CN112455677A - Unmanned aerial vehicle for patrolling national soil resources - Google Patents
Unmanned aerial vehicle for patrolling national soil resources Download PDFInfo
- Publication number
- CN112455677A CN112455677A CN202011175666.2A CN202011175666A CN112455677A CN 112455677 A CN112455677 A CN 112455677A CN 202011175666 A CN202011175666 A CN 202011175666A CN 112455677 A CN112455677 A CN 112455677A
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- Prior art keywords
- fixedly connected
- unmanned aerial
- aerial vehicle
- main shell
- patrolling
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- 239000002689 soil Substances 0.000 title claims abstract description 15
- 238000010248 power generation Methods 0.000 claims abstract description 18
- 230000017525 heat dissipation Effects 0.000 claims description 6
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 3
- 238000007689 inspection Methods 0.000 claims 3
- 239000013589 supplement Substances 0.000 abstract 1
- 238000012544 monitoring process Methods 0.000 description 2
- 230000009469 supplementation Effects 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000005065 mining Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Classifications
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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
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
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- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Power Engineering (AREA)
- Photovoltaic Devices (AREA)
Abstract
The invention provides an unmanned aerial vehicle for patrolling national soil resources, which comprises a main shell, wherein eight spiral arms are fixedly connected to the periphery of the main shell, the eight spiral arms are symmetrical about the center of the main shell, a motor is fixedly connected to the end part of each spiral arm, a rotor wing is fixedly connected to the output end of each motor, and a data acquisition system is fixedly connected to the bottom of the main shell. According to the invention, through the arrangement of the solar power generation assembly, the electric power can be supplemented when the unmanned aerial vehicle flies, the electric power supplement can be reduced when the electric power of the unmanned aerial vehicle is exhausted, and through the arrangement of the electric telescopic rod and the rotating arm, the angle of the solar cell panel can be timely adjusted, the optimal flying posture is ensured, the flying resistance is reduced, meanwhile, the angle can be adjusted according to the sunlight irradiation direction, the power generation efficiency is improved, the cruising ability of the unmanned aerial vehicle is further increased, the structure design of the invention is simple, reasonable, convenient and rapid to use, and the practicability is very strong.
Description
Technical Field
The invention relates to the field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle for patrolling national soil resources.
Background
At present, the phenomenon that illegal construction occupies cultivated land and the phenomenon that mining resources are stolen frequently occur, the land utilization change condition is monitored mainly by technical means such as satellite remote sensing monitoring and the like during monitoring, and the illegal land conditions of all the places are checked through the change of land remote sensing images at the time before and after different years. Compare in the tradition mode of patrolling and examining, patrol and examine through unmanned aerial vehicle more high-efficient and accurate.
Generally because the homeland resource is comparatively huge, when patrolling and examining the task, current unmanned aerial vehicle electric power continuation of the journey is the problem that must face, and unmanned aerial vehicle often can lead to patrolling and examining the unable completion of task because of electric power is not enough, the efficiency and the degree of accuracy of patrolling and examining that have reduced.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle for patrolling the soil resources, which has the advantages of long endurance, high efficiency and accurate patrolling.
In order to achieve the above purpose, the invention provides the following technical scheme: an unmanned aerial vehicle for patrolling soil resources comprises a main shell, wherein eight spiral arms are fixedly connected to the periphery of the main shell, the eight spiral arms are symmetrical about the center of the main shell, a motor is fixedly connected to the end part of each spiral arm, a rotor wing is fixedly connected to the output end of each motor, and a data acquisition system is fixedly connected to the bottom of the main shell;
the solar power generation assembly is installed at the top of the main casing body, the solar power generation assembly includes the fixed plate, the bottom fixed connection of fixed plate is at the top of the main casing body, the fixedly connected with fixed column of center department at fixed plate top, the top fixedly connected with mounting panel of fixed column, it has electric telescopic handle to articulate on the mounting panel, it has the rotor arm to articulate on the fixed plate, electric telescopic handle's output is articulated with the rotor arm, electric telescopic handle can adjust the angle of rotor arm, the tip fixedly connected with solar cell panel of rotor arm.
Further, in the invention, two sides of the bottom of the main shell are fixedly connected with a landing gear, the landing gear comprises two support rods and a bottom rod, the top ends of the two support rods are fixedly connected with the main shell, and the bottom ends of the two support rods are fixedly connected with the bottom rod.
Further, in the invention, the number of the solar cell panels is five, the five solar cell panels are symmetrical about the center of the fixed plate, and the installation plate, the electric telescopic rod and the rotating arm corresponding to the solar cell panels are all five.
Further, in the invention, the end part of the rotating arm is fixedly connected with a connecting plate, the connecting plate is connected with a clamping plate through a bolt, the clamping plate is in threaded connection with a threaded column, and the solar cell panel is provided with a bolt hole matched with the threaded column.
Further, in the invention, the number of the clamping plates and the threaded columns is three, and the number of the bolt holes matched with the threaded columns is also three.
Further, in the invention, the top of the threaded column is fixedly connected with a handle, and the handle is provided with anti-skid threads.
Further, in the invention, the top of the main shell is provided with a heat dissipation hole.
Further, in the invention, the solar power generation assembly further comprises a controller, an inverter and a storage battery, the solar panel is connected with the controller, the controller is connected with the inverter, and the storage battery is respectively connected with the controller and the inverter.
Furthermore, in the invention, an avionics system is arranged in the main shell, and the avionics system comprises a battery, a UBEC, a flight control panel, a remote controller, a receiver, a GPS, a relay, a starting motor, a direct current brush electric regulator, a Hall element, a CDI igniter, an ECU and a steering engine.
The beneficial effects are that the technical scheme of this application possesses following technological effect: according to the invention, through the arrangement of the solar power generation assembly, the electric power can be supplemented when the unmanned aerial vehicle flies, the electric power supplementation can also be reduced when the electric power of the unmanned aerial vehicle is exhausted, and through the arrangement of the electric telescopic rod and the rotating arm, the angle of the solar cell panel can be timely adjusted, the optimal flying posture is ensured, the flying resistance is reduced, meanwhile, the angle can be adjusted according to the sunlight irradiation direction, the power generation efficiency is improved, the cruising ability of the unmanned aerial vehicle is further increased, the solar power generation assembly is simple, reasonable, convenient and rapid to use, and has strong practicability.
It should be understood that all combinations of the foregoing concepts and additional concepts described in greater detail below can be considered as part of the inventive subject matter of this disclosure unless such concepts are mutually inconsistent.
The foregoing and other aspects, embodiments and features of the present teachings can be more fully understood from the following description taken in conjunction with the accompanying drawings. Additional aspects of the invention, e.g., features and/or advantages of exemplary embodiments, will be set forth in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the specific embodiments in accordance with the teachings of the invention.
Drawings
The drawings are not intended to be drawn to scale. In the drawings, each identical or nearly identical component that is illustrated in various figures may be represented by a like numeral. For purposes of clarity, not every component may be labeled in every drawing. Embodiments of various aspects of the present invention will now be described, by way of example, with reference to the accompanying drawings, in which:
FIG. 1 is a schematic view of the structure of the present invention.
Fig. 2 is a schematic perspective view of the solar power generation module according to the present invention.
Fig. 3 is a schematic view of a partial structure of the solar power generation module of the present invention.
Fig. 4 is an enlarged view of a portion of a in fig. 2 according to the present invention.
In the figures, the meaning of the reference numerals is as follows: 1. a main housing; 2. a swing arm; 3. a motor; 4. A rotor; 5. a landing gear; 6. a data acquisition system; 7. a fixing plate; 8. fixing a column; 9. mounting a plate; 10. an electric telescopic rod; 11. a rotating arm; 12. a solar panel; 13. a clamping plate; 14. a threaded post; 15. a handle; 16. and (4) heat dissipation holes.
Detailed Description
In order to better understand the technical content of the present invention, specific embodiments are described below with reference to the accompanying drawings. In this disclosure, aspects of the present invention are described with reference to the accompanying drawings, in which a number of illustrative embodiments are shown. Embodiments of the present disclosure are not necessarily intended to include all aspects of the invention. It should be appreciated that the various concepts and embodiments described above, as well as those described in greater detail below, may be implemented in any of numerous ways, as the disclosed concepts and embodiments are not limited to any one implementation. In addition, some aspects of the present disclosure may be used alone, or in any suitable combination with other aspects of the present disclosure.
As shown in fig. 1-4, an unmanned aerial vehicle for inspecting national soil resources comprises a main shell 1, preferably, an avionic system is arranged in the main shell 1, and the avionic system comprises a battery, a UBEC, a flight control panel, a remote controller, a receiver, a GPS, a relay, a starting motor, a direct current brushed electric regulator, a hall element, a CDI igniter, an ECU and a steering engine.
The periphery of the main shell 1 is fixedly connected with eight radial arms 2, the eight radial arms 2 are centrosymmetric about the main shell 1, the end parts of the radial arms 2 are fixedly connected with a motor 3, the output end of the motor 3 is fixedly connected with a rotor 4, and the bottom of the main shell 1 is fixedly connected with a data acquisition system 6;
the top of main casing 1 installs the solar energy power generation subassembly, and the solar energy power generation subassembly includes fixed plate 7, and is preferred, and the solar energy power generation subassembly still includes controller, dc-to-ac converter and battery, and solar cell panel 12 is connected with the controller, and the controller is connected with the dc-to-ac converter, and the battery is connected with controller and dc-to-ac converter respectively. The bottom fixed connection of fixed plate 7 is at the top of main casing body 1, the fixedly connected with fixed column 8 is located at the center at fixed plate 7 top, the top fixed connection of fixed column 8 is connected with mounting panel 9, it has electric telescopic handle 10 to articulate on the mounting panel 9, it has rotor arm 11 to articulate on the fixed plate 7, electric telescopic handle 10's output is articulated with rotor arm 11, electric telescopic handle 10 can adjust rotor arm 11's angle, rotor arm 11's tip fixedly connected with solar cell panel 12. When the electric telescopic rod 10 is started during use, the output end of the electric telescopic rod 10 drives the rotating arm 11 to rotate, namely, the angle of the solar cell panel 12 can be adjusted, so that the solar cell panel 12 is at the optimal flying angle. According to the invention, through the arrangement of the solar power generation assembly, the electric power can be supplemented when the unmanned aerial vehicle flies, the electric power supplementation can be reduced when the electric power of the unmanned aerial vehicle is exhausted, and through the arrangement of the electric telescopic rod 10 and the rotating arm 11, the angle of the solar cell panel 12 can be timely adjusted, the optimal flying posture is ensured, the flying resistance is reduced, meanwhile, the angle can be adjusted according to the sunlight irradiation direction, the power generation efficiency is improved, the cruising ability of the unmanned aerial vehicle is further increased, the structure of the invention is simple, reasonable, convenient and rapid to use, and has strong practicability
In the preferred embodiment, the landing gear 5 is fixedly connected to two sides of the bottom of the main housing 1, the landing gear 5 includes two support rods and a bottom rod, the top ends of the two support rods are fixedly connected to the main housing 1, and the bottom ends of the two support rods are fixedly connected to the bottom rod.
In the preferred embodiment, the number of the solar cell panels 12 is five, the five solar cell panels 12 are symmetrical about the center of the fixing plate 7, and the mounting plate 9, the electric telescopic rod 10 and the rotating arm 11 corresponding to the solar cell panels 12 are all five.
Preferably, the tip fixedly connected with connecting plate of rotor arm 11 has splint 13 through bolted connection on the connecting plate, and threaded connection has screw post 14 on splint 13, has seted up on solar cell panel 12 with 14 looks adaptation bolt holes of screw post, through the setting of connecting plate, splint 13 and screw post 14, can fix solar cell panel 12 at the tip of rotor arm 11. Further preferably, the number of the clamping plates 13 and the threaded columns 14 is three, the number of the bolt holes matched with the threaded columns 14 is also three, and the three clamping plates 13 and the threaded columns 14 can increase the stability of connection.
The preferred, top fixedly connected with handle 15 of screw thread post 14 of this embodiment is provided with anti-skidding line on the handle 15, and through the setting of handle 15, the convenience of customers rotates screw thread post 14, has brought the convenience for the user.
In the present embodiment, the heat dissipation hole 16 is preferably formed at the top of the main housing 1, and the heat dissipation performance of the main housing 1 can be increased by the heat dissipation hole 16.
Although the present invention has been described with reference to the preferred embodiments, it is not intended to be limited thereto. Those skilled in the art can make various changes and modifications without departing from the spirit and scope of the invention. Therefore, the protection scope of the present invention should be determined by the appended claims.
Claims (9)
1. The utility model provides an unmanned aerial vehicle is patrolled and examined to homeland resource, includes main casing body (1), its characterized in that: the periphery of the main shell (1) is fixedly connected with eight radial arms (2), the eight radial arms (2) are centrosymmetric about the main shell (1), the end part of each radial arm (2) is fixedly connected with a motor (3), the output end of each motor (3) is fixedly connected with a rotor wing (4), and the bottom of the main shell (1) is fixedly connected with a data acquisition system (6);
the solar energy power generation subassembly is installed at the top of the main casing body (1), the solar energy power generation subassembly includes fixed plate (7), the bottom fixed connection of fixed plate (7) is at the top of the main casing body (1), the center fixedly connected with fixed column (8) of department at fixed plate (7) top, the top fixedly connected with mounting panel (9) of fixed column (8), it has electric telescopic handle (10) to articulate on mounting panel (9), it has rotor arm (11) to articulate on fixed plate (7), electric telescopic handle's (10) output is articulated with rotor arm (11), the angle of rotor arm (11) can be adjusted in electric telescopic handle (10), the tip fixedly connected with solar cell panel (12) of rotor arm (11).
2. The unmanned aerial vehicle for patrolling soil resources according to claim 1, wherein: the both sides fixedly connected with undercarriage (5) of main casing body (1) bottom, undercarriage (5) include two spinal branch poles and a sill bar, two the top and the main casing body (1) fixed connection of branch, two the bottom and the sill bar fixed connection of branch.
3. The soil resource inspection unmanned aerial vehicle of claim 2, wherein: the solar cell panel (12) number is five, and five solar cell panels (12) are symmetrical about the center of fixed plate (7), and corresponding mounting panel (9), electric telescopic handle (10) and rotor arm (11) of solar cell panel (12) are five.
4. The unmanned aerial vehicle for patrolling soil resources according to claim 1, wherein: the end part of the rotating arm (11) is fixedly connected with a connecting plate, the connecting plate is connected with a clamping plate (13) through a bolt, the clamping plate (13) is connected with a threaded column (14) through a thread, and a bolt hole matched with the threaded column (14) is formed in the solar cell panel (12).
5. The soil resource inspection unmanned aerial vehicle of claim 4, wherein: the number of the clamping plates (13) and the threaded columns (14) is three, and the number of the bolt holes matched with the threaded columns (14) is also three.
6. The soil resource inspection unmanned aerial vehicle of claim 4, wherein: the top of the threaded column (14) is fixedly connected with a handle (15), and anti-skid lines are arranged on the handle (15).
7. The unmanned aerial vehicle for patrolling soil resources according to claim 1, wherein: the top of the main shell (1) is provided with a heat dissipation hole (16).
8. The unmanned aerial vehicle for patrolling soil resources according to claim 1, wherein: the solar power generation assembly further comprises a controller, an inverter and a storage battery, wherein the solar panel (12) is connected with the controller, the controller is connected with the inverter, and the storage battery is respectively connected with the controller and the inverter.
9. The unmanned aerial vehicle for patrolling soil resources according to claim 1, wherein: the main shell (1) is internally provided with an avionics system, and the avionics system comprises a battery, a UBEC (universal UBEC), a flight control panel, a remote controller, a receiver, a GPS (global positioning system), a relay, a starting motor, a direct current brush and electric regulator, a Hall element, a CDI (compact disc ignition) igniter, an ECU (electronic control unit) and a steering engine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011175666.2A CN112455677A (en) | 2020-10-28 | 2020-10-28 | Unmanned aerial vehicle for patrolling national soil resources |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011175666.2A CN112455677A (en) | 2020-10-28 | 2020-10-28 | Unmanned aerial vehicle for patrolling national soil resources |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112455677A true CN112455677A (en) | 2021-03-09 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011175666.2A Pending CN112455677A (en) | 2020-10-28 | 2020-10-28 | Unmanned aerial vehicle for patrolling national soil resources |
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| Country | Link |
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| CN (1) | CN112455677A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107315423A (en) * | 2017-08-23 | 2017-11-03 | 吉林省彬生蓝航天际无人机科技有限公司 | A kind of new patrol unmanned machine inspection device and method for inspecting |
| CN107600425A (en) * | 2017-10-29 | 2018-01-19 | 成都常明信息技术有限公司 | A kind of solar energy transports unmanned plane |
| CN108820229A (en) * | 2018-06-22 | 2018-11-16 | 李帷笳 | Hybrid power unmanned plane based on computer mode control |
| CN209112436U (en) * | 2018-09-07 | 2019-07-16 | 广东诚进科技股份有限公司 | A kind of police unmanned plane big data acquisition device |
| CN211519843U (en) * | 2019-12-27 | 2020-09-18 | 杭州慧桐信息科技有限公司 | Unmanned aerial vehicle is used in wisdom city |
-
2020
- 2020-10-28 CN CN202011175666.2A patent/CN112455677A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107315423A (en) * | 2017-08-23 | 2017-11-03 | 吉林省彬生蓝航天际无人机科技有限公司 | A kind of new patrol unmanned machine inspection device and method for inspecting |
| CN107600425A (en) * | 2017-10-29 | 2018-01-19 | 成都常明信息技术有限公司 | A kind of solar energy transports unmanned plane |
| CN108820229A (en) * | 2018-06-22 | 2018-11-16 | 李帷笳 | Hybrid power unmanned plane based on computer mode control |
| CN209112436U (en) * | 2018-09-07 | 2019-07-16 | 广东诚进科技股份有限公司 | A kind of police unmanned plane big data acquisition device |
| CN211519843U (en) * | 2019-12-27 | 2020-09-18 | 杭州慧桐信息科技有限公司 | Unmanned aerial vehicle is used in wisdom city |
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Application publication date: 20210309 |