CN203414597U - Remote control flight chi-gamma dose rate measurement instrument - Google Patents
Remote control flight chi-gamma dose rate measurement instrument Download PDFInfo
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- CN203414597U CN203414597U CN201320528668.4U CN201320528668U CN203414597U CN 203414597 U CN203414597 U CN 203414597U CN 201320528668 U CN201320528668 U CN 201320528668U CN 203414597 U CN203414597 U CN 203414597U
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- dose rate
- detector
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- controller
- gamma dose
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Abstract
The utility model relates to the technical field of dose rate measurement instruments, and especially relates to a remote control flight chi-gamma dose rate measurement instrument. The structure comprises a remote controller, a detector and a receiving controller. The detector is provided with a remote control signal receiving device, a driving mechanism, a probe device and a wireless transmitting device. The remote control signal receiving device controls the driving mechanism. The driving mechanism, the probe device and the wireless transmitting device are electrically connected in turn. The receiving controller is provided with a wireless receiver, a control module and a G-M tube. The wireless receiver and the G-M tube are respectively connected with a control module. According to the utility model, the detector and the receiving controller can realize wireless signal connection; the detector is provided with a motor and a propeller; the detector can carry out remote control flight and detection; and the remote control flight chi-gamma dose rate measurement instrument can prevent staff from radiation injury in a measurement process and has the characteristic of convenient measurement.
Description
Technical field
The utility model relates to dose rate measuring instrument technical field, particularly relates to a kind of χ-gamma dose rate measuring instrument of remote-controlled flight.
Background technology
χ-gamma dose rate measuring instrument is for measuring radiomaterial χ ray and gamma-ray dose equivalent rate and absorbed dose rate.χ-gamma dose rate measuring instrument is widely used in the occasions such as airport, customs, station, harbour, harbour, hospital, nuclear facilities and nuclear tests chamber to carry out radiation protection detection.
The structure of χ-gamma dose rate measuring instrument of the prior art generally comprises contact unit and master machine control unit, between contact unit and master machine control unit by the cable connection that communicates with one another.Because the contact unit of χ-gamma dose rate measuring instrument and master machine control unit are by wired connection, therefore, while surveying the radiation in certain region, need staff in person χ-gamma dose rate measuring instrument to be put to measured zone.χ-gamma dose rate measuring instrument is in the airport that nuclear radiation leakage accident does not occur, customs, station, harbour, harbour, hospital, nuclear facilities and nuclear tests chamber etc. during the application of place, and staff is generally safer.But, when χ-gamma dose rate measuring instrument is applied to the dangerously steep field of physical features or nuclear radiation leakage accident place, on the one hand, the dangerously steep field of physical features easily causes casualties, on the other hand, the radiation intensity in the place of nuclear radiation leakage accident is generally larger, when staff parent goes to in-site measurement χ ray and gamma-ray dose equivalent rate and absorbed dose rate, easily human body is caused to radiation injury.Therefore, χ-gamma dose rate measuring instrument of the prior art exists measures inconvenient shortcoming, and in measuring process, is difficult to avoid not raying of staff injury.
Summary of the invention
The purpose of this utility model is to provide for weak point of the prior art a kind of χ-gamma dose rate measuring instrument of remote-controlled flight, χ-gamma dose rate measuring instrument of this remote-controlled flight can be avoided not raying of staff injury in measuring process, and has the feature easily of measuring.
For achieving the above object, the utility model is achieved through the following technical solutions.
χ-gamma dose rate measuring instrument that a kind of remote-controlled flight is provided, comprises telepilot, detector and reception controller, and described telepilot is connected by wireless signal with described detector, and described detector is connected by wireless signal with described reception controller;
Described detector is provided with remote control signal receiver, driving mechanism, probe apparatus and wireless launcher, described remote control signal receiver is controlled described driving mechanism, and described driving mechanism, described probe apparatus and described wireless launcher are electrically connected to successively;
Described reception controller is provided with wireless receiver, control module and G-M pipe; Described wireless receiver is connected with described control module respectively with described G-M pipe.
Described driving mechanism comprises motor, screw propeller and power supply, and described power supply is electrically connected to described motor, and the output shaft of described motor drives and is connected with described screw propeller; Described remote control signal receiver is electrically connected to described power supply.
Described driving mechanism also comprises turning axle, and described turning axle is connected with described screw propeller with the output shaft of described motor respectively.
Described probe apparatus is provided with high-voltage power supply element, photomultiplier, photocon, detecting element, current frequency converter element, control element and memory element; The signal output part of described high-voltage power supply element connects described photomultiplier, described photocon and described detecting element successively; The signal output part of described current frequency converter element connects described control element and described memory element successively; The output terminal of described photomultiplier is connected with the input end of described current frequency converter element; Described control element is connected with described wireless launcher.
Described control module comprises amplifier, discriminator, controller, display, alarm, storer, high-voltage power supply and low-tension supply; The signal input part of described amplifier is connected with the signal output part of described G-M pipe, the signal output part of described amplifier connects described discriminator and described controller successively, described controller connects respectively described display, described alarm and described storer, described low-tension supply connects respectively described amplifier, described discriminator, described controller, described display, described alarm, described storer and described high-voltage power supply, and the signal output part of described high-voltage power supply is connected with the signal input part of described G-M pipe; The output terminal of described wireless receiver is connected with the input end of described controller.
Described display is set to digital indicator.
Described detector is provided with GPS locating device, and the output terminal of described GPS locating device is connected with described wireless launcher.
Described detector is provided with distance measuring equipment, and the output terminal of described distance measuring equipment is connected with described wireless launcher.
Described detector is provided with camera head, and the output terminal of described camera head is connected with described wireless launcher.
The beneficial effects of the utility model: χ-gamma dose rate measuring instrument of a kind of remote-controlled flight of the present utility model, comprise telepilot, detector and reception controller, telepilot is connected by wireless signal with detector, and detector is connected by wireless signal with reception controller; Detector is provided with remote control signal receiver, driving mechanism, probe apparatus and wireless launcher, and remote control signal receiver is controlled driving mechanism, and driving mechanism, probe apparatus and wireless launcher are electrically connected to successively; Receive controller and be provided with wireless receiver, control module and G-M pipe; Wireless receiver is connected with control module respectively with G-M pipe.Because detector is provided with remote control signal receiver and wireless launcher, receive controller and be provided with wireless receiver and control module, and be provided with telepilot, therefore, detector can be realized wireless signal with reception controller and be connected, and because detector is provided with motor and screw propeller, thereby make the detector can remote control distributor and survey, therefore, χ-gamma dose rate measuring instrument of this remote-controlled flight can be avoided not raying of staff injury in measuring process, and has the feature easily of measuring.
Accompanying drawing explanation
Fig. 1 is the circuit principle structure schematic diagram of χ-gamma dose rate measuring instrument of a kind of remote-controlled flight of the present utility model.
Fig. 2 is the circuit principle structure schematic diagram of probe apparatus of the present utility model.
In Fig. 1 and Fig. 2, include:
1---telepilot,
2---detector, 21---remote control signal receiver, 22---probe apparatus,
23---wireless launcher, 24---motor, 25---screw propeller, 26---power supply, 251---turning axle,
27---GPS locating device, 28---distance measuring equipment, 29---camera head,
201---high-voltage power supply element, 202---photomultiplier, 203---photocon, 204---detecting element, 205---current frequency converter element, 206---control element, 207---memory element,
3---receive controller, 31---wireless receiver, 32---control module, 33---G-M pipe,
301---amplifier, 302---discriminator, 303---controller, 304---display, 305---alarm, 306---storer, 307---high-voltage power supply, 308---low-tension supplies.
Embodiment
The utility model is described in further detail with the following Examples.
See Fig. 1 and Fig. 2.χ-gamma dose rate measuring instrument of a kind of remote-controlled flight of the present embodiment, comprises telepilot 1, detector 2 and receives controller 3, telepilot 1 is connected by wireless signal with detector 2, and detector 2 is connected by wireless signal with reception controller 3; Detector 2 is provided with remote control signal receiver 21, driving mechanism, probe apparatus 22 and wireless launcher 23, and remote control signal receiver 21 is controlled driving mechanism, and driving mechanism, probe apparatus 22 and wireless launcher 23 are electrically connected to successively; Receive controller 3 and be provided with wireless receiver 31, control module 32 and G-M pipe 33; Wireless receiver 31 is connected with control module 32 respectively with G-M pipe 33.
Wherein, telepilot 1 can implement to survey χ ray and gamma-ray dose equivalent rate and absorbed dose rate by telemeter device 2, and the result of detection of detector 2 can be sent to and be received in controller 3 by wireless launcher 23.Probe apparatus 22 in detector 2 can be sent to by wireless launcher 23 data-signal detecting receive controller 3, receive wireless receiver 31 in controller 3 and receive after the data-signal that detector 2 sends over, data-signal is delivered to control module 32 and process.Because detector 2 is provided with remote control signal receiver 21 and wireless launcher 23, receive controller 3 and be provided with wireless receiver 31 and control module 32, and be provided with telepilot 1, therefore, detector 2 can be realized wireless signal with reception controller 3 and be connected, therefore, χ-gamma dose rate measuring instrument of this remote-controlled flight can be avoided not raying of staff injury in measuring process, and has the feature easily of measuring.
In the present embodiment, driving mechanism comprises motor 24, screw propeller 25 and power supply 26, and power supply 26 is electrically connected to motor 24, and the output shaft of motor 24 drives and is connected with screw propeller 25; Remote control signal receiver 21 is electrically connected to power supply 26.Remote control signal receiver 21 receives after the flight signal of telepilot 1, remote control signal receiver 21 passes to power supply 26 by flight signal, now, power supply 26 is discharge condition, be power supply 26 by electrical energy transfer to motor 24, motor 24 converts electrical energy into mechanical energy, thereby the output shaft of motor 24 drives screw propeller 25 rotations, thereby realizes detector 2 remote control distributors.Gamma radiation detector 2 is implemented to survey in remote control distributor process.
In the present embodiment, driving mechanism also comprises turning axle 251, and turning axle 251 is connected with screw propeller 25 with the output shaft of motor 24 respectively.The output shaft of motor 24 drives turning axle 251 to rotate, and turning axle 251 drives screw propeller 25 rotations, thereby realizes detector 2 remote control distributors.In the dangerously steep and nuclear radiation leakage accident of physical features, χ-gamma dose rate measuring instrument of this remote-controlled flight can be avoided not raying of staff injury in measuring process, and has the feature easily of measuring.
In the present embodiment, probe apparatus 22 is provided with high-voltage power supply element 201, photomultiplier 202, photocon 203, detecting element 204, current frequency converter element 205, control element 206 and memory element 207; The signal output part of high-voltage power supply element 201 connects photomultiplier 202, photocon 203 and detecting element 204 successively; The signal output part of current frequency converter element 205 connects control element 206 and memory element 207 successively; The output terminal of photomultiplier 202 is connected with the input end of current frequency converter element 205; Control element 206 is connected with wireless launcher 23.The result of detection of probe apparatus 22 is transferred to wireless launcher 23 by control element 206, and wireless launcher 23 receives after result of detection, and result of that probe is sent in wireless receiver 31 with the form of electric signal.
In the present embodiment, control module 32 comprises amplifier 301, discriminator 302, controller 303, display 304, alarm 305, storer 306, high-voltage power supply 307 and low-tension supply 308; The signal input part of amplifier 301 is connected with the signal output part of G-M pipe 33, the signal output part of amplifier 301 connects discriminator 302 and controller 303 successively, controller 303 connects respectively display 304, alarm 305 and storer 306, low-tension supply 308 connects respectively amplifier 301, discriminator 302, controller 303, display 304, alarm 305, storer 306 and high-voltage power supply 307, and the signal output part of high-voltage power supply 307 is connected with the signal input part of G-M pipe 33.The output terminal of wireless receiver 31 is connected with the input end of controller 303.Wireless receiver 31 receives after the electric signal of wireless launcher 23 transmissions, and wireless receiver 31 is sent to controller 303 by the electric signal receiving.
In the present embodiment, display 304 is set to digital indicator, thereby makes display effect good.
In the present embodiment, detector 2 is provided with GPS locating device 27, and the output terminal of GPS locating device 27 is connected with wireless launcher 23.This GPS locating device 27 is sent to the locator data of the GPS of measurement to receive by wireless launcher 23 and in controller 3, carries out analysis to measure and put residing particular location, automatically determines and measures place.
In the present embodiment, detector 2 is provided with distance measuring equipment 28, and the output terminal of distance measuring equipment 28 is connected with wireless launcher 23.This distance measuring equipment 28 can be measured the distance between detector 2 and measured object, and distance measuring equipment 28 also can be sent to measurement result in reception controller 3 and be read for operating personnel by wireless launcher 23.
In the present embodiment, detector 2 is provided with camera head 29, and the output terminal of camera head 29 is connected with wireless launcher 23.This camera head 29 can be sent to the image in captured tested region to receive in controller 3 by wireless launcher 23 and obtain for operating personnel.
Finally should be noted that; above embodiment is the restriction for the technical solution of the utility model is described but not to the utility model protection domain only; although the utility model is explained in detail with reference to preferred embodiment; those of ordinary skill in the art is to be understood that; can modify or be equal to replacement the technical solution of the utility model, and not depart from essence and the scope of technical solutions of the utility model.
Claims (9)
1. χ-gamma dose rate measuring instrument of a remote-controlled flight, it is characterized in that: comprise telepilot, detector and reception controller, described telepilot is connected by wireless signal with described detector, and described detector is connected by wireless signal with described reception controller;
Described detector is provided with remote control signal receiver, driving mechanism, probe apparatus and wireless launcher, described remote control signal receiver is controlled described driving mechanism, and described driving mechanism, described probe apparatus and described wireless launcher are electrically connected to successively;
Described reception controller is provided with wireless receiver, control module and G-M pipe; Described wireless receiver is connected with described control module respectively with described G-M pipe.
2. χ-gamma dose rate measuring instrument of a kind of remote-controlled flight according to claim 1, it is characterized in that: described driving mechanism comprises motor, screw propeller and power supply, described power supply is electrically connected to described motor, and the output shaft of described motor drives and is connected with described screw propeller; Described remote control signal receiver is electrically connected to described power supply.
3. χ-gamma dose rate measuring instrument of a kind of remote-controlled flight according to claim 2, is characterized in that: described driving mechanism also comprises turning axle, and described turning axle is connected with described screw propeller with the output shaft of described motor respectively.
4. χ-gamma dose rate measuring instrument of a kind of remote-controlled flight according to claim 1, is characterized in that: described probe apparatus is provided with high-voltage power supply element, photomultiplier, photocon, detecting element, current frequency converter element, control element and memory element; The signal output part of described high-voltage power supply element connects described photomultiplier, described photocon and described detecting element successively; The signal output part of described current frequency converter element connects described control element and described memory element successively; The output terminal of described photomultiplier is connected with the input end of described current frequency converter element; Described control element is connected with described wireless launcher.
5. χ-gamma dose rate measuring instrument of a kind of remote-controlled flight according to claim 1, is characterized in that: described control module comprises amplifier, discriminator, controller, display, alarm, storer, high-voltage power supply and low-tension supply; The signal input part of described amplifier is connected with the signal output part of described G-M pipe, the signal output part of described amplifier connects described discriminator and described controller successively, described controller connects respectively described display, described alarm and described storer, described low-tension supply connects respectively described amplifier, described discriminator, described controller, described display, described alarm, described storer and described high-voltage power supply, and the signal output part of described high-voltage power supply is connected with the signal input part of described G-M pipe; The output terminal of described wireless receiver is connected with the input end of described controller.
6. χ-gamma dose rate measuring instrument of a kind of remote-controlled flight according to claim 5, is characterized in that: described display is set to digital indicator.
7. χ-gamma dose rate measuring instrument of a kind of remote-controlled flight according to claim 1, is characterized in that: described detector is provided with GPS locating device, and the output terminal of described GPS locating device is connected with described wireless launcher.
8. χ-gamma dose rate measuring instrument of a kind of remote-controlled flight according to claim 1, is characterized in that: described detector is provided with distance measuring equipment, and the output terminal of described distance measuring equipment is connected with described wireless launcher.
9. χ-gamma dose rate measuring instrument of a kind of remote-controlled flight according to claim 1, is characterized in that: described detector is provided with camera head, and the output terminal of described camera head is connected with described wireless launcher.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320528668.4U CN203414597U (en) | 2013-08-28 | 2013-08-28 | Remote control flight chi-gamma dose rate measurement instrument |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320528668.4U CN203414597U (en) | 2013-08-28 | 2013-08-28 | Remote control flight chi-gamma dose rate measurement instrument |
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| Publication Number | Publication Date |
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| CN203414597U true CN203414597U (en) | 2014-01-29 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320528668.4U Expired - Fee Related CN203414597U (en) | 2013-08-28 | 2013-08-28 | Remote control flight chi-gamma dose rate measurement instrument |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105510951A (en) * | 2015-11-24 | 2016-04-20 | 中国原子能科学研究院 | Radiation monitoring system |
| CN105866823A (en) * | 2016-04-19 | 2016-08-17 | 成都新核泰科科技有限公司 | Nuclear emergency radiation monitoring system based on unmanned aerial vehicle |
-
2013
- 2013-08-28 CN CN201320528668.4U patent/CN203414597U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105510951A (en) * | 2015-11-24 | 2016-04-20 | 中国原子能科学研究院 | Radiation monitoring system |
| CN105866823A (en) * | 2016-04-19 | 2016-08-17 | 成都新核泰科科技有限公司 | Nuclear emergency radiation monitoring system based on unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140129 Termination date: 20200828 |
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| CF01 | Termination of patent right due to non-payment of annual fee |