CN107187584A - It is a kind of that there is the convenient unmanned plane for stopping function - Google Patents
It is a kind of that there is the convenient unmanned plane for stopping function Download PDFInfo
- Publication number
- CN107187584A CN107187584A CN201710318529.1A CN201710318529A CN107187584A CN 107187584 A CN107187584 A CN 107187584A CN 201710318529 A CN201710318529 A CN 201710318529A CN 107187584 A CN107187584 A CN 107187584A
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- Prior art keywords
- block
- unmanned plane
- sucker
- detection
- stopping function
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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)
- Mechanical Engineering (AREA)
- Toys (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
There is the convenient unmanned plane for stopping function the present invention relates to a kind of, including aviation mechanism, fuselage and support feet, PLC is additionally provided with the fuselage, stop mechanism and testing agency, the stop mechanism includes the first fixed block, first motor, Knucle-gear, bar gear, sliding bar and the first sucker, the fixed block of testing agency second, second motor, screw mandrel, the collar and detection unit, the detection unit includes the first contact block, first spring and the second contact block, there is the convenient unmanned plane for stopping function to promote the first sucker by stopping the sliding bar in mechanism for this, make the first sucker suction in vertical plane, so as to be that there is convenient unmanned function for stopping function to rest in vertical plane for this, it is operated or standby, it can detect whether stopped perpendicular is smooth by testing agency, it is easily sucker suction, so as to ensure that this has the convenient unmanned plane for stopping function safety and stability when stopping.
Description
Technical field
It is more particularly to a kind of that there is the convenient unmanned plane for stopping function the present invention relates to unmanned plane field.
Background technology
Unmanned plane is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself.From technology
Angle definition can be divided into：Unmanned fixed-wing aircraft, unmanned VTOL machine, unmanned airship, depopulated helicopter, nobody many rotors fly
Row device, unmanned parasol etc..
Unmanned plane press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane is divided into reconnaissance plane and target drone.The people
With aspect, unmanned plane+sector application is that unmanned plane has really just been needed；At present taking photo by plane, agricultural, plant protection, miniature auto heterodyne, express delivery
Transport, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, system
The application in romance etc. field is made, the purposes of unmanned plane in itself has greatly been expanded, developed country also answers in actively extension industry
With with developing unmanned air vehicle technique.
Present unmanned plane can only typically be stopped on the ground, in complicated working environment, it is impossible to which it is vertical to rest in
In plane, such as on building, so that operation is operated, and on the perpendicular of building, structure is more complicated, has
Place is uneven, is unfavorable for the stop of unmanned plane, and being stopped in unfavorable environment easily makes unmanned plane stop shakiness, or even leads
Cause air crash.
The content of the invention
The technical problem to be solved in the present invention is：In order to overcome the deficiencies in the prior art that there is convenient stop there is provided one kind
The unmanned plane of function.
The technical solution adopted for the present invention to solve the technical problems is：It is a kind of that there is the convenient unmanned plane for stopping function,
Including aviation mechanism, fuselage and support feet, PLC is additionally provided with the fuselage, mechanism and testing agency is stopped；
The stop mechanism includes the first fixed block, the first motor, Knucle-gear, bar gear, sliding bar and the first sucker, institute
State and stop the side that mechanism is arranged on fuselage, the sliding bar is horizontally disposed with, the first motor driving Knucle-gear rotation is described
Bar gear is engaged with Knucle-gear, and bar gear fixation parallel with sliding bar, first motor is fixedly installed on the first fixation
On block, first fixed block is fixedly installed on fuselage, and the sliding bar is slidably connected with the first fixed block, the sliding bar
One end penetrate the first fixed block, first sucker is fixedly installed on the one end of sliding bar away from the first fixed block, described
One sucker is vertically arranged with sliding bar；
The fixed block of testing agency second, the second motor, screw mandrel, the collar and detection unit, the testing agency are set
In fuselage provided with the side for stopping mechanism, second fixed block is fixedly installed with fuselage, and second motor is fixedly installed
On the second fixed block, the second motor drive screw rotation, the collar is provided with internal thread, the external screw thread of the screw mandrel
Matched with the internal thread of screw mandrel, the one end of the screw mandrel away from the second motor penetrates the collar, the detection unit is arranged on the collar
One end away from screw mandrel.
Preferably, in order to detect whether stopped perpendicular is smooth, the detection unit includes the first contact block, the
One spring and the second contact block, first contact block are connected by the first spring with the second contact block, and first contact block is fixedly installed
On the collar, first contact block is connected with external power source, and second contact block is electrically connected with PLC, if the detection unit has
Dry, each detection unit is arranged on side of the collar away from screw mandrel.
Second motor drive screw is rotated, and the set ring side is subjected to displacement, be arranged on detection unit on the collar with
The perpendicular detected against, each detection unit is detected to perpendicular, when each second contact block and the first contact block against
When, electric signal is sent to PLC, PLC receives the electric signal of each detection unit, the electric signal time occurred when each detection unit
When consistent, the plane for illustrating detection is smooth, when the Time Inconsistency of the transmission electric signal of each detection unit, illustrates the inspection
The plane of survey is out-of-flatness.
Preferably, in order to detect whether stopped perpendicular is smooth, the detection unit includes detection block, cunning
Block, cylinder, detection pin and second spring, the cylinder are fixedly installed with detection unit, and push rod and the sliding block of the cylinder are hinged,
The sliding block is by second spring and detection block against the detection block is provided with detect tank, and the detection pin is fixedly installed on
On sliding block, one end of the detection pin is located in detect tank, is provided with gap in detection pin and the detect tank, the detect tank with
Sliding block is be arranged in parallel, and the detect tank is electrically connected with external power source, and the detection pin is electrically connected with PLC, and the cylinder passes through electricity
Magnet valve is electrically connected with PLC.
Detection when, PLC control cylinder promote sliding block slide, detection pin is slided in detect tank, detect pin not with detection
Groove is against when slip is slided in perpendicular, if perpendicular is smooth, sliding block does not shake, and detects pin all the time not
In detect tank against, when perpendicular out-of-flatness, sliding block shakes, and makes to be fixed on the detection pin on sliding block and shakes,
So that detection pin intermittence and detect tank are against so that electric signal is occurred to PLC, it is out-of-flatness to illustrate the perpendicular
, be not suitable for stopping.
Preferably, sliding block is slided for convenience, the one end of the sliding block away from second spring is additionally provided with wheel.
Preferably, the second sucker and connecting rod are additionally provided with the adsorption capacity in order to stop mechanism, the sliding bar, it is described
Second sucker is fixedly installed by connecting rod with sliding bar, and second sucker is parallel with the first sucker.
Preferably, firmness and resistance to usability in order to improve the first sucker and the second sucker, first sucker and
The making material of second sucker is nitrile rubber.
Preferably, controlling for convenience, first motor and the second motor are servomotor.
Preferably, applying organic oil on Knucle-gear and bar gear, Knucle-gear and the bar gear to protect.
Preferably, in order to increase conductive effect, the making material of the detection pin and detection block is copper.
Preferably, in order to be subjected to displacement to the collar to guiding, gag lever post is additionally provided with the collar, the gag lever post
One end is fixedly installed with the second fixed block, and the other end of the gag lever post penetrates the collar.
The beneficial effects of the invention are as follows should be pushed away with the convenient unmanned plane for stopping function by the sliding bar stopped in mechanism
Dynamic first sucker, makes the first sucker suction in vertical plane, so as to be that there is the convenient unmanned function for stopping function to stop for this
Lean against in vertical plane, be operated or standby, can detect whether stopped perpendicular is smooth by testing agency,
It is easily sucker suction, so as to ensure that this has the convenient unmanned plane for stopping function safety and stability when stopping.
Brief description of the drawings
The present invention is further described with reference to the accompanying drawings and examples.
Fig. 1 is the structural representation with the convenient unmanned plane for stopping function of the present invention；
Fig. 2 is the structural representation of the stop mechanism with the convenient unmanned plane for stopping function of the present invention；
Fig. 3 is the structural representation of the testing agency with the convenient unmanned plane for stopping function of the present invention；
Fig. 4 is that the structure of a preferred embodiment of the detection unit with the convenient unmanned plane for stopping function of the present invention is shown
It is intended to；
Fig. 5 is the structure of another preferred embodiment of the detection unit with the convenient unmanned plane for stopping function of the present invention
Schematic diagram；
In figure：1. aviation mechanism, 2. fuselages, 3. support feets, 4. testing agencies, 5. stop mechanism, 6. first fixed blocks, 7.
Sliding bar, 8. gears, 9. Knucle-gears, 10. first motors, 11. first suckers, 12. second suckers, 13. connecting rods, 14. second
Fixed block, 15. second motors, 16. gag lever posts, 17. screw mandrels, 18. collars, 19. detection units, 20. first contact blocks, 21. first
Spring, 22. second contact blocks, 23. detection blocks, 24. detect tanks, 25. detection pins, 26. second springs, 27. cylinders, 28. sliding blocks.
Embodiment
In conjunction with the accompanying drawings, the present invention is further explained in detail.These accompanying drawings are simplified schematic diagram, only with
Illustration illustrates the basic structure of the present invention, therefore it only shows the composition relevant with the present invention.
As shown in Figure 1-Figure 3, it is a kind of that there is the convenient unmanned plane for stopping function, including aviation mechanism 1, fuselage 2 and support
PLC is additionally provided with pin 3, the fuselage 2, mechanism 5 and testing agency 4 is stopped；
The stop mechanism 5 includes the first fixed block 6, the first motor 10, Knucle-gear 9, bar gear 8, sliding bar 7 and first
Sucker 11, described to stop the side that mechanism 5 is arranged on fuselage 2, the sliding bar 7 is horizontally disposed with, and first motor 10 drives
Knucle-gear 9 is rotated, and the bar gear 8 is engaged with Knucle-gear 9, the bar gear 8 and the parallel fixation of sliding bar 7, first electricity
Machine 10 is fixedly installed on the first fixed block 6, and first fixed block 6 is fixedly installed on fuselage 2, the sliding bar 7 and
One fixed block 6 is slidably connected, and one end of the sliding bar 7 penetrates the first fixed block 6, and first sucker 11 is fixedly installed on cunning
The one end of lever 7 away from the first fixed block 6, first sucker 11 is vertically arranged with sliding bar 7；
The fixed block 14 of testing agency 4 second, the second motor 15, screw mandrel 17, the collar 18 and detection unit 19, the inspection
Survey mechanism 4 and be arranged on fuselage 2 provided with the side for stopping mechanism 5, second fixed block 14 is fixedly installed with fuselage 2, described
Second motor 15 is fixedly installed on the second fixed block 14, and the drive screw 17 of the second motor 15 rotates, on the collar 18
Provided with internal thread, the external screw thread of the screw mandrel 17 is matched with the internal thread of screw mandrel 17, and the screw mandrel 17 is away from the second motor 15
One end penetrates the collar 18, and the detection unit 19 is arranged on the one end of the collar 18 away from screw mandrel 17.
When there is the convenient unmanned plane for stopping function to need to stop for this, PLC controls the first motor 10 driving Knucle-gear 9 to revolve
Turn, because Knucle-gear 9 and bar gear 8 are engaged, the sliding bar 7 being integrally fixed on bar gear 8 is skidded off, and makes to be fixed on the principle of sliding bar 7
First sucker 11 of the one end of the first fixed block 6 is adsorbed on the perpendicular of required stop.
As shown in figure 4, preferably, in order to detect whether stopped perpendicular is smooth, the detection unit 19 is wrapped
The first contact block 20, the first spring 21 and the second contact block 22 are included, first contact block 20 passes through the first spring 21 and the second contact block 22
Connection, first contact block 20 is fixedly installed on the collar 18, and first contact block 20 is connected with external power source, and described second touches
Block 22 is electrically connected with PLC, and the detection unit 19 has several, and each detection unit 19 is arranged at the collar 18 away from screw mandrel 17
On side.
The drive screw 17 of second motor 15 is rotated, and the collar 18 is subjected to displacement to side, is arranged on the inspection on the collar 18
Unit 19 and the perpendicular detected are surveyed against each detection unit 19 is detected to perpendicular, when each second contact block 22
With the first contact block 20 against when, electric signal is sent to PLC, PLC receives the electric signal of each detection unit 19, when each detection is single
During the electric signal time consistency that member 19 occurs, the plane for illustrating detection is smooth, when the transmission electric signal of each detection unit 19
Time Inconsistency when, the plane for illustrating the detection is out-of-flatness.
As shown in figure 5, preferably, in order to detect whether stopped perpendicular is smooth, the detection unit 19 is wrapped
Detection block 23, sliding block 28, cylinder 27, detection pin 25 and second spring 26 are included, the cylinder 27 is fixedly installed with detection unit 19,
The push rod of the cylinder 27 is with sliding block 28 against the sliding block 28 is hinged by second spring 26 with detection block 23, the detection
Block 23 is provided with detect tank 24, and the detection pin 25 is fixedly installed on sliding block 28, and one end of the detection pin 25 is located at detection
In groove 24, the detection pin 25 be arranged in parallel with being provided with gap, the detect tank 24 in detect tank 24 with sliding block 28, the detection
Groove 24 is electrically connected with external power source, and the detection pin 25 is electrically connected with PLC, and the cylinder 27 is electrically connected by magnetic valve with PLC.
In detection, PLC control cylinders 27 promote sliding block 28 to slide, and detection pin 25 is slided in detect tank 24, detects pin
25 not with detect tank 24 against, slide slided in perpendicular when, if perpendicular is smooth, sliding block 28 does not shake
Dynamic, detection pin 25 is all the time not in detect tank 24 against when perpendicular out-of-flatness, sliding block 28 shakes, and makes to be fixed on cunning
Detection pin 25 on block 28 shakes, so that the detection intermittence of pin 25 and detect tank 24 are against so as to occur electric signal
To PLC, it is out-of-flatness to illustrate the perpendicular, is not suitable for stopping.
Preferably, sliding block 28 is slided for convenience, the described one end of sliding block 28 away from second spring 26 is additionally provided with wheel.
Preferably, being additionally provided with the second sucker 12 and connecting rod on the adsorption capacity in order to stop mechanism 5, the sliding bar 7
13, second sucker 12 is fixedly installed by connecting rod 13 with sliding bar 7, and second sucker 12 is parallel with the first sucker 11.
Preferably, firmness and resistance to usability in order to improve the first sucker 11 and the second sucker 12, described first inhales
The making material of the sucker 12 of disk 11 and second is nitrile rubber.
Preferably, controlling for convenience, the motor 15 of the first motor 10 and second is servomotor.
Preferably, in order to protect oiling machine oil on Knucle-gear 9 and bar gear 8, the Knucle-gear 9 and bar gear 8.
Preferably, in order to increase conductive effect, the making material of the detection pin 25 and detection block 23 is copper.
Preferably, in order to be subjected to displacement to the collar 18 to guiding, gag lever post 16, the limit are additionally provided with the collar 18
One end of position bar 16 is fixedly installed with the second fixed block 14, and the other end of the gag lever post 16 penetrates the collar 18.
Compared with prior art, it should be promoted with the convenient unmanned plane for stopping function by the sliding bar 7 stopped in mechanism 5
First sucker 11, makes the first sucker 11 adsorb in vertical plane, so as to be that this has the convenient unmanned function for stopping function
Rest in vertical plane, be operated or standby, can detect whether stopped perpendicular puts down by testing agency 4
It is whole, it is easily sucker suction, so as to ensure that this has the convenient unmanned plane for stopping function safety and stability when stopping.
Using the above-mentioned desirable embodiment according to the present invention as enlightenment, by above-mentioned description, relevant staff is complete
Various changes and amendments can be carried out without departing from the scope of the technological thought of the present invention' entirely.The technology of this invention
Property scope is not limited to the content on specification, it is necessary to its technical scope is determined according to right.
Claims (10)
1. a kind of have the convenient unmanned plane for stopping function, it is characterised in that including aviation mechanism (1), fuselage (2) and support feet
(3) PLC, is additionally provided with the fuselage (2), mechanism (5) and testing agency (4) is stopped；
The stop mechanism (5) includes the first fixed block (6), the first motor (10), Knucle-gear (9), bar gear (8), sliding bar
(7) and the first sucker (11), described to stop the side that mechanism (5) is arranged on fuselage (2), the sliding bar (7) is horizontally disposed with, institute
State the first motor (10) driving Knucle-gear (9) rotation, the bar gear (8) engages with Knucle-gear (9), the bar gear (8) and
Sliding bar (7) is parallel, and first motor (10) is fixedly installed on the first fixed block (6), and first fixed block (6) is fixed
It is arranged on fuselage (2), the sliding bar (7) is slidably connected with the first fixed block (6), one end of the sliding bar (7) is penetrated
First fixed block (6), first sucker (11) is fixedly installed on the one end of sliding bar (7) away from the first fixed block (6), described
First sucker (11) is vertically arranged with sliding bar (7)；
It is single that the testing agency (4) includes the second fixed block (14), the second motor (15), screw mandrel (17), the collar (18) and detection
First (19), the testing agency (4) is arranged on side of the fuselage (2) provided with stop mechanism (5), second fixed block (14)
It is fixedly installed with fuselage (2), second motor (15) is fixedly installed on the second fixed block (14), second motor (15)
Drive screw (17) rotates, and the collar (18) is provided with internal thread, and the external screw thread of the screw mandrel (17) is interior with screw mandrel (17)
Screw thread is matched, and the one end of the screw mandrel (17) away from the second motor (15) penetrates the collar (18), and the detection unit (19) is set
In the one end of the collar (18) away from screw mandrel (17).
2. as claimed in claim 1 have the convenient unmanned plane for stopping function, it is characterised in that detection unit (19) bag
Include the first contact block (20), the first spring (21) and the second contact block (22), first contact block (20) by the first spring (21) with
Second contact block (22) is connected, and first contact block (20) is fixedly installed on the collar (18), first contact block (20) and outside
Power supply is connected, and second contact block (22) electrically connects with PLC, and the detection unit (19) has several, each detection unit (19)
It is arranged on side of the collar (18) away from screw mandrel (17).
3. as claimed in claim 1 have the convenient unmanned plane for stopping function, it is characterised in that detection unit (19) bag
Detection block (23), sliding block (28), cylinder (27), detection pin (25) and second spring (26) are included, the cylinder (27) is single with detection
First (19) are fixedly installed, and push rod and the sliding block (28) of the cylinder (27) are hinged, and the sliding block (28) passes through second spring (26)
With detection block (23) against the detection block (23) is provided with detect tank (24), and the detection pin (25) is fixedly installed on sliding block
(28) on, one end of the detection pin (25) is located in detect tank (24), and the detection pin (25) in detect tank (24) with being provided with
Gap, the detect tank (24) is parallel with sliding block (28), and the detect tank (24) electrically connects with external power source, the detection pin
(25) electrically connected with PLC, the cylinder (27) is electrically connected by magnetic valve with PLC.
4. as claimed in claim 3 have the convenient unmanned plane for stopping function, it is characterised in that the sliding block (28) is away from the
One end of two springs (26) is additionally provided with wheel.
5. as claimed in claim 1 have the convenient unmanned plane for stopping function, it is characterised in that on the sliding bar (7) also
Provided with the second sucker (12) and connecting rod (13), second sucker (12) is fixed by connecting rod (13) and sliding bar (7), and described the
Two suckers (12) are parallel with the first sucker (11).
6. as claimed in claim 1 have the convenient unmanned plane for stopping function, it is characterised in that first sucker (11) and
The making material of second sucker (12) is nitrile rubber.
7. as claimed in claim 1 have the convenient unmanned plane for stopping function, it is characterised in that first motor (10) and
Second motor (15) is servomotor.
8. as claimed in claim 1 have the convenient unmanned plane for stopping function, it is characterised in that the Knucle-gear (9) and bar
Gear applies organic oil on (8).
9. as claimed in claim 3 have the convenient unmanned plane for stopping function, it is characterised in that the detection pin (25) and inspection
The making material for surveying block (23) is copper.
10. as claimed in claim 1 have the convenient unmanned plane for stopping function, it is characterised in that on the collar (18) also
Provided with gag lever post (16), one end and the second fixed block (14) of the gag lever post (16) are fixedly installed, the gag lever post (16)
The other end penetrates the collar (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710318529.1A CN107187584B (en) | 2017-05-08 | 2017-05-08 | Unmanned aerial vehicle with conveniently stop function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710318529.1A CN107187584B (en) | 2017-05-08 | 2017-05-08 | Unmanned aerial vehicle with conveniently stop function |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107187584A true CN107187584A (en) | 2017-09-22 |
| CN107187584B CN107187584B (en) | 2020-05-01 |
Family
ID=59874059
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710318529.1A Expired - Fee Related CN107187584B (en) | 2017-05-08 | 2017-05-08 | Unmanned aerial vehicle with conveniently stop function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107187584B (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104443391A (en) * | 2014-12-04 | 2015-03-25 | 吉林大学 | Adsorbable multifunctional micro flight device |
| CN104619591A (en) * | 2012-10-04 | 2015-05-13 | 波音公司 | Configuring landing supports for landing on uneven terrain |
| US9033276B1 (en) * | 2015-01-07 | 2015-05-19 | TLL Associates | Telescoping landing leg system |
| CN105109674A (en) * | 2015-09-14 | 2015-12-02 | 南京工程学院 | Intelligent landing bracket of multi-rotor aircraft as well as control system and method of intelligent landing bracket |
| CN205952297U (en) * | 2016-06-03 | 2017-02-15 | 全蕊 | Rotor unmanned aerial vehicle undercarriage and rotor unmanned aerial vehicle |
| CN206031790U (en) * | 2016-07-02 | 2017-03-22 | 江西联博科技有限公司 | Unmanned aerial vehicle sprinkler convenient to berth |
-
2017
- 2017-05-08 CN CN201710318529.1A patent/CN107187584B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104619591A (en) * | 2012-10-04 | 2015-05-13 | 波音公司 | Configuring landing supports for landing on uneven terrain |
| CN104443391A (en) * | 2014-12-04 | 2015-03-25 | 吉林大学 | Adsorbable multifunctional micro flight device |
| US9033276B1 (en) * | 2015-01-07 | 2015-05-19 | TLL Associates | Telescoping landing leg system |
| CN105109674A (en) * | 2015-09-14 | 2015-12-02 | 南京工程学院 | Intelligent landing bracket of multi-rotor aircraft as well as control system and method of intelligent landing bracket |
| CN205952297U (en) * | 2016-06-03 | 2017-02-15 | 全蕊 | Rotor unmanned aerial vehicle undercarriage and rotor unmanned aerial vehicle |
| CN206031790U (en) * | 2016-07-02 | 2017-03-22 | 江西联博科技有限公司 | Unmanned aerial vehicle sprinkler convenient to berth |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107187584B (en) | 2020-05-01 |
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Effective date of registration: 20200403 Address after: 430000 room 07, floor 3, building 3, international enterprise center, No.1, Guanggu Avenue, Donghu New Technology Development Zone, Wuhan City, Hubei Province (g561) Applicant after: Wuhan Aneta Technology Co.,Ltd. Address before: 518000 Guangdong city of Shenzhen province Qianhai Shenzhen Hong Kong cooperation zone before Bay Road No. 1 building 201 room A Applicant before: SHENZHEN LEILING GUANGTONG TECHNOLOGY DEVELOPMENT Co.,Ltd. |
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Effective date of registration: 20210508 Address after: Room 011-385, room 01, 6 / F, building 1, sage technology R & D center, 26 Binhu Road, Donghu New Technology Development Zone, Wuhan City, Hubei Province 430070 Patentee after: Hubei Zhenye Technology Co.,Ltd. Address before: No.07, 3rd floor, building 3, phase III, international enterprise center, special 1, Guanggu Avenue, Donghu New Technology Development Zone, Wuhan City, Hubei Province (g561) Patentee before: Wuhan Aneta Technology Co.,Ltd. |
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200501 |