CN204173650U - With the feeding distribution mechanism of jet structure - Google Patents
With the feeding distribution mechanism of jet structure Download PDFInfo
- Publication number
- CN204173650U CN204173650U CN201420620046.9U CN201420620046U CN204173650U CN 204173650 U CN204173650 U CN 204173650U CN 201420620046 U CN201420620046 U CN 201420620046U CN 204173650 U CN204173650 U CN 204173650U
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- China
- Prior art keywords
- books
- air
- splicing plate
- inlet pipe
- distribution mechanism
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Abstract
The utility model discloses a kind of feeding distribution mechanism with jet structure, include the turning cylinder be arranged between fuselage two side, turning cylinder is provided with 2 blocks of side plates, splicing plate is provided with between side plate, splicing plate is evenly equipped with gas hole, every block side plate is provided with 1 chute, the push rod be connected with cylinder is snapped in chute, cylinder is arranged on fuselage madial wall, be provided with the draw-in groove of more than 2 on the rotating shaft, 2 pieces of baffle plates have been snapped in draw-in groove, fixed frame is provided with bottom splicing plate, fixed frame is connected with air bag, air bag is connected with Air compressor by air inlet pipe, desicator is provided with between air inlet pipe and Air compressor.In the utility model use procedure air inlet pipe by compressed air delivery in air bag, air blows out and acts on the bottom surface of books from the gas hole splicing plate, books are made to drop in process, friction force between its bottom surface and splicing plate surface reduces, and avoids the phenomenon that the word that occurs books bottom surface in books landing process or pattern scratch.
Description
Technical field
The utility model relates to the feeding distribution mechanism of the automatic stacker of a kind of staple books, particularly a kind of feeding distribution mechanism with jet structure.
Background technology
Existing books are all generally use saddle stitching automatic production lines to process, its master operation include join leaf, order staple, severing and this few procedure stacking, is all generally the automatic collection using the automatic stacker of saddle stitching books to carry out books in stacking process.But in use there is a problem in the automatic stacker of existing saddle stitching books, that is exactly when books are delivered to feeding distribution mechanism from connecting gear, fall to the process of the stacking groove of books from feeding distribution mechanism again, the surface contact of the splicing plate of books bottom surface and feeding distribution mechanism, due to the effect of friction force, the word of books bottom surface or pattern easily scratch by splicing plate surface.Simultaneously for the books of some heavier mass, when it falls on splicing plate, because the friction force between splicing plate is comparatively large, may be stuck on the surface of splicing plate, and downward landing cannot be continued.
Summary of the invention
The purpose of this utility model is, provides a kind of feeding distribution mechanism with jet structure.This feeding distribution mechanism can avoid books to fall to the process of the stacking groove of books from feeding distribution mechanism, and the word of books bottom surface or pattern are easily scratched, fog.
The technical solution of the utility model: a kind of feeding distribution mechanism with jet structure, include the turning cylinder be arranged between fuselage two side, turning cylinder is provided with 2 blocks of side plates, splicing plate is provided with between side plate, splicing plate is evenly equipped with gas hole, every block side plate is provided with 1 chute, the push rod be connected with cylinder is snapped in chute, cylinder is arranged on fuselage madial wall, be provided with the draw-in groove of more than 2 on the rotating shaft, 2 pieces of baffle plates have been snapped in draw-in groove, fixed frame is provided with bottom splicing plate, fixed frame is connected with air bag, air bag is connected with Air compressor by air inlet pipe, desicator is provided with between air inlet pipe and Air compressor.
The feeding distribution mechanism of the jet structure of aforesaid band, described air inlet pipe is provided with by-pass cock.
The feeding distribution mechanism of the jet structure of aforesaid band, the air inlet pipe between described desicator and air bag is provided with humidity chart.
The feeding distribution mechanism of the jet structure of aforesaid band, described baffle plate is curved baffle, and its head end outwards bends.
The beneficial effects of the utility model: compared with prior art, in the utility model use procedure air inlet pipe by the compressed air delivery in Air compressor in air bag, air blows out and acts on the bottom surface of books from the gas hole splicing plate, books are made to drop in process, friction force between its bottom surface and splicing plate surface reduces, thus avoid the phenomenon that the word that occurs books bottom surface in books landing process or pattern scratch, and friction force reduces, books can also be made to fall to books fast to drop in groove, books are avoided to be stuck in splicing plate on the surface, downward landing cannot be continued, and be provided with drying box, drying can be carried out to the air after Air compressor compression, avoid air effect containing large quantity of moisture bottom books, make easily to bond together between books, and being provided with by-pass cock, workman can according to the difference of books thickness, the size of adjustment gas hole blowout wind-force, and be provided with humidity chart, dried air humidity can be detected in good time, be convenient to workman and change desiccant in desicator in time.And be provided with two pieces of baffle plates, and the books sent from load-transfer device can be made to fall to after the stacking groove of books through splicing plate, stacking more neat.The books of corresponding different size size, can be positioned over baffle plate in different draw-in grooves.Baffle plate is curved baffle, and its head end outwards bends, and when books can be avoided to fall to splicing wrench end from load-transfer device, books head end can collide with the head end of baffle plate, causes books to damage, and even blocks books landing passage.
Accompanying drawing explanation
Accompanying drawing 1 is structural representation of the present utility model;
Accompanying drawing 2 is the fragmentary top TV structure schematic diagram of accompanying drawing 1;
Reference numeral: 1-fuselage, 2-turning cylinder, 3-side plate, 4-splicing plate, 5-chute, 6-push rod, 7-cylinder, 8-draw-in groove, 9-baffle plate, 10-fixed frame, 11-air bag, 12-air inlet pipe, 13-Air compressor, 14-desicator, 15-gas hole, 16-by-pass cock, 17-humidity chart.
Detailed description of the invention
Below in conjunction with drawings and Examples, the utility model is further described, but not as the foundation limited the utility model.
Embodiment of the present utility model: a kind of feeding distribution mechanism with jet structure, as shown in accompanying drawing 1-2, include 1 turning cylinder 2 be arranged between fuselage 1 two side, turning cylinder 2 is fixed with 2 blocks of side plates be parallel to each other 3, 1 block of splicing plate 4 is provided with between 2 blocks of side plates 3, splicing plate 4 is evenly distributed with a lot of gas holes 15, every block side plate 3 is provided with 1 chute 5, the push rod 6 be connected with cylinder 7 is snapped in each chute 5, on the oblique madial wall being arranged on fuselage 1 of cylinder 7, turning cylinder 2 is provided with the draw-in groove 8 of more than 2, 2 pieces of baffle plates 9 have been snapped in draw-in groove 8, 1 fixed frame 10 is then fixed with in the bottom of splicing plate 4, this fixed frame 10 is installed with 1 air bag 11, this air bag 11 is connected with Air compressor 13 by air inlet pipe 12, fuselage side wall between air inlet pipe 12 and Air compressor 13 is provided with 1 desicator 14.
In the utility model use procedure, the books that severing is good are delivered on feeding distribution mechanism through load-transfer device, and landing, on the splicing plate 4 of feeding distribution mechanism, gets off to fall in the stacking groove of books corresponding to feeding distribution mechanism end along splicing plate 4 landing.Books are from landing process splicing plate 4, counting machine on fuselage 1 top board counts it, when books reach stacking specified quantity by quantity, counting machine can give control circuit 1 signal, control circuit control cylinder 7 action, in push rod 6 push of cylinder 7, side plate 3 moving axis 2 that rotates together with splicing plate 4 is driven to rotate certain angle, make the end of feeding distribution mechanism be positioned at the top of the stacking groove of another one books, now will fall in 1 other stacking groove of books from the books of landing splicing plate 4.Pile the books folded in the stacking groove of books originally then to push out by the push pedal in the stacking groove of books.In whole process, by release, the recovery effect of cylinder 7, realize the alternately stacking of books.When avoiding only being provided with the stacking groove of 1 books, touch in the downward landing of books to the process of the stacking groove of books and between the slurcam releasing books, occur mutually to interfere, may the situations such as stalling be caused.In order to make books neatly stacking in whole stacking process, therefore be provided with between 2 pieces of baffle plates, 9,2 pieces of baffle plates 9 and form books landing passage, books from landing passage by falling in the stacking groove of books, avoid sideslip in books landing process, cause the stacking shape of last books irregular.Because books have many sizes such as A3, A4, A5, when processing the books of different size, 1 piece of baffle plate 9 being taken out from draw-in groove 8, puts in the draw-in groove 8 of corresponding size.In use procedure, the pressurized air that Air compressor 13 produces enters into air bag 11 through air inlet pipe 12, then blow out from the gas hole 15 splicing plate 4, act on the bottom surface of books, 1 towing force is upwards formed to books, thus the friction force between books bottom surface and splicing plate 4 surface is reduced, the reduction of friction force can avoid occurring in books landing process the phenomenon that the word of books bottom surface or pattern scratch; And for the books of some heavier mass, when it falls on splicing plate 4, because the friction force between splicing plate 4 is comparatively large, may be stuck on the surface of splicing plate 4, and downward landing cannot be continued.Now, the friction force reducing each other by the air of blowout from gas hole 15, friction force reduces, and books just can fall in the stacking groove of books rapidly.Pressurized air can first through desicator 14 before air inlet pipe 12 enters into air bag 11, moisture in pressurized air can absorb by the desiccant in dried case 14, avoid the pressurized air being rich in moisture to act directly on books bottom surface, easily make mutually to bond together between books.
Air inlet pipe 12 is provided with 1 by-pass cock 16, and this by-pass cock 16 is arranged on the sidewall of fuselage 1, such convenient operation.Because the books quality of processing is not necessarily the same at every turn, for the books of different quality, the size acting on the wind-force bottom it also should be different, and this moment can carry out the size of the wind-force of corrective action bottom books by adjustment in use switch 16.
Air inlet pipe 12 between desicator 14 and air bag 11 is provided with 1 humidity chart 17.This humidity chart 17 is arranged on the sidewall of fuselage 1, and conveniently work observation.Humidity chart 17 Main Function is for carrying out Humidity Detection to through the dried air of desicator 14, when the humidity that humidity chart 17 shows rises to certain numerical value, illustrate that the desiccant in desicator 14 is unable to undergo desiccation, prompting staff changes the desiccant in desicator 14 in time.
Be curved baffle when baffle plate 9 makes, its head end outwards bends, and time such arranging can avoid books to fall to feeding distribution mechanism head end from load-transfer device, books head end can collide with the head end of baffle plate 9, causes books to damage, and even blocks books landing passage.
Claims (4)
1. the feeding distribution mechanism of the jet structure of band, it is characterized in that: include the turning cylinder (2) be arranged between fuselage (1) two side, turning cylinder (2) is provided with 2 pieces of side plates (3), splicing plate (4) is provided with between side plate (3), splicing plate (4) is evenly equipped with gas hole (15), every block side plate (3) is provided with 1 chute (5), the push rod (6) be connected with cylinder (7) is snapped in chute (5), cylinder (7) is arranged on fuselage (1) madial wall, turning cylinder (2) is provided with the draw-in groove (8) of more than 2, 2 pieces of baffle plates (9) have been snapped in draw-in groove (8), splicing plate (4) bottom is provided with fixed frame (10), fixed frame (10) is connected with air bag (11), air bag (11) is connected with Air compressor (13) by air inlet pipe (12), desicator (14) is provided with between air inlet pipe (12) and Air compressor (13).
2. the feeding distribution mechanism of the jet structure of band according to claim 1, is characterized in that: described air inlet pipe (12) is provided with by-pass cock (16).
3. the feeding distribution mechanism of the jet structure of band according to claim 1, is characterized in that: the air inlet pipe (12) between described desicator (14) and air bag (11) is provided with humidity chart (17).
4. the feeding distribution mechanism of the jet structure of band according to claim 1, is characterized in that: described baffle plate (9) is curved baffle, and its head end outwards bends.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201420620046.9U CN204173650U (en) | 2014-10-25 | 2014-10-25 | With the feeding distribution mechanism of jet structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201420620046.9U CN204173650U (en) | 2014-10-25 | 2014-10-25 | With the feeding distribution mechanism of jet structure |
Publications (1)
Publication Number | Publication Date |
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CN204173650U true CN204173650U (en) | 2015-02-25 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201420620046.9U Withdrawn - After Issue CN204173650U (en) | 2014-10-25 | 2014-10-25 | With the feeding distribution mechanism of jet structure |
Country Status (1)
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CN (1) | CN204173650U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104444524A (en) * | 2014-10-25 | 2015-03-25 | 湖州佳宁印刷有限公司 | Material dividing mechanism with air injection structure |
-
2014
- 2014-10-25 CN CN201420620046.9U patent/CN204173650U/en not_active Withdrawn - After Issue
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104444524A (en) * | 2014-10-25 | 2015-03-25 | 湖州佳宁印刷有限公司 | Material dividing mechanism with air injection structure |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
AV01 | Patent right actively abandoned |
Granted publication date: 20150225 Effective date of abandoning: 20160907 |
|
C25 | Abandonment of patent right or utility model to avoid double patenting |