CN206604971U - A kind of braid material cutting machine - Google Patents
A kind of braid material cutting machine Download PDFInfo
- Publication number
- CN206604971U CN206604971U CN201720002569.0U CN201720002569U CN206604971U CN 206604971 U CN206604971 U CN 206604971U CN 201720002569 U CN201720002569 U CN 201720002569U CN 206604971 U CN206604971 U CN 206604971U
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- CN
- China
- Prior art keywords
- braid
- fuselage
- knife
- cutting
- baffle plate
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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.)
- Expired - Fee Related
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Abstract
The technical solution of the utility model is a kind of braid material cutting machine, including fuselage, cutting structure, charging-discharging structure, control structure, braid input channel, scrap belt output channel are provided with fuselage, charging-discharging structure is arranged on the left side of fuselage, control structure is arranged on the right side of fuselage, and cutting structure is arranged between charging-discharging structure and control structure；The side of charging-discharging structure is set to feed end, the opposite side of charging-discharging structure is set to discharge end, braid input channel sequentially passes through control structure, cutting structure and connected with feed end, scrap belt output channel sequentially passes through control structure, cutting structure and connected with discharge end, the guide frame being connected with braid input channel is provided with outside fuselage, fuselage is provided with disassembly and assembly structure close to the side of control structure.The beneficial effects of the utility model are：Cut after can component be positioned from volume material strip, be fixed on component and cut for carrying out grafting after the accurate pickup of inserter on position, the fitness with inserter is high.
Description
Technical field
The utility model is related to plug-in unit cutting technique field, the high braid material cutting of more particularly to a kind of automaticity
Machine.
Background technology
Inserter, automatic (also crying " the automatism card machine ") study plot of some well-regulated electronic components is inserted into
Plant equipment in printed circuit board conductive through hole.The unit of special trimming electronic component pin can be set in inserter,
Shape and length electronic component pin to be cut to standard.And the defect that prior art is present is：Braid material is entering
In the presence of discharging structure unit blanking structure unit, blanking structure list are reached by material guide structure unit by airframe structure unit
After member positioning cut-out, resupply other plug-in component machines and be used in conjunction with, such structure setting on the one hand can be by component shape difference
Different limitation, when inserter pickup carries out plug-in unit, the accurate pickup of inserter is influenceed due to the difference of shape, so that
The quality of automatic insertion is influenceed, on the other hand, pin and braid need separately to be cut, complex procedures, it would therefore be highly desirable to a kind of
Braid material cutting machine can not be limited by component shape difference and that the accurate pickup of plug-in unit part can be coordinated.
Utility model content
The technical problem that the utility model is solved is to provide a kind of braid material cutting machine, can expect component from volume
Cut after taking positioning one by one, and component is fixed on and cut for carrying out grafting after the accurate pickup of inserter on position,
Fitness with inserter is high.
The technical solution of the utility model is：It is provided with and cuts on a kind of braid material cutting machine, including fuselage, the fuselage
Structure, charging-discharging structure, control structure, braid input channel, scrap belt output channel, the charging-discharging structure are arranged on fuselage
Left side, the control structure is arranged on the right side of fuselage, the cutting structure be arranged on charging-discharging structure and control structure it
Between；The side of the charging-discharging structure is set to feed end, and the opposite side of the charging-discharging structure is set to discharge end, the volume
Band input channel sequentially passes through control structure, cutting structure and connected with feed end, and the scrap belt output channel sequentially passes through behaviour
Control structure, cutting structure are connected with discharge end, and the guide frame being connected with braid input channel is provided with outside the fuselage, described
Fuselage is provided with disassembly and assembly structure close to the side of control structure.
Preferably, the charging-discharging structure includes workbench, be provided with the workbench rotating disk and
The press material structure coordinated with rotating disk, the workbench is arranged with outside the stepper motor of driving rotating disk rotation, the rotating disk
Annular array is provided with some bayonet locks on the wall of side；The press material structure includes fixed block and binder block A, the fixed block and binder
By some axis of guide A connections between block A, the outer surface of some axis of guide A is arranged with spring A；The binder block A with
The relative one side of rotating disk is provided with the arc-shaped concave matched with rotating disk.
Preferably, the cutting structure includes base, the cylinder being fixed on base, side and cylinder connection
Knife rest, be fixed on the binder block C being equipped with base with knife rest, the base and be provided with guide rail, the knife rest it is another
Side bottom is provided with the sliding block being slidably connected with guide rail；The top of the knife rest is provided with activity above cutting knife, the cutting knife and set
Binder block B is equipped with, the cutting knife is connected with binder block B by axis of guide B, the outer surface of the axis of guide B is arranged with spring B,
The cutting knife is set to edge of a knife position towards the side of braid input channel, and binder block B positions corresponding with edge of a knife position are set
There is binder projection；The binder block C is provided with the seal face corresponding with binder projection, the seal face close to the side of knife rest
Lower section be provided with and cut space for what edge of a knife position entered, the binder projection and binder block C distance are less than edge of a knife position and pressure
Expect block C distance.
Preferably, the control structure includes control button and the supply unit being connected with control button.
Preferably, the braid input channel is by being disposed in parallel in fuselage side baffle plate A corresponding with feed end
With baffle plate B compositions.
Preferably, the scrap belt output channel is by being disposed in parallel in fuselage side baffle plate corresponding with discharge end
C and baffle plate D compositions.
Preferably, the disassembly and assembly structure includes extending to the control lever of fuselage upper surface, extends to fuselage following table
The lock catch arm in face, the inverted U fixed seat that fuselage bottom is connected with lock catch arm is fixed on, passed through between the control lever and lock catch arm
Gangbar is connected, and the control lever is connected by one end of rotating shaft A and gangbar, and the other end of the gangbar passes through rotating shaft B
It is connected with one end of lock catch arm；The other end of the lock catch arm is connected by rotating shaft C with inverted U fixed seat；The lock catch arm
Afterbody is provided with matrix and fastens position；The fuselage includes upper cover plate and lower cover, upper cover plate position corresponding with control lever
Stopper slot A is offered, lower cover position corresponding with lock catch arm is provided with stopper slot B；The upper cover plate is tied close to manipulation
The position of structure is provided with handle.
Preferably, the guide frame includes roller and the baffle plate E and baffle plate that are connected respectively with roller two ends
F, the afterbody of the baffle plate E and baffle plate F are progressive to come closer to form the braid entrance corresponding with braid input channel；It is described to lead
It is connected to structure by L-type stator with fuselage.
Compared with prior art, set cutting structure that the pin of component is cut to needed for inserter into length simultaneously on fuselage
And the component cut is fixed on to the position cut for inserter progress pickup, so as to avoid due to the difference of component shape
Accurate pickup problem that is different and influenceing inserter, so that it is guaranteed that the quality of automatic insertion；Band disassembly and assembly structure, makes the utility model easy
In assembly and disassembly, so that convenient use cooperatively from different inserters；By charging-discharging structure, make braid material with the side of stepping
Formula is moved to cutting structure and cut, and in a stepping manner exports scrap belt；Guide frame is set, enables braid material
Putting position is enough adjusted, is entered in an orderly manner in braid input channel.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the structural solid figure of fuselage open mode.
Fig. 3 is the three-dimensional view of charging-discharging structure.
Fig. 4 is the three-dimensional view of cutting structure.
Fig. 5 is the three-dimensional view for removing cutting structure after binder block C.
Fig. 6 is the sectional view of cutting structure.
Fig. 7 is the structure chart of disassembly and assembly structure.
Fig. 8 is the front view of disassembly and assembly structure.
Fig. 9 is the structural representation of guide frame.
In figure：Fuselage 1, charging-discharging structure 2, cutting structure 3, control structure 4, braid input channel 5, scrap belt output are logical
Road 6, guide frame 7, disassembly and assembly structure 8, handle 9, upper cover plate 10, lower cover 11, stopper slot A12, stopper slot B13, press material structure
210th, bayonet lock 20, rotating disk 21, binder block A22, fixed block 23, arc-shaped concave 24, axis of guide A25, spring A26, stepper motor 27,
Cylinder 30, base 31, guide rail 32, sliding block 33, knife rest 34, cutting knife 35, spring B 36, axis of guide B37, binder block B38, binder block
C39, seal face 301, edge of a knife position 302, binder projection 303, roller 71, baffle plate E72, baffle plate F73, L-type stator 74, braid enter
Mouth 75, control lever 80, gangbar 81, lock catch arm 82, U-shaped fixed seat 83, matrix fasten position 84, rotating shaft A85, rotating shaft B86, rotating shaft
C87。
Embodiment
The technical solution of the utility model is illustrated with embodiment below in conjunction with the accompanying drawings.
, it is necessary to illustrate in description of the present utility model, what term " side " " opposite side " " left side " " right side " was indicated
Orientation or position relationship are, based on orientation shown in the drawings or position relationship, to be for only for ease of description the utility model and simplification
Description, rather than indicate or imply that the device or element of meaning must have specific orientation, with specific azimuth configuration and behaviour
Make, therefore it is not intended that to limitation of the present utility model.
As shown in Figure 1 and Figure 2, cutting structure 3, input and output material knot are provided with braid material cutting machine, including fuselage 1, fuselage 1
Structure 2, control structure 4, braid input channel 5, scrap belt output channel 6, charging-discharging structure 2 are arranged on the left side of fuselage, manipulation
Structure 4 is arranged on the right side of fuselage, and cutting structure 3 is arranged between charging-discharging structure 2 and control structure 4；Charging-discharging structure 2
Side is set to feed end 28, and the opposite side of charging-discharging structure 2 is set to discharge end 29, and braid input channel 5 sequentially passes through behaviour
Control structure 4, cutting structure 3 are connected with feed end 28, and the scrap belt output channel 6 sequentially passes through control structure 4, cutting structure
3 connect with discharge end 29, the guide frame 7 being connected with braid input channel 5 are provided with outside fuselage 1, the fuselage 1 is close to manipulation
The side of structure 4 is provided with disassembly and assembly structure 8.Braid input channel 5 is by being disposed in parallel in the side of machine 1 gear corresponding with feed end 28
Plate A51 and baffle plate B52 compositions, the distance between baffle plate A51 and baffle plate B52 are adapted to the tranverse sectional thickness of braid material.Scrap belt
Output channel 6 is constituted by being disposed in parallel in the side of fuselage 1 baffle plate C62 corresponding with discharge end 29 and baffle plate D61, baffle plate C62 and
The distance between baffle plate D61 is adapted to the tranverse sectional thickness of braid material.Control structure 4 includes control button 41 and pressed with control
The supply unit that button 41 is connected, cutting structure 3, charging-discharging structure 2 are manipulated by control structure 4.
As shown in figure 3, charging-discharging structure 2 includes workbench, be provided with workbench rotating disk 21 and with rotating disk 21
The press material structure 210 of cooperation, the workbench is arranged with the stepper motor 27 of the rotation of driving rotating disk 21, the outside of rotating disk 21
Annular array is provided with some bayonet locks 20 on wall；Press material structure 210 includes fixed block 23 and binder block A22, fixed block 23 and pressure
Connected between material block A22 by axis of guide A25, axis of guide A25 outer surface is arranged with spring A26, the utility model
Axis of guide A25 is set to 2.One side relative with rotating disk 21 binder block A22 is provided with the arc-shaped concave matched with rotating disk 21
24。
When the utility model is run, the driving rotating disk 21 of stepper motor 27 is rotated, and the hole in braid material is fastened on bayonet lock 20,
The rotation of rotating disk 21 drives the rotation of braid material so that the component being pasted onto on braid material in braid input channel 5 and
Moved in scrap belt output channel 6.Press material structure 210 is adjacent to the lateral surface of rotating disk 21 to promote braid material to try one's best, it is to avoid braid
Expect that the skew of position occurs during movement.In press material structure 210, fixed block 23 provides a fixed active force, pressure
Material block A22 keeps close toward the direction of rotating disk 21 under spring A26 elastic force effect.Axis of guide A25 is moved through binder block A22's
The effect that Cheng Zhongqi is oriented to, prevents that position skew occurs during movement.
As shown in Fig. 4, Fig. 5, Fig. 6, cutting structure 3 includes base 31, cylinder 30, side and the gas being fixed on base 31
Knife rest 34 that cylinder 30 is connected, it is fixed on the binder block C39 being equipped with base 31 with knife rest 34, base 31 and is provided with guide rail
32, another side bottom of knife rest 34 is provided with the sliding block 33 being slidably connected with guide rail 32；The top of knife rest 34 is provided with cutting knife 35,
The top of cutting knife 35 is movably set with binder block B38, and cutting knife 35 is connected with binder block B38 by axis of guide B37, axis of guide B37's
Outer surface is arranged with spring B 36, and cutting knife 35 is set to edge of a knife position 302, binder block B38 and knife towards the side of braid input channel
The mouth corresponding position in position 302 is provided with binder projection 303；Binder block C39 is provided with and binder projection close to the side of knife rest 34
303 corresponding seal faces 301, the lower section of seal face 301 is provided with cuts space for what edge of a knife position 302 entered.
When the utility model is run, cylinder 30 drives direction of the knife rest 34 along guide rail 32 to binder block C39 to move, first
Binder block B38 can press to the pin by component in the braid material of cutting structure binder block C39, binder projection 303 and pressure
After the tight common pin by component in face 301 is compressed, edge of a knife position 302 makes member to space movement is cut so as to complete to cut action
Device is separated with braid material, and completion is cut after action, and binder projection 303 still pushes down the first device just cut with seal face 301
The pin of part, after inserter takes component away, the stepping of rotating disk 21 of charging-discharging structure 2 is rotated, and is made next to be processed
The relevant position that component in braid material is moved to cutting structure is cut, so circulation.
Binder block B38 is movably arranged on the top of cutting knife 35, is connected by axis of guide B37, binder block B38 is existed with cutting knife 35
Coaxial direction is moved, after binder projection 303 is compressed with the common pin by component of seal face 301, edge of a knife position 302
It may proceed to space movement is cut, now, spring B 36 is compressed by the pressure between cutting knife 35 and binder block B38, so that
Binder projection 303 is promoted to press tighter with seal face 301, so that component is stably pressed in cutting structure 3.Complete to cut out
Cut action, direction of the cylinder 30 with movable knife rack 34 along guide rail 32 resets, be that the action that cuts next time is prepared.
Binder projection 303 and binder block C39 distance is less than edge of a knife position 302 and binder block C39 distance, such structure
Setting is able to allow binder projection 303 first to contact with seal face 301, and the component in volume material strip to be cut is determined
Position, is then accurately cut again.
As shown in Fig. 2, Fig. 7, Fig. 8, disassembly and assembly structure 8 includes extending to the control lever 80 of the upper surface of fuselage 1, extends to fuselage
The lock catch arm 82 of 1 lower surface, it is fixed on the inverted U fixed seat 83 that the bottom of fuselage 1 is connected with lock catch arm 82, control lever 80 and lock
Connected between arm 82 by gangbar 81, control lever 80 is connected by rotating shaft A85 with one end of gangbar 81, gangbar 81 it is another
One end is connected by rotating shaft B86 with one end of lock catch arm 82；The other end of lock catch arm 82 passes through rotating shaft C 87 and inverted U fixed seat
83 connections；The afterbody of lock catch arm 82 is provided with matrix and fastens position 84；Fuselage 1 includes upper cover plate 10 and lower cover 11, upper cover plate 10
Stopper slot A12 is offered with the corresponding position of control lever 80, lower cover 11 is provided with stopper slot with the corresponding position of lock catch arm 82
B13。
When being dismantled to this structure, the side of the directional guiding structure 7 of control lever 80 is pulled, control lever 80 promotes gangbar
81 drive lock catch arm 82, and C87 carries out axial rotation around the shaft, matrix is fastened position 84 and departs from fastening from inserter.Upper cover plate 10
The position of control structure 4 is provided with handle 9, convenient in dismounting or installation, one pulls control lever 80 and operates, separately
One pulls handle 9 and braid material cutting machine is detached into inserter.
As shown in figure 9, guide frame 7 includes roller 71 and the baffle plate E72 and baffle plate that are connected respectively with the two ends of roller 71
F73, baffle plate E72 and baffle plate F73 afterbody are progressive to come closer to form the braid entrance 75 corresponding with braid input channel 5.
Guide frame 7 is connected by L-type stator 74 with fuselage 1.
During actual production, braid material to be cut is placed on the roller 71 of guide frame 7, and braid is aided in by roller 71
Braid input channel 5 is entered back into after expecting pre-adjusted correct position.
Operating principle of the present utility model is：First by without the braid material fore-end of component along braid input channel
5 are fastened on rotating disk 21, start stepper motor 27, promote rotating disk 21 to drive braid material to be moved in braid input channel 5, the first device of band
The braid material of part can be moved to cutting structure 3 along braid input channel 5 and be cut, and completing the component after cutting can stop
Position is being cut for inserter pickup, after component is removed, it is to be cut that next component can be moved to cutting structure 3 etc.
Cut, and the useless braid material being cut can be moved to scrap belt output channel 6 with the rotation of rotating disk 21, the braid material that gives up can edge
The outside that scrap belt output channel 6 is output to braid material cutting machine；Such do action.
Above-described embodiment is only that general principle of the present utility model, principal character and advantage has been shown and described.The industry
Technical staff it should be appreciated that the utility model is not restricted to the described embodiments, do not departing from the utility model spirit and model
On the premise of enclosing, the utility model also has various changes and modifications, and these changes and improvements both fall within this claimed reality
With in new scope.
Claims (8)
1. a kind of braid material cutting machine, it is characterised in that：Including fuselage (1), be provided with the fuselage (1) cutting structure (3),
Charging-discharging structure (2), control structure (4), braid input channel (5), scrap belt output channel (6), the charging-discharging structure (2)
The left side of fuselage is arranged on, the control structure (4) is arranged on the right side of fuselage, and the cutting structure (3) is arranged on input and output material
Between structure (2) and control structure (4)；The side of the charging-discharging structure (2) is set to feed end (28), the input and output material knot
The opposite side of structure (2) is set to discharge end (29), and the braid input channel (5) sequentially passes through control structure (4), cutting structure
(3) connected with feed end (28), the scrap belt output channel (6) sequentially passes through control structure (4), cutting structure (3) with going out
Expect to be provided with the guide frame (7) being connected with braid input channel (5), the fuselage outside end (29) connection, the fuselage (1)
(1) side close to control structure (4) is provided with disassembly and assembly structure (8).
2. a kind of braid material cutting machine according to claim 1, it is characterised in that：The charging-discharging structure (2) includes work
Make the press material structure (210) that rotating disk (21) is provided with platform, the workbench and is coordinated with rotating disk (21), the work
Platform is arranged with annular array on the stepper motor (27) of driving rotating disk (21) rotation, the lateral wall of the rotating disk (21) and set
There are some bayonet locks (20)；The press material structure (210) include fixed block (23) and binder block A (22), the fixed block (23) and
Connected between binder block A (22) by some axis of guide A (25), the outer surface of some axis of guide A (25) is arranged with bullet
Spring A (26)；The binder block A (22) one side relative with rotating disk (21) is provided with the arc-shaped concave matched with rotating disk (21)
(24)。
3. a kind of braid material cutting machine according to claim 1, it is characterised in that：The cutting structure (3) includes base
(31) cylinder (30) that, is fixed on base (31), the knife rest (34) of side and cylinder (30) connection, it is fixed on base (31)
Be provided with guide rail (32) on the binder block C (39) being equipped with knife rest (34), the base (31), the knife rest (34) it is another
One side bottom is provided with the sliding block (33) being slidably connected with guide rail (32)；The top of the knife rest (34) is provided with cutting knife (35),
Binder block B (38) is movably set with above the cutting knife (35), the cutting knife (35) passes through axis of guide B with binder block B (38)
(37) connect, the outer surface of the axis of guide B (37) is arranged with spring B (36), the cutting knife (35) is towards braid input channel
Side be set to edge of a knife position (302), the corresponding position of the binder block B (38) and the edge of a knife (302) is provided with binder projection
(303)；The binder block C (39) is provided with the seal face corresponding with binder projection (303) close to the side of knife rest (34)
(301), it is provided with below the seal face (301) and cuts space for what edge of a knife position (302) entered；The binder projection
(303) distance with binder block C (39) is less than edge of a knife position (302) and binder block C (39) distance.
4. a kind of braid material cutting machine according to claim 1, it is characterised in that：The control structure (4) includes control
Button (41) and the supply unit being connected with control button (41).
5. a kind of braid material cutting machine according to claim 1, it is characterised in that：The braid input channel (5) is by simultaneously
Row are arranged on fuselage (1) side baffle plate A (51) corresponding with feed end (28) and baffle plate B (52) compositions.
6. a kind of braid material cutting machine according to claim 1, it is characterised in that：The scrap belt output channel (6) by
It is disposed in parallel in fuselage (1) side baffle plate C (62) corresponding with discharge end (29) and baffle plate D (61) compositions.
7. a kind of braid material cutting machine according to claim 1, it is characterised in that：The disassembly and assembly structure (8) includes extension
Control lever (80) to fuselage (1) upper surface, extend to the lock catch arm (82) of fuselage (1) lower surface, be fixed on fuselage (1) bottom
The inverted U fixed seat (83) being connected with lock catch arm (82), gangbar is passed through between the control lever (80) and lock catch arm (82)
(81) connect, the control lever (80) is connected by rotating shaft A (85) with one end of gangbar (81), the gangbar (81) it is another
One end is connected by rotating shaft B (86) with one end of lock catch arm (82)；The other end of the lock catch arm (82) by rotating shaft C (87) with
Inverted U fixed seat (83) is connected；The afterbody of the lock catch arm (82) is provided with matrix and fastens position (84)；The fuselage (1) includes
Upper cover plate (10) and lower cover (11), the upper cover plate (10) position corresponding with control lever (80) offer stopper slot A (12),
The lower cover (11) position corresponding with lock catch arm (82) is provided with stopper slot B (13)；The upper cover plate (10) is close to manipulation
The position of structure (4) is provided with handle (9).
8. a kind of braid material cutting machine according to claim 1, it is characterised in that：The guide frame (7) includes roller
(71) the baffle plate E (72) and baffle plate F (73) and being respectively connected with roller (71) two ends, the baffle plate E (72) and baffle plate F (73)
Afterbody progressive come closer to form the braid entrance (75) corresponding with braid input channel (5)；The guide frame (7) is led to
L-type stator (74) is crossed to be connected with fuselage (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720002569.0U CN206604971U (en) | 2017-01-03 | 2017-01-03 | A kind of braid material cutting machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720002569.0U CN206604971U (en) | 2017-01-03 | 2017-01-03 | A kind of braid material cutting machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206604971U true CN206604971U (en) | 2017-11-03 |
Family
ID=60172351
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720002569.0U Expired - Fee Related CN206604971U (en) | 2017-01-03 | 2017-01-03 | A kind of braid material cutting machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206604971U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109292144A (en) * | 2018-10-25 | 2019-02-01 | 广东华技达精密机械有限公司 | A kind of vertical braid loader and braid method of feeding |
| CN112369134A (en) * | 2018-07-06 | 2021-02-12 | 株式会社富士 | Component supply device |
-
2017
- 2017-01-03 CN CN201720002569.0U patent/CN206604971U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112369134A (en) * | 2018-07-06 | 2021-02-12 | 株式会社富士 | Component supply device |
| CN112369134B (en) * | 2018-07-06 | 2022-09-09 | 株式会社富士 | Component supply device |
| CN109292144A (en) * | 2018-10-25 | 2019-02-01 | 广东华技达精密机械有限公司 | A kind of vertical braid loader and braid method of feeding |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| 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: 20171103 Termination date: 20190103 |