CN112327349B - Air identification device for air radiation monitoring - Google Patents
Air identification device for air radiation monitoring Download PDFInfo
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- CN112327349B CN112327349B CN202011315061.9A CN202011315061A CN112327349B CN 112327349 B CN112327349 B CN 112327349B CN 202011315061 A CN202011315061 A CN 202011315061A CN 112327349 B CN112327349 B CN 112327349B
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- 230000005855 radiation Effects 0.000 title claims abstract description 109
- 238000012544 monitoring process Methods 0.000 title claims abstract description 50
- 238000004891 communication Methods 0.000 claims abstract description 140
- 230000006855 networking Effects 0.000 claims abstract description 55
- 238000005259 measurement Methods 0.000 claims abstract description 44
- 238000009434 installation Methods 0.000 claims abstract description 18
- 238000007789 sealing Methods 0.000 claims abstract description 4
- 239000000463 material Substances 0.000 claims description 7
- 230000002093 peripheral effect Effects 0.000 claims description 7
- 239000010410 layer Substances 0.000 claims description 6
- 230000000149 penetrating effect Effects 0.000 claims description 4
- 239000011241 protective layer Substances 0.000 claims description 2
- 230000000694 effects Effects 0.000 description 13
- 239000003550 marker Substances 0.000 description 10
- 238000000034 method Methods 0.000 description 9
- 230000008569 process Effects 0.000 description 8
- 239000002245 particle Substances 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 238000007405 data analysis Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01T—MEASUREMENT OF NUCLEAR OR X-RADIATION
- G01T7/00—Details of radiation-measuring instruments
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- General Physics & Mathematics (AREA)
- High Energy & Nuclear Physics (AREA)
- Molecular Biology (AREA)
- Spectroscopy & Molecular Physics (AREA)
- Measurement Of Radiation (AREA)
Abstract
The invention relates to an aerial identification device for aerial radiation monitoring, which comprises a measurement communication part and a flight unit for driving the measurement communication part to fly to a corresponding monitoring point, wherein the measurement communication part is connected with the flight unit; the measurement communication part comprises a shell with a mounting cavity inside; the installation cavity of the shell is internally provided with a plurality of independent cavities, including a communication room provided with a networking communication unit and a measurement room provided with a radiation measurement unit; a positioning unit for acquiring air position data is also arranged in the mounting cavity of the shell; the communication chamber is a closed chamber; the networking communication unit is arranged in the communication room in a sealing way when being installed; the measuring chamber penetrates through the shell and is communicated with the outside; the radiation measuring unit is arranged with its measuring end facing outwards and capable of contacting the outside when mounted. The aerial identification device for aerial radiation monitoring can fly to the corresponding monitoring point of the airspace of the radiation pollution area, and can finish radiation intensity data measurement and return.
Description
Technical Field
The invention relates to the technical field of marker measurement, in particular to an air identification device for air radiation monitoring.
Background
Radiation refers to the phenomenon in which a portion of the electromagnetic energy emitted by a field source travels away from the field source and then no longer returns to the field source, and the energy diffuses outward in the form of electromagnetic waves or particles (e.g., alpha particles, beta particles, etc.). Radiation is extremely harmful to the human body, so when a radiation pollution accident (such as nuclear leakage or radiation pollution caused by chemical leakage) occurs, it is necessary to monitor the radiation pollution area in time to reduce the influence of radiation pollution as much as possible.
The land radiation pollution monitoring is to set a marker throwing device on a monitoring vehicle, then control the monitoring vehicle to move in a radiation pollution area and throw a radiation marker at the position of a monitoring point so as to mark each monitoring point through the radiation marker. The existing radiation marker generally comprises a bearing part and a marking rod fixedly arranged at the top of the bearing part. Of course, when the radiation pollution accident occurs, radiation pollution exists not only on land, but also in the air, because radiation source substances can fly in the air along with wind, and radiation 'diffusion' is realized in the air. To monitor radiation pollution in the air, the applicant has devised an air marker that can be flown to a designated monitoring point in the air of a radiation pollution area for marking.
To accomplish the airborne radiation pollution monitoring, the applicant further envisages providing radiation measurement units on the airborne markers, by means of which the radiation intensity of the surrounding area can be measured when the airborne markers fly to the corresponding monitoring points.
However, how to design an air marker that can fly and can perform radiation intensity measurement is an urgent technical problem to be solved. In addition, after the air identifier finishes the measurement of the radiation intensity data of the corresponding monitoring point, the data also need to be transmitted back to the set management terminal for data analysis. That is, the air identifier is further required to be provided with a networking communication unit for networking communication with the management terminal and transmitting back measurement data, and the networking communication of the networking communication unit is easily interfered by external radiation and the radiation measurement unit (the radiation measurement unit needs to be in contact with external radiation pollution as much as possible during working), so that the networking communication effect of the networking communication unit and the management terminal is poor. In view of the above problems, the applicant has devised an air marker device for air radiation monitoring that is capable of flying to the monitoring point of the airspace of a radiation contaminated area and completing the measurement and return of radiation intensity data.
Disclosure of Invention
Aiming at the defects in the prior art, the invention aims to solve the technical problems that: how to provide a can fly to the corresponding monitoring point in the radiation pollution area airspace, and can accomplish the aerial identification device that is used for aerial radiation monitoring of radiation intensity data measurement and passback to can assist the monitoring effect who promotes aerial radiation monitoring.
In order to solve the technical problems, the invention adopts the following technical scheme:
an aerial identification device for aerial radiation monitoring comprises a measurement communication part and a flight unit for driving the measurement communication part to fly to a corresponding monitoring point;
the measurement communication part comprises a shell with a mounting cavity inside; the installation cavity of the shell is internally provided with a plurality of independent cavities, including a communication room provided with a networking communication unit and a measurement room provided with a radiation measurement unit; a positioning unit for acquiring air position data is also arranged in the mounting cavity of the shell; the communication chamber is a closed chamber; the networking communication unit is arranged in the communication room in a sealing way when being installed; the measuring chamber penetrates through the shell and is communicated with the outside; the radiation measuring unit is arranged with its measuring end facing outwards and capable of contacting the outside when mounted.
Preferably, the shell comprises a lower shell body with a hollow inside and an open top, and a top cover plate which can be detachably matched with the open end of the lower shell body; the communication chamber and the measuring chamber are arranged in the hollow part of the lower shell; the flying unit is fixedly connected with the top cover plate through a connecting rod.
Preferably, the networking communication unit is provided with a communication antenna; the connecting rod of the flying unit is provided with a hollow part which is arranged in a penetrating way along the central axis and penetrates through the flying unit; the communication chamber is arranged close to the top cover plate, and the top cover plate is provided with a hollow part for communicating the connecting rod and an installation through hole of the communication chamber; when the networking communication unit is installed, a communication antenna of the networking communication unit can penetrate through the installation through hole of the top cover plate and be inserted into the hollow part of the connecting rod.
Preferably, the open end of the lower shell is circular, the top cover plate is a circular plate, and the external dimension of the top cover plate is adapted to the open end of the lower shell; the inner peripheral side edge of the open end of the lower shell is provided with an internal thread, the outer peripheral side edge of the top cover plate is provided with an external thread which is matched with the internal thread of the open end of the lower shell, and the top cover plate is detachably matched with the thread of the open end of the lower shell.
Preferably, the installation through hole is arranged at the axle center of the top cover plate; the connecting rod is coaxially arranged with the top cover plate, and the central axis of the middle part is coincident with the central axis of the mounting through hole.
Preferably, the measuring chamber is arranged below the communication chamber, and a radiation shielding layer is further arranged between the measuring chamber and the communication chamber.
Preferably, the installation cavity of the shell is also provided with a power supply chamber provided with an independent power supply; the independent power supply is used for providing electric energy for the networking communication unit, the radiation measurement unit and the positioning unit.
Preferably, the positioning unit is disposed in the communication chamber.
Preferably, the flying unit is an unmanned plane.
Preferably, the lower shell body and the top cover plate are made of lead materials, and the thickness of the lower shell body and the top cover plate is greater than or equal to 2cm.
Compared with the prior art, the invention has the following advantages:
1. according to the invention, the flight unit can drive the measurement communication part to fly in the airspace of the radiation pollution area and reach the appointed monitoring point, the radiation measurement unit can acquire the radiation intensity data at the monitoring point, the positioning unit can acquire the air position data of the monitoring point, the networking communication unit can carry out networking communication with the management terminal and transmit the radiation intensity data and the air position data back to the management terminal, so that the air radiation monitoring can be well assisted.
2. In the invention, the inner cavity of the shell is divided into a communication chamber and a measuring chamber which are mutually independent (in order to divide the inner cavity of the shell into a plurality of independent chambers, radiation-proof concrete megaohm lead is filled in the inner cavity of the shell), so that the networking communication of the networking communication unit is not easily influenced by the operation of the radiation measuring unit (the radiation measuring unit needs to be contacted with external radiation pollution as much as possible during the operation).
3. In the invention, the networking communication unit is hermetically arranged in the communication room and is not easily influenced by external radiation. In addition, the measuring chamber runs through the casing and is communicated with the outside, so that the measuring end of the radiation measuring unit is outwards arranged and can be in direct contact with the outside radiation pollution, the measuring effect and the accuracy of the radiation measuring unit can be well ensured, and the monitoring effect of aerial radiation monitoring can be assisted and promoted.
4. According to the invention, the hollow part is arranged on the connecting rod, and the communication antenna of the networking communication unit can penetrate through the mounting through hole of the top cover plate to be inserted into the hollow part of the connecting rod during use, so that the stretching and the unfolding of the communication antenna are realized, and the communication effect of the networking communication unit can be ensured. Meanwhile, the matching structure of the communication antenna and the connecting rod has the advantages of compact and concise structure, and the protection layer can be formed on the periphery side of the communication antenna, so that better auxiliary networking communication unit communication is facilitated.
Drawings
For the purpose of making the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in further detail with reference to the accompanying drawings, in which:
FIG. 1 is a schematic diagram of an air identification device for air radiation monitoring in an embodiment;
fig. 2 is a front cross-sectional view of an air identification device for air radiation monitoring in an embodiment.
Reference numerals in the drawings of the specification include: the device comprises a shell 1, a lower shell 11, a top cover plate 12, a flying unit 2, a connecting rod 3, a hollow part 31, a networking communication unit 4, a communication room 41, a positioning unit 5, a radiation measurement unit 6, a measurement room 61, an independent power supply 7, a power supply room 71 and a communication antenna 8.
Detailed Description
The following is a further detailed description of the embodiments:
examples:
the embodiment discloses an air identification device for air radiation monitoring.
As shown in fig. 1 and 2, an air marking device for air radiation monitoring comprises a measurement communication part and a flight unit 2 for driving the measurement communication part to fly to a corresponding monitoring point.
The measurement communication part includes a housing 1 having a mounting cavity therein; the installation cavity of the shell 1 is provided with a plurality of independent cavities, including a communication room 41 provided with a networking communication unit 4 and a measurement room 61 provided with a radiation measurement unit 6; a positioning unit 5 for acquiring air position data is also arranged in the installation cavity of the shell 1; the communication chamber 41 is a closed chamber; the networking communication unit 4 is hermetically arranged in the communication room 41 when installed; the measuring chamber 61 penetrates the casing 1 and is provided in communication with the outside; the radiation measuring unit 6 is mounted with its measuring end facing outwards and capable of contacting the outside. In this embodiment, the flight unit 2 is an unmanned aerial vehicle used in the prior art; the radiation measuring unit 6 is an existing radiation intensity measuring instrument; the positioning unit 5 is a positioning module used on the existing unmanned aerial vehicle, and can acquire current position data and height data; the networking communication mode of the networking communication unit 4 and the management terminal is GPRS network communication; the management terminal is an existing background server, and can control the flight unit 2 to drive the measurement communication part to fly, and can receive and process radiation intensity data and air position data.
In the invention, the flight unit 2 can drive the measurement communication part to fly in the airspace of the radiation pollution area and reach the appointed monitoring point, the radiation measurement unit 6 can acquire the radiation intensity data at the monitoring point, the positioning unit 5 can acquire the air position data of the monitoring point, the networking communication unit 4 can carry out networking communication with the management terminal and transmit the radiation intensity data and the air position data back to the management terminal, thereby being capable of well assisting in completing the air radiation monitoring. Secondly, the inner cavity of the housing 1 is divided into a communication chamber 41 and a measuring chamber 61 which are independent from each other (in order to divide the inner cavity of the housing 1 into a plurality of independent chambers, radiation-proof concrete megaohm lead is filled in the inner cavity of the housing 1), so that the networking communication of the networking communication unit 4 is not easily affected by the operation of the radiation measuring unit 6 (the radiation measuring unit 6 needs to be in contact with external radiation pollution as much as possible during the operation). Meanwhile, the networking communication unit 4 is hermetically installed in the communication room 41, and is not easily affected by external radiation. In addition, the measuring chamber 61 penetrates the casing 1 and is communicated with the outside, so that the measuring end of the radiation measuring unit 6 is arranged outwards and can be in direct contact with the outside radiation pollution, the measuring effect and the accuracy of the radiation measuring unit 6 can be well guaranteed, and the monitoring effect of aerial radiation monitoring can be improved in an auxiliary mode.
In the implementation process, the shell 1 comprises a lower shell 11 with a hollow inside and an open top, and a top cover plate 12 which can be detachably matched with the open end of the lower shell 11; the communication chamber 41 and the measurement chamber 61 are provided in the hollow portion 31 of the lower case 11; the flying unit 2 is fixedly connected with the top cover plate 12 through a connecting rod 3.
The shell 1 of the invention is a detachable lower shell 11 and a top cover 12, so that the networking communication unit 4, the positioning unit 5 and other necessary components can be conveniently replaced or installed by disassembling and assembling the top cover 12, and the use convenience of the radiation marker can be improved.
In the specific implementation process, the networking communication unit 4 is provided with a communication antenna 8; the connecting rod 3 of the flying unit 2 has a hollow portion 31 penetrating the flying unit 2 and penetrating along the central axis; the communication chamber 41 is arranged near the top cover plate 12, and the top cover plate 12 is provided with an installation through hole for communicating the hollow part 31 of the connecting rod 3 and the communication chamber 41; when the networking communication unit 4 is installed, the communication antenna 8 can be inserted into the hollow part 31 of the connecting rod 3 through the installation through hole of the top cover plate 12.
The networking communication unit 4 has the communication antenna 8, and when in use, the communication antenna 8 needs to be stretched and unfolded to achieve the ideal networking communication effect. Therefore, in the invention, the hollow part 31 is arranged on the connecting rod 3, and the communication antenna 8 of the networking communication unit 4 can be inserted into the hollow part 31 of the connecting rod 3 through the mounting through hole of the top cover plate 12 when in use, so that the stretching and unfolding of the communication antenna 8 are realized, and the communication effect of the networking communication unit 4 can be ensured. Meanwhile, the matching structure of the communication antenna 8 and the connecting rod 3 not only has the advantages of compact and simple structure, but also can form a protective layer on the outer periphery side of the communication antenna 8, thereby being beneficial to better communication of the auxiliary networking communication unit 4.
In the specific implementation process, the open end of the lower shell 11 is circular, the top cover plate 12 is a circular plate, and the external dimension of the top cover plate is adapted to the open end of the lower shell 11; the inner peripheral side edge of the open end of the lower shell 11 is provided with an internal thread, the outer peripheral side edge of the top cover 12 is provided with an external thread adapted to the internal thread of the open end of the lower shell 11, and the top cover 12 is detachably engaged with the thread of the open end of the lower shell 11.
In the present invention, the lower case 11 may be provided in a hollow hemispherical or rectangular parallelepiped shape; the mounting mode of the detachable thread has the advantages of convenient dismounting and good sealing performance.
In the specific implementation process, the installation through hole is arranged at the axle center of the top cover plate 12; the connecting rod 3 is arranged coaxially with the top cover plate 12, and the central axis of the middle portion 31 coincides with the central axis of the mounting through hole.
The top cover plate 12 needs to be rotated for installation or removal. Therefore, the connecting rod 3 and the top cover plate 12 are coaxially arranged, the central axis of the hollow part 31 coincides with the central axis of the mounting through hole (the mounting through hole is arranged at the central axis of the top cover plate 12), so that the communication antenna 8 is not affected or damaged by rotation of the top cover plate 12 during mounting or dismounting, and better communication of the auxiliary networking communication unit 4 is facilitated.
In the implementation process, the measuring chamber 61 is arranged below the communication chamber 41, and a radiation shielding layer is further arranged between the measuring chamber 61 and the communication chamber 41. In this embodiment, the radiation shielding layer is made of lead.
Since the radiation measuring unit 6 needs to be in contact with the external radiation pollution as much as possible during operation, the networking communication effect of the communication networking unit is easily affected by the radiation. Therefore, the present invention provides a radiation shielding layer between the measuring chamber 61 and the communication chamber 41 for better isolation of the networking communication unit 4. Ensuring the communication effect. Meanwhile, lead is one of the best radiation-proof materials, which is beneficial to better communication of the auxiliary networking communication unit 4.
In the specific implementation process, a power supply chamber 71 provided with an independent power supply 7 is also arranged in the installation cavity of the shell 1; the independent power supply 7 is used to supply the networking communication unit 4, the radiation measuring unit 6 and the positioning unit 5 with electrical energy. In the present embodiment, the power supply chamber 71 is provided at a position beside the measurement chamber 61 and the communication chamber 41.
The existing networking communication unit 4 and the radiation measurement unit 6 generally have self-powered sources, but the power of the self-powered sources is limited, and radiation monitoring is a long-time monitoring process. Therefore, the independent power supply 7 is arranged in the inner cavity of the shell 1 and is used for providing electric energy for the networking communication unit 4, the radiation measurement unit 6 and the positioning unit 5, so that the cruising effect of the radiation marker can be ensured. Meanwhile, the power supply chamber 71 is provided at a side position of the measuring chamber 61 and the communication chamber 41, which is advantageous in better arrangement of the independent power supply 7.
In the implementation, the positioning unit 5 is disposed in the communication chamber 41.
In the invention, the positioning unit 5 is arranged in the communication room 41, so that the positioning unit 5 is prevented from being influenced by the operation of the radiation measuring unit 6 (the radiation measuring unit 6 needs to be contacted with external radiation pollution as much as possible when in operation), and the positioning accuracy of the positioning unit 5 is ensured.
In the specific implementation process, the lower shell 11 and the top cover plate 12 are made of lead materials, and the thickness of the lower shell 11 and the top cover plate 12 is greater than or equal to 2cm.
In the invention, the lower shell 11 and the top cover plate 12 are made of lead material, and the lead material is one of the best radiation-proof materials, so that better communication of the auxiliary networking communication unit 4 is facilitated. Meanwhile, the thickness of the lower case 11 and the top cover 12 is greater than or equal to 2cm for better shielding of radiation.
The foregoing is merely an embodiment of the present invention, and a specific structure and characteristics of common knowledge in the art, which are well known in the scheme, are not described herein, so that a person of ordinary skill in the art knows all the prior art in the application day or before the priority date of the present invention, and can know all the prior art in the field, and have the capability of applying the conventional experimental means before the date, so that a person of ordinary skill in the art can complete and implement the present embodiment in combination with his own capability in the light of the present application, and some typical known structures or known methods should not be an obstacle for a person of ordinary skill in the art to implement the present application. It should be noted that modifications and improvements can be made by those skilled in the art without departing from the structure of the present invention, and these should also be considered as the scope of the present invention, which does not affect the effect of the implementation of the present invention and the utility of the patent. The protection scope of the present application shall be subject to the content of the claims, and the description of the specific embodiments and the like in the specification can be used for explaining the content of the claims.
Claims (6)
1. An aerial marking device for aerial radiation monitoring, characterized in that: the device comprises a measurement communication part and a flight unit, wherein the flight unit is used for driving the measurement communication part to fly to a corresponding monitoring point;
the measurement communication part comprises a shell with a mounting cavity inside; the installation cavity of the shell is internally provided with a plurality of independent cavities, including a communication room provided with a networking communication unit and a measurement room provided with a radiation measurement unit; a positioning unit for acquiring air position data is also arranged in the mounting cavity of the shell;
the communication chamber is a closed chamber; the networking communication unit is arranged in the communication room in a sealing way when being installed;
the measuring chamber penetrates through the shell and is communicated with the outside; the radiation measuring unit is arranged with the measuring end facing outwards and can contact with the outside when being installed;
the shell comprises a lower shell body with a hollow inside and an open top, and a top cover plate which can be detachably matched with the open end of the lower shell body; the communication chamber and the measuring chamber are arranged in the hollow part of the lower shell; the flying unit is fixedly connected with the top cover plate through a connecting rod;
the networking communication unit is provided with a communication antenna;
the connecting rod of the flying unit is provided with a hollow part which is arranged in a penetrating way along the central axis and penetrates through the flying unit; the communication chamber is arranged close to the top cover plate, and the top cover plate is provided with a hollow part for communicating the connecting rod and an installation through hole of the communication chamber; when the networking communication unit is installed, a communication antenna of the networking communication unit can penetrate through the installation through hole of the top cover plate and be inserted into the hollow part of the connecting rod; forming a protective layer on the outer peripheral side of the communication antenna through the connecting rod;
the open end of the lower shell body is circular, the top cover plate is a circular plate, and the external dimension of the top cover plate is matched with the open end of the lower shell body; the inner peripheral side edge of the open end of the lower shell is provided with an internal thread, the outer peripheral side edge of the top cover plate is provided with an external thread which is matched with the internal thread of the open end of the lower shell, and the top cover plate is detachably matched with the thread of the open end of the lower shell;
the mounting through hole is arranged at the axle center of the top cover plate; the connecting rod and the top cover plate are coaxially arranged, and the central axis of the middle part is coincident with the central axis of the mounting through hole; rotation of the top cover plate during installation or removal does not affect or damage the communication antenna.
2. An air identification device for air radiation monitoring as defined in claim 1, wherein: the measuring chamber is arranged below the communication chamber, and a radiation shielding layer is further arranged between the measuring chamber and the communication chamber.
3. An air identification device for air radiation monitoring as defined in claim 1, wherein: the installation cavity of the shell is also internally provided with a power supply chamber provided with an independent power supply; the independent power supply is used for providing electric energy for the networking communication unit, the radiation measurement unit and the positioning unit.
4. An air identification device for air radiation monitoring as defined in claim 1, wherein: the positioning unit is arranged in the communication chamber.
5. An air identification device for air radiation monitoring as defined in claim 1, wherein: the flying unit is an unmanned plane.
6. An air identification device for air radiation monitoring as defined in claim 1, wherein: the lower shell body and the top cover plate are made of lead materials, and the thickness of the lower shell body and the top cover plate is larger than or equal to 2cm.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202011315061.9A CN112327349B (en) | 2020-11-20 | 2020-11-20 | Air identification device for air radiation monitoring |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011315061.9A CN112327349B (en) | 2020-11-20 | 2020-11-20 | Air identification device for air radiation monitoring |
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| CN112327349A CN112327349A (en) | 2021-02-05 |
| CN112327349B true CN112327349B (en) | 2024-01-23 |
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| CN112327349A (en) | 2021-02-05 |
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