CN218172617U - Be applied to unmanned aerial vehicle's land area mapping device - Google Patents

Be applied to unmanned aerial vehicle's land area mapping device Download PDF

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Publication number
CN218172617U
CN218172617U CN202222125010.0U CN202222125010U CN218172617U CN 218172617 U CN218172617 U CN 218172617U CN 202222125010 U CN202222125010 U CN 202222125010U CN 218172617 U CN218172617 U CN 218172617U
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CN
China
Prior art keywords
spacing
unmanned aerial
aerial vehicle
mapping device
fixed
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Expired - Fee Related
Application number
CN202222125010.0U
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Chinese (zh)
Inventor
张俊卿
张俊磊
魏传涛
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Mengcheng Yongshun Intelligent Technology Co ltd
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Mengcheng Yongshun Intelligent Technology Co ltd
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Priority to CN202222125010.0U priority Critical patent/CN218172617U/en
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Publication of CN218172617U publication Critical patent/CN218172617U/en
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Abstract

The utility model relates to an unmanned aerial vehicle soil survey and drawing technical field especially relates to a be applied to unmanned aerial vehicle's soil area mapping device, including the unmanned aerial vehicle body to and set up in the mapper body that is used for soil area survey and drawing in unmanned aerial vehicle body bottom, mapper body top is equipped with and is used for its fixed mounting's chucking mechanism, and chucking mechanism is including setting up respectively in mapper body both ends and with the spacing pin of unmanned aerial vehicle body fastening, and fixed the spacing post that sets up in mapper body top. The utility model discloses be favorable to carrying out the dismouting to the surveying instrument body that can be quick, user's dismouting mapping device's trouble has been reduced, this land area mapping device's practicality has been promoted, the stability of surveying instrument body installation on the unmanned aerial vehicle body has been promoted simultaneously, it is comparatively troublesome to have avoided dismouting mapping device operation on unmanned aerial vehicle, be difficult to quick dismantlement down mapping device accomodate it and unmanned aerial vehicle, install mapping device also and inconvenient problem when using unmanned aerial vehicle survey and drawing simultaneously.

Description

Be applied to unmanned aerial vehicle's land area mapping device
Technical Field
The utility model relates to an unmanned aerial vehicle land survey and drawing technical field especially relates to a be applied to unmanned aerial vehicle's land area mapping device.
Background
Unmanned aerial vehicle mapping land area that takes photo by plane, can acquire earth's surface information fast, acquire the image that has the high resolution, and then acquire more accurate data, carry out land area survey and drawing through carrying on mapping device on unmanned aerial vehicle at present, current land area mapping device is fixed on unmanned aerial vehicle through a plurality of screws for the most part, dismouting mapping device operation is comparatively troublesome on unmanned aerial vehicle, it accomodates it and unmanned aerial vehicle to be difficult to quick dismantlement, it is also inconvenient to install mapping device when using unmanned aerial vehicle survey and drawing simultaneously, great trouble has been brought for the user, the practicality is relatively poor.
SUMMERY OF THE UTILITY MODEL
Not enough to prior art, the utility model provides a be applied to unmanned aerial vehicle's land area mapping device has solved on unmanned aerial vehicle dismouting mapping device operation comparatively troublesome, is difficult to quick dismantlement down mapping device accomodate it and unmanned aerial vehicle, installs mapping device also and inconvenient technical problem when using unmanned aerial vehicle survey and drawing simultaneously, has reached the purpose that reduces the user and be not convenient for dismouting mapping device.
In order to solve the technical problem, the utility model provides a following technical scheme: a land area surveying and mapping device applied to an unmanned aerial vehicle comprises an unmanned aerial vehicle body and a surveying and mapping instrument body which is arranged at the bottom of the unmanned aerial vehicle body and used for surveying and mapping the land area, wherein a clamping mechanism used for fixedly mounting the surveying and mapping instrument body is arranged at the top of the surveying and mapping instrument body;
chucking mechanism is including setting up respectively in surveying instrument body both ends and with the fixed spacing pin of the unmanned aerial vehicle body to and fixed setting in the spacing post at surveying instrument body top, spacing capital portion is equipped with the spacing pipe of fixing with the unmanned aerial vehicle body, spacing intraductal inboard bottom is pegged graft and is had the inserted bar of fixing with spacing post, spacing socle portion is equipped with the coupling assembling that is used for connecting its and spacing post, still including setting up in the locating component that is used for fixing a position surveying instrument body in spacing pin bottom.
Furthermore, coupling assembling is including setting up in spacing post top and rather than the movable ring cover that cup joints to and the fixed spacing montant that sets up in spacing post both sides, the spacing groove of erecting with spacing montant sliding connection is seted up to movable ring cover both sides, and spacing montant top is fixed with the limit stop who is used for blockking movable ring cover.
Furthermore, a limiting ring sleeve is sleeved on the outer side of the middle part of the limiting pipe, connecting vertical plates are fixed on two sides between the movable ring sleeve and the limiting ring sleeve, and a clamping part used for clamping the limiting ring sleeve on the limiting pipe is arranged on the limiting ring sleeve.
Furthermore, the clamping part comprises arc clamping rods arranged on two sides of the outer portion of the limit ring sleeve respectively and sliding transverse rods fixedly arranged on two sides of the inner portion of each arc clamping rod, supporting arc rods fixed with the limit tubes are arranged on two sides of the bottom of each arc clamping rod, limit clamping grooves are formed in the surfaces of two sides of each limit tube, and the sliding transverse rods penetrate through one side of the limit ring sleeve and are fixedly connected with movable clamping blocks matched with the inner sides of the limit clamping grooves in a matched mode.
Furthermore, the top of the limit ring sleeve is provided with a sliding groove in sliding connection with the movable fixture block, a first spring fixed with the movable fixture block is sleeved on the outer side of the sliding cross rod, and the other end of the first spring is fixedly connected with the limit ring sleeve.
Furthermore, the positioning assembly comprises a movable stop block arranged at the bottom of the limit stop rod, a placing groove matched with the end part of the surveying instrument body is formed in one side of the movable stop block, and a sliding vertical groove is formed in the surface of the bottom of the limit stop rod.
Furthermore, the inner side of the sliding vertical groove is connected with a sliding vertical plate fixed with the movable stop block in a sliding mode, and two ends of the top of the sliding vertical plate are both fixed with a second spring of the limiting stop lever.
The utility model provides a be applied to unmanned aerial vehicle's land area mapping device possesses following beneficial effect:
1. the utility model discloses a set up chucking mechanism and come the fixed chucking of surveying instrument body on unmanned aerial vehicle body, provide spacingly for the surveying instrument body through two spacing pin, the inserted bar and the spacing pipe at spacing capital portion are pegged graft each other, be favorable to can be quick carrying out the dismouting to the surveying instrument body, convenient operation is swift, user's dismouting mapping device's trouble has been reduced, this land area mapping device's practicality has been promoted, it is comparatively troublesome to have avoided dismouting mapping device operation on unmanned aerial vehicle, it accomodates its and unmanned aerial vehicle to be difficult to quick dismantlement down mapping device, install mapping device also and inconvenient problem when using unmanned aerial vehicle survey and draw simultaneously.
2. The utility model discloses a set up spacing post that coupling assembling will cup joint each other and be connected with spacing pipe, insert spacing post to spacing intraductal, upwards stimulate spacing ring cover after that, spacing ring cover drives movable ring cover upward movement through connection riser, spacing ring cover passes through the fixed chucking of chucking and contacts with limit stop at the same time on spacing pipe, thereby be connected spacing post and spacing pipe chucking together, moreover, the steam generator is simple in structure and reasonable, the stability of installing on unmanned organism of surveying instrument body has been promoted.
3. The utility model discloses a set up locating component and fix a position the surveying instrument body between two spacing montants, surveying instrument body both ends card respectively in the standing groove of two activity dog one sides, the riser that slides simultaneously erects the inslot side in the slip and slides, and adjusts the position of activity dog to fix a position the surveying instrument body between two spacing montants, to the simple operation of surveying instrument body location, make more stable when the surveying instrument body is installed.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a partial side perspective sectional view of the present invention;
FIG. 3 is a partial front perspective sectional view of the present invention;
fig. 4 is an exploded view of the clamping mechanism of the present invention;
fig. 5 is an exploded view of the connection assembly of the present invention;
FIG. 6 is an exploded view of the positioning assembly of the present invention;
fig. 7 is an enlarged schematic view of a portion a of fig. 2 according to the present invention.
In the figure: 1. an unmanned body; 2. a surveying instrument body; 3. a chucking mechanism; 31. a limit stop lever; 32. a limiting column; 33. a limiting pipe; 34. a rod is inserted; 35. a connection assembly; 351. a movable ring sleeve; 352. a limiting vertical rod; 353. a limit stop; 354. a limiting vertical groove; 355. a position-limiting ring sleeve; 356. connecting a vertical plate; 357. a clamping part; 3571. an arc-shaped clamping rod; 3572. a sliding rail; 3573. a support arc bar; 3574. a limiting clamping groove; 3575. a movable clamping block; 3576. a first spring; 36. a positioning assembly; 361. a movable stop block; 362. a placement groove; 363. a sliding vertical slot; 364. a sliding vertical plate; 365. and a second spring.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-7, the present invention provides a technical solution: the utility model provides a be applied to unmanned aerial vehicle's land area mapping device, includes unmanned aerial vehicle body 1 to and set up in 1 bottom of unmanned aerial vehicle body and be used for surveying and mapping appearance body 2 of land area survey and drawing, 2 tops of surveying and mapping appearance body are equipped with and are used for its fixed mounting's chucking mechanism 3, and unmanned aerial vehicle body 1 and surveying and mapping appearance body 2 are technical personnel's common general knowledge in the field, do not do too much in its inner structure this scheme and describe repeatedly.
Chucking mechanism 3 is including setting up respectively in surveying instrument body 2 both ends and with the spacing pin 31 of unmanned aerial vehicle 1 fixed, and fixed the spacing post 32 that sets up in surveying instrument body 2 top, spacing post 32 top is equipped with the spacing pipe 33 fixed with unmanned aerial vehicle 1, peg graft in the inboard bottom of spacing pipe 33 has the inserted bar 34 of fixing with spacing post 32, spacing pipe 33 bottom sets up to the same with the diameter of spacing post 32, when the inserted bar 34 cover at spacing post 32 top is established in spacing pipe 33, spacing pipe 33 and spacing post 32 contact each other, spacing pipe 33 bottom is equipped with the coupling assembling 35 that is used for connecting it with spacing post 32, still including setting up in the locating component 36 that is used for fixing a position surveying instrument body 2 in spacing pin 31 bottom.
Chucking mechanism 3 is used for fixing chucking with surveying instrument body 2 on unmanned aerial vehicle body 1, when fixing a position surveying instrument body 2 through locating component 36, coupling assembling 35 is in the same place the inserted bar 34 at spacing post 32 top and spacing pipe 33 are pegged graft each other, be favorable to can be quick carrying out the dismouting to surveying instrument body 2, user's dismouting mapping device's trouble has been reduced, the stability of surveying instrument body 2 installation on unmanned aerial vehicle body 1 has been promoted simultaneously.
Specifically, the positioning component 36 includes a movable stopper 361 disposed at the bottom of the limit stop lever 31, a placement groove 362 disposed on one side of the movable stopper 361 and matched with the end of the surveying instrument body 2, a sliding vertical groove 363 disposed on the bottom surface of the limit stop lever 31, a sliding vertical plate 364 fixed to the movable stopper 361 and slidably connected to the inner side of the sliding vertical groove 363, a second spring 365 fixed to the limit stop lever 31 and disposed at both ends of the top of the sliding vertical plate 364, when the surveying instrument body 2 is positioned, the movable stopper 361 is pulled downwards, the sliding vertical plate 364 drives the sliding vertical plate 364 to move downwards in the sliding vertical groove 363, one end of the sliding vertical plate 364 is pulled downwards, the second spring 365 generates elastic deformation and is stretched, then, the two ends of the surveying instrument body 2 are respectively disposed at the inner sides of the placement grooves 362 on one side of the two movable stoppers 361, and simultaneously, the insertion rod 34 disposed at the top of the limit post 32 on the surveying instrument body 2 is located at the bottom of the limit tube 33, and then the movable stopper 361 is released, the surveying instrument body 2 pushes the surveying instrument body 2 to move upwards, and the insertion rod 34 disposed at the top of the limit post 32 is inserted into the limit tube 33.
Specifically, coupling assembling 35 is including setting up in spacing post 32 top and rather than the activity ring cover 351 that cup joints, and fixed the spacing montant 352 that sets up in spacing post 32 both sides, activity ring cover 351 both sides are seted up with spacing montant 352 sliding connection's spacing vertical slot 354, activity ring cover 351 slides more stably in the spacing montant 352 outside, spacing montant 352 top is fixed with the limit stop 353 who is used for blockking activity ring cover 351, spacing pipe 33 middle part outside has cup jointed spacing ring cover 355, both sides all are fixed with connection riser 356 between activity ring cover 351 and the spacing ring cover 355, be provided with on spacing ring cover 355 and be used for its chucking part 357 on spacing pipe 33.
Specifically, the clamping portion 357 includes arc-shaped clamping rods 3571 respectively disposed at two sides of an outer portion of the position-limiting ring sleeve 355, the two arc-shaped clamping rods 3571 are matched with the position-limiting ring sleeve 355, and sliding cross rods 3572 fixedly disposed at two sides of an inner portion of the arc-shaped clamping rods 3571, supporting arc rods 3573 fixed to the position-limiting tube 33 are disposed at two sides of a bottom of the arc-shaped clamping rods 3571, position-limiting clamping grooves 3574 are disposed on two side surfaces of the position-limiting tube 33, the sliding cross rods 3572 penetrate through one side of the position-limiting ring sleeve 355 and are fixedly connected with movable clamping blocks 3575 matched with an inner side of the position-limiting clamping grooves 3574, an arc surface disposed at one side of the movable clamping blocks 3575 is matched with an outer side of the position-limiting tube 33, a sliding groove slidably connected with the movable clamping blocks 3575 is disposed at a top of the position-limiting ring sleeve 355, a spring 3576 fixed to the movable clamping block 3575 is sleeved at an outer side of the sliding cross rod 3572, and another end of the spring 3576 is fixedly connected with the position-limiting ring sleeve 355.
In this embodiment, when the surveying instrument body 2 is installed on the unmanned aerial vehicle 1, the surveying instrument body 2 is first positioned, the movable stopper 361 is pulled downwards, the movable stopper 361 drives the sliding vertical plate 364 at the top of the movable stopper 361 to move downwards, the sliding vertical plate 364 moves downwards in the sliding vertical groove 363, the sliding vertical plate 364 pulls one end of the spring 365 downwards, the spring 365 is stretched due to elastic deformation, then the two ends of the surveying instrument body 2 are respectively placed inside the placing grooves 362 at one sides of the two movable stoppers 361, meanwhile, the inserting rod 34 at the top of the limiting column 32 on the surveying instrument body 2 is positioned at the bottom of the limiting tube 33, then the movable stopper 361 is released, the movable stopper 361 pushes the surveying instrument body 2 to move upwards, and the surveying instrument body 2 pushes the inserting rod 34 at the top of the limiting column 32 to be inserted into the limiting tube 33;
then, the position-limiting ring sleeve 355 is pulled upwards, the position-limiting ring sleeve 355 drives the connecting vertical plate 356 to move upwards, the connecting vertical plate 356 drives the movable ring sleeve 351 to move upwards outside the position-limiting vertical rod 352, the top of the movable ring sleeve 351 is in contact with the position-limiting stop 353, meanwhile, the position-limiting ring sleeve 355 drives the movable clamping block 3575 to move upwards, when the movable clamping block 3575 moves to be matched with the position-limiting clamping groove 3574, the first spring 3576 restores elastic deformation to push the movable clamping block 3575 to slide on the inner side of the sliding groove, the movable clamping block 3575 enters the position-limiting clamping groove 3574, the position-limiting ring sleeve 355 is fixedly clamped on the position-limiting pipe 33, the movable clamping block 3575 pulls the sliding cross rod 3572 to move, the sliding cross rod 3572 pulls the arc-shaped clamping rods 3571 to move, the two arc-shaped clamping rods 3571 move towards the middle simultaneously, the two arc-shaped clamping rods 3571 respectively move to two sides of the position-limiting ring sleeve 355 and are in contact with the supporting arc-rods 3573 at the bottom of the position-limiting pipe 33, so that the position-limiting column 32 and the surveying instrument body 2 are fixedly installed on the unmanned machine body 1;
when the surveying instrument body 2 needs to be detached from the unmanned aerial vehicle body 1, the two arc-shaped clamping rods 3571 are respectively pulled towards two sides, the two arc-shaped clamping rods 3571 respectively move towards two sides of the limit ring sleeve 355, the arc-shaped clamping rods 3571 pull the sliding cross rod 3572 to move, the sliding cross rod 3572 drives the movable clamping block 3575 to move out of the limit clamping groove 3574, the movable clamping block 3575 extrudes the first spring 3576, the first spring 3576 generates elastic deformation and is compressed, then the limit ring sleeve 355 is pulled downwards, the limit ring sleeve 355 drives the connecting vertical plate 356 to move downwards, the connecting vertical plate 356 drives the movable ring sleeve 351 to move downwards outside the limit vertical rod 352, the top of the movable ring sleeve 351 is far away from the limit stop 353, and meanwhile, the limit ring sleeve 355 drives the movable clamping rods to move downwards outside the limit pipe 33 until the limit ring sleeve 355 completely moves onto the limit post 32;
then pull down movable stop 361 again, movable stop 361 drives the slip riser 364 of its top to move down, slip riser 364 is in the downward motion of slip vertical slot 363, slip riser 364 pulls down spring two 365 one end, spring two 365 produces elastic deformation and is stretched, surveying instrument body 2 is the downward motion simultaneously, when the inserted bar 34 of the spacing post 32 top on surveying instrument body 2 comes out from spacing pipe 33 completely, rotate certain angle with surveying instrument body 2, surveying instrument body 2 both ends respectively with two movable stop 361 one side standing groove 362 emergence separation, dismantle the separation from two movable stop 361 with surveying instrument body 2.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (7)

1. The utility model provides a be applied to unmanned aerial vehicle's land area mapping device, includes unmanned aerial vehicle body (1) to and set up in surveying instrument body (2) that are used for land area survey and drawing in unmanned aerial vehicle body (1) bottom, its characterized in that: the top of the surveying instrument body (2) is provided with a clamping mechanism (3) for fixedly mounting the surveying instrument body;
chucking mechanism (3) including set up respectively in surveying instrument body (2) both ends and with the fixed spacing pin (31) of the unmanned aerial vehicle body (1), and fixed set up in spacing post (32) at surveying instrument body (2) top, spacing post (32) top is equipped with spacing pipe (33) fixed with the unmanned aerial vehicle body (1), peg graft in spacing pipe (33) inboard bottom has inserted bar (34) fixed with spacing post (32), spacing pipe (33) bottom is equipped with coupling assembling (35) that are used for connecting its and spacing post (32), still including setting up in locating component (36) that spacing pin (31) bottom is used for fixing a position surveying instrument body (2).
2. A land area mapping device applied to unmanned aerial vehicles according to claim 1, characterized in that: coupling assembling (35) including set up in spacing post (32) top and rather than activity ring cover (351) that cup joints to and fixed the spacing montant (352) that set up in spacing post (32) both sides, activity ring cover (351) both sides are seted up with spacing montant (352) sliding connection's spacing vertical groove (354), and spacing montant (352) top is fixed with limit stop (353) that are used for blockking activity ring cover (351).
3. Land area surveying and mapping device applied to unmanned aerial vehicles according to claim 2, characterized in that: the limiting ring sleeve (355) is sleeved on the outer side of the middle of the limiting pipe (33), a connecting vertical plate (356) is fixed on each of two sides between the movable ring sleeve (351) and the limiting ring sleeve (355), and a clamping part (357) used for clamping the limiting ring sleeve (355) on the limiting pipe (33) is arranged on the limiting ring sleeve (355).
4. A land area mapping device applied to unmanned aerial vehicles according to claim 3, characterized in that: chucking portion (357) including set up arc kelly (3571) in spacing ring cover (355) outside both sides respectively to and fixed sliding cross bar (3572) that set up in arc kelly (3571) inside both sides, arc kelly (3571) bottom both sides all are equipped with support arc pole (3573) fixed with spacing pipe (33), spacing draw-in groove (3574) have all been seted up on spacing pipe (33) both sides surface, and sliding cross bar (3572) run through spacing ring cover (355) one side and spacing draw-in groove (3574) inboard assorted activity fixture block (3575) fixed connection.
5. A land area mapping device applied to unmanned aerial vehicles according to claim 4, characterized in that: the top of the limit ring sleeve (355) is provided with a sliding groove in sliding connection with the movable clamping block (3575), the outer side of the sliding cross bar (3572) is sleeved with a first spring (3576) fixed with the movable clamping block (3575), and the other end of the first spring (3576) is fixedly connected with the limit ring sleeve (355).
6. A land area mapping device applied to unmanned aerial vehicles according to claim 1, characterized in that: locating component (36) is including setting up in activity dog (361) of spacing pin (31) bottom, and activity dog (361) one side is seted up with surveying instrument body (2) tip assorted standing groove (362), and the perpendicular groove of slip (363) has been seted up on spacing pin (31) bottom surface.
7. A land area mapping device applied to unmanned aerial vehicles according to claim 6, characterized in that: the inner side of the sliding vertical groove (363) is connected with a sliding vertical plate (364) fixed with a movable stop block (361) in a sliding mode, and two ends of the top of the sliding vertical plate (364) are both fixed with a second spring (365) used for limiting the stop lever (31).
CN202222125010.0U 2022-08-12 2022-08-12 Be applied to unmanned aerial vehicle's land area mapping device Expired - Fee Related CN218172617U (en)

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Application Number Priority Date Filing Date Title
CN202222125010.0U CN218172617U (en) 2022-08-12 2022-08-12 Be applied to unmanned aerial vehicle's land area mapping device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202222125010.0U CN218172617U (en) 2022-08-12 2022-08-12 Be applied to unmanned aerial vehicle's land area mapping device

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CN218172617U true CN218172617U (en) 2022-12-30

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CN202222125010.0U Expired - Fee Related CN218172617U (en) 2022-08-12 2022-08-12 Be applied to unmanned aerial vehicle's land area mapping device

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116443288A (en) * 2023-05-08 2023-07-18 杭州东网电力科技有限公司 Unmanned aerial vehicle for land area mapping

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116443288A (en) * 2023-05-08 2023-07-18 杭州东网电力科技有限公司 Unmanned aerial vehicle for land area mapping

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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20221230

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