CN202743926U - Full-automatic intelligent conveying line - Google Patents
Full-automatic intelligent conveying line Download PDFInfo
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- CN202743926U CN202743926U CN 201220312233 CN201220312233U CN202743926U CN 202743926 U CN202743926 U CN 202743926U CN 201220312233 CN201220312233 CN 201220312233 CN 201220312233 U CN201220312233 U CN 201220312233U CN 202743926 U CN202743926 U CN 202743926U
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- handpiece
- headstock
- lifting drive
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Abstract
The utility model discloses a full-automatic intelligent conveying line. The full-automatic intelligent conveying line comprises a handpiece, and more than one connected main body and an afterbody; the handpiece comprises a handpiece rack, a transverse drive device of the handpiece, a transverse push rack of the handpiece, a lifting drive device of the handpiece, and a handpiece lifting bracket; the transverse drive device of the handpiece is fixed on the handpiece rack; the transverse push rack of the handpiece is arranged on the transverse drive device of the handpiece; the transverse push rack of the handpiece can be pushed to move in a straight line through the transverse drive device of the handpiece; the lifting drive device of the handpiece is fixed on the handpiece rack; the handpiece lifting bracket is arranged on the lifting drive device of the handpiece; the handpiece lifting bracket can be driven to move up and down through the lifting drive device of the handpiece; and the front surface and the top surface of the handpiece rack are in slant transition, and a liquid crystal panel and/or an operating key are arranged on the inclined plane. With the adoption of the structure of the full-automatic intelligent conveying line, operation of operating personnel can be facilitated, and the liquid crystal panel and/or the operating key are/is not easily damaged.
Description
Technical field
The utility model relates to the fully-automatic intelligent conveying pipeline, particularly is applied in the fully-automatic intelligent conveying pipeline in garment production, the case and bag production.
Background technology
To have in the production technology of multiple tracks production process at clothes, case and bag etc., in order enhancing productivity, usually to adopt the mode of conveyor line to operate, in the stream line operation process, then keep away unavoidable transmission to material.Traditional mode that material is transmitted like this, not only manually have high input, and efficient is low, also easily makes mistakes by manually realizing.
And along with the develop rapidly of existing machinery, automatic technology, for overcoming the defective of above-mentioned traditional operation mode, begun to utilize semi-automation or full-automatic equipment to substitute traditional approach in the industry.As being to be to be to disclose a kind of garment sewing conveyor line automatic conveying device in the patent documentation on May 25th, 2011 Granted publication day on November 2nd, 2010 at application number 201020587328.5 applyings date, it comprises the Turnround basket of dense arrangement on the transmitting device, described transmitting device divides upper and lower two-layer, but every layer bottom is provided with the roller bearing of the flexible rotating of proper alignment; Respectively establish one by the lifting table of cylinder control at the initial and end two ends of transmitting device; Be provided with the cylinder of a horizontal direction at transmitting device upper strata left end, be used for promoting moving ahead of upper strata Turnround basket; Be provided with the cylinder of another horizontal direction at transmitting device lower floor right-hand member, be used for promoting moving ahead of lower floor's Turnround basket.Although this transmitting device can be realized automatic transport, but in order to be applicable to workman's operation height, the height of transmitting device can be lower, therefore, certain operations button etc. can only be arranged on the side, and operating personal need to couchantly just can operate when operation, like this, bring many inconvenience to operation, in addition, button etc. are also easily run into, and easily cause the impaired phenomenon of button.
Summary of the invention
The purpose of this utility model provides a kind of fully-automatic intelligent conveying pipeline, structure of the present utility model, can handled easily personnel's operation, and liquid crystal panel and/or operation push-button are difficult for damaged.
For achieving the above object.A kind of fully-automatic intelligent conveying pipeline comprises head, interconnective fuselage and tail more than one; Head comprises that headstock, head lateral driver device, head laterally promote frame, head lifting drive, head crane; The head lateral driver device is fixed on the headstock; Head laterally promotes to be erected on the head lateral driver device, can promote head by the head lateral driver device and laterally promote the frame straight-line motion; The head lifting drive is fixed on the headstock; The head crane is located on the head lifting drive, can drive head crane up-and-down movement by the head lifting drive; The front of headstock and end face are chamfered transition, are provided with liquid crystal panel and/or operation push-button on the inclined-plane.
Said structure, because front and the end face of headstock are chamfered transition, liquid crystal panel and/or operation push-button are provided in a side of on the inclined-plane, and operating personal is when operation, erectility can operate, watch liquid crystal panel and operation push-button, has made things convenient for the operation of operating personal; In addition, the direction of impact is common from horizontal and vertical, so, liquid crystal panel and/or operation push-button is located on the inclined-plane, then can avoid being clashed into by actv., thereby reduces the probability that damages liquid crystal panel, operation push-button.
As specializing, the angle of headstock inclined-plane and headstock end face is 45 °.
As improvement, close fuselage one side is provided with the head blend stop to downward-extension on the described head crane.After having the head blend stop, after rising such as the head crane, can prevent under the effect of keeping out of head blend stop Turnover Box enter into the head crane below and stuck phenomenon appears, guaranteed continuity and the reliability carried.
As improvement, be provided with the head chute at headstock; Head laterally promotes frame and comprises head sliding rack, head roller, head adjust bar, head pushing block, the head roller is located at the two ends of head sliding rack, the head roller can slide in the head chute, and the head adjust bar is located on the head sliding rack, and the head pushing block is located at an end of head adjust bar.In this improvement structure, under the directional tagging of head chute and head roller, the motion that head laterally promotes frame steadily, good directionality, and the head roller is when the head chute moves, its friction force is little, needed propulsive effort is little, energy-conservation.In addition, by the relative position of regulating frame head adjust bar with respect to the head sliding rack, the position of regulating frame head pushing block indirectly is to adapt to the Turnover Boxes of different sizes.
As specializing, described fuselage comprises fuselage cradle and is installed in two groups of above cylinder group on the fuselage cradle, and cylinder group is comprised of cylinder.
As specializing, described tail comprises that aircraft tail shelf, tail lateral driver device, tail laterally promote frame, tail lifting drive, tail crane; The tail lateral driver device is fixed on the aircraft tail shelf; Tail laterally promotes to be erected on the tail lateral driver device, can promote tail by the tail lateral driver device and laterally promote the frame straight-line motion; The tail lifting drive is fixed on the aircraft tail shelf; The tail crane is located on the tail lifting drive, can drive tail crane up-and-down movement by the tail lifting drive.
As improvement, close fuselage one side is provided with the tail blend stop to downward-extension on the described tail crane.After having the tail blend stop, after rising such as the tail crane, can prevent under the effect of keeping out of tail blend stop Turnover Box enter into the tail crane below and stuck phenomenon appears, guaranteed continuity and the reliability carried.
As improvement, be provided with the tail chute at aircraft tail shelf; Tail laterally promotes frame and comprises tail sliding rack, tail roller, tail adjust bar, tail pushing block, the tail roller is located at the two ends of tail sliding rack, the tail roller can slide in the tail chute, and the tail adjust bar is located on the tail sliding rack, and the tail pushing block is located at an end of tail adjust bar.In this improvement structure, under the directional tagging of tail chute and tail roller, the motion that tail laterally promotes frame steadily, good directionality, and the tail roller is when the tail chute moves, its friction force is little, needed propulsive effort is little, energy-conservation.In addition, by regulating the tail adjust bar with respect to the relative position of tail sliding rack, can indirectly regulate the position of tail pushing block, to adapt to the Turnover Box of different sizes.
As improvement, the left and right sides of headstock has extended upward head left side board and head right side board from the headstock end face; The left and right sides of fuselage has extended upward fuselage left side board and fuselage right side board from the fuselage end face; The left and right sides of tail has extended upward tail left side board and tail right side board from the tail end face.After head left side board and head right side board, fuselage left side board and fuselage right side board, tail left side board and tail right side board are set, can improve the safety performance of operation.
As specializing, described head lateral driver device, head lifting drive, tail lateral driver device and tail lifting drive are cylinder.
Description of drawings
Fig. 1 is front view of the present utility model.
Fig. 2 is birds-eye view of the present utility model.
Fig. 3 is the front view of right of headstock.
Fig. 4 is the left view of right of headstock.
Fig. 5 is the enlarged drawing of A.
Fig. 6 is the structural representation of right of aircraft tail shelf.
Fig. 7 is the block diagram that head laterally promotes frame.
Fig. 8 is the birds-eye view that head laterally promotes frame.
Fig. 9 is the right elevation that head laterally promotes frame.
Figure 10 is the front view that head laterally promotes frame.
The specific embodiment
Below in conjunction with the drawings and specific embodiments the utility model is further elaborated.
As depicted in figs. 1 and 2, the fully-automatic intelligent conveying pipeline comprises head 1, the interconnective fuselage 2 more than and tail 3.
Head 1 comprises that headstock 11, head lateral driver device 12, head laterally promote frame 13, head lifting drive 14 and head crane 15.
The front of headstock 11 and end face are inclined-plane 1111 transition, and 1111 are provided with liquid crystal panel and/or operation push-button on the inclined-plane, preferred 45 ° of the angle of inclined-plane 1111 and headstock end face.Headstock 11 is by left 111 of headstock, right 112 of headstock and headstock link span 113, and headstock link span 113 links together left 111 of headstock and right 112 of headstock; To shown in Figure 5, right 112 of headstock is provided with head chute 1121 such as Fig. 3, and be same, also is provided with the head chute on the position of left 111 correspondences of headstock.Lateral driver device 12 is cylinder, and cylinder is fixed on the headstock 11 by cylinder frame 4.Extremely shown in Figure 10 such as Fig. 7, head laterally promotes frame 13 and comprises head sliding rack 131, head roller 132, head adjust bar 133, head pushing block 134, head roller 132 is installed in the two ends of head sliding rack 131, head roller 132 can slide in the head chute, head adjust bar 133 is screw rod, head adjust bar 133 is located on the head sliding rack 131, with respect to the distance in the middle of the head sliding rack 131, head pushing block 134 is located at an end of head adjust bar 133 by rotating head adjust bar energy regulating frame head pushing block 134; Head lateral driver device 12 is captiveed joint with head sliding rack 131, when the head lateral driver device is started working, then can drive the motion of head sliding rack by the head lateral driver device.Head lifting drive 14 is cylinder, and cylinder is fixed on the headstock 11 by cylinder frame 5; Head crane 15 is located on the head lifting drive 14, can drive head crane 15 up-and-down movements by head lifting drive 14; In order to withstand Turnover Box, on head crane 15, be extended with head blend stop 6 downwards.
Described fuselage 2 comprises fuselage cradle 21 and is installed on the fuselage cradle 21 two groups above cylinder group, and cylinder group is comprised of cylinder 22.Cylinder group is comprised of two-layer, and is two-layer about namely being divided into, and realizes the periodical duty of Turnover Box.
Aircraft tail shelf 31 is by left 311 of aircraft tail shelf, right 312 of aircraft tail shelf and aircraft tail shelf link span 313, and aircraft tail shelf link span 313 links together left 311 of aircraft tail shelf and right 312 of aircraft tail shelf; As shown in Figure 6, right 312 of aircraft tail shelf is provided with tail chute 3121, and be same, also is provided with the tail chute on the position of left 311 correspondences of aircraft tail shelf.Tail lateral driver device 32 is cylinder, and cylinder is fixed on the aircraft tail shelf 31 by cylinder frame 8.It is the same with the structure that head laterally promotes frame 13 that tail laterally promotes frame 33, tail laterally promotes frame and comprises tail sliding rack, tail roller, tail adjust bar, tail pushing block, the tail roller is installed in the two ends of tail sliding rack, the tail roller can slide in the tail chute, the tail adjust bar is screw rod, the tail adjust bar is located on the tail sliding rack, can regulate the tail pushing block distance middle with respect to the tail sliding rack by rotation tail adjust bar, and the tail pushing block is located at an end of tail adjust bar; The tail lateral driver device is captiveed joint with the tail sliding rack, when the tail lateral driver device is started working, then can drive the motion of tail sliding rack by the tail lateral driver device.Tail lifting drive 34 is cylinder, and cylinder is fixed on the aircraft tail shelf 31 by cylinder frame 9; Tail crane 35 is located on the tail lifting drive 34, can drive tail crane 35 up-and-down movements by tail lifting drive 34; In order to withstand Turnover Box, on tail crane 35, be extended with tail blend stop 10 downwards.
The working process of above-mentioned fully-automatic intelligent conveying pipeline is: by liquid crystal panel corresponding parameter is set in PLC, Turnover Box is placed on the cylinder group, operating personal is in operating process, in the time the mass transport of a station need to being arrived next station, head lateral driver device 12 drives head promotion frame 13 and moves backward, the Turnover Box that head promotes the head pushing block promotion upper strata of frame 13 moves right a station, meanwhile, tail lifting drive 34 drives tail crane 35 and rises, and is used for the Turnover Box of support caudal end; After said process was finished, head lateral driver device 12 drive heads promotion framves 13 were return and are resetted, and tail lifting drive 34 drives 35 declines of tail cranes and resets; Then, tail lateral driver device 32 drives tail promotion frame 33 and travels forward, the band layer Turnover Box station that moves that makes a movement, afterwards, head lifting drive 14 drives head crane 15 and rises, Turnover Box on the head crane is risen up on the position corresponding with the upper strata cylinder group, be convenient to next step work.Said process is realized the full automaticity of Turnover Box is carried so repeatedly, to reduce artificial input, increases work efficiency and accuracy.
In the utility model, liquid crystal panel and/or operation push-button are provided in a side of on the inclined-plane, and operating personal is when operation, and erectility can operate, watch liquid crystal panel and operation push-button, has made things convenient for the operation of operating personal; In addition, the direction of impact is common from horizontal and vertical, so, liquid crystal panel and/or operation push-button is located on the inclined-plane, then can avoid being clashed into by actv., thereby reduces the probability that damages liquid crystal panel, operation push-button.
In addition, conveying pipeline of the present utility model before promoting Turnover Box, has the function of informing in advance operating personal in when work so that operating personal can be in time, accurately material is put in the Turnover Box.Have, conveying pipeline of the present utility model can arrange the mechanical action pitch time by liquid crystal panel, and the automatic pouring timing again, and countdown can excite buzzer warning to zero the time, reminds operating personal.Conveying pipeline of the present utility model also provides 485 data-interfaces, can realize data exchange with PC.
As to further improvement of the utility model, the left and right sides of headstock 11 has extended upward head left side board and head right side board from the headstock end face; The left and right sides of fuselage 12 has extended upward fuselage left side board and fuselage right side board from the fuselage end face; The left and right sides of tail 13 has extended upward tail left side board and tail right side board from the tail end face.After head left side board and head right side board, fuselage left side board and fuselage right side board, tail left side board and tail right side board are set, can improve the safety performance of operation.
Claims (10)
1. a fully-automatic intelligent conveying pipeline comprises head, interconnective fuselage and tail more than one;
Head comprises that headstock, head lateral driver device, head laterally promote frame, head lifting drive, head crane; The head lateral driver device is fixed on the headstock; Head laterally promotes to be erected on the head lateral driver device, can promote head by the head lateral driver device and laterally promote the frame straight-line motion; The head lifting drive is fixed on the headstock; The head crane is located on the head lifting drive, can drive head crane up-and-down movement by the head lifting drive;
It is characterized in that: the front of headstock and end face are chamfered transition, are provided with liquid crystal panel and/or operation push-button on the inclined-plane.
2. fully-automatic intelligent conveying pipeline according to claim 1, it is characterized in that: the angle of headstock inclined-plane and headstock end face is 45 °.
3. fully-automatic intelligent conveying pipeline according to claim 1 is characterized in that: be provided with head blend stop to downward-extension near fuselage one side on the described head crane.
4. fully-automatic intelligent conveying pipeline according to claim 1 is characterized in that: be provided with the head chute at headstock; Head laterally promotes frame and comprises head sliding rack, head roller, head adjust bar, head pushing block, the head roller is located at the two ends of head sliding rack, the head roller can slide in the head chute, and the head adjust bar is located on the head sliding rack, and the head pushing block is located at an end of head adjust bar.
5. fully-automatic intelligent conveying pipeline according to claim 1 is characterized in that: described fuselage comprises fuselage cradle and is installed in two groups of above cylinder group on the fuselage cradle, and cylinder group is comprised of cylinder.
6. fully-automatic intelligent conveying pipeline according to claim 1, it is characterized in that: described tail comprises that aircraft tail shelf, tail lateral driver device, tail laterally promote frame, tail lifting drive, tail crane; The tail lateral driver device is fixed on the aircraft tail shelf; Tail laterally promotes to be erected on the tail lateral driver device, can promote tail by the tail lateral driver device and laterally promote the frame straight-line motion; The tail lifting drive is fixed on the aircraft tail shelf; The tail crane is located on the tail lifting drive, can drive tail crane up-and-down movement by the tail lifting drive.
7. fully-automatic intelligent conveying pipeline according to claim 6 is characterized in that: be provided with tail blend stop to downward-extension near fuselage one side on the described tail crane.
8. fully-automatic intelligent conveying pipeline according to claim 6 is characterized in that: be provided with the tail chute at aircraft tail shelf; Tail laterally promotes frame and comprises tail sliding rack, tail roller, tail adjust bar, tail pushing block, the tail roller is located at the two ends of tail sliding rack, the tail roller can slide in the tail chute, and the tail adjust bar is located on the tail sliding rack, and the tail pushing block is located at an end of tail adjust bar.
9. according to claim 1 to 8 each described fully-automatic intelligent conveying pipelines, it is characterized in that: the left and right sides of headstock has extended upward head left side board and head right side board from the headstock end face; The left and right sides of fuselage has extended upward fuselage left side board and fuselage right side board from the fuselage end face; The left and right sides of tail has extended upward tail left side board and tail right side board from the tail end face.
10. fully-automatic intelligent conveying pipeline according to claim 6, it is characterized in that: described head lateral driver device, head lifting drive, tail lateral driver device and tail lifting drive are cylinder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220312233 CN202743926U (en) | 2012-06-30 | 2012-06-30 | Full-automatic intelligent conveying line |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220312233 CN202743926U (en) | 2012-06-30 | 2012-06-30 | Full-automatic intelligent conveying line |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202743926U true CN202743926U (en) | 2013-02-20 |
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ID=47703360
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220312233 Expired - Fee Related CN202743926U (en) | 2012-06-30 | 2012-06-30 | Full-automatic intelligent conveying line |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202743926U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104259856A (en) * | 2014-09-24 | 2015-01-07 | 成都雅斯特家私有限公司 | Automatic sofa assembling line and control method thereof |
| CN106516633A (en) * | 2016-12-09 | 2017-03-22 | 广东天机工业智能系统有限公司 | Circulating production line |
-
2012
- 2012-06-30 CN CN 201220312233 patent/CN202743926U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104259856A (en) * | 2014-09-24 | 2015-01-07 | 成都雅斯特家私有限公司 | Automatic sofa assembling line and control method thereof |
| CN106516633A (en) * | 2016-12-09 | 2017-03-22 | 广东天机工业智能系统有限公司 | Circulating production line |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130220 Termination date: 20140630 |
|
| EXPY | Termination of patent right or utility model |