CN107123496B - 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
- CN107123496B CN107123496B CN201710405681.3A CN201710405681A CN107123496B CN 107123496 B CN107123496 B CN 107123496B CN 201710405681 A CN201710405681 A CN 201710405681A CN 107123496 B CN107123496 B CN 107123496B
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- Prior art keywords
- coiling
- gear
- clamping
- resistance
- screw rod
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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 bobbin winder device field, when work, coiling electric motor rotation drives to be rotated around line gear, it is rotated around line gear and drives coiling disk rotational, to drive the wire winding pole for being connected in coiling disk border to be rotated around wire resistor outer wall, resistive conductor to be wrapped on wire resistor, which 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 bobbin winder device 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 generally using with certain resistivity
The alloys such as nickel chromium triangle, copper-manganese be made.Insulation framework be by ceramics, plastics, apply insulating layer coating the materials such as metal be made it is tubular, flat
Shape etc. is variously-shaped.Resistance wire as needed can be one layer with coiling on skeleton, also can coiling multilayer, or use noninductive winding
Deng present invention is generally directed to the Winding Designs of tubular dielectric skeleton.
The bobbin winder device of existing resistor coiling machine generallys include transmission group and a coiling stepping horse that one connect with cursor
It reaches, transmission group is engaged by the threaded shaft of tool with thread slider and coiling stepper motor；And micro computer master control system
System, has generally included：Central processing unit, memory module, input/output interface module, when m- tally control module,
Driver module and output driver module are inputted, the relationship of above-mentioned each module is total by address bus, data/address bus and control
Line interconnects.
Although above-mentioned resistance bobbin winder device coiling effect is good, mechanism is complex, and equipment cost is higher, is not suitable for
Small Cost Management, in consideration of it, the present invention provides a kind of simple in structure, equipment cost is low, and once can be around the one of multiple resistance
Kind wire resistor automatic coiling device.
Invention content
In order to make up for the deficiencies of the prior art, it the present invention provides a kind of wire resistor automatic coiling device, compensates for
Existing resistance bobbin winder device mechanism is complex and the high disadvantage of equipment cost, provide it is a kind of it is simple in structure, equipment cost is low,
And it once can be around the resistance bobbin winder device of multiple resistance.
The technical solution adopted by the present invention to solve the technical problems is：A kind of wire resistor automatic coiling device, including
Fuselage, resistance clamping device, bobbin winder device, clamping motor and coiling electric motor, the fuselage include left supported plate and right supported plate, institute
The resistance clamping device stated is mounted on the left supported plate of fuselage, and the bobbin winder device is mounted on the right supported plate of fuselage, described
Clamping motor be located on the left of resistance clamping device, the coiling electric motor is located at bobbin winder device right side.
The resistance clamping device includes screw rod, swivel nut, rotating mechanism and clamping gear, is fixed on the left of the screw rod
On left supported plate, waist is located on the right side of screw rod, makes wire resistor when being located at the purpose of waist on the right side of screw rod
One end can penetrate resistance clamping device on the left of fuselage, and be provided with cylindrical boss, the swivel nut and spiral shell on the right side of screw rod
Bar is intermeshed, and when work, screw rod rotates so that swivel nut moves forward and backward on screw rod, the rotating mechanism be divided into left-hand rotation bar and
Right-hand rotation bar, left-hand rotation bar left end are hinged with swivel nut, and right-hand rotation bar right end 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 installed along axis there are three rotating mechanism, when work, swivel nut moves forward and backward, left-hand rotation bar and right-hand rotation bar
Around hinge mutually rotates, be sleeved on the wire resistor on the outside of screw rod be clamped and fixed from inside under the action of rotating mechanism it is motionless,
According to the difference of wire resistor internal diameter, the rotational angle of rotating mechanism is different, and the clamping gear is fixedly connected with screw rod, and presss from both sides
It holds gear to be located on the left of left supported plate, is installed with belt pulley on the left of the clamping gear, the clamping motor passes through skin
Band is connected with clamping gear, and motor is clamped and is fixedly mounted on ground by anchor (bolt) hole, when work, clamping motor rotation
The rotation of clamping tooth wheel is driven, to drive the screw rod being fixedly connected with clamping gear to rotate, and then rotating mechanism is controlled with movable snail sleeve
Movement, to achieve the purpose that clamp different inner diameters wire resistor, the effect of the resistance clamping device be by different inner diameters around
Line resistance is fixed on fuselage.
The bobbin winder device includes shaft, coiling disk, wire winding pole and the fixed peace in the middle part of line gear, the shaft
On right supported plate, and the screw coaxial heart of shaft and resistance clamping device, the center of circle phase of shaft left end face and coiling disk
Be connected, the wire winding pole is oval mast, is fixedly connected with coiling disk left side edge on the right side of wire winding pole, wire winding pole and screw rod it
Between be spaced in 20 centimetres or more, when being sleeved on screw rod so as to meet most wire resistors, wire winding pole still with coiling electricity
It is at regular intervals to hinder outer wall 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, when 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, to which resistive conductor to be wrapped on wire resistor, is fixed with around line gear on the right side of the shaft, around line gear
Right side is installed with belt pulley, and the 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, and when work, coiling electric motor rotation drives to be rotated around line gear, around line gear rotation drive around
Line disk rotational, 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, which makes of being to carry out coiling work to the wire resistor being fixed on resistance clamping device
Make.
The resistance clamping device along fuselage left supported plate at least uniformly installation there are five, and resistance clamping device with around
Line apparatus corresponds, and each be clamped between gear is intermeshed, and is respectively intermeshed between line gear, when work, a clamping
Gear rotation drives each clamping tooth wheel rotation to be sleeved on each resistance clamping device to drive each resistance clamping device to work
Wire resistor is clamped, and one drives around line gear rotation respectively around line gear rotation, to drive each bobbin winder device to work, with
Coiling work is carried out to the resistance on corresponding resistance clamping device, the purpose of above-mentioned design is to enable invention right simultaneously
Multiple resistance carry out coiling work.
The present invention rotates band movable snail sleeve using screw rod and rotates, and then clamps wire resistor, is transported around resistance using wire winding pole
Dynamic to carry out coiling, the relatively existing resistor coiling machine of the present invention is of simple structure and low cost and once can be around multiple resistance, coiling
Efficiency is preferable.
Description of the drawings
The present invention is further described with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is the structural schematic diagram of the present invention；
Fig. 2 is the structural schematic diagram of the resistance clamping device of the present invention；
Fig. 3 is the structural schematic diagram of the bobbin winder device of the present invention；
Fig. 4 is the resistance clamping device of the present invention and corresponding bobbin winder device position relationship schematic diagram；
Fig. 5 is multiple resistance clamping device dimensional structure diagrams of the present invention；
Fig. 6 is multiple bobbin winder device dimensional structure diagrams of the present invention.
In figure：Fuselage 1, resistance clamping device 2, bobbin winder device 3, clamping motor 4, coiling electric motor 5, left supported plate 11, right branch
Plate 12, swivel nut 22, rotating mechanism 23, clamping gear 24, cylindrical boss 211, left-hand rotation bar 231, right-hand rotation bar 232, turns screw rod 21
Axis 31, coiling disk 32, wire winding pole 33, around line gear 34.
Specific implementation mode
In order to make the technical means, the creative features, the aims and the efficiencies achieved by the present invention be easy to understand, tie below
Conjunction is specifically illustrating, and the present invention is further explained.
As shown in Figure 1, a kind of wire resistor automatic coiling device of the present invention, including fuselage 1, resistance clamping device
2, bobbin winder device 3, clamping motor 4 and coiling electric motor 5, the fuselage 1 include left supported plate 11 and right supported plate 12, the resistance
Clamping device 2 is mounted on the left supported plate 11 of fuselage 1, and the bobbin winder device 3 is mounted on the right supported plate 12 of fuselage 1, described
Clamping motor 4 be located at the left side of resistance clamping device 2, the coiling electric motor 5 is located on the right side of bobbin winder device 3.
As depicted in figs. 1 and 2, a kind of wire resistor automatic coiling device of the present invention, resistance clamping dress
It includes screw rod 21, swivel nut 22, rotating mechanism 23 and clamping gear 24 to set 2, and 21 left side of screw rod is fixedly mounted on left supported plate
On 11,21 right side of screw rod is located at 1 middle part of fuselage, and 21 right side of screw rod makes wire resistor one end when being located at the purpose at 1 middle part of fuselage
Resistance clamping device 2 can be penetrated from 1 left side of fuselage, and 21 right side of screw rod is provided with cylindrical boss 211, the swivel nut 22
It is intermeshed with screw rod 21, when work, screw rod 21 rotates so that swivel nut 22 moves forward and backward on screw rod 21, the rotating mechanism
23 points are left-hand rotation bar 231 and right-hand rotation bar 232, and 231 left end of left-hand rotation bar is hinged with swivel nut 22,232 right end of right-hand rotation bar and boss 211
Be hinged, and the middle part of left-hand rotation bar 231 is hinged with 232 middle part of right-hand rotation bar, and screw rod 21 uniformly install along axis there are three rotate
Mechanism 23, when work, swivel nut 22 moves forward and backward, and left-hand rotation bar 231 is mutually rotated with 232 around hinge of right-hand rotation bar, is sleeved on outside screw rod 21
The wire resistor of side be clamped and fixed from inside under the action of rotating mechanism 23 it is motionless, according to the difference of wire resistor internal diameter,
The rotational angle of rotating mechanism 23 is different, and the clamping gear 24 is fixedly connected with screw rod 21, and gear 24 is clamped and is located at left branch
11 left side of plate, 24 left side of clamping gear are installed with belt pulley, and the clamping motor 4 passes through belt and clamping tooth
Wheel 24 is connected, and motor 25 is clamped and is fixedly mounted on ground by anchor (bolt) hole, and when work, the clamping rotation of motor 4 drives
Gear 24 is clamped to rotate, to drive the screw rod 21 being fixedly connected with clamping gear 24 to rotate, and then controls and rotates with movable snail sleeve 22
The movement of mechanism 23, to achieve the purpose that clamp different inner diameters wire resistor, the effect of the resistance clamping device 2 is will be in difference
The wire resistor of diameter 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, the bobbin winder device 3 packet
It includes shaft 31, coiling disk 32, wire winding pole 33 and is fixedly mounted on right supported plate 12 in the middle part of line gear 34, the shaft 31
On, and shaft 31 and the screw rod 21 of resistance clamping device 2 are concentric, 31 left end face of shaft and the center of circle of coiling disk 32 are mutually solid
Even, the wire winding pole 33 is oval mast, and the right side of wire winding pole 33 is fixedly connected with 32 left side edge of coiling disk, wire winding pole 33 and
20 centimetres or more are spaced between screw rod 21, when being sleeved on screw rod 21 so as to meet most wire resistors, 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, 33 left side distance of wire winding pole
When work, the resistive conductor of required winding is wound in advance on wire winding pole 33 for 11 to two centimetres of 1 left supported plate of fuselage, then by around
Line bar 33 does circular-rotation around wire resistor, and to which resistive conductor to be wrapped on wire resistor, the shaft 31 is right
Side is fixed with around line gear 34, and belt pulley is installed with around 34 right side of line gear, the 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, when work, 5 turns of coiling electric motor
Dynamic drive rotates around line gear 34, is rotated around line gear 34 and coiling disk 32 is driven to rotate, and coiling disk is connected in 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 bobbin winder device 3
It makes 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, the electricity
Clamping device 2 is hindered along the left supported plate 11 of fuselage 1 at least uniformly there are five installations, and resistance clamping device 2 and bobbin winder device 3 are one by one
Corresponding, each be clamped between gear 24 is intermeshed, and is respectively intermeshed between line gear 34, when work, a clamping gear 24
Rotation drives each clamping gear 24 to rotate, and to drive each resistance clamping device 2 to work, is sleeved on each resistance clamping device 2
Wire resistor is clamped, and one drives around the rotation of line gear 34 respectively around the rotation of line gear 34, to drive 3 work of each bobbin winder device
Make, to carry out coiling work to the resistance on corresponding resistance clamping device 2, the purpose of above-mentioned design is to enable invention
Coiling work is carried out to multiple resistance simultaneously.
When work, each resistive conductor is first uniformly wrapped on the wire winding pole 33 of bobbin winder device 3 by worker, resistive conductor right-hand end
Portion fastens on wire winding pole 33, and then wire resistor is sleeved on resistance clamping device 2, and later, resistance clamping device 2 works.
When resistance clamping device 2 works, clamping motor 4, which rotates, drives clamping gear 24 to rotate, to drive and clamping tooth
The screw rod 21 that wheel 24 is fixedly connected with rotates, and the rotation band movable snail sleeve 22 of screw rod 21 moves forward and backward, and swivel nut 22 moves forward and backward so that turns left
Bar 231 is mutually rotated with 232 around hinge of right-hand rotation bar, be sleeved on the wire resistor in the outside of screw rod 21 under the action 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, is clamped with reaching
The purpose of different inner diameters wire resistor, meanwhile, a clamping rotation of gear 24 drives each clamping gear 24 to rotate, to each resistance
Clamping device 2 works to clamp wire resistor, and after clamping wire resistor, worker is by the resistive conductor left end on wire winding pole 33
Tie up to wire resistor left end.
Then, bobbin winder device 3 works, and the rotation of coiling electric motor 5 drives to be rotated around line gear 34, is rotated and is driven around line gear 34
Coiling disk 32 rotates, to drive the wire winding pole 33 for being connected in 32 edge of coiling disk to be rotated around wire resistor outer wall, with
Resistive conductor is from left to right wrapped on wire resistor, meanwhile, one respectively rotates around line gear 34 around the rotation of line gear 34 drive,
To which each bobbin winder device 3 works to carry out coiling to wire resistor.
The basic principles, main features and advantages of the 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, and the description in above embodiments and description only illustrates the present invention
Principle, without departing from the spirit and scope of the present invention, various changes and improvements may be made to the invention, these change and change
Into all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appended claims and its equivalent
It defines.
Claims (3)
1. a kind of method for winding of wire resistor automatic coiling device, which includes fuselage (1), electricity
Hinder clamping device (2), bobbin winder device (3), clamping motor (4) and coiling electric motor (5), it is characterised in that：Fuselage (1) packet
Left supported plate (11) and right supported plate (12) are included, the resistance clamping device (2) is mounted on the left supported plate (11) of fuselage (1), institute
The bobbin winder device (3) stated is mounted on the right supported plate (12) of fuselage (1), and the clamping motor (4) is located at resistance clamping device
(2) left side, the coiling electric motor (5) are located on the right side of bobbin winder device (3)；Wherein：The resistance clamping device (2) includes spiral shell
Bar (21), swivel nut (22), rotating mechanism (23) and clamping gear (24), the screw rod (21) left side are fixedly mounted on left supported plate
(11) on, it is located in the middle part of fuselage (1) on the right side of screw rod (21), and cylindrical boss (211) is provided on the right side of screw rod (21), it is described
Swivel nut (22) and screw rod (21) be intermeshed, the rotating mechanism (23) 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), and right-hand rotation bar (232) right end is hinged with boss (211), and left-hand rotation bar
(231) it is hinged in the middle part of middle part and right-hand rotation bar (232), and screw rod (21) is uniformly installed along axis there are three rotating mechanism (23),
The clamping gear (24) is fixedly connected with screw rod (21), and gear (24) is clamped and is located on the left of left supported plate (11), the folder
It holds and is installed with belt pulley on the left of gear (24), the clamping motor (4) is connected by belt with clamping gear (24),
And clamping motor (4) is fixedly mounted on ground by anchor (bolt) hole；When coiling works, coiling electric motor rotation drives around line gear
Rotation rotates around line gear and drives coiling disk rotational, to drive the wire winding pole for being connected in coiling disk border to surround coiling
Resistance outer wall rotates, and resistive conductor is wrapped on wire resistor, and the effect of the bobbin winder device is to clamp dress to being fixed on resistance
The wire resistor set carries out coiling work.
2. method for winding according to claim 1, it is characterised in that：The bobbin winder device (3) include shaft (31), around
Line disk (32), wire winding pole (33) and around line gear (34), are fixedly mounted in the middle part of the shaft (31) on right supported plate (12),
And shaft (31) and the screw rod (21) of resistance clamping device (2) are concentric, shaft (31) left end face and coiling disk (32)
The center of circle is fixedly connected with, and the wire winding pole (33) is oval mast, wire winding pole (33) right side and coiling disk (32) left side edge phase
It is connected, is fixed on the right side of (11) one to two centimetres of fuselage (1) left supported plate, the shaft (31) on the left of wire winding pole (33)
Around line gear (34), it is installed with belt pulley on the right side of line gear (34), the coiling electric motor (5) passes through belt and coiling
Gear (34) is connected, and coiling electric motor (5) is fixedly mounted on ground by anchor (bolt) hole.
3. method for winding according to claim 1, it is characterised in that：The resistance clamping device (2) is along fuselage (1)
There are five left supported plate (11) is at least uniformly installed, and resistance clamping device (2) is corresponded with bobbin winder device (3), each clamping tooth
It is intermeshed between wheel (24), 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 CN107123496A (en) | 2017-09-01 |
| CN107123496B true 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) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111462973B (en) * | 2020-05-21 | 2020-12-29 | 温州骐铭电子设备有限公司 | Resistor winding machine for electronic component |
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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104882238A (en) | 2015-09-02 |
| CN107123496A (en) | 2017-09-01 |
| 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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