CN102199822A - Dual-beam warping machine - Google Patents
Dual-beam warping machine Download PDFInfo
- Publication number
- CN102199822A CN102199822A CN2011101376653A CN201110137665A CN102199822A CN 102199822 A CN102199822 A CN 102199822A CN 2011101376653 A CN2011101376653 A CN 2011101376653A CN 201110137665 A CN201110137665 A CN 201110137665A CN 102199822 A CN102199822 A CN 102199822A
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- China
- Prior art keywords
- level
- fuselage
- coiled hair
- leading screw
- tailing axle
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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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Links
- 235000014676 Phragmites communis Nutrition 0.000 claims abstract description 36
- 210000004209 hair Anatomy 0.000 claims description 85
- 238000010079 rubber tapping Methods 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 244000089486 Phragmites australis subsp australis Species 0.000 abstract description 2
- 230000009977 dual effect Effects 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 4
- 229920000742 Cotton Polymers 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- FGRBYDKOBBBPOI-UHFFFAOYSA-N 10,10-dioxo-2-[4-(N-phenylanilino)phenyl]thioxanthen-9-one Chemical compound O=C1c2ccccc2S(=O)(=O)c2ccc(cc12)-c1ccc(cc1)N(c1ccccc1)c1ccccc1 FGRBYDKOBBBPOI-UHFFFAOYSA-N 0.000 description 1
- 229920000297 Rayon Polymers 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000002146 bilateral effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
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- Warping, Beaming, Or Leasing (AREA)
Abstract
The invention belongs to the field of warping machines and in particular provides a copying type dual-beam warping machine. The warping machine comprises a machine body, a yarn guide roller mechanism on the machine body, a zigzag reed mechanism, a beam assembly, a clamping mechanism and a bracket mechanism, wherein the beam assembly, the clamping mechanism and the bracket mechanism are arranged in the machine body. The warping machine has the following advantages: the warping machine adopts the dual-beam positioning mode, has stable structure and high precision, adopts the pneumatic dual-side beam pushing mode, adopts the zigzag reeds which can be adjusted in an assembled manner, is fast and convenient to disassemble and assemble, is suitable for dual beams and long beams, improves the working efficiency, lowers the use cost and saves the production sites.
Description
Technical field
The invention belongs to the warping machines field, especially a kind of double-warp beam warper that copies type.
Background technology
Existing warping machines is the single-deck head generally speaking, especially the warping machines of copy type, be single-deck head warping machines, be mainly used in cotton, wash long filament, the warping of low-stretch yarn, viscose, cotton yarn, ACRYLIC YARNS etc., because the single-deck head working time is long, a plurality of warping machiness take up an area of very big again, so production efficiency is not high.
Summary of the invention
The present invention is directed to a plurality of single-deck head warping machiness that exist in the above-mentioned technology and take up an area of the weak point big, that the working time is long, production efficiency is low, a kind of double-warp beam warper is proposed, it can carry out warping with two coiled hairs simultaneously, has improved production efficiency, has saved mechanical occupation of land.
The technical scheme that realizes the object of the invention is as follows:
Double-warp beam warper, it comprises coiled hair combination, clamping device, carriage mechanism in cord roller mechanism, herringbone reed mechanism and the fuselage on fuselage, the fuselage, the coiled hair combination is located in the clamping device, is provided with two benchmark guide pillars up and down in the fuselage; Clamping device comprises left clamping and right clamping, left side clamping comprises tailing axle combination with tailing axle and the support that supports the tailing axle combination, the support two ends are located on the benchmark guide pillar, support is provided with driver part and tailing axle is connected, right clamping comprises drive unit and the traversing carriage that main shaft, driving main shaft are rotated, main shaft is located on the drive unit, drive unit is fixed on the traversing carriage, traversing carriage is snug fit on the benchmark guide pillar, is provided with the main shaft drives parts between fuselage inner side surface and the traversing carriage; Carriage mechanism comprises driving mechanism and hoisting mechanism, and hoisting mechanism is located at the coiled hair combination down, and driving mechanism is located at the fuselage side and is connected with hoisting mechanism.
Adopt this technical scheme, the coiled hair combination can be set as a long coiled hair or two coiled hairs and a coiled hair bracing frame, can select as required like this, support, traversing carriage, can on the benchmark guide pillar, move and adjust the position, main shaft and tailing axle are used for the combination of clamping coiled hair, carriage mechanism can be promoted to the main shaft position coaxial with tailing axle with the coiled hair that is placed on the hoisting mechanism, by driver part and the work of main shaft drives parts coiled hair is fixed between main shaft and the tailing axle then, drive by drive unit again and carry out warping work, improved the utilization rate of warping machines, practical face strengthens, and can use alone or the coiled hair alone of two coiled hairs or different size.
The combination of described coiled hair comprises coiled hair bracing frame and alone or two coiled hairs, and the coiled hair bracing frame is slidingly fitted on the benchmark guide pillar; During coiled hair, the coiled hair bracing frame moves to left clamping one side alone, and coiled hair is located between coiled hair bracing frame and the right clamping alone; During two coiled hairs, the coiled hair bracing frame is moved to centre position between left clamping and the right clamping, two coiled hairs are located at the both sides of coiled hair bracing frame respectively.
When selecting to use alone coiled hair, the position that can adjust the coiled hair bracing frame according to the length of coiled hair alone, thus coiled hair is alone fixed; When selecting to use two coiled hairs, the work that original two warping machiness are done just can be finished in the present invention, saved the working time, improved production efficiency, saved the use place.
Described hoisting mechanism comprises the rotating shaft being located at fuselage bottom and stretching out fuselage, rotating shaft one end is connected with driving mechanism by a master pendulum arm, hoisting mechanism also comprises lifting subassembly, these lifting subassembly two ends are fixed with slide block, two interior swing arms are located at the lifting subassembly both sides, and interior swing arm is provided with axial bar shaped movable span, and slide block passes this bar shaped movable span and is connected on the guide plate of fuselage both sides, vertically be provided with guide groove on the guide plate, the slide block end is located in this guide groove.
Master pendulum arm drives main shaft and rotates under the effect of driving mechanism, swing arm was rotated in main shaft drove, axial bar shaped movable span in the interior swing arm is used for the slide block uphill process and moves in swing arm, guide groove on the guide plate is used for leading longitudinally to slide block, slide block is slided in guide groove, move up and down thereby drive lifting subassembly.
Described herringbone reed mechanism comprises two herringbone reed devices, and two herringbone reed devices are oppositely arranged, and herringbone reed device comprises herringbone reed, one-level guiding mechanism and secondary guiding mechanism; The one-level guiding mechanism comprises one-level slide block, one-level leading screw, one-level leading screw frame and one-level motor, the both sides of herringbone reed are connected with an one-level slide block respectively, the one-level slide block is connected with the one-level threads of lead screw, the one-level motor is fixed on the side of one-level leading screw frame and is connected with the one-level leading screw, and the one-level leading screw is located on the one-level leading screw frame; The secondary guiding mechanism comprises secondary slide block, secondary leading screw, secondary motor and axially directed post, guide block, one-level leading screw frame one end is connected with the secondary leading screw by the secondary slide block, the secondary leading screw is threaded with the secondary slide block, the one-level leading screw frame other end is located on the axially directed post by guide block, the secondary leading screw is connected with the secondary motor and is fixed on the fuselage, and lead is fixed on the fuselage.
When being chosen as alone coiled hair, drive one-level guiding mechanism and secondary guiding mechanism, carry out work with two herringbone reed devices are close, when being chosen as two coiled hairs, driving two herringbone reeds and separately cooperate two coiled hairs to carry out work.
Described tailing axle combination comprises tailing axle, tailing axle head and sliding sleeve, and the tailing axle head is fixed at the tailing axle end, and tailing axle is fixed in the sliding sleeve, and sliding sleeve is snug fit in the support, and tailing axle is provided with connecting plate, and described driver part is connected with this connecting plate.
Drive connecting plate by driver part, sliding sleeve can slide in the sleeve on support, thereby can stretch into spindle nose in the coiled hair or pull out coiled hair, realize to coiled hair load and unload, work etc.
Described spindle nose is provided with main tapping.
Described driver part is a cylinder.
Described drive unit is main motor.
Described main shaft drives parts are the main shaft cylinder, and main shaft cylinder one end is fixed on the traversing carriage, and the other end is fixed on the fuselage.
Described driving mechanism is for driving cylinder.
Advantage of the present invention is to adopt the twin shaft locate mode, Stability Analysis of Structures, precision height, coiled hair holds out against the pneumatic bilateral mode that holds out against that adopts, adopt adjustment type herringbone reed capable of being combined, partition combination rapid and convenient, it is long through axle to be applicable to that the double ends axle arrives, and has improved operating efficiency, reduce use cost, saved production site.
Description of drawings
Fig. 1 is the first embodiment structural representation of the present invention;
Fig. 2 is that the A-A of Fig. 1 is to cutaway view;
Fig. 3 is that the B of Fig. 1 is to view;
Fig. 4 is that the C of Fig. 3 is to view;
Fig. 5 is the view of carriage mechanism when driving cylinder operation;
Fig. 6 is a herringbone reed mechanism structure schematic diagram;
Fig. 7 is the structural representation that herringbone reed mechanism cooperates with two coiled hairs;
Fig. 8 is the second embodiment structural representation of the present invention;
Fig. 9 is the schematic diagram that herringbone reed mechanism cooperates with coiled hair alone in second embodiment.
The specific embodiment
Embodiment one, as Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6, Fig. 7 double-warp beam warper, it comprises coiled hair combination, clamping device, carriage mechanism in cord roller mechanism 2, herringbone reed mechanism and the fuselage on fuselage 1, the fuselage 1, the coiled hair combination is located in the clamping device, is provided with two benchmark guide pillars 3 up and down in the fuselage 1; Clamping device comprises left clamping and right clamping, left side clamping comprises tailing axle combination with tailing axle 4 and the support 5 that supports the tailing axle combination, support 5 two ends are located on the benchmark guide pillar 3, support 5 is provided with driver part and tailing axle is connected, right clamping comprises drive unit and the traversing carriage 7 that main shaft 6, driving main shaft are rotated, main shaft 6 is located on the drive unit, drive unit is fixed on the traversing carriage 7, traversing carriage 7 is snug fit on the benchmark guide pillar 3, is provided with the main shaft drives parts between fuselage 1 inner side surface and the traversing carriage 7; The tailing axle combination comprises tailing axle 4, tailing axle head 11 and sliding sleeve 12, tailing axle head 11 is fixed at tailing axle 4 ends, tailing axle 4 is fixed in the sliding sleeve 12, sliding sleeve 12 is snug fit in the sleeve of support 5, tailing axle 4 is provided with connecting plate 13, described driver part is connected with this connecting plate 13, main shaft 6 ends are provided with main tapping 14, wherein driver part is a cylinder, drive unit is main motor 16, the main shaft drives parts are main shaft cylinder 17, and main shaft cylinder 17 1 ends are fixed on the traversing carriage 7, and the other end is fixed on the fuselage 1; Carriage mechanism comprises driving mechanism and hoisting mechanism, and driving mechanism is for driving cylinder 18, and hoisting mechanism is located at the coiled hair combination down, and driving cylinder 18 is located at fuselage 1 side and is connected with hoisting mechanism; The coiled hair combination comprises coiled hair bracing frame 8 and two coiled hairs, and coiled hair 8a and coiled hair 8b, coiled hair bracing frame 8 are slidingly fitted on the benchmark guide pillar 3; Coiled hair bracing frame 8 is moved to centre position between left clamping and the right clamping, and two coiled hair 8a, 8b are located at the both sides of coiled hair bracing frame 8 respectively; As Fig. 3, Fig. 4, shown in Figure 5, hoisting mechanism comprises the rotating shaft 9 being located at fuselage 1 bottom and stretching out fuselage 1, rotating shaft 9 one ends are connected with driving cylinder 18 by a master pendulum arm 10, hoisting mechanism also comprises lifting subassembly 19, these lifting subassembly 19 two ends are fixed with slide block 20, two interior swing arms 21 are located at the lifting subassembly both sides, interior swing arm 21 is provided with axial bar shaped movable span 21a, slide block 20 passes this bar shaped movable span 21a and is connected on the guide plate 22 of fuselage 1 both sides, vertically be provided with guide groove 22a on the guide plate 22, slide block 20 ends are located among this guide groove 22a; As Fig. 6, shown in Figure 7, herringbone reed mechanism comprises two herringbone reed devices, and two herringbone reed devices are oppositely arranged, and herringbone reed device comprises herringbone reed 23, one-level guiding mechanism and secondary guiding mechanism; The one-level guiding mechanism comprises one-level slide block 23a, one-level leading screw 23b, one-level leading screw frame 23c and one-level motor 23d, the both sides of herringbone reed are connected with an one-level slide block respectively, the one-level slide block is connected with the one-level threads of lead screw, the one-level motor is fixed on the side of one-level leading screw frame and is connected with the one-level leading screw, and the one-level leading screw is located on the one-level leading screw frame; The secondary guiding mechanism comprises secondary slide block 23j, secondary leading screw 23e, secondary motor 23f and axially directed post 23g, guide block 23h, one-level leading screw frame one end is connected with the secondary leading screw by the secondary slide block, the secondary leading screw is threaded with the secondary slide block, the one-level leading screw frame other end is located on the axially directed post by guide block, the secondary leading screw is connected with the secondary motor and is fixed on the fuselage, and lead is fixed on the fuselage.
Coiled hair is promptly through axle, with coiled hair 8a and 8b, be placed on the lifting subassembly 19, start the cylinder 18 lifting work that drive, master pendulum arm 10 drives rotating shaft 9 and rotates, swing arm 21 moved upward in rotating shaft 9 drove, slide block 20 moves upward under the effect of the movable span 21a of interior swing arm 21 and guide groove 22a, lifting subassembly 19 moves upward under the effect of slide block, coiled hair is promoted to tailing axle 4 and main shaft 6 when coaxial, make cylinder 15, cylinder 17 work are stretched into tailing axle head 11 to push up among the coiled hair 8a to coiled hair bracing frame 8 coiled hair 8a opposite side are located on the coiled hair bracing frame 8, main tapping 14 stretches into to push up among the coiled hair 8b to coiled hair bracing frame 8 coiled hair 8b opposite side is located on the coiled hair bracing frame 8, drive the one-level motor 23d and the secondary motor 23f work of herringbone reed mechanism, make the herringbone reed launch the angle match with two coiled hairs as shown in Figure 7, when driving one-level motor 23d work, one-level leading screw 23b rotates, one-level slide block 23a can move left and right, therefore herringbone reed 23 can launch bigger angle or shrink relatively, when driving secondary motor 23f work, secondary leading screw 23c rotates, secondary slide block 23j can move left and right under the effect of secondary leading screw 23c, guide block 23h moves on axially directed post 23g, the herringbone reed can move left and right be found the position of matching with coiled hair accurately on fuselage like this, for the herringbone reed can be moved as required, the one-level guiding mechanism can also comprise by movable slider, be connected by movable slider on the guide rail column of one-level leading screw 23b end, can slide.
Embodiment two, as Fig. 8, shown in Figure 9, when adopting a coiled hair, coiled hair bracing frame 8 is moved to left clamping one side, have more back, coiled hair length location and adopt a kind of same operation principle of embodiment that coiled hair is fixed between coiled hair bracing frame 8 and the main shaft, adjust herringbone reed position equally the herringbone reed is matched with single coiled hair work.
Claims (10)
1. double-warp beam warper, it comprises coiled hair combination, clamping device, carriage mechanism in cord roller mechanism, herringbone reed mechanism and the fuselage on fuselage, the fuselage, the coiled hair combination is located in the clamping device, is provided with two benchmark guide pillars up and down in the fuselage; Clamping device comprises left clamping and right clamping, left side clamping comprises tailing axle combination with tailing axle and the support that supports the tailing axle combination, the support two ends are located on the benchmark guide pillar, support is provided with driver part and tailing axle is connected, right clamping comprises drive unit and the traversing carriage that main shaft, driving main shaft are rotated, main shaft is located on the drive unit, drive unit is fixed on the traversing carriage, traversing carriage is snug fit on the benchmark guide pillar, is provided with the main shaft drives parts between fuselage inner side surface and the traversing carriage; Carriage mechanism comprises driving mechanism and hoisting mechanism, and hoisting mechanism is located at the coiled hair combination down, and driving mechanism is located at the fuselage side and is connected with hoisting mechanism.
2. double-warp beam warper according to claim 1 is characterized in that: the combination of described coiled hair comprises coiled hair bracing frame and alone or two coiled hairs, and the coiled hair bracing frame is slidingly fitted on the benchmark guide pillar; During coiled hair, the coiled hair bracing frame moves to left clamping one side alone, and coiled hair is located between coiled hair bracing frame and the right clamping alone; During two coiled hairs, the coiled hair bracing frame is moved to centre position between left clamping and the right clamping, two coiled hairs are located at the both sides of coiled hair bracing frame respectively.
3. double-warp beam warper according to claim 1, it is characterized in that: described hoisting mechanism comprises the rotating shaft being located at fuselage bottom and stretching out fuselage, rotating shaft one end is connected with driving mechanism by a master pendulum arm, hoisting mechanism also comprises lifting subassembly, these lifting subassembly two ends are fixed with slide block, two interior swing arms are located at the lifting subassembly both sides, interior swing arm is provided with axial bar shaped movable span, slide block passes this bar shaped movable span and is connected on the guide plate of fuselage both sides, vertically be provided with guide groove on the guide plate, the slide block end is located in this guide groove.
4. double-warp beam warper according to claim 1 is characterized in that: described herringbone reed mechanism comprises two herringbone reed devices, and two herringbone reed devices are oppositely arranged, and herringbone reed device comprises herringbone reed, one-level guiding mechanism and secondary guiding mechanism; The one-level guiding mechanism comprises one-level slide block, one-level leading screw, one-level leading screw frame and one-level motor, the both sides of herringbone reed are connected with an one-level slide block respectively, the one-level slide block is connected with the one-level threads of lead screw, the one-level motor is fixed on the side of one-level leading screw frame and is connected with the one-level leading screw, and the one-level leading screw is located on the one-level leading screw frame; The secondary guiding mechanism comprises secondary slide block, secondary leading screw, secondary motor and axially directed post, guide block, one-level leading screw frame one end is connected with the secondary leading screw by the secondary slide block, the secondary leading screw is threaded with the secondary slide block, the one-level leading screw frame other end is located on the axially directed post by guide block, the secondary leading screw is connected with the secondary motor and is fixed on the fuselage, and lead is fixed on the fuselage.
5. double-warp beam warper according to claim 1, it is characterized in that: described tailing axle combination comprises tailing axle, tailing axle head and sliding sleeve, the tailing axle head is fixed at the tailing axle end, tailing axle is fixed in the sliding sleeve, sliding sleeve is snug fit in the support, tailing axle is provided with connecting plate, and described driver part is connected with this connecting plate.
6. double-warp beam warper according to claim 1 is characterized in that: described spindle nose is provided with main tapping.
7. double-warp beam warper according to claim 1 or 5, it is characterized in that: described driver part is a cylinder.
8. double-warp beam warper according to claim 1 is characterized in that: described drive unit is main motor.
9. double-warp beam warper according to claim 1 is characterized in that: described main shaft drives parts are the main shaft cylinder, and main shaft cylinder one end is fixed on the traversing carriage, and the other end is fixed on the fuselage.
10. double-warp beam warper according to claim 1 is characterized in that: described driving mechanism is for driving cylinder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110137665 CN102199822B (en) | 2011-05-26 | 2011-05-26 | Dual-beam warping machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110137665 CN102199822B (en) | 2011-05-26 | 2011-05-26 | Dual-beam warping machine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102199822A true CN102199822A (en) | 2011-09-28 |
| CN102199822B CN102199822B (en) | 2013-04-03 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201110137665 Active CN102199822B (en) | 2011-05-26 | 2011-05-26 | Dual-beam warping machine |
Country Status (1)
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| CN (1) | CN102199822B (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103215721A (en) * | 2013-04-26 | 2013-07-24 | 鲁泰纺织股份有限公司 | Method for simultaneous multiple-beam warping |
| CN103361813A (en) * | 2013-08-02 | 2013-10-23 | 福建省航韩机械科技有限公司 | Pan head installing and positioning device of devillicate warping machine |
| CN104032457A (en) * | 2014-02-12 | 2014-09-10 | 苏州金源泰纺织机械有限公司 | Let-off device provided with shuttle loom |
| CN105537900A (en) * | 2016-03-04 | 2016-05-04 | 郑州纺机工程技术有限公司 | Automatic beam mounting and dismounting device for slasher |
| CN107345330A (en) * | 2017-07-12 | 2017-11-14 | 常州市睿晟机械有限公司 | Warping winder is wrapped in a kind of double deep bid |
| CN109778380A (en) * | 2019-04-02 | 2019-05-21 | 海宁市泰德纺织有限公司 | A kind of holding structure fixed for coiled hair support the end of the shaft |
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| GB2044816A (en) * | 1979-03-15 | 1980-10-22 | American Fabrics Co | Beaming machine |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103215721A (en) * | 2013-04-26 | 2013-07-24 | 鲁泰纺织股份有限公司 | Method for simultaneous multiple-beam warping |
| CN103361813A (en) * | 2013-08-02 | 2013-10-23 | 福建省航韩机械科技有限公司 | Pan head installing and positioning device of devillicate warping machine |
| CN103361813B (en) * | 2013-08-02 | 2015-08-12 | 福建省航韩机械科技有限公司 | Divide silk warper coiled hair mounting and positioning device |
| CN104032457A (en) * | 2014-02-12 | 2014-09-10 | 苏州金源泰纺织机械有限公司 | Let-off device provided with shuttle loom |
| CN105537900A (en) * | 2016-03-04 | 2016-05-04 | 郑州纺机工程技术有限公司 | Automatic beam mounting and dismounting device for slasher |
| CN107345330A (en) * | 2017-07-12 | 2017-11-14 | 常州市睿晟机械有限公司 | Warping winder is wrapped in a kind of double deep bid |
| CN107345330B (en) * | 2017-07-12 | 2022-11-22 | 常州市睿晟机械有限公司 | Double-station large-coil loading warping winder |
| CN109778380A (en) * | 2019-04-02 | 2019-05-21 | 海宁市泰德纺织有限公司 | A kind of holding structure fixed for coiled hair support the end of the shaft |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102199822B (en) | 2013-04-03 |
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