthening the support bar 14 of described L-shaped support frame structure intensity, described support bar 14 two ends are solid respectively
On described first square box the 12, second square box 13, described installing rack 11 is positioned at inside L-shaped bracing frame, described installing rack
11 are provided with the installing hole 111 passed through for bolt, and described fixed flange 30 card is flat with the frame face of described first square box 12
OK, described first square box 12 its be provided with the gimbal lever 16 back to the side of described installing rack 11 and for described rotating pin 40
The first installed part 15 passed through, wherein said first installed part 15 is near the company of described first square box the 12, second square box 13
Meeting place to arrange, the described gimbal lever 16 is arranged away from the junction of described first square box the 12, second square box 13, described fixation
First square box 12 is supported when turning to be positioned at horizontal plane by blue dish 30 card by the described gimbal lever 16；
As in figure 2 it is shown, described second support 20 includes that third party's shape frame 21, the frame face of described third party's shape frame 21 are positioned at water
Square to, be provided with bracing piece 22 in described third party's shape frame 21 between adjacent frame limit, one group of described third party's shape frame 21 relative
The second installed part 23 passed through for described rotating pin 40 it is connected to above limit；
Such as Fig. 3, shown in 6, this radar test frock also includes the 3rd support 50 being made up of straight-bar, described fixed flange
By described 3rd support 50, first support 10 is supported fixing when 30 cards turn to be positioned at vertical guide, described 3rd support 50 1
End be fixed on described first square box 12 its back to the side of described installing rack 11, described 3rd support 50 other end is fixed on institute
State on third party's shape frame 21.
When fixed flange 30 card the most described in the utility model is positioned at horizontal plane, the frame face of described first square box 12
Parallel with the frame face of third party's shape frame 21, the frame face of described second square box 13 is vertical with the frame face of third party's shape frame 21, described
First square box 12 is supported in above third party's shape frame 21 by the described gimbal lever 16, as shown in Figure 5；Described fixed flange 30
When card is positioned at vertical guide, the frame face of described first square box 12 is vertical with the frame face of third party's shape frame 21, described second party
The frame face of shape frame 13 is parallel with the frame face of third party's shape frame 21, and described third party's shape frame 21 directly supports described second square box
13, additionally by described 3rd support 50, described first support 10 is supported, it is ensured that structural stability, prevents test process
In the first support 10 back overturn, as shown in Figure 6.
It is connected with pedestal by connecting bolt 60 bottom described third party's shape frame 21.Connecting bolt 60 described in the utility model
For connecting the second support 20 and pedestal, the height of described pedestal can be customized as required, the most described second support
Distance between 20 and pedestal slightly can also be adjusted by connecting bolt 60.
Described second square box 13 is provided with on frame limit away from the first square box 12 described angle is finely adjusted
Trimming bolt 70.Fixed flange 30 card described in the utility model is overturn 90 ° by being positioned at horizontal plane state, is then adjusted to
When being positioned at vertical guide, in order to improve Adjustment precision further, can be adjusted by described trimming bolt 70, described fine setting spiral shell
Bolt 70 turns, and can realize the first support 10 around micro-turn of described rotating pin 40 so that described fixed flange 30 card is tight
Case, in vertical guide, improves the test result reliability of radar equipment to be tested further.
In described first square box 12, the frame limit away from the second square box 13 is provided with the lifting part being connected with crane gear,
Described lifting part is provided with hole for hoist 17.After radar equipment to be tested being installed on first support 10 described in the utility model, need
When overturning, can be attached with crane gear by described hole for hoist 17, by the assosting effect of crane gear so that
Above-mentioned switching process is the easiest.
Described first support the 10, second support the 20, the 3rd support 50, fixed flange 30 all process through surface lacquer.
Described surface lacquer processing procedure can improve the corrosion resistance of Surface of profile further.
Length direction between the mounting hole that fixing hole is mounting hole 51 and two ends at described 3rd support 50 two ends is vertical,
Described 3rd support 50 is positioned at vertical with the length direction of the mounting hole that described first square box 12 is connected.This utility model
The mounting hole 51 at described 3rd support 50 two ends can be convenient to installing rack 11 perpendicularity when being supported the first support 10
It is adjusted, to reach radar test purpose.
Claims (9)
1. a radar test frock, it is characterised in that: include the first support (10), the second support (20) and treat for installation
The fixed flange (30) of test radar equipment, described first support (10) is provided with installing rack (11), described fixed flange
(30) be bolted on described installing rack (11), described first support (10) be positioned at the second support (20) top and the two
Between be attached by rotating pin (40), described first support (10) realizes described around the axial rotation of rotating pin (40)
Fixed flange (30) between card and horizontal plane angle in the adjustment of 0-90 ° of scope.
2. radar test frock as claimed in claim 1, it is characterised in that: described first support (10) includes by first square
Frame (12), the second square box (13) are arranged vertically the L-shaped bracing frame of composition and strong for strengthening described L-shaped support frame structure
The support bar (14) of degree, described support bar (14) two ends are individually fixed in described first square box (12), the second square box (13)
On, described installing rack (11) is positioned at inside L-shaped bracing frame, and described installing rack (11) is provided with the installing hole passed through for bolt
(111), described fixed flange (30) card is parallel with the frame face of described first square box (12), described first square box (12)
It is provided with the gimbal lever (16) and the first installed part passed through for described rotating pin (40) back to the side of described installing rack
(15), wherein said first installed part (15) is arranged near the junction of described first square box (12), the second square box (13),
The described gimbal lever (16) is arranged away from the junction of described first square box (12), the second square box (13), described mounting flange
By the described gimbal lever (16), the first square box (12) is supported when dish (30) card turns to be positioned at horizontal plane.
3. radar test frock as claimed in claim 2, it is characterised in that: described second support (20) includes third party's shape frame
(21), the frame face of described third party's shape frame (21) is positioned at horizontal direction, sets between described third party's shape frame (21) interior adjacent frame limit
There is bracing piece (22), be connected to above one group of relative edge of described third party's shape frame (21) lead to for described rotating pin (40)
The second installed part (23) crossed.
4. radar test frock as claimed in claim 3, it is characterised in that: this radar test frock also includes being made up of straight-bar
The 3rd support (50), by described 3rd support (50) to when described fixed flange (30) card turns to be positioned at vertical guide
One support (10) supports fixing, described 3rd support (50) one end be fixed on described first square box (12) its back to described installation
The side of frame (11), described 3rd support (50) other end is fixed on described third party's shape frame (21).
5. radar test frock as claimed in claim 3, it is characterised in that: described third party's shape frame (21) bottom is by connecting
Bolt (60) is connected with pedestal.
6. radar test frock as claimed in claim 3, it is characterised in that: away from first party in described second square box (13)
The trimming bolt (70) being finely adjusted described angle is installed on the frame limit of shape frame (12).
7. radar test frock as claimed in claim 3, it is characterised in that: away from second party in described first square box (12)
The frame limit of shape frame (13) is provided with the lifting part being connected with crane gear, and described lifting part is provided with hole for hoist (17).
8. radar test frock as claimed in claim 4, it is characterised in that: described first support (10), the second support (20),
3rd support (50), fixed flange (30) all process through surface lacquer.
9. radar test frock as claimed in claim 4, it is characterised in that: the fixing hole at described 3rd support (50) two ends is
Between mounting hole (51) and the mounting hole at two ends, length direction is vertical, described 3rd support (50) and described first square box (12)
The length direction of the mounting hole connected is positioned at vertical.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620541711.4U CN205749877U (en) | 2016-05-31 | 2016-05-31 | A kind of radar test frock |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620541711.4U CN205749877U (en) | 2016-05-31 | 2016-05-31 | A kind of radar test frock |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205749877U true CN205749877U (en) | 2016-11-30 |
Family
ID=57359894
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620541711.4U Withdrawn - After Issue CN205749877U (en) | 2016-05-31 | 2016-05-31 | A kind of radar test frock |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205749877U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105974381A (en) * | 2016-05-31 | 2016-09-28 | 安徽四创电子股份有限公司 | Radar test tool |
-
2016
- 2016-05-31 CN CN201620541711.4U patent/CN205749877U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105974381A (en) * | 2016-05-31 | 2016-09-28 | 安徽四创电子股份有限公司 | Radar test tool |
| CN105974381B (en) * | 2016-05-31 | 2019-05-14 | 安徽四创电子股份有限公司 | A kind of radar test tooling |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20161130 Effective date of abandoning: 20190514 |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20161130 Effective date of abandoning: 20190514 |