CN107745813B - A kind of quadrotor drone control of intelligent terminal - Google Patents
A kind of quadrotor drone control of intelligent terminal Download PDFInfo
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- CN107745813B CN107745813B CN201710951003.7A CN201710951003A CN107745813B CN 107745813 B CN107745813 B CN 107745813B CN 201710951003 A CN201710951003 A CN 201710951003A CN 107745813 B CN107745813 B CN 107745813B
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- shell
- fixedly connected
- pedestal
- bevel gear
- idler wheel
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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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of quadrotor drone control of intelligent terminal, including shell and pedestal, the shell is located at the upper end of pedestal, the top of the shell is equipped with fan, and the inside of shell is equipped with controlling terminal, the both ends of the controlling terminal bottom are welded with stabilizer blade, the lower end of the stabilizer blade is equipped with threaded hole, running through in the threaded hole has stud, the lower end of the stud is fixedly connected with first bevel gear, the downside of the first bevel gear is equipped with screw rod, the second bevel gear and third hand tap gear engaged is wanted with first bevel gear on the screw rod, one end of the screw rod is fixedly connected with flywheel, the interior bottom of the shell is equipped with fluting, the fluting is equipped with dirt filtrating screen, one end of the dust filtration net is equipped with pushing block, one end of the pushing block and dirt filtrating screen offsets.Structure of the invention is novel, solves the problem of that unmanned aerial vehicle (UAV) control terminal is difficult to adapt to the manipulation of multi-environment operation while solving unmanned plane influenced and operational shock noise by dust.
Description
Technical field
The present invention relates to air vehicle technique field more particularly to a kind of quadrotor drone control of intelligent terminal.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer.With someone
It drives an airplane and compares, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Unmanned plane presses application field,
Can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+industrial application are
Unmanned plane has really just needed；It taking photo by plane at present, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observing wild move
The application in object, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, greatly
The big purposes for having expanded unmanned plane itself, developed country also in actively extension industrial application and develop unmanned air vehicle technique.Nobody
Machine belongs to emerging technology, high-new frontier science and technology industry.With the development of science and technology, unmanned plane is applied in addition to military use, civilian
Field is also more and more wide, has been successfully applied to that video display take photo by plane, survey and draw aerial survey, high-voltage line inspection, long-range monitoring, the disaster relief are rescued
It helps, pesticide spraying, the commercially fields such as performance.And current unmanned plane is to realize the important portion of aerial photography function in addition to itself overall structure
Exceptionally, the technology of ground control segment is also very crucial, and can it is related to unmanned plane normally realize aerial photography function, normal
It makes a return voyage, therefore is also the core of unmanned plane research now, unmanned aerial vehicle (UAV) control terminal is led by dust invasion in the prior art
Fluctuation of service is caused the problem of element fault occur, while generating biggish vibration and noise when controlling terminal operating also to lead to zero
Component service life is reduced, and it is multi-party to cope with to the adjusting of height that last unmanned aerial vehicle (UAV) control terminal can adapt to multi-environment manipulation
Face purposes demand is also the existing difficulty for needing to solve.
Summary of the invention
The purpose of the present invention is to solve disadvantages existing in the prior art, and a kind of quadrotor drone intelligence proposed
It can control terminal.
To achieve the goals above, present invention employs following technical solutions: a kind of quadrotor drone intelligent control is whole
End, including shell and pedestal, the shell are located at the upper end of pedestal, and the top of the shell is equipped with fan, and the inside of shell
Equipped with controlling terminal, the both ends of the controlling terminal bottom are welded with stabilizer blade, and the lower end of the stabilizer blade is equipped with threaded hole, the spiral shell
Through there is stud in pit, the lower end of the stud is fixedly connected with first bevel gear, and the downside of the first bevel gear is equipped with
Screw rod wants the second bevel gear engaged and third hand tap gear with first bevel gear on the screw rod, and one end of the screw rod is fixed
It is connected with flywheel, the interior bottom of the shell is equipped with fluting, and the fluting is equipped with dirt filtrating screen, and one end of the dust filtration net is equipped with
One end of pushing block, the pushing block and dirt filtrating screen offsets, and pushing block is fixedly connected with pull rod, the pull rod far from one end of dirt filtrating screen
One end far from pushing block is equipped with pull ring, and the outer sheath of pull rod is equipped with the first spring, and the lower end of the shell is fixedly connected with ox
Muscle wheel, the housing bottom are rotatably connected to set square far from one end of Cowhells wheel, and the set square is far from the diagonal equal of shell
It is fixedly connected with idler wheel, pedestal position corresponding with idler wheel is equipped with arcwall face, and the idler wheel offsets with arcwall face, described
The inside of pedestal is fixedly connected with fixed block, and the fixed block is fixedly connected with telescopic rod close to one end of idler wheel, described flexible
Bar is fixedly connected with limited block far from one end of fixed block, and the outer sheath of the telescopic rod is equipped with second spring, the pedestal
Lower end is fixedly connected with walking mechanism.
Preferably, the interior bottom symmetrical of the shell is fixedly connected there are two right angle frame, the upper end of two right angle frames
It is fixedly connected with the inner sidewall of shell, and the lower end of two right angle frames is fixedly connected with the interior bottom of shell.
Preferably, the inside of the shell is fixedly connected with support plate, and axle sleeve is equipped between the support plate and right angle frame,
The axle sleeve is set in the outside of stud.
Preferably, the fixed block is equipped with air bag far from the side of telescopic rod, and the outer sheath of the air bag is equipped with rubber
The lower end of gum cover, the rubber sleeve is fixedly connected with pedestal, and the upside of rubber sleeve and the lower end of shell offset.
Preferably, the telescopic rod is fixedly connected with rubber stopper close to one end of idler wheel, and the rubber stopper offsets with idler wheel.
Preferably, the walking mechanism is universal wheel.
In the present invention, user when using the device, shakes flywheel as needed first, and flywheel drives screw rod rotation.
Second bevel gear and third hand tap gear engagement in rotation a pair of first bevel gears on screw rod, first bevel gear rotates upper stud at this time
Rotation, stud are rotated in the inside of right angle frame and axle sleeve, while in the threaded hole of the stabilizer blade of controlling terminal, make controlling terminal
Stabilizer blade moves on stud, adjusts and arrives proper height, can open controlling terminal running, open simultaneously fan, fan by air-flow from
The inner upper end of shell is blown downwards, and the intracorporal dust impurity of shell is precipitated by air motion moving at dirt filtrating screen at this time, by
Noise and vibration can be generated when the running of unmanned aerial vehicle (UAV) control terminal, the device of a variety of comprehensive vibration and noise reducings is designed on pedestal, works as shell
When body is operated vibration by controlling terminal, idler wheel can roll on the arc inner wall of pedestal with vibration, when idler wheel scrolls down through, squeeze
When pressing the rubber stopper on telescopic rod, second spring absorbs vibration force and compressive deformation, while the release when idler wheel moves upwards occurs
Potential energy guarantees the vibration weakening of shell, and the Cowhells wheel on right side and air bag absorb by elastic bearing and weaken the vibration of shell
It is dynamic, and the walking mechanism of pedestal lower end is universal wheel, facilitate controlling terminal position is freely rotated control adjustment convenient for operation.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of quadrotor drone control of intelligent terminal proposed by the present invention.
In figure: 1 fan, 2 shells, 3 controlling terminals, 4 stabilizer blades, 5 studs, 6 axle sleeves, 7 right angle frames, 8 third hand tap gears, 9 fly
Wheel, 10 pushing blocks, 11 pull rods, 12 first springs, 13 rubber sleeves, 14 air bags, 15 Cowhells wheels, 16 pedestals, 17 first bevel gears, 18
Second bevel gear, 19 screw rods, 20 dirt filtrating screens, 21 set squares, 22 idler wheels, 23 walking mechanisms, 24 rubber stoppers, 25 limited blocks, 26
Two springs, 27 telescopic rods, 28 fixed blocks.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.
Referring to Fig.1, a kind of quadrotor drone control of intelligent terminal, including shell 2 and pedestal 16, shell 2 are located at pedestal
The top of 16 upper end, shell 2 is equipped with fan 1, to blow the impurity dust bin bottom in shell 2, guarantees controlling terminal 3
Appearance there is no a dust attachment, and the inside of shell 2 is equipped with controlling terminal 3, and the both ends of 3 bottom of controlling terminal are welded with stabilizer blade 4,
The lower end of stabilizer blade 4 is equipped with threaded hole, and running through in threaded hole has stud 5, and the lower end of stud 5 is fixedly connected with first bevel gear 17,
The downside of first bevel gear 17 is equipped with screw rod 19, wants the second bevel gear 18 engaged and third with first bevel gear 17 on screw rod 19
Bevel gear 8, one end of screw rod 19 are fixedly connected with flywheel 9, and to constitute the mechanism of 3 height adjustment of controlling terminal, flywheel 9 is driven
Screw rod 19 rotates.Second bevel gear 18 on screw rod 19 and 8 engagement in rotation a pair of first bevel gears 17 of third hand tap gear, at this time the
One bevel gear 17 rotates upper stud 5 and rotates, and stud 5 is in the inside of right angle frame 7 and axle sleeve 6, while in the stabilizer blade of controlling terminal 34
Threaded hole in rotation, move the stabilizer blade 4 of controlling terminal 3 on stud 5, adjust arrive proper height, the interior bottom of shell 2 is set
There is fluting, fluting is equipped with dirt filtrating screen 20, and to the dust magazine in assembling supporting member 2, one end of the dust filtration net 20, which is equipped with, to be pushed away
Block 10, to dirt filtrating screen 20 easy to disassemble and install, convenient replacement in time, pushing block 10 and one end of dirt filtrating screen 20 offset, and push away
Block 10 is fixedly connected with pull rod 11 far from one end of dirt filtrating screen 20, and pull rod 11 is equipped with pull ring, and pull rod far from one end of pushing block 10
11 outer sheath is equipped with the first spring 12, pulls the pull ring on pull rod 11, and pushing block 10 is subjected to displacement, detachable dirt filtrating screen 20, together
When the first spring 12 pushing block 10 can be made to reset, the lower end of shell 2 is fixedly connected with Cowhells wheel 15, and 2 bottom of shell is far from Cowhells
One end of wheel 15 is rotatably connected to set square 21, and set square 21 is diagonally fixedly connected to idler wheel 22, pedestal 16 far from shell 2
Position corresponding with idler wheel 22 is equipped with arcwall face, and idler wheel 22 offsets with arcwall face, and the inside of pedestal 16 is fixedly connected with fixation
Block 28, fixed block 28 are fixedly connected with telescopic rod 27 close to one end of idler wheel 22, and the one end of telescopic rod 27 far from fixed block 28 is solid
Surely it is connected with limited block 25, the outer sheath of telescopic rod 27 is equipped with second spring 26, and the lower end of pedestal 16 is fixedly connected with vehicle with walking machine
Structure 23, to be moved easily and adjust the position of controlling terminal 3 so as to multi-environment operation.
In the present invention, the interior bottom symmetrical of shell 2 is fixedly connected there are two right angle frame 7, the upper end of two right angle frames 7 and shell
The inner sidewall of body 2 is fixedly connected, and the lower end of two right angle frames 7 is fixedly connected with the interior bottom of shell 2, to fix and support
The controlling terminal 3 of upper end, while the elements such as stud 5 are limited and supported, the inside of shell 2 is fixedly connected with support plate,
Axle sleeve 6 is equipped between support plate and right angle frame 7, axle sleeve 6 is set in the outside of stud 5, to protect stud 5, rotates in stud 5
When, it is not influencing to avoid the position of stud 5 from shifting while stud 5 rotates, it can not be quasi- when leading to device height adjustment
Really in time, fixed block 28 is equipped with air bag 14 far from the side of telescopic rod 27, and the outer sheath of air bag 14 is equipped with rubber sleeve 13, rubber
The lower end of gum cover 13 is fixedly connected with pedestal 16, and the upside of rubber sleeve 13 and the lower end of shell 2 offset, to for 16 He of pedestal
Resilient support is provided between shell 2, guarantees to generate vibration drive 2 synchronous vibrating of shell when controlling terminal 3 operates, and air bag 14
When shell 2 is oppressed downwards, absorption pressure generates elastic deformation, and elastic potential energy is discharged when shell shifts up, entire elasticity shape
The process of change reduces and absorbs the Oscillation Amplitude and shockproofness of shell 2, and rubber sleeve 13 fixes air bag 14
There is provided elastic bearing simultaneously for shell 2, telescopic rod 27 is fixedly connected with rubber stopper 24 close to one end of idler wheel 22, rubber stopper 24 with
Idler wheel 22 offsets, and when shell 2 is operated by controlling terminal 3 to be vibrated, idler wheel 22 can roll on the arc inner wall of pedestal 16 with vibration
Dynamic, when idler wheel 22 scrolls down through, when squeezing the rubber stopper 24 on telescopic rod 27, second spring 27 absorbs vibration force and compresses
Deformation, while potential energy is discharged when idler wheel 22 moves upwards, guarantee the vibration weakening of shell 2, walking mechanism 23 is universal wheel, is used
To be moved easily and adjust the position of controlling terminal 3 so as to multi-environment operation.
In the present invention, user when using the device, shakes flywheel 9 as needed first, and flywheel 9 drives 19 turns of screw rod
It is dynamic.Second bevel gear 18 on screw rod 19 and 8 engagement in rotation a pair of first bevel gears 17 of third hand tap gear, at this time first bevel gear
17 rotation upper studs 5 rotate, and stud 5 is in the inside of right angle frame 7 and axle sleeve 6, while in the threaded hole of the stabilizer blade of controlling terminal 34
Interior rotation moves the stabilizer blade 4 of controlling terminal 3 on stud 5, adjusts and arrives proper height, can open the running of controlling terminal 3, together
When open fan 1, fan 1 blows downwards air-flow from the inner upper end of shell 2, and the dust impurity in shell 2 is by air-flow at this time
Movement is precipitated moving at dirt filtrating screen 21, due to that can generate noise and vibration, pedestal 16 when unmanned aerial vehicle (UAV) control terminal 3 operates
The device of the upper a variety of comprehensive vibration and noise reducings of design, when shell 2 is operated by controlling terminal 3 to be vibrated, idler wheel 22 can be with vibration the bottom of at
It is rolled on the arc inner wall of seat 16, when idler wheel 22 scrolls down through, when squeezing the rubber stopper 24 on telescopic rod 27, second spring 27
It absorbs vibration force and compressive deformation occurs, while discharging potential energy when idler wheel 22 moves upwards, guarantee the vibration weakening of shell 2, and
The Cowhells wheel 15 and air bag 14 on right side are absorbed by elastic bearing and the vibration of decrease shell 2, and the walking of 16 lower end of pedestal
Mechanism 23 is universal wheel, and facilitate 3 position of controlling terminal is freely rotated control adjustment convenient for operation.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto,
Anyone skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (6)
1. a kind of quadrotor drone control of intelligent terminal, including shell (2) and pedestal (16), which is characterized in that the shell
(2) it is located at the upper end of pedestal (16), the top of the shell (2) is equipped with fan (1), and the inside of shell (2) is equipped with control eventually
It holds (3), the both ends of controlling terminal (3) bottom are welded with stabilizer blade (4), and the lower end of the stabilizer blade (4) is equipped with threaded hole, described
Through having stud (5) in threaded hole, the lower end of the stud (5) is fixedly connected with first bevel gear (17), the first cone tooth
The downside for taking turns (17) is equipped with screw rod (19), wants the second bevel gear (18) engaged with first bevel gear (17) on the screw rod (19)
It is fixedly connected with flywheel (9) with one end of third hand tap gear (8), the screw rod (19), the interior bottom of the shell (2), which is equipped with, opens
Slot, the fluting are equipped with dirt filtrating screen (20), and one end of the dust filtration net (20) is equipped with pushing block (10), the pushing block (10) and filter
One end of dirt net (20) offsets, and pushing block (10) is fixedly connected with pull rod (11), the pull rod far from the one end of dirt filtrating screen (20)
(11) one end far from pushing block (10) is equipped with pull ring, and the outer sheath of pull rod (11) is equipped with the first spring (12), the shell (2)
Lower end be fixedly connected with Cowhells wheel (15), shell (2) bottom is rotatably connected to triangle far from one end of Cowhells wheel (15)
Plate (21), the set square (21) are diagonally fixedly connected to idler wheel (22) far from shell (2), the pedestal (16) and idler wheel
(22) corresponding position is equipped with arcwall face, and the idler wheel (22) offsets with arcwall face, and the inside of the pedestal (16) is fixed to be connected
It is connected to fixed block (28), the fixed block (28) is fixedly connected with telescopic rod (27) close to the one end of idler wheel (22), described flexible
Bar (27) is fixedly connected with limited block (25) far from the one end of fixed block (28), and the outer sheath of the telescopic rod (27) is equipped with second
The lower end of spring (26), the pedestal (16) is fixedly connected with walking mechanism (23).
2. a kind of quadrotor drone control of intelligent terminal according to claim 1, which is characterized in that the shell (2)
Interior bottom symmetrical be fixedly connected there are two right angle frame (7), the upper end of two right angle frames (7) and the inner sidewall of shell (2)
It is fixedly connected, and the lower end of two right angle frames (7) is fixedly connected with the interior bottom of shell (2).
3. a kind of quadrotor drone control of intelligent terminal according to claim 1, which is characterized in that the shell (2)
Inside be fixedly connected with support plate, be equipped with axle sleeve (6) between the support plate and right angle frame (7), the axle sleeve (6) is set in
The outside of stud (5).
4. a kind of quadrotor drone control of intelligent terminal according to claim 1, which is characterized in that the fixed block
(28) side far from telescopic rod (27) is equipped with air bag (14), and the outer sheath of the air bag (14) is equipped with rubber sleeve (13),
The lower end of the rubber sleeve (13) is fixedly connected with pedestal (16), and the upside of rubber sleeve (13) and the lower end of shell (2) offset.
5. a kind of quadrotor drone control of intelligent terminal according to claim 1, which is characterized in that the telescopic rod
(27) one end close to idler wheel (22) is fixedly connected with rubber stopper (24), and the rubber stopper (24) offsets with idler wheel (22).
6. a kind of quadrotor drone control of intelligent terminal according to claim 1, which is characterized in that the walking mechanism
It (23) is universal wheel.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910813347.0A CN110654537B (en) | 2017-10-13 | 2017-10-13 | Four rotor unmanned aerial vehicle intelligent control terminals |
| CN201710951003.7A CN107745813B (en) | 2017-10-13 | 2017-10-13 | A kind of quadrotor drone control of intelligent terminal |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710951003.7A CN107745813B (en) | 2017-10-13 | 2017-10-13 | A kind of quadrotor drone control of intelligent terminal |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910813347.0A Division CN110654537B (en) | 2017-10-13 | 2017-10-13 | Four rotor unmanned aerial vehicle intelligent control terminals |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107745813A CN107745813A (en) | 2018-03-02 |
| CN107745813B true CN107745813B (en) | 2019-08-02 |
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Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910813347.0A Active CN110654537B (en) | 2017-10-13 | 2017-10-13 | Four rotor unmanned aerial vehicle intelligent control terminals |
| CN201710951003.7A Active CN107745813B (en) | 2017-10-13 | 2017-10-13 | A kind of quadrotor drone control of intelligent terminal |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910813347.0A Active CN110654537B (en) | 2017-10-13 | 2017-10-13 | Four rotor unmanned aerial vehicle intelligent control terminals |
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| CN (2) | CN110654537B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111587021B (en) * | 2020-05-09 | 2021-07-30 | 骏沣联锐商务咨询(深圳)有限公司 | Base of electric power marketing and distribution business data synchronization equipment |
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| CN105620731B (en) * | 2016-01-06 | 2019-03-05 | 北京臻迪机器人有限公司 | A kind of unmanned aerial vehicle (UAV) control method and unmanned aerial vehicle control system |
| CN105700548A (en) * | 2016-01-20 | 2016-06-22 | 杭州米为科技有限公司 | Unmanned plane and unmanned plane control method |
| KR101796193B1 (en) * | 2016-02-24 | 2017-11-09 | 제주한라대학교산학협력단 | System and method for tracking position using drone |
| CN206057972U (en) * | 2016-09-19 | 2017-03-29 | 高域（北京）智能科技研究院有限公司 | For controlling the control terminal and its unmanned aerial vehicle control system of unmanned vehicle |
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- 2017-10-13 CN CN201710951003.7A patent/CN107745813B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204421204U (en) * | 2014-12-26 | 2015-06-24 | 湛江通用电气有限公司 | A kind of air cleaning unit |
| CN104991478A (en) * | 2015-08-04 | 2015-10-21 | 安徽泽众安全科技有限公司 | Unmanned aerial vehicle handheld portable control terminal |
| CN205405270U (en) * | 2016-03-07 | 2016-07-27 | 魏燕鸿 | Main control system for unmanned aerial vehicle |
| CN205831320U (en) * | 2016-06-28 | 2016-12-28 | 马仁贵 | A kind of outdoor multifunctional operation command case |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN110654537B (en) | 2021-05-28 |
| CN110654537A (en) | 2020-01-07 |
| CN107745813A (en) | 2018-03-02 |
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Effective date of registration: 20201218 Address after: Room 107, no.379 Pingshan Avenue, Yufeng District, Liuzhou City, Guangxi Zhuang Autonomous Region Patentee after: Xu Jinlan Address before: 211100 two, B unit 300, Zhihui Road, Kirin science and Technology Innovation Park, Jiangning District, Nanjing, Jiangsu. Patentee before: NANJING HANXIYUE AUTOMATION TECHNOLOGY Co.,Ltd. |
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