CN205691773U - One is rotatable freezes deep self-operated measuring unit - Google Patents
One is rotatable freezes deep self-operated measuring unit Download PDFInfo
- Publication number
- CN205691773U CN205691773U CN201620546674.6U CN201620546674U CN205691773U CN 205691773 U CN205691773 U CN 205691773U CN 201620546674 U CN201620546674 U CN 201620546674U CN 205691773 U CN205691773 U CN 205691773U
- Authority
- CN
- China
- Prior art keywords
- antenna
- gpr
- radar
- rotatable
- motor
- 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.)
- Expired - Fee Related
Links
Landscapes
- Radar Systems Or Details Thereof (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
One is rotatable freezes deep self-operated measuring unit, relates to GPR field.It is to solve the problem that the existing manual portable antenna of measuring method visiting ground is readily incorporated error.Rotatable freeze deep self-operated measuring unit and be grouped into by part of data acquisition and data processing division.Part of data acquisition includes: GPR launches antenna, GPR reception antenna, scalable circuit orbit, Telescopic rotary bar, motor, rotatable interface, fixed tray and clip.Telescopic rotary bar is made up of outer bar and interior loop bar, and its stretching motion is by step motor control.The reception antenna launching antenna and GPR of GPR is connected to the two ends of swingle and is arranged on circuit orbit by pulley.The radius of circuit orbit is controlled by motor.This utility model is applicable to freeze deep measurement automatically.
Description
Technical field
This utility model relates to GPR field, is specifically related to one and freezes deep self-operated measuring unit.
Background technology
GPR is a kind of electromagnetic wave detection skill utilizing high-frequency impulse electromagnetic wave Underground geologic structure and feature
Art.It uses a pair antenna to be operated, and launches sky alignment underground medium and launches high frequency, broadband laser pulse electromagnetic wave, electromagnetic wave
Reflection and transmission is there is when running into electro permanent magnetic difference separating surface in underground medium communication process;The electromagnetic wave of reflection passes earth's surface back
Received by reception antenna;And then grind by analyzing the time lag of reflection electromagnetic wave, same to phasic property, similarity and wave character
Study carefully geologic body.
Suitably choosing the distance launched between antenna and reception antenna can make the echo-signal from target strengthen.Existing
Document shows, the selection of antenna distance S should make the deepest target relative to reception antenna and subtended angle is critical angle the 2 of transmitting antenna
Times, i.e. antenna distance S refers to formula (1) result of calculation and chooses.
In actual measurement, the inconvenience of work on the spot can be increased owing to strengthening antenna distance and resolution can be made to reduce, therefore
The antenna distance selected is usually less than this numerical value, often takes about 1/5th of depth capacity.Although but having theoretical formula
Computation and measurement parameter, but owing to the geological condition of each department varies, add the existence of other interference factors, so in reality
Border operating process is wanted the most rule of thumb data select several groups of different parameters to carry out comparison and detection, choose according to Detection results
Good antenna distance completes Detection task.
The method of work of GPR generally has two kinds: the widest horn cupping and profile method.
Wide horn cupping has two kinds of different modes, and the first is to launch antenna to be fixed on a fixing point of survey line, receives
Antenna moves along survey line, and measuring point is the position of reception antenna.Second method is also called CMP method, keeps launching antenna
Motionless with the central point of reception antenna, it is gradually increased the spacing sending out, receiving antenna, measuring point is the midpoint sending out, receiving antenna, but corresponding
Different transmitting-receivings away from.Therefore, the spacing between dual-mode antenna can not keep optimum distance, so can inevitably produce bigger
Deviation.
Profile method be by transmitting antenna and reception antenna with constant spacing along the synchronization-moving a kind of metering system of survey line, send out
Penetrate antenna and reception antenna moves simultaneously and obtains once record the most afterwards.But the gap ratio generally, sending out receipts antenna is visited
Depth measurement degree is little many, and the distance between dual-mode antenna is frequently not optimum distance, so also can produce relatively large deviation.
Summary of the invention
This utility model is the problem being readily incorporated error in order to solve the existing manual portable antenna of measuring method visiting ground,
Thus provide a kind of and rotatable freeze deep self-operated measuring unit.
One is rotatable freezes deep self-operated measuring unit, and it includes that GPR launches antenna 1, detection radar reception antenna
2 and radar host computer, GPR launches the radar emission signal input part of antenna 1 and the radar emission signal output of radar host computer
End connects;The radar emission signal output part of detection radar reception antenna 2 connects with the radar emission signal input part of radar host computer
Connect;
It also includes telescopic circuit orbit 3, Telescopic rotary bar 4, motor 5, rotatable interface 6 and computer;
GPR transmitting antenna 1 and detection radar reception antenna 2 are separately fixed at the two ends of Telescopic rotary bar 4;Institute
State GPR transmitting antenna 1 and detection radar reception antenna 2 is arranged on telescopic circuit orbit 3, and all can edge
Telescopic circuit orbit 3 slides;Telescopic circuit orbit 3 is horizontally disposed with;Motor 5 is arranged on Telescopic rotary bar 4
Lower section, and the output shaft of described motor 5 is vertically fixed in Telescopic rotary bar 4 lower surface by rotatable interface 6
The heart;The FPDP of radar host computer is connected with the FPDP of computer;The motor control signal outfan of described computer with
The control signal input of motor 5 connects.
Telescopic rotary bar 4 includes the outer bar 9 of interior loop bar 10, two and two clips 11;
Each outer bar 9 is an opening and the rectangular structure of hollow;The outer bar 9 of said two is respectively fitted over interior loop bar 10
Two ends, and all can be movable along the length direction of interior loop bar 10;
GPR launches antenna 1 and detection radar reception antenna 2 is fixed on outside two by two clips 11 respectively
On bar 9.
The beneficial effects of the utility model: technical problem to be solved in the utility model is for above-mentioned prior art
Deficiency, it is provided that a kind of novel GPR, the distance of dual-mode antenna can be maintained at an optimum state by this system, and
The different azimuth to same place can be realized and gather multiple data automatically, substantially increase the true and accurate of data, gram
Having taken the manual portable antenna of traditional measurement method and be readily incorporated error, big and dual-mode antenna the spacing of labor intensity is improper
Problem.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is for data acquisition unit structural representation of the present utility model;
Fig. 3 is for holder part schematic diagram of the present utility model;A in figure, B are that interior loop bar 10 can move freely direction.
Detailed description of the invention
Detailed description of the invention one, combining Fig. 1 to Fig. 3 this detailed description of the invention is described, a kind of rotatable freezing deep is surveyed automatically
Amount device, it includes that GPR launches antenna 1, detection radar reception antenna 2 and radar host computer, GPR transmitting antenna 1
Radar emission signal input part be connected with the radar emission signal output part of radar host computer;The thunder of detection radar reception antenna 2
Reach transmitting signal output part to be connected with the radar emission signal input part of radar host computer;
It also includes telescopic circuit orbit 3, Telescopic rotary bar 4, motor 5, rotatable interface 6 and computer;
GPR transmitting antenna 1 and detection radar reception antenna 2 are separately fixed at the two ends of Telescopic rotary bar 4;Institute
State GPR transmitting antenna 1 and detection radar reception antenna 2 is arranged on telescopic circuit orbit 3, and all can edge
Telescopic circuit orbit 3 slides;Telescopic circuit orbit 3 is horizontally disposed with;Motor 5 is arranged on Telescopic rotary bar 4
Lower section, and the output shaft of described motor 5 is vertically fixed in Telescopic rotary bar 4 lower surface by rotatable interface 6
The heart;The FPDP of radar host computer is connected with the FPDP of computer;The motor control signal outfan of described computer with
The control signal input of motor 5 connects.
Detailed description of the invention two, this detailed description of the invention be rotatable with one described in detailed description of the invention one freeze deep from
The difference of dynamic measurement apparatus is, Telescopic rotary bar 4 includes the outer bar 9 of interior loop bar 10, two and two clips 11;
Each outer bar 9 is an opening and the rectangular structure of hollow;The outer bar 9 of said two is respectively fitted over interior loop bar 10
Two ends, and all can be movable along the length direction of interior loop bar 10;
GPR launches antenna 1 and detection radar reception antenna 2 is fixed on outside two by two clips 11 respectively
On bar 9.
Detailed description of the invention three, this detailed description of the invention be rotatable with one described in detailed description of the invention one freeze deep from
The difference of dynamic measurement apparatus is, it also includes that pallet 8, described pallet 8 are horizontally disposed with, and the fixed part of motor 5 is fixed on
On pallet 8.
This utility model is made up of two parts, and outdoor automatic Observation part and indoor acquisition terminal process storage part.
Operation principle: telescopic circuit orbit 3 is placed on and needs the position of the measuring frozen degree of depth, according to reference data
Or measure after freezing deep general numerical value, the radius of track is adjusted to an optimum position, the most again measures, when
Obtain one group freeze deep data after, by computer-controlled stepper motor 5, make to be connected in the spy ground at Telescopic rotary bar 4 two
After the transmitting antenna 1 of radar and reception antenna 2 rotate a certain angle simultaneously, again measure and obtain second group of data.Then will
Several groups of data the obtained value that is averaged calculates, and completes the automatic Observation task of frost penetration, and by data with the data of regulation
Form is sent to the synthetical collection terminal of indoor and processes.
This frost penetration automatic observation device is positioned on ground.With scale, resolution on telescopic circuit orbit 3
It it is 15 degree.The length of Telescopic rotary bar 4 can change, and Telescopic rotary bar 4 is fixed on pallet 8 through motor 5
On, the GPR that is respectively fixed at two ends with of Telescopic rotary bar 4 launches antenna 1 and GPR reception antenna 2.GPR
Launch antenna 1 and GPR reception antenna 2 is placed on the track 3, connect with pulley between them.Antenna can be by stepping electricity
The angle controlling rotation regulation of machine 5.
Computer is connected with motor 5 and radar host computer by data wire, and motor and radar host computer synchronize respectively
The position controlling GPR transmitting antenna and GPR reception radar is moved and radar data acquisition, and motor 5 leads to
Cross swingle 4 to control GPR and launch antenna 1 and GPR reception antenna 2 rightabout and angularly rotate.Radar host computer
Control GPR transmitting antenna 1 and radiate frequency electromagnetic waves to underground medium, and recorded from ground by GPR reception antenna 2
The reflection echo of lower target.GPR is launched antenna 1 and the control of GPR reception antenna 2 and radar by motor 5
The collection of radar data is synchronized to realize by main frame respectively by computer, thus effectively realizes the Quick Acquisition of radar data.
Indoor section is made up of terminal computing system, on the socket that communication cable is connected to outdoor control box, real
The communication of existing indoor and outdoor.
Claims (3)
1. rotatable freezing a deep self-operated measuring unit, it includes that GPR launches antenna (1), detection radar reception antenna
(2) and radar host computer, GPR launches the radar emission signal input part of antenna (1) and the radar emission signal of radar host computer
Outfan connects;The radar emission signal output part of detection radar reception antenna (2) is defeated with the radar emission signal of radar host computer
Enter end to connect;
It is characterized in that: further comprising telescopic circuit orbit (3), Telescopic rotary bar (4), motor (5), rotatable interface
And computer (6);
GPR transmitting antenna (1) and detection radar reception antenna (2) are separately fixed at the two ends of Telescopic rotary bar (4);
Described GPR launches antenna (1) and detection radar reception antenna (2) is arranged on telescopic circuit orbit (3), and
All can slide along telescopic circuit orbit (3);Telescopic circuit orbit (3) is horizontally disposed with;Motor (5) is arranged on
The lower section of Telescopic rotary bar (4), and the output shaft of described motor (5) is vertically fixed on and can be stretched by rotatable interface (6)
The center of contracting swingle (4) lower surface;The FPDP of radar host computer is connected with the FPDP of computer;Described computer
Motor control signal outfan is connected with the control signal input of motor (5).
One the most according to claim 1 is rotatable freezes deep self-operated measuring unit, it is characterised in that Telescopic rotary bar
(4) interior loop bar (10), two outer bars (9) and two clips (11) are included;
Each outer bar (9) is an opening and the rectangular structure of hollow;The outer bar (9) of said two is respectively fitted over interior loop bar
(10) two ends, and all can be movable along the length direction of interior loop bar (10);
GPR launches antenna (1) and detection radar reception antenna (2) is fixed on two by two clips (11) respectively
On outer bar (9).
One the most according to claim 1 is rotatable freezes deep self-operated measuring unit, it is characterised in that it also includes pallet
(8), described pallet (8) is horizontally disposed with, and the fixed part of motor (5) is fixed on pallet (8).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201620546674.6U CN205691773U (en) | 2016-06-07 | 2016-06-07 | One is rotatable freezes deep self-operated measuring unit |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201620546674.6U CN205691773U (en) | 2016-06-07 | 2016-06-07 | One is rotatable freezes deep self-operated measuring unit |
Publications (1)
Publication Number | Publication Date |
---|---|
CN205691773U true CN205691773U (en) | 2016-11-16 |
Family
ID=57260272
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201620546674.6U Expired - Fee Related CN205691773U (en) | 2016-06-07 | 2016-06-07 | One is rotatable freezes deep self-operated measuring unit |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN205691773U (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107436435A (en) * | 2017-08-07 | 2017-12-05 | 广州地铁设计研究院有限公司 | A kind of the GPR device and its detection method of single hole detection boulder |
CN109212616A (en) * | 2018-11-30 | 2019-01-15 | 中国矿业大学(北京) | A kind of Ground Penetrating Radar CT transmission detection experimental provision |
CN111608645A (en) * | 2020-05-28 | 2020-09-01 | 中国矿业大学(北京) | Directional ground penetrating radar device for drilling |
-
2016
- 2016-06-07 CN CN201620546674.6U patent/CN205691773U/en not_active Expired - Fee Related
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107436435A (en) * | 2017-08-07 | 2017-12-05 | 广州地铁设计研究院有限公司 | A kind of the GPR device and its detection method of single hole detection boulder |
CN109212616A (en) * | 2018-11-30 | 2019-01-15 | 中国矿业大学(北京) | A kind of Ground Penetrating Radar CT transmission detection experimental provision |
CN111608645A (en) * | 2020-05-28 | 2020-09-01 | 中国矿业大学(北京) | Directional ground penetrating radar device for drilling |
CN111608645B (en) * | 2020-05-28 | 2021-10-08 | 中国矿业大学(北京) | Directional ground penetrating radar device for drilling |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN205691773U (en) | One is rotatable freezes deep self-operated measuring unit | |
CN107024621B (en) | Massive-MIMO antenna measurement device and its directivity measurement method | |
CN105548729B (en) | A kind of method for fast measuring of array antenna radiation characteristic | |
US7167124B2 (en) | Data acquisition for a ground penetrating radar system | |
CN104515909B (en) | A kind of large antenna pattern measurement method based on correlation method | |
CN104569625B (en) | A kind of large-scale antenna directional diagram measuring method based on rotatable auxiliary antenna | |
CN103412286B (en) | Transmitting polarization optimizing DOA (direction of arrival) evaluation method based on MIMO (multiple-input multiple-output) radar | |
CN104656154B (en) | The automatic Fast measurement system of emission source Ground Penetrating Radar multiple offset distance data altogether | |
CN106569203B (en) | The electronic fuse and its detection method of the complete full airspace covering of coherent multichannel | |
US20140226850A1 (en) | Imaging, object detection, and change detection with a polarized multistatic gpr array | |
CN104267440A (en) | Common middle point (CMP) detection method used for ground penetrating radar (GPR) | |
CN106526532A (en) | Doppler direction finder based on four-dimensional antenna array | |
CN106771673A (en) | A kind of gps antenna directionality method of testing and system | |
US2472212A (en) | Method of locating beacons | |
CN110850409B (en) | Double-station synthetic aperture radar imaging method based on time reversal | |
CN104659491A (en) | Miniature receiving antenna and azimuth estimation method for HF/VHF radar | |
CN104635275B (en) | The automatic Fast measurement system of CMP Coherent Noise in GPR Record | |
KR101780783B1 (en) | Method of detecting parking lot with rader | |
CN205333746U (en) | Frequency sweep measurement system based on diversity notion | |
CN110470915A (en) | A kind of circular polarized antenna test macro, calibration and signal testing method | |
CN109856628A (en) | A kind of target three-dimensional acceleration motion model calculation method based on scanning radar | |
Zöchmann et al. | Resolving the angular profile of 60 GHz wireless channels by delay-Doppler measurements | |
CN210665889U (en) | Probe slide rail test system | |
RU105466U1 (en) | AUTOMATED COMPLEX FOR MEASUREMENTS OF RADIOTECHNICAL CHARACTERISTICS OF Aperture Antennas | |
CN105277916A (en) | Search method of wireless transmission signal source |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161116 Termination date: 20170607 |