CN202784872U - Stacker crane - Google Patents
Stacker crane Download PDFInfo
- Publication number
- CN202784872U CN202784872U CN201220448088.XU CN201220448088U CN202784872U CN 202784872 U CN202784872 U CN 202784872U CN 201220448088 U CN201220448088 U CN 201220448088U CN 202784872 U CN202784872 U CN 202784872U
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- CN
- China
- Prior art keywords
- fuselage
- connecting rod
- axle
- stirring arm
- drive
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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 - Lifetime
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Abstract
A stacker crane comprises turnover arms and side baffles that are arranged on crane bodies. The stacker crane is characterized in that the crane bodies are discrete right and left, are arranged on bases with linear guide rails and slide along the linear guide rails driven by crane body driving motors. The stacker crane has the characteristics that 1, the crane bodies are mounted on the linear guide rails and driven by the motors to be adjusted according to widths of different plates; separate adjustment of the turnover arms and the side baffles is avoided; the efficiency and equipment reliability are improved; 2, carrier rollers are horseshoe cone rollers innovatively and are driven by the motors through chain wheels and chains to ensure that the carrier rollers have power to prevent the plates from off tracking effectively; 3, link mechanisms are driven by the motors to drive the turnover arms to turn over materials; blanking is stable; noise is low; and 4, air cylinders are added to knock the materials to ensure that a plate pile is tidy.
Description
Technical field
The utility model stacker is used for the blanking piling of hot rolling plate iron sheet material.Blanking piling for slab sheet material has widely promotional value.
Background technology
At present, existing stacker structure as illustrated in fig. 1 and 2, for the sheet material 14 of different in width, by motor 1 band movable sprocket 2, pass to sprocket wheel 3 through chain, sprocket wheel 3 is fixing by key and leading screw 6, drive leading screw 6 rotations, in the stirring arm 7 nut is housed, leading screw 6 rotations, it is mobile to the left or to the right to drive the stirring arm, to hold up different in width sheet material 14.13 rotations of motor 12 band movable sprockets, through 10 rotations of chain-driving sprocket wheel, it is mobile to the left or to the right with side shield 11 to drive leading screw 9 through the leading screw pair of nut, and two side shields form a casing, to adapt to the blanking of different in width sheet material.Sheet material 14 provides power by clamping and conveying device 15, pinches sheet material 14 and advances forward on supporting material roller 8.After to be conveyed the putting in place, swung by cylinder 4 drivening rods 5, swing thereby drive stirring arm 7, realize that sheet material 14 falls.There is number of drawbacks in this stacker in the process of using: 1, stirring arm and side shield will be adjusted respectively according to the sheet material width, and efficient is lower.2, supporting material roller is unpowered, is subjected to the restrictions such as assembling, working accuracy, and sheet material easy sideslip when supporting material roller is advanced causes difficulty to blanking.3, without side dnockout function, if backward uneven under the plate, can't adjust.4, cylinder drives the stirring arm swing, and blanking is not steady, and noise is large.
Summary of the invention
We in conjunction with design and use experience for many years, have manufactured and designed this novel stacker for above defective.
The technical scheme that the utility model adopts is: a kind of stacker, it comprises stirring arm and the side shield that is arranged on the fuselage, it is characterized in that described fuselage is the discrete fuselage in the left and right sides, fuselage is arranged at sliding along line slideway on the base of line slideway and under the driving of fuselage drive motor.
The concrete characteristics of this programme also have, and are arranged at supporting material roller at the stirring arm, and the supporting material roller drive motor pivots by sprocket wheel and chain drive supporting material roller.
Described supporting material roller is the cone roller.
Described stirring arm is arranged on the fuselage pivotly, on fuselage, also be provided with the blanking drive motor and turn round axle by first of blanking drive motor driving, the first axle head of turning round axle is connected with first connecting rod and as first connecting rod hinged point rotatably, first turns round axle drive first connecting rod pivots around the first axle head of turning round axle, first connecting rod connects by bearing pin and second connecting rod, the other end of second connecting rod and second is turned round axle one end and is connected, drive second connecting rod by bearing pin during the first connecting rod rotation and turn round the axle swing around second, stirring arm and second is turned round the axle other end and is rigidly connected, and the second torsion bar drives stirring arm upset blanking in the rotation of fixed angle Inner.
At fuselage cylinder is set and promotes the side shield dnockout.
The beneficial effects of the utility model are: 1, the main frame body is installed on the line slideway, according to different sheet material width adjustment, has avoided stirring arm and side shield to adjust respectively by driven by motor, has improved the reliability of efficient and equipment.2, the horseshoe-shaped cone roller design of the employing of carrying roller novelty, the while through the sprocket wheel chain gear, makes the carrying roller drive by motor, can effectively prevent the sheet material sideslip.3, by the motor-driven connecting rod mechanism, drive stirring arm stirring, fall down stably, noise is little.4, increase the cylinder dnockout, make the sheet material piling neat.
Description of drawings
Below in conjunction with drawings and Examples this stacker is further specified.Fig. 1 is former stacker structure diagram.Fig. 2 is that the A of Fig. 1 is to view.Among the figure: 1-motor, 2-sprocket wheel, 3-sprocket wheel, 4-cylinder, 5-connecting rod, 6-leading screw, 7-stirring arm, 8-supporting material roller, 9-leading screw, 10-sprocket wheel, 11-side shield, 12-motor, 13-sprocket wheel, 14-sheet material, 15-clamping and conveying device.
Fig. 3 is the Novel palletizer structure diagram.Fig. 4 is that the A of Fig. 3 is to view.Fig. 5 is retainer cone roller work scheme drawing.Among the figure: 16-retainer cone roller, 17-sprocket wheel, 18-sprocket wheel, 19-fuselage drive motor, 20-leading screw, 21-screw, 22-cylinder, 23-line slideway, 24-fuselage, 25-stirring arm, 26-side shield, 27-second connecting rod, 28-bearing pin, 29-tooth bar, 30-gear; The 31-sprocket wheel, 32-supporting material roller drive motor, the 33-first connecting rod, 34-first turns round axle, 35-blanking drive motor, the 36-coupler, the 37-rolling bearing units, the 38-rolling bearing units, the 39-axle head, 40-second turns round axle.
The specific embodiment
Shown in Fig. 3 and 4, a kind of stacker, it comprises stirring arm 25 and the side shield 26 that is arranged at respectively on the left and right sides fuselage 24, fuselage 24 is arranged at sliding along line slideway 23 on the base of line slideway 23 and under the driving of fuselage drive motor 19.At stirring arm 25 retainer cone roller 16 is set, supporting material roller drive motor 32 pivots by the chain drive retainer cone roller 16 that holds sprocket wheel 31 and sprocket wheel 18.
Described stirring arm 25 is arranged on the fuselage 24 pivotly, on fuselage 24, also be provided with blanking drive motor 35 and turn round axle 34 by first of blanking drive motor 35 drivings, the first axle head of turning round axle 34 is connected with first connecting rod 33 and as first connecting rod 33 hinged point rotatably, first turns round axle 34 drive first connecting rods 33 pivots around the first axle head of turning round axle 34, first connecting rod 33 connects by bearing pin 28 and second connecting rod 27, the other end of second connecting rod 27 and second is turned round axle 40 1 ends and is connected, drive second connecting rod 27 by bearing pin 28 during first connecting rod 33 rotation and turn round axle 40 swings around second, stirring arm 25 and second is turned round axle 40 other ends and is rigidly connected, and second turns round axle 40 drives stirring arm 25 upset blankings in the rotation of fixed angle Inner.
At fuselage 24 cylinder 22 is set and promotes side shield 26 dnockouts; After plate falls, promote side shield 26 dnockouts by cylinder 22.
During work, for the sheet material 14 of different in width, drive leading screw 20 rotations by fuselage drive motor 19 through reductor, under the cooperation of screw 21, fuselage 24 on line slideway 23 sway to adapt to different in width sheet material blanking.31 rotations of supporting material roller drive motor 32 band movable sprockets, sprocket wheel 31 are by chain-driving sprocket wheel 17 and sprocket wheel 18 rotations, and sprocket wheel 18 drives 16 rotations of retainer cone roller, make retainer cone roller 16 have power, drive sheet material 14 and advance.When sheet material 14 advance put in place after, blanking motor 35 rotation drives first connecting rods 33 and rotates through turning round axle 34, drives second connecting rods 27 through bearing pin 28 and swings, and drives stirring arm 25 and swings blankings.
As shown in Figure 5, bore the work scheme drawing of roller for retainer.When 16 rotation of retainer cone roller, the angular velocity omega that each point A, B, C, D are ordered on the roller edge is identical, and each point linear velocity v=r * ω is because some A is maximum with respect to the radius r of roller center line with some C, so some A is maximum with the linear velocity v of some C.Because the design of this cone roller causes the roll surface each point to produce velocity contrast, when in the process that plate 14 is being advanced during sideslip, will automatically just run.
Claims (5)
1. stacker, it comprises stirring arm and the side shield that is arranged on the fuselage, it is characterized in that described fuselage is the discrete fuselage in the left and right sides, fuselage is arranged at sliding along line slideway on the base of line slideway and under the driving of fuselage drive motor.
2. stacker according to claim 1 is characterized in that being arranged at supporting material roller at the stirring arm, and the supporting material roller drive motor pivots by sprocket wheel and chain drive supporting material roller.
3. stacker according to claim 2 is characterized in that described supporting material roller is the cone roller.
4. stacker according to claim 1, it is characterized in that described stirring arm is arranged on the fuselage pivotly, on fuselage, also be provided with the blanking drive motor and turn round axle by first of blanking drive motor driving, the first axle head of turning round axle is connected with first connecting rod and as first connecting rod hinged point rotatably, first turns round axle drive first connecting rod pivots around the first axle head of turning round axle, first connecting rod connects by bearing pin and second connecting rod, the other end of second connecting rod and second is turned round axle one end and is connected, drive second connecting rod by bearing pin during the first connecting rod rotation and turn round the axle swing around second, stirring arm and second is turned round the axle other end and is rigidly connected, and the second torsion bar drives stirring arm upset blanking in the rotation of fixed angle Inner.
5. stacker according to claim 1 is characterized in that at fuselage cylinder being set promotes the side shield dnockout.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201220448088.XU CN202784872U (en) | 2012-09-05 | 2012-09-05 | Stacker crane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201220448088.XU CN202784872U (en) | 2012-09-05 | 2012-09-05 | Stacker crane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202784872U true CN202784872U (en) | 2013-03-13 |
Family
ID=47812183
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201220448088.XU Expired - Lifetime CN202784872U (en) | 2012-09-05 | 2012-09-05 | Stacker crane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202784872U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104828619A (en) * | 2015-03-31 | 2015-08-12 | 中国重型机械研究院股份公司 | Gravity stacking device |
| CN106429172A (en) * | 2016-08-31 | 2017-02-22 | 浙江恒立数控科技股份有限公司 | Plate receiving mechanism |
| CN106966174A (en) * | 2017-03-21 | 2017-07-21 | 山东同利智能科技有限公司 | A kind of sheet material stacking machine |
| CN106965272A (en) * | 2017-03-21 | 2017-07-21 | 山东同利智能科技有限公司 | A kind of composite board processing line and processing technology |
| CN110420998A (en) * | 2019-08-14 | 2019-11-08 | 陶忠梅 | A kind of hot rolled steel plate production technology |
| RU2726583C1 (en) * | 2019-12-09 | 2020-07-14 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Рыбинский государственный авиационный технический университет имени П.А. Соловьева" | Manipulator mechanism |
-
2012
- 2012-09-05 CN CN201220448088.XU patent/CN202784872U/en not_active Expired - Lifetime
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104828619A (en) * | 2015-03-31 | 2015-08-12 | 中国重型机械研究院股份公司 | Gravity stacking device |
| CN106429172A (en) * | 2016-08-31 | 2017-02-22 | 浙江恒立数控科技股份有限公司 | Plate receiving mechanism |
| CN106966174A (en) * | 2017-03-21 | 2017-07-21 | 山东同利智能科技有限公司 | A kind of sheet material stacking machine |
| CN106965272A (en) * | 2017-03-21 | 2017-07-21 | 山东同利智能科技有限公司 | A kind of composite board processing line and processing technology |
| CN110420998A (en) * | 2019-08-14 | 2019-11-08 | 陶忠梅 | A kind of hot rolled steel plate production technology |
| CN110420998B (en) * | 2019-08-14 | 2020-09-15 | 唐山宏润实业有限公司 | Production process of hot rolled steel plate |
| RU2726583C1 (en) * | 2019-12-09 | 2020-07-14 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Рыбинский государственный авиационный технический университет имени П.А. Соловьева" | Manipulator mechanism |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PP01 | Preservation of patent right |
Effective date of registration: 20180613 Granted publication date: 20130313 |
|
| PP01 | Preservation of patent right | ||
| PD01 | Discharge of preservation of patent |
Date of cancellation: 20200613 Granted publication date: 20130313 |
|
| PD01 | Discharge of preservation of patent | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20201022 Address after: Room 9a102, No.8, Yushan Industrial Park, Guangzhu Road, Shangni village, Lanhe Town, Nansha District, Guangzhou City, Guangdong Province Patentee after: Guangzhou Liding Auto Parts Co.,Ltd. Address before: 250306 No. 500 Fenghuang Road, Changqing District, Shandong, Ji'nan Patentee before: JINAN FOUNDRY AND METAL FORMING MACHINERY RESEARCH INSTITUTE Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| CX01 | Expiry of patent term |
Granted publication date: 20130313 |
|
| CX01 | Expiry of patent term |