CN107123496A - A kind of method for winding of wire resistor automatic coiling device - Google Patents
A kind of method for winding of wire resistor automatic coiling device Download PDFInfo
- Publication number
- CN107123496A CN107123496A CN201710405681.3A CN201710405681A CN107123496A CN 107123496 A CN107123496 A CN 107123496A CN 201710405681 A CN201710405681 A CN 201710405681A CN 107123496 A CN107123496 A CN 107123496A
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- Prior art keywords
- coiling
- clamping
- screw rod
- resistance
- wire
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01C—RESISTORS
- H01C17/00—Apparatus or processes specially adapted for manufacturing resistors
- H01C17/04—Apparatus or processes specially adapted for manufacturing resistors adapted for winding the resistive element
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- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Coil Winding Methods And Apparatuses (AREA)
- Hand Tools For Fitting Together And Separating, Or Other Hand Tools (AREA)
Abstract
The present invention relates to the method for winding in resistance Winder field, during work, coiling electric motor, which is rotated, drives coiling pinion rotation, coiling pinion rotation drives coiling disk rotational, so as to drive the wire winding pole for being connected in coiling disk border to be rotated around wire resistor outer wall, so that resistive conductor is wrapped on wire resistor, the Winder makes of being to carry out coiling work to the wire resistor being fixed on resistance clamping device.
Description
Technical field
The present invention relates to resistance Winder field, specifically a kind of wire resistor automatic coiling device.
Background technology
Wirewound resistor is constituted with resistance filament winding in insulation framework.Resistance wire is typically using the nickel with certain resistivity
The alloys such as chromium, copper-manganese are made.Insulation framework is that tubular, flat etc. is made by the material such as ceramics, plastics, the metal for applying insulating layer coating
It is variously-shaped.Resistance wire as needed can be one layer with coiling on skeleton, also can coiling multilayer, or using noninductive winding etc., this
Winding Design of the invention mainly for tubular dielectric skeleton.
The Winder of existing resistor coiling machine, generallys include a transmission group being connected with cursor and a coiling stepping horse
Reach, transmission group is engaged by the threaded axostylus axostyle of tool with thread slider and coiling stepper motor；And micro computer master control system
System, has been generally included：CPU, memory module, input/output interface module, when m- tally control module,
Driver module and output driver module are inputted, the relation of above-mentioned each module is total by address bus, data/address bus and control
Line, is interconnected.
Although above-mentioned resistance Winder coiling effect is good, mechanism is complex, and equipment cost is higher, is not suitable for
Small Cost Management, in consideration of it, the invention provides one kind it is simple in construction, equipment cost is low, and once can be around the one of multiple resistance
Plant wire resistor automatic coiling device.
The content of the invention
In order to make up the deficiencies in the prior art, the invention provides a kind of wire resistor automatic coiling device, it compensate for existing
Resistance Winder mechanism is complex and the high shortcoming of equipment cost is there is provided a kind of simple in construction, equipment cost is low, and one
It is secondary can around multiple resistance resistance Winder.
The technical solution adopted for the present invention to solve the technical problems is：A kind of wire resistor automatic coiling device, including
Fuselage, resistance clamping device, Winder, clamping motor and coiling electric motor, described fuselage include left supported plate and right supported plate, institute
The resistance clamping device stated is arranged on the left supported plate of fuselage, and described Winder is arranged on the right supported plate of fuselage, described
Clamping motor be located on the left of resistance clamping device, described coiling electric motor is located on the right side of Winder.
Described resistance clamping device includes fixed on the left of screw rod, swivel nut, rotating mechanism and clamping gear, described screw rod
Cause wire resistor when being located at the purpose for being located at waist on the right side of waist, screw rod on left supported plate, on the right side of screw rod
One end can penetrate on the right side of resistance clamping device, and screw rod on the left of fuselage and be provided with cylindrical boss, described swivel nut and spiral shell
Bar be intermeshed, during work, screw rod rotate cause swivel nut moved forward and backward on screw rod, described rotating mechanism be divided into left-hand rotation bar and
Right-hand rotation bar, left-hand rotation bar left end is hinged with swivel nut, and right-hand rotation bar right-hand member is hinged with boss, and in the middle part of left-hand rotation bar and in the middle part of right-hand rotation bar
It is hinged, and screw rod is uniformly provided with three rotating mechanisms along axis, during work, swivel nut is moved forward and backward, left-hand rotation bar and right-hand rotation bar
Around hinge is mutually rotated, be enclosed on the wire resistor on the outside of screw rod be clamped and fixed in the presence of rotating mechanism from inside it is motionless,
According to the difference of wire resistor internal diameter, the rotational angle of rotating mechanism is different, and described clamping gear is fixedly connected with screw rod, and folder
Gear is held on the left of left supported plate, belt pulley is installed with the left of described clamping gear, described clamping motor passes through skin
Band is connected with clamping gear, and clamping motor is fixedly mounted on ground by anchor (bolt) hole, during work, and clamping motor is rotated
Clamping pinion rotation is driven, so as to drive the screw rod being fixedly connected with clamping gear to rotate, and then rotating mechanism is controlled with movable snail sleeve
Motion, to reach the purpose for clamping different inner diameters wire resistor, the effect of the resistance clamping device be by different inner diameters around
Line resistance is fixed on fuselage.
Described Winder includes rotating shaft, coiling disk, wire winding pole and the fixed peace in the middle part of line gear, described rotating shaft
On right supported plate, and rotating shaft and the screw coaxial heart of resistance clamping device, rotating shaft left end face and the center of circle phase of coiling disk
Be connected, described wire winding pole is to be fixedly connected with the right side of oval mast, wire winding pole with coiling disk left side edge, wire winding pole and screw rod it
Between be spaced in more than 20 centimetres, when being enclosed on so as to meet most wire resistors on screw rod, wire winding pole still with coiling electricity
Hinder outer wall at regular intervals so that wire winding pole can carry out next step coiling work, on the left of wire winding pole apart from fuselage left supported plate one to
Two centimetres, during work, the resistive conductor of required winding is wound on wire winding pole in advance, then by wire winding pole around wire resistor
Circular-rotation is done, so that resistive conductor is wrapped on wire resistor, is fixed with the right side of described rotating shaft around line gear, around line gear
Right side is installed with belt pulley, and described coiling electric motor is connected by belt with around line gear, and coiling electric motor passes through ground
Bolt holes are fixedly mounted on ground, during work, coiling electric motor rotate drive coiling pinion rotation, coiling pinion rotation drive around
Line disk rotational, so as to drive the wire winding pole for being connected in coiling disk border to be rotated around wire resistor outer wall, by resistive conductor
It is wrapped on wire resistor, the Winder makes of being to carry out coiling work to the wire resistor being fixed on resistance clamping device
Make.
Left supported plate of the described resistance clamping device along fuselage is at least uniformly provided with five, and resistance clamping device with around
Line apparatus is corresponded, and is intermeshed, is respectively intermeshed between line gear between each clamping gear, during work, a clamping
Pinion rotation drives each clamping pinion rotation, so as to drive each resistance clamping device to work, is enclosed on each resistance clamping device
Wire resistor is clamped, and a coiling pinion rotation drives each coiling pinion rotation, so that drive each Winder to work, with
Coiling work is carried out to the resistance on corresponding resistance clamping device, the purpose of above-mentioned design is so that invention can be simultaneously right
Multiple resistance carry out coiling work.
The present invention is rotated using screw rod rotational band movable snail sleeve, and then clamps wire resistor, is transported using wire winding pole around resistance
Dynamic to carry out coiling, the relatively existing resistor coiling machine of the present invention is simple in construction, with low cost and once can be around multiple resistance, coiling
Efficiency is preferable.
Brief description of the drawings
The present invention is further described with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is the structural representation of the present invention；
Fig. 2 is the structural representation of the resistance clamping device of the present invention；
Fig. 3 is the structural representation of the Winder of the present invention；
Fig. 4 is the resistance clamping device and corresponding Winder position relationship schematic diagram of the present invention；
Fig. 5 is multiple resistance clamping device dimensional structure diagrams of the present invention；
Fig. 6 is multiple Winder dimensional structure diagrams of the present invention.
In figure：Fuselage 1, resistance clamping device 2, Winder 3, clamping motor 4, coiling electric motor 5, left supported plate 11, right branch
Plate 12, screw rod 21, swivel nut 22, rotating mechanism 23, clamping gear 24, cylindrical boss 211, left-hand rotation bar 231, right-hand rotation bar 232, turn
Axle 31, coiling disk 32, wire winding pole 33, around line gear 34.
Embodiment
In order that the technical means, the inventive features, the objects and the advantages of the present invention are easy to understand, with reference to tool
Body is illustrated, and the present invention is expanded on further.
As shown in figure 1, a kind of wire resistor automatic coiling device of the present invention, including fuselage 1, resistance clamping device
2nd, Winder 3, clamping motor 4 and coiling electric motor 5, described fuselage 1 include left supported plate 11 and right supported plate 12, described resistance
Clamping device 2 is arranged on the left supported plate 11 of fuselage 1, and described Winder 3 is arranged on the right supported plate 12 of fuselage 1, described
Clamping motor 4 be located at the left side of resistance clamping device 2, described coiling electric motor 5 is located at the right side of Winder 3.
As depicted in figs. 1 and 2, a kind of wire resistor automatic coiling device of the present invention, described resistance clamping dress
Putting 2 includes screw rod 21, swivel nut 22, rotating mechanism 23 and clamping gear 24, and the described left side of screw rod 21 is fixedly mounted on left supported plate
On 11, the right side of screw rod 21 is located at the middle part of fuselage 1, and the right side of screw rod 21 causes wire resistor one end when being located at the purpose at the middle part of fuselage 1
Resistance clamping device 2 can be penetrated from the left side of fuselage 1, and the right side of screw rod 21 is provided with cylindrical boss 211, described swivel nut 22
It is intermeshed with screw rod 21, during work, screw rod 21, which is rotated, causes swivel nut 22 to be moved forward and backward on screw rod 21, described rotating mechanism
23 points are left-hand rotation bar 231 and right-hand rotation bar 232, and the left end of left-hand rotation bar 231 is hinged with swivel nut 22, the right-hand member of right-hand rotation bar 232 and boss 211
It is hinged, and the middle part of left-hand rotation bar 231 is hinged with the middle part of right-hand rotation bar 232, and screw rod 21 is uniformly provided with three rotations along axis
Mechanism 23, during work, swivel nut 22 is moved forward and backward, and left-hand rotation bar 231 is mutually rotated with the around hinge of right-hand rotation bar 232, is enclosed on outside screw rod 21
The wire resistor of side be clamped and fixed in the presence of rotating mechanism 23 from inside it is motionless, according to the difference of wire resistor internal diameter,
The rotational angle of rotating mechanism 23 is different, and described clamping gear 24 is fixedly connected with screw rod 21, and clamping gear 24 is located at left branch
The left side of plate 11, the described left side of clamping gear 24 is installed with belt pulley, and described clamping motor 4 passes through belt and clamping tooth
Wheel 24 is connected, and clamping motor 25 is fixedly mounted on ground by anchor (bolt) hole, during work, and clamping motor 4, which is rotated, to be driven
Clamping gear 24 is rotated, so as to drive the screw rod 21 being fixedly connected with clamping gear 24 to rotate, and then controls rotation with movable snail sleeve 22
The motion of mechanism 23, to reach the purpose for clamping different inner diameters wire resistor, the effect of the resistance clamping device 2 is by difference
The wire resistor in footpath is fixed on the fuselage 1.
As shown in figures 1 and 3, a kind of wire resistor automatic coiling device of the present invention, described Winder 3 is wrapped
Include rotating shaft 31, coiling disk 32, wire winding pole 33 and be fixedly mounted on right supported plate 12 in the middle part of line gear 34, described rotating shaft 31
On, and rotating shaft 31 and the screw rod 21 of resistance clamping device 2 are concentric, the left end face of rotating shaft 31 and the center of circle of coiling disk 32 are mutually solid
Even, described wire winding pole 33 is oval mast, and the right side of wire winding pole 33 is fixedly connected with the left side edge of coiling disk 32, wire winding pole 33 and
More than 20 centimetres are spaced between screw rod 21, when being enclosed on so as to meet most wire resistors on screw rod 21, wire winding pole
33 is still at regular intervals with wire resistor outer wall so that wire winding pole can carry out next step coiling work, the left side distance of wire winding pole 33
11 one to two centimetres of 1 left supported plate of fuselage, during work, the resistive conductor of required winding is wound on wire winding pole 33 in advance, then by around
Line bar 33 does circular-rotation around wire resistor, so that resistive conductor is wrapped on wire resistor, described rotating shaft 31 is right
Side is fixed with around line gear 34, and belt pulley is installed with around the right side of line gear 34, described coiling electric motor 35 by belt with
It is connected around line gear 34, and coiling electric motor 35 is fixedly mounted on ground by anchor (bolt) hole, during work, 5 turns of coiling electric motor
Dynamic drive rotates around line gear 34, is rotated around line gear 34 and drives coiling disk 32 to rotate, coiling disk is connected in so as to drive
The wire winding pole 33 at 32 edges is rotated around wire resistor outer wall, and resistive conductor is wrapped on wire resistor, the Winder 3
Make of being to carry out coiling work to the wire resistor being fixed on resistance clamping device 2.
As shown in Fig. 1, Fig. 4, Fig. 5 and Fig. 6, a kind of wire resistor automatic coiling device of the present invention, described electricity
Hinder left supported plate 11 of the clamping device 2 along fuselage 1 and be at least uniformly provided with five, and resistance clamping device 2 and Winder 3 are one by one
It is intermeshed, is respectively intermeshed between line gear 34 between correspondence, each clamping gear 24, during work, a clamping gear 24
Rotate and drive each clamping gear 24 to rotate, so as to drive each resistance clamping device 2 to work, be enclosed on each resistance clamping device 2
Wire resistor is clamped, and one rotates drive around line gear 34 and respectively rotated around line gear 34, so as to drive each work of Winder 3
Make, to carry out coiling work to the resistance on corresponding resistance clamping device 2, the purpose of above-mentioned design is so that invention can
Coiling work is carried out to multiple resistance simultaneously.
During work, each resistive conductor is first uniformly wrapped on the wire winding pole 33 of Winder 3 by workman, resistive conductor right-hand end
Portion is fastened on wire winding pole 33, and then wire resistor is enclosed on resistance clamping device 2, afterwards, and resistance clamping device 2 works.
When resistance clamping device 2 works, clamping motor 4, which is rotated, drives clamping tooth wheel 24 to rotate, so as to drive and clamping tooth
The screw rods 21 that are fixedly connected with of wheel 24 are rotated, the rotational band movable snail sleeve 22 of screw rod 21 is moved forward and backward, and swivel nut 22 is moved forward and backward so that turned left
Bar 231 is mutually rotated with the around hinge of right-hand rotation bar 232, be enclosed on the wire resistor in the outside of screw rod 21 in the presence of rotating mechanism 23 from
Inside is clamped and fixed motionless, and according to the difference of wire resistor internal diameter, the rotational angle of rotating mechanism 23 is different, to reach clamping
The purpose of different inner diameters wire resistor, meanwhile, a clamping gear 24, which is rotated, drives each clamping gear 24 to rotate, so that each resistance
Clamping device 2 works to clamp wire resistor, clamps after wire resistor, and workman is by the resistive conductor left end on wire winding pole 33
Tie up to wire resistor left end.
Then, Winder 3 works, and coiling electric motor 5, which is rotated, drives coiling gear 34 to rotate, and rotates and drives around line gear 34
Coiling disk 32 is rotated, so that drive the wire winding pole 33 for being connected in the edge of coiling disk 32 to be rotated around wire resistor outer wall, with
Resistive conductor is from left to right wrapped on wire resistor, meanwhile, one rotates drive around line gear 34 and is respectively rotated around line gear 34,
So as to which each Winder 3 works to carry out coiling to wire resistor.
The basic principles, principal features and advantages of the present invention have been shown and described above.The technical staff of the industry should
Understand, the present invention is not limited to the above embodiments, the simply explanation present invention of the description in above-described embodiment and specification
Principle, without departing from the spirit and scope of the present invention, various changes and modifications of the present invention are possible, and these change and changed
Enter all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appended claims and its equivalent
Define.
Claims (4)
1. a kind of method for winding of wire resistor automatic coiling device, during work, coiling electric motor, which is rotated, drives coiling pinion rotation,
Coiling pinion rotation drives coiling disk rotational, and the wire winding pole of coiling disk border is connected in outside wire resistor so as to drive
Wall is rotated, and resistive conductor is wrapped on wire resistor, and the Winder makes of being to being fixed on resistance clamping device
Wire resistor carries out coiling work.
2. method for winding according to claim 1, the wire resistor automatic coiling device includes fuselage (1), resistance and clamped
Device (2), Winder (3), clamping motor (4) and coiling electric motor (5), it is characterised in that：Described fuselage (1) includes left branch
Plate (11) and right supported plate (12), described resistance clamping device (2) are arranged on the left supported plate (11) of fuselage (1), it is described around
Line apparatus (3) is arranged on the right supported plate (12) of fuselage (1), and it is left that described clamping motor (4) is located at resistance clamping device (2)
Side, described coiling electric motor (5) is located on the right side of Winder (3)；Wherein：
Described resistance clamping device (2) includes screw rod (21), swivel nut (22), rotating mechanism (23) and clamping gear (24), institute
It is fixedly mounted on left supported plate (11), is located on the right side of screw rod (21) in the middle part of fuselage (1) on the left of the screw rod (21) stated, and screw rod (21)
Right side is provided with cylindrical boss (211), and described swivel nut (22) is intermeshed with screw rod (21), described rotating mechanism (23)
It is divided into left-hand rotation bar (231) and right-hand rotation bar (232), left-hand rotation bar (231) left end is hinged with swivel nut (22), right-hand rotation bar (232) right-hand member
It is hinged with boss (211), and with being hinged in the middle part of right-hand rotation bar (232) in the middle part of left-hand rotation bar (231), and screw rod (21) is equal along axis
Even to be provided with three rotating mechanisms (23), described clamping gear (24) is fixedly connected with screw rod (21), and clamping gear (24) position
On the left of left supported plate (11), belt pulley is installed with the left of described clamping gear (24), described clamping motor (4) passes through
Belt is connected with clamping gear (24), and clamping motor (4) is fixedly mounted on ground by anchor (bolt) hole.
3. method for winding according to claim 2, it is characterised in that：Described Winder (3) include rotating shaft (31), around
Line disk (32), wire winding pole (33) and around line gear (34), are fixedly mounted on right supported plate (12) in the middle part of described rotating shaft (31),
And rotating shaft (31) and the screw rod (21) of resistance clamping device (2) are concentric, rotating shaft (31) left end face and coiling disk (32)
The center of circle is fixedly connected with, and described wire winding pole (33) is oval mast, wire winding pole (33) right side and coiling disk (32) left side edge phase
Gu, be even fixed with the left of wire winding pole (33) on the right side of (11) one to two centimetres of fuselage (1) left supported plate, described rotating shaft (31) around
Line gear (34), is installed with belt pulley, described coiling electric motor (5) passes through belt and coiling tooth on the right side of line gear (34)
Wheel (34) is connected, and coiling electric motor (5) is fixedly mounted on ground by anchor (bolt) hole.
4. method for winding according to claim 2, it is characterised in that：Described resistance clamping device (2) is along fuselage (1)
Left supported plate (11) is at least uniformly provided with five, and resistance clamping device (2) is corresponded with Winder (3), each clamping tooth
Intermeshing between (24) is taken turns, is respectively intermeshed between line gear (34).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710405681.3A CN107123496B (en) | 2015-05-01 | 2015-05-01 | A kind of method for winding of wire resistor automatic coiling device |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510218789.2A CN104882238B (en) | 2015-05-01 | 2015-05-01 | A kind of wire resistor automatic coiling device |
| CN201710405681.3A CN107123496B (en) | 2015-05-01 | 2015-05-01 | A kind of method for winding of wire resistor automatic coiling device |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510218789.2A Division CN104882238B (en) | 2015-05-01 | 2015-05-01 | A kind of wire resistor automatic coiling device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107123496A true CN107123496A (en) | 2017-09-01 |
| CN107123496B CN107123496B (en) | 2018-09-18 |
Family
ID=53949701
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510218789.2A Active CN104882238B (en) | 2015-05-01 | 2015-05-01 | A kind of wire resistor automatic coiling device |
| CN201710405681.3A Expired - Fee Related CN107123496B (en) | 2015-05-01 | 2015-05-01 | A kind of method for winding of wire resistor automatic coiling device |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510218789.2A Active CN104882238B (en) | 2015-05-01 | 2015-05-01 | A kind of wire resistor automatic coiling device |
Country Status (1)
| Country | Link |
|---|---|
| CN (2) | CN104882238B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2021183353A (en) * | 2020-05-21 | 2021-12-02 | 潘文橋 | Resistor copper wire winding machine for electronic part |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0590015A (en) * | 1991-09-27 | 1993-04-09 | Mitsunori Yokoyama | Automatic resistance-wire winding machine |
| CN201369200Y (en) * | 2008-11-18 | 2009-12-23 | 成都承宏机电有限公司 | Precision parallel winding machine |
| CN201590297U (en) * | 2009-12-31 | 2010-09-22 | 刘德鸿 | Coaxial winding device of high-pressure ignition wire core |
| CN102915817A (en) * | 2012-10-30 | 2013-02-06 | 深圳市华力特电气股份有限公司 | Automatic assembling equipment for cylindrical helical spring-like resistor element |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5806782A (en) * | 1997-06-13 | 1998-09-15 | U Gear Automatic Machinery Co., Ltd. | Double track wire arranging device for winding machines |
| CN202678015U (en) * | 2012-06-01 | 2013-01-16 | 张家港市泓溢电源科技有限公司 | Coiling device for special resistor board |
| CN203644489U (en) * | 2013-10-18 | 2014-06-11 | 蚌埠市微欧电子科技有限责任公司 | Novel resistor winder |
| CN204695896U (en) * | 2015-05-01 | 2015-10-07 | 安庆安星电气有限公司 | A kind of wire resistor automatic coiling device |
-
2015
- 2015-05-01 CN CN201510218789.2A patent/CN104882238B/en active Active
- 2015-05-01 CN CN201710405681.3A patent/CN107123496B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0590015A (en) * | 1991-09-27 | 1993-04-09 | Mitsunori Yokoyama | Automatic resistance-wire winding machine |
| CN201369200Y (en) * | 2008-11-18 | 2009-12-23 | 成都承宏机电有限公司 | Precision parallel winding machine |
| CN201590297U (en) * | 2009-12-31 | 2010-09-22 | 刘德鸿 | Coaxial winding device of high-pressure ignition wire core |
| CN102915817A (en) * | 2012-10-30 | 2013-02-06 | 深圳市华力特电气股份有限公司 | Automatic assembling equipment for cylindrical helical spring-like resistor element |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2021183353A (en) * | 2020-05-21 | 2021-12-02 | 潘文橋 | Resistor copper wire winding machine for electronic part |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104882238A (en) | 2015-09-02 |
| CN107123496B (en) | 2018-09-18 |
| CN104882238B (en) | 2017-07-07 |
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Effective date of registration: 20180806 Address after: 362000 Fujian Quanzhou economic development Chong min street 4 hatching base complex building 4. Applicant after: Fujian Baiyun Power Technology Co., Ltd. Address before: 246001 37 Hu Xin Road, Anqing, Anhui Applicant before: He Hongchang |
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Granted publication date: 20180918 Termination date: 20210501 |