CN206671542U - A kind of radar operational reliability test system - Google Patents
A kind of radar operational reliability test system Download PDFInfo
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- CN206671542U CN206671542U CN201621165973.1U CN201621165973U CN206671542U CN 206671542 U CN206671542 U CN 206671542U CN 201621165973 U CN201621165973 U CN 201621165973U CN 206671542 U CN206671542 U CN 206671542U
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- angled trapezium
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Abstract
A kind of radar operational reliability test system, belong to radar performance detection device technical field, solve the problems, such as the Validity Test of radar operational reliability under different temperatures environment, solution is:Casing is hexahedron, air blower is provided with the inside of wall box, chamber door is provided with before casing, wave transparent door is provided with behind casing, T-slot is provided with remaining four sides inwall of casing, suction wave apparatus is accordingly provided with T-slot, radar receiver panel is provided with box house bottom surface, receiver panel is just facing to wave transparent door slant setting;Right-angled trapezium is inhaled wave apparatus and is arranged in casing left and right sides, and the oblique waist that right-angled trapezium inhales wave apparatus is parallel with receiver panel, and the both sides right-angled trapezium shape inhales wave apparatus connection by rectangle respectively between inhaling the upper bottom of wave apparatus.The utility model is set in the wall of casing four inhales wave apparatus, effectively reduces interference of the external environment to the electromagnetic wave of radar emission, improves the accuracy that reliability detects in radar running.
Description
Technical field
The utility model patent belongs to radar performance detection device technical field, more particularly to a kind of radar operational reliability
Test system.
Background technology
Radar, it is English Radar transliteration, comes from radio detection and ranging abbreviation, looking like is
" radio detection and ranging ", i.e., find target with the method for radio and determine their locus, thus radar also by
Referred to as " radio-positioning ".Radar is the electronic equipment using electromagnetic wave detection target, and its principle is radar emission electromagnetic wave pair
Target is irradiated and receives its echo, is derived from distance of the target to electromagnetic emission point, range rate(Radially speed
Degree), orientation, the information such as height.The particular use and structure of various radars are not quite similar, but citation form be it is consistent, mainly
Including:Emitter, transmitting antenna, receiver, reception antenna, process part and display, in addition also power-supply device, data
Enroll the auxiliary equipments such as equipment, anti-interference equipment.Radar is often positioned in bad environments, unfrequented position, some thunders
Up to need it is on the move complete radio-positioning function, this higher requirement just is proposed to the operational reliability of radar, it is necessary to
The operational reliability of radar is detected before radar comes into operation.
Utility model content
The utility model patent technical problems to be solved are:In order to which Validity Test radar is run under different temperatures environment
The problem of reliability, the utility model patent provide a kind of radar operational reliability test system, facilitate operating personnel in difference
The operational reliability of radar is tested in temperature environment.
The utility model patent is achieved by the following technical programs.
A kind of radar operational reliability test system, it includes casing, radar and air blower, and temperature tune is provided with casing
Regulating device, it is characterised in that:Casing is hexahedron, is provided with air blower on the inside of wall box, chamber door, case are provided with before casing
By hasp connection between door and casing, chamber door middle and lower part is provided with handle, is provided with wave transparent door behind casing, casing remaining four
T-slot is provided with the inwall of face, suction wave apparatus is accordingly provided with T-slot, the suction wave apparatus includes rectangle and inhales ripple
Device and right-angled trapezium inhale wave apparatus, inhale wave apparatus and surround wave transparent area;Radar is provided with box house bottom surface, radar includes connecing
Device panel is received, receiver panel is just facing to wave transparent door slant setting;The right-angled trapezium inhales wave apparatus and is arranged on casing or so
On two sides, the oblique waist that right-angled trapezium inhales wave apparatus is parallel with receiver panel, and the both sides right-angled trapezium shape inhales wave apparatus
Wave apparatus is inhaled between upper bottom by rectangle respectively to connect.
Further, it is mm that right-angled trapezium, which inhales the distance between bottom and box top on wave apparatus,.
Further, for the suction wave apparatus to inhale ripple sheet material, its material is rare silicon materials, inhale the thickness of wave apparatus according to
The shape of radar transmitter is adjusted.
Further, the casing is incubator.
Further, the wave transparent door is metal panels, and metal panels core adds insulation material.
The utility model patent has the advantages that compared with prior art.
State of the utility model patent guinea pig in different use environments, test radar operational reliability.This reality
Set with new patent in the wall of casing four and inhale wave apparatus, effectively reduce interference of the external environment to the electromagnetic wave of radar emission,
Improve the accuracy that reliability detects in radar running.
Brief description of the drawings
Fig. 1 is that the utility model patent omits overall structure schematic cross-sectional view after air blower.
Fig. 2 is that the utility model patent overall structure overlooks schematic cross-sectional view.
Fig. 3 is the utility model patent overall structure left view schematic diagram.
In figure, 1 is casing, and 2 be chamber door, and 3 be wave transparent door, and 41 be that rectangle inhales wave apparatus, and 42 be that right-angled trapezium inhales wave apparatus,
5 be receiver panel, and 6 be handle, and 7 be air blower, and 8 be wave transparent area.
Embodiment
The utility model patent is elaborated with reference to embodiment:The present embodiment is with the utility model patent skill
Implemented premised on art scheme, give detailed embodiment and specific operating process, but the utility model patent
Protection domain is not limited to the following examples.
As shown in Fig. 1 ~ 3, a kind of radar operational reliability test system, it includes casing 1, radar and air blower 7, casing
Temperature-adjusting device is provided with 1, it is characterised in that:Casing 1 is hexahedron, and the inside sidewalls of casing 1 are provided with air blower 7, case
Body 1 is above provided with chamber door 2, and hasp connection, the middle and lower part of chamber door 2 are provided with handle 6, casing 1 between chamber door 2 and casing 1
Wave transparent door 3 is provided with below, and T-slot is provided with remaining the four sides inwall of casing 1, suction ripple is accordingly provided with T-slot
Device, the suction wave apparatus include rectangle and inhale wave apparatus 41 and right-angled trapezium suction wave apparatus 42, inhale wave apparatus and surround wave transparent area 8;
Radar is provided with the inner bottom surface of casing 1, radar includes receiver panel 5, and receiver panel 5 just tilts facing to wave transparent door 3
Place;The right-angled trapezium is inhaled wave apparatus 41 and is arranged in the left and right sides of casing 1, right-angled trapezium inhale the oblique waist of wave apparatus 42 with
Receiver panel 5 is parallel, and the both sides right-angled trapezium shape inhales wave apparatus by rectangle respectively between inhaling the upper bottom of wave apparatus 42
41 connections.
Further, it is 50mm that right-angled trapezium, which inhales the distance between bottom and the top surface of casing 1 on wave apparatus 42,.
Further, for the suction wave apparatus to inhale ripple sheet material, its material is rare silicon materials, inhale the thickness of wave apparatus according to
The shape of radar transmitter is adjusted.
Further, the casing 1 is incubator.It ensure that the temperature of radar test environment.
Further, the wave transparent door 3 is metal panels, and metal panels core adds insulation material.Be advantageous to radar hair
The Electromgnetically-transparent penetrated goes out extraneous and is detected.
It is described above, the only embodiment of the utility model patent, but the protection domain of the utility model patent
It is not limited thereto, it is any to be familiar with those skilled in the art in the technical scope that the utility model patent discloses, can be light
The change or replacement being readily conceivable that, it should all cover within the protection domain of the utility model patent.Therefore, the utility model patent
Protection domain should be based on the protection scope of the described claims.
Claims (5)
1. a kind of radar operational reliability test system, it includes casing(1), radar and air blower(7), casing(1)Interior setting
There is temperature-adjusting device, it is characterised in that:Casing(1)For hexahedron, casing(1)Inside sidewalls are provided with air blower(7), casing
(1)Above it is provided with chamber door(2), chamber door(2)With casing(1)Between pass through hasp connection, chamber door(2)Middle and lower part is provided with handle
(6), casing(1)Wave transparent door is provided with below(3), casing(1)It is provided with T-slot on remaining four sides inwall, it is relative in T-slot
It is provided with suction wave apparatus with answering, the suction wave apparatus includes rectangle and inhales wave apparatus(41)Wave apparatus is inhaled with right-angled trapezium(42), inhale
Wave apparatus surrounds wave transparent area(8);Casing(1)Radar is provided with inner bottom surface, radar includes receiver panel(5), receiver
Panel(5)Just facing to wave transparent door(3)Slant setting;The right-angled trapezium inhales wave apparatus(41)It is arranged on casing(1)Left and right two
On side, right-angled trapezium inhales wave apparatus(42)Oblique waist and receiver panel(5)Parallel, the both sides right-angled trapezium inhales wave apparatus
(42)Upper bottom between wave apparatus is inhaled by rectangle respectively(41)Connection.
A kind of 2. radar operational reliability test system according to claim 1, it is characterised in that:Right-angled trapezium inhales ripple dress
Put(42)Upper bottom and casing(1)The distance between top surface is 50mm.
A kind of 3. radar operational reliability test system according to claim 1, it is characterised in that:It is described suction wave apparatus be
Ripple sheet material is inhaled, its material is rare silicon materials, and the thickness for inhaling wave apparatus is adjusted according to the shape of radar transmitter.
A kind of 4. radar operational reliability test system according to claim 1, it is characterised in that:The casing(1)For
Incubator.
A kind of 5. radar operational reliability test system according to claim 1, it is characterised in that:The wave transparent door(3)
For metal panels, metal panels core addition insulation material.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201621165973.1U CN206671542U (en) | 2016-10-26 | 2016-10-26 | A kind of radar operational reliability test system |
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CN201621165973.1U CN206671542U (en) | 2016-10-26 | 2016-10-26 | A kind of radar operational reliability test system |
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CN206671542U true CN206671542U (en) | 2017-11-24 |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106371077A (en) * | 2016-10-26 | 2017-02-01 | 上海汉测试验设备有限公司 | Testing system for radar operation reliability |
CN117388587A (en) * | 2023-12-07 | 2024-01-12 | 南京捷希科技有限公司 | High low temperature terminal test darkroom |
-
2016
- 2016-10-26 CN CN201621165973.1U patent/CN206671542U/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106371077A (en) * | 2016-10-26 | 2017-02-01 | 上海汉测试验设备有限公司 | Testing system for radar operation reliability |
CN117388587A (en) * | 2023-12-07 | 2024-01-12 | 南京捷希科技有限公司 | High low temperature terminal test darkroom |
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