CN201102834Y - Horizontal barreled steel wire rewinding unit - Google Patents
Horizontal barreled steel wire rewinding unit Download PDFInfo
- Publication number
- CN201102834Y CN201102834Y CNU2007200450314U CN200720045031U CN201102834Y CN 201102834 Y CN201102834 Y CN 201102834Y CN U2007200450314 U CNU2007200450314 U CN U2007200450314U CN 200720045031 U CN200720045031 U CN 200720045031U CN 201102834 Y CN201102834 Y CN 201102834Y
- Authority
- CN
- China
- Prior art keywords
- rotary disk
- take
- bearing
- wire
- fuselage
- Prior art date
- 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
Links
Images
Abstract
The utility model relates to a horizontal barreled steel wire take-up unit, which comprises a frame (1), a cycloidal needle wheel decelerator (2), a take-up reel (4), a wire roller (5), a damper (3), a wire frame rotary disk (9), a rotary disk transmission mechanism (10), a wire-accumulate backing plate (8) and a vibrating mechanism (11), wherein, the frame (1) is a lateral L-shaped structure, the cycloidal needle wheel decelerator (2) is arranged on the upper part of a footboard back of the frame, the take-up reel (4) and the wire roller (5) are arranged on the upper part of the front of the footboard, the wire roller (5) is arranged on the right side and the left side of the take-up reel (4), the take-up reel (4) is arranged on an output end of the cycloidal needle wheel decelerator (2), the wire frame rotary disk (9) is arranged on the front of a transverse plate (1.2) of the frame, the wire frame rotary disk (9) is connected with the rotary disk transmission mechanism (10), the rotary disk transmission mechanism (10) is connected with the cycloidal needle wheel decelerator (2), the wire-accumulate backing plate (8) is arranged on the wire frame rotary disk (9), and the vibrating mechanism (11) comprises a lug (11.1), a bearing (11.3), a support (11.5) and a pin roll (11.6). The horizontal barreled steel wire take-up unit has the advantage of neat and compact wire-accumulate array.
Description
Technical field
The utility model relates to a kind of horizontal barreled steel wire take-up unit, is mainly used in the stainless steel wire solid solution take-up of line footpath φ 0.7～1.2mm.Belong to stainless steel wire production facilities technical field.
Background technology
Steel wire take-up unit is the key equipment of take-up in the Steel Wire Heat Treatment production process.The quality of this equipment take-up performance directly affect the lopping product design of steel wire and down the road winding displacement can be neatly, the not random line problem of unwrapping wire.
The take-up of steel wire at present all adopts inverted take-up unit to realize.Because the axial line of the axial line of inverted admission machine take-up reel and take-up stand is on same vertical axis, promptly the axial line of take-up stand places on the extended line of axial line of take-up reel.During take-up, drive the passive rotation of take-up stand by the driving lever on the reel, cause the long-pending line lamination on the take-up stand more open, long-pending line is arranged also irregular.
The utility model content
The purpose of this utility model is to overcome above-mentioned deficiency, and the horizontal closely steel wire take-up of a kind of long-pending line marshalling unit is provided.
The purpose of this utility model is achieved in that a kind of horizontal barreled steel wire take-up unit, it is characterized in that: described unit comprises fuselage, cycloidal planetary gear speed reducer, take-up reel, wire-crossing wheel, damper, coil holder rotary disk, rotary disk transmission device, long-pending line bucket backing plate and vibrating mechanism
Described fuselage is side " L " type structure, comprise riser and transverse slat, described cycloidal planetary gear speed reducer is installed on the riser upper rear portion of fuselage, described take-up reel and wire-crossing wheel are arranged at the riser front upper, wire-crossing wheel is arranged at the left and right both sides of take-up reel, take-up reel is installed on the mouth of cycloidal planetary gear speed reducer, and wire-crossing wheel is installed on the riser front
Described damper device is in the riser top,
Described coil holder rotary disk is arranged at the transverse slat front of fuselage, and the coil holder rotary disk links to each other with single-revolution dish transmission device, and the rotary disk transmission device links to each other with cycloidal planetary gear speed reducer,
Described long-pending line bucket backing plate is positioned on the coil holder rotary disk,
Described vibrating mechanism comprises projection, bearing, bearing and bearing pin, described projection has one at least, projection is fixedly connected on the long-pending line bucket backing plate back side downwards, corresponding to described projection, offer through hole on the coil holder rotary disk under the projection, projection places in this through hole, and corresponding to described projection, the transverse slat of the fuselage under the projection faces up and is provided with the bearing that contacts with it and cooperate.
The cycloidal planetary gear speed reducer transmission drives the take-up reel rotation on the one hand, and simultaneously through the rotation of sprocket chain band moving-wire frame rotary disk, the long-pending line bucket that is driven on the long-pending line bucket backing plate by the rotary disk transmission device rotates.During take-up, steel wire enters Y type take-up reel through damper and take-up reel wire-crossing wheel on one side, and going out behind the take-up reel again, the wire-crossing wheel through the take-up reel another side imports down in the long-pending line bucket.
Because the axial line level of take-up reel of the present utility model is installed, the axial line of long-pending line bucket vertically is provided with, and that is to say the axial line vertical setting mutually of axial line with the long-pending line bucket of take-up reel.Drive long-pending line bucket active rotation by the rotary disk transmission device, the vibrating mechanism that the moving circle of long-pending simultaneously line bucket revolution is arranged at long-pending line bucket backing plate bottom carries out one or many to the long-pending line bucket on the long-pending line bucket backing plate and ejects, make long-pending line bucket while rotating the process that realizes interstitial vibration, can make long-pending line on the long-pending line bucket arrange very closely and scatter like this and arrange and form the arrangement of plum blossom shape specification.
Description of drawings
Fig. 1 is the construction profile scheme drawing of the horizontal barreled steel wire of the utility model take-up unit.
Fig. 2 is the right side view of Fig. 1.
Fig. 3 is the bottom enlarged drawing of Fig. 2.
Fig. 4 is the structural representation of long-pending line bucket backing plate of the present utility model.
Fig. 5 is the structural representation of the utility model projection.
Fig. 6 is the birds-eye view of Fig. 5.
Fig. 7 is the structural representation of coil holder rotary disk of the present utility model.
The birds-eye view of Fig. 8 Fig. 7.
Among the figure: fuselage 1, cycloidal planetary gear speed reducer 2, damper 3, take-up reel 4, wire-crossing wheel 5, swelling device 6, long-pending line bucket 7, long-pending line bucket backing plate 8, coil holder rotary disk 9, rotary disk transmission device 10, vibrating mechanism 11; Riser 1.1, transverse slat 1.2, dust ring 1.2.1; Through hole 9.1; Drive sprocket 10.1, chain 10.2, driven sprocket 10.3, transmission shaft 10.4, bearing cap shim II 10.5, bearing carrier ring 10.6, support set II 10.7, driving bevel gear 10.8, support set I 10.9, bearing cap shim I 10.10, driven bevel pinion 10.11, axis of revolution 10.12, bearing seat 10.13, bearing cap shim III 10.14, projection 11.1, screw 11.2, bearing 11.3, support set III11.4, bearing 11.5, bearing pin 11.6.
The specific embodiment
Referring to Fig. 1～2, the utility model relates to a kind of horizontal barreled steel wire take-up unit, mainly is made up of fuselage 1, cycloidal planetary gear speed reducer 2, take-up reel 4, wire-crossing wheel 5, damper 3, swelling device 6, coil holder rotary disk 9, rotary disk transmission device 10, long-pending line bucket backing plate 8 and vibrating mechanism 11.
Described fuselage 1 is side " L " type structure, form by riser 1.1 and transverse slat 1.2, described cycloidal planetary gear speed reducer 2 is installed on riser 1.1 upper rear portion of fuselage, described take-up reel 4 and wire-crossing wheel 5 are arranged at riser 1.1 front upper, wire-crossing wheel 5 is arranged at the left and right both sides of take-up reel 4, and take-up reel 4 is installed on the mouth of cycloidal planetary gear speed reducer 2, and wire-crossing wheel 5 is installed on riser 1.1 fronts, described damper 3 is installed on riser 1.1 tops, and described swelling device 6 is installed on riser 1.1 positive middle parts.
Described coil holder rotary disk 9 is arranged on the transverse slat 1.2 of fuselage, and coil holder rotary disk 9 links to each other with single-revolution dish transmission device 10, and long-pending line bucket backing plate 8 is positioned on the coil holder rotary disk 9, and long-pending line bucket 7 is positioned on the long-pending line bucket backing plate 8.Be provided with on the transverse slat 1.2 of the fuselage of coil holder rotary disk 9 belows dust ring 1.2.1 is upwards arranged.Dust ring 1.2.1 places coil holder rotary disk 9 peripheries.
Referring to Fig. 1,3, described rotary disk transmission device 10 is made up of drive sprocket 10.1, chain 10.2, driven sprocket 10.3, transmission shaft 10.4, bearing cap shim II 10.5, bearing carrier ring 10.6, driving bevel gear 10.8, bearing cap shim I 10.10, driven bevel pinion 10.11, axis of revolution 10.12, bearing seat 10.13 and bearing cap shim III10.14.Drive sprocket 10.1 devices are on the output shaft of cycloidal planetary gear speed reducer 2, drive sprocket 10.1 links to each other with driven sprocket 10.3 by chain 10.2, driven sprocket 10.3 is installed on transmission shaft 10.4 one ends, in the middle of the transmission shaft 10.4 by bearing arrangement in bearing carrier ring 10.6, bearing cap shim II 10.5 lids are loaded on bearing carrier ring 10.6 one ends, bearing carrier ring 10.6 other ends are captiveed joint with bearing seat 10.13 one sides, driving bevel gear 10.8 is installed on the other end of transmission shaft 10.4, and place in the bearing seat 10.13, driving bevel gear 10.8 and driven bevel pinion 10.11 engagements, driven bevel pinion 10.11 is installed on the axis of revolution 10.12, axis of revolution 10.12 by bearing arrangement in bearing seat 10.13, axis of revolution 10.12 upper ends are connected with coil holder rotary disk 9 lower surface center fixation, bearing cap shim I 10.10 lids place bearing seat 10.13 lower ends, bearing seat 10.13 upper ends are installed on the transverse slat 1.2 of fuselage, and bearing cap shim III10.14 lid places bearing seat 10.13 upper ends.
Described vibrating mechanism 11 is made up of projection 11.1, bearing 11.3, bearing 11.5 and bearing pin 11.6.Described projection 11.1 has one at least, is fixedly connected on long-pending line bucket backing plate 8 back sides downwards with screw 11.2, as Fig. 4,5 and 6.Corresponding to described projection 11.1, offer oval shape through hole 9.1 on the coil holder rotary disk 9 under the projection 11.1, as Fig. 7,8, described projection 11.1 places in this through hole 9.1, corresponding to described projection 11.1, the riser 1.1 of the fuselage under the projection 11.1 faces up and is provided with the bearing 11.3 that contacts with it and cooperate, and described bearing 11.3 usefulness bearing pins 11.6 are pinned on the bearing 11.5, and described bearing 11.5 upwards is connected in riser 1.1 fronts of fuselage.
The fuselage of the horizontal barreled steel wire of the utility model take-up unit adopts steel plate and shaped steel welding fabrication, multiple computer desk disjunctor.The horizontal barreled steel wire of the utility model take-up unit can be according to many combinations arbitrarily of output needs, adopt variable frequency control, but multifibres is with speed or monofilament single speed, in the speed range of setting, can regulate the speed arbitrarily, satisfy the dislocation of lopping silk and arrange in the wire range of setting, compression volume increases unit weight, packing is neat, unwrapping wire is reliable.
Claims (4)
1, a kind of horizontal barreled steel wire take-up unit, it is characterized in that: described unit comprises fuselage (1), cycloidal planetary gear speed reducer (2), take-up reel (4), wire-crossing wheel (5), damper (3), coil holder rotary disk (9), rotary disk transmission device (10), long-pending line bucket backing plate (8) and vibrating mechanism (11)
Described fuselage (1) is side " L " type structure, comprise riser (1.1) and transverse slat (1.2), described cycloidal planetary gear speed reducer (2) is installed on riser (1.1) upper rear portion of fuselage, described take-up reel (4) and wire-crossing wheel (5) are arranged at riser (1.1) front upper, wire-crossing wheel (5) is arranged at the left and right both sides of take-up reel (4), take-up reel (4) is installed on the mouth of cycloidal planetary gear speed reducer (2), and wire-crossing wheel (5) is installed on riser (1.1) front
Described damper (3) is installed on riser (1.1) top,
Described coil holder rotary disk (9) is arranged at transverse slat (1.2) front of fuselage, and coil holder rotary disk (9) links to each other with single-revolution dish transmission device (10), and rotary disk transmission device (10) links to each other with cycloidal planetary gear speed reducer (2),
Described long-pending line bucket backing plate (8) is positioned on the coil holder rotary disk (9),
Described vibrating mechanism (11) comprises projection (11.1), bearing (11.3), bearing (11.5) and bearing pin (11.6), described projection (11.1) has one at least, projection (11.1) is fixedly connected on long-pending line bucket backing plate (8) back side downwards, corresponding to described projection (11.1), offer through hole (9.1) on the coil holder rotary disk (9) under the projection (11.1), projection (11.1) places in this through hole (9.1), corresponding to described projection (11.1), the transverse slat (1.2) of the fuselage under the projection (11.1) faces up and is provided with the bearing (11.3) that contacts with it and cooperate.
2, a kind of horizontal barreled steel wire take-up unit according to claim 1, it is characterized in that: described bearing (11.3) is pinned on the bearing (11.5) with bearing pin (11.6), and described bearing (11.5) upwards is connected in transverse slat (1.2) front of fuselage.
3, a kind of horizontal barreled steel wire take-up unit according to claim 1 and 2, it is characterized in that: described rotary disk transmission device (10) comprises drive sprocket (10.1), chain (10.2), driven sprocket (10.3), transmission shaft (10.4), bearing carrier ring (10.6), driving bevel gear (10.8), driven bevel pinion (10.11), axis of revolution (10.12) and bearing seat (10.13), drive sprocket (10.1) device is on the output shaft of cycloidal planetary gear speed reducer (2), drive sprocket (10.1) links to each other with driven sprocket (10.3) by chain (10.2), driven sprocket (10.3) is installed on transmission shaft (10.4) one ends, transmission shaft (10.4) middle device is in bearing carrier ring (10.6), bearing carrier ring (10.6) is captiveed joint with bearing seat (10.13) one sides, driving bevel gear (10.8) is installed on the other end of transmission shaft (10.4), and place in the bearing seat (10.13), driving bevel gear (10.8) and driven bevel pinion (10.11) engagement, driven bevel pinion (10.11) is installed on the axis of revolution (10.12), axis of revolution (10.12) is installed in the bearing seat (10.13), axis of revolution (10.12) upper end is connected with coil holder rotary disk (9) lower surface center fixation, and bearing seat (10.13) is installed on the transverse slat (1.2) of fuselage.
4, a kind of horizontal barreled steel wire take-up unit according to claim 1 and 2 is characterized in that: the transverse slat (1.2) of the fuselage of described coil holder rotary disk (9) below is provided with dust ring (1.2.1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200450314U CN201102834Y (en) | 2007-11-02 | 2007-11-02 | Horizontal barreled steel wire rewinding unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200450314U CN201102834Y (en) | 2007-11-02 | 2007-11-02 | Horizontal barreled steel wire rewinding unit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201102834Y true CN201102834Y (en) | 2008-08-20 |
Family
ID=39949857
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2007200450314U Expired - Fee Related CN201102834Y (en) | 2007-11-02 | 2007-11-02 | Horizontal barreled steel wire rewinding unit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201102834Y (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101695979B (en) * | 2009-10-29 | 2012-05-23 | 台州海翔焊接材料有限公司 | Wire receiving machine for recovering steel wires |
-
2007
- 2007-11-02 CN CNU2007200450314U patent/CN201102834Y/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101695979B (en) * | 2009-10-29 | 2012-05-23 | 台州海翔焊接材料有限公司 | Wire receiving machine for recovering steel wires |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206552385U (en) | A kind of tea packaging machine finished product delivery mechanism | |
| CN102870544A (en) | Mower | |
| CN211340006U (en) | Soak device is used in aseptic weaving production | |
| CN206010668U (en) | A kind of novel steel tube burr remover | |
| CN208742706U (en) | A kind of high-efficient machine tooling waste material crushing plant | |
| CN201102834Y (en) | Horizontal barreled steel wire rewinding unit | |
| CN202896907U (en) | Vertical cutting all-in-one machine for light medium mesh bag containers | |
| CN206686610U (en) | A kind of hand propelled afforests weeder | |
| CN108622603A (en) | A kind of rotatable mobile material-receiving device | |
| CN201901262U (en) | Laminated caching device for packaging machine | |
| CN202297760U (en) | Coating equipment workpiece rotating frame | |
| CN206586295U (en) | A kind of leaf kneading machine of tea processing | |
| CN202529165U (en) | Low-position online winding packaging machine | |
| CN209304630U (en) | A kind of cystosepiment cutting bed vise cutting bed lifting device | |
| CN205733293U (en) | A kind of Gear Root burnishing device | |
| CN201970186U (en) | Double-rotation rough grinding machine | |
| CN201370421Y (en) | Prayer wheel transmission mechanism | |
| CN209521909U (en) | A kind of interior packet sugar tidy-up device | |
| CN208034295U (en) | A kind of three steel brush machines | |
| CN201722468U (en) | Flexible graphite strip spinning equipment | |
| CN212126840U (en) | Tea discharging device for tea making machine | |
| CN203340930U (en) | Tea leaf rolling equipment | |
| CN205998499U (en) | A kind of liftable transporter being applied to bill storage device | |
| CN215775301U (en) | Energy-saving tea processing is with package machine of rubbing | |
| CN202343157U (en) | Novel biomass granular fuel forming machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| EE01 | Entry into force of recordation of patent licensing contract |
Assignee: Dongming Industrial (Jiaxing) Co., Ltd. Assignor: Jiangyin Sanlian Machinery Manufacturing Co., Ltd. Contract fulfillment period: 2008.12.15 to 2016.12.14 Contract record no.: 2009330000242 Denomination of utility model: Horizontal barreled steel wire rewinding unit Granted publication date: 20080820 License type: Exclusive license Record date: 20090211 |
|
| LIC | Patent licence contract for exploitation submitted for record |
Free format text: EXCLUSIVE LICENSE; TIME LIMIT OF IMPLEMENTING CONTACT: 2008.12.15 TO 2016.12.14; CHANGE OF CONTRACT Name of requester: DONGMING INDUSTRY ( JIAXING ) CO., LTD. Effective date: 20090211 |
|
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20080820 Termination date: 20131102 |