CN201415510Y - Double rank forming system for making flexible package bags - Google Patents
Double rank forming system for making flexible package bags Download PDFInfo
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- CN201415510Y CN201415510Y CN2009201575814U CN200920157581U CN201415510Y CN 201415510 Y CN201415510 Y CN 201415510Y CN 2009201575814 U CN2009201575814 U CN 2009201575814U CN 200920157581 U CN200920157581 U CN 200920157581U CN 201415510 Y CN201415510 Y CN 201415510Y
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- biserial
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Abstract
The utility model discloses a double rank forming system for making flexible package bags, relates to the bag making machine technical field and includes a forming element, a traction element, a discharge swing arm (3) and a cutter device (18). The forming element includes a double rank middle-sealed primary preformed element, a double rank middle-sealed secondary preformed element and a double rank middle-sealed forming element. The traction element includes a traction rubber roller (16) and a film conveying roller (17) composed of a film conveying roller A (9) and a film conveying roller B (11). The discharge swing arm (3) is arranged under the traction element and connected with a displacement inductor on one side. The sort order of the system elements connected on wallboards at two sides of the frame (10) from front to back and from bottom to top is that double rank middle-sealed primary preformed element (38), traction rubber roller (16), discharge swing arm (3), a film conveyingroller A (9), cutter device (18), film conveying roller B (11), double rank middle-sealed secondary preformed element and double rank middle-sealed forming element. The system has advantages of energysaving, high efficiency and full automation.
Description
Technical field
The utility model relates to a kind of bag field of mechanical technique, particularly relates to the biserial formation system that is used for the flexible package bag in a kind of full automatic bag-making machine.
Background technology
Along with improving constantly of people's quality of life, more and more higher to commodity, food pack modeling requirement.The dark client of being subjected to of three-dimensional bag elegant in appearance that generally differs from one another at present favors, press for the Bag Making Machine that can satisfy this demand, businessmans catch this business opportunity one after another, cause and emerge Bag Making Machine in enormous quantities in recent years on the market, especially envelope Bag Making Machine in full-automatic, make a general survey of these Bag Making Machines, even be furnished with formation system, but because of machinery all adopts single printed volume film is raw material (formation system that is bag is single-row), can only produce a film bag at every turn, cause overall efficiency low, waste energy, be unfavorable for fierce competitive market.
The utility model content
The purpose of this utility model is to overcome above-mentioned weak point of the prior art, and a kind of biserial formation system that is used for the flexible package bag is provided.
Technical problem to be solved in the utility model is achieved through the following technical solutions:
A kind of biserial formation system that is used for the flexible package bag comprises profiled part, traction element, blowing swing arm, cutter device; Profiled part comprises in the biserial in envelope preformed for the first time parts, the biserial and seals profiled part in envelope preformed for the second time parts, the biserial, traction element comprises the traction rubber roll, comprised film roller A and crosses the two-part film roller of crossing of film roller B, the traction element below is located in the blowing swing arm, and a side is connected with displacement sensor; The native system parts by the order that is connected in the fuselage two side wall panels from A-P from bottom to top are: seal the parts of preformed for the first time, traction rubber roll, blowing swing arm in the biserial, cross film roller A, cutter device, cross to seal in the parts of preformed for the second time, the biserial in film roller B, the biserial and seal profiled part.
In the biserial envelope for the first time the preformed parts comprise the pedestal that connects the fuselage both sides, moulding support component, two ends by bolt be connected in pedestal some rubber rolls, be connected in three couples preformed for the first time spoon that the pedestal bilateral symmetry distributes, the three pairs of moulding of the preformed for the first time awl pinch rollers, are formed forming roll; The moulding support component comprises that the bottom is connected in the vertical preformed first time support of fuselage by bolt, be connected to the L shaped suspension holdfast of this support by bolt and securing member, be connected to the moulding supporting steel plate of suspension holdfast bottom by bolt, the spoon of preformed for the first time comprises horizontal type moulding spoon spoon body, securing member, be tightened in the fastening adjustment handle of securing member one side, the moulding of preformed for the first time awl pinch roller comprises vertical support bar, the curved lever of horizontal type and both securing members, be tightened in the fastening adjustment handle of securing member one side, format roll comprises the format roll roll shaft of horizontal type, securing member and be tightened in the fastening adjustment handle of securing member one side.
Envelope preformed for the second time parts comprise the pedestal that connects the fuselage both sides in the biserial, the support component of preformed for the second time, the pinch roller of preformed for the second time, the depression bar of preformed for the second time, the pedestal of preformed for the second time, the support component of preformed for the second time comprises that the bottom is connected in the vertical preformed second time support of fuselage by bolt, two L shaped suspension holdfasts that are connected to this support by bolt and securing member that are set up in parallel, horizontal edge is mounted with the strip shaped steel plate under the support, the pedestal of preformed for the second time comprises the parts composition of two spikes of stapling together, its foot is secured to pedestal by bolt, be connected with securing member on the pedestal, securing member is tightened by adjusting screw(rod), and the securing member lower end is connected with two pairs of preformed second time depression bars that are set up in parallel, two groups of preformed second time pinch rollers that are set up in parallel.
The envelope profiled part comprises that two side wall panels is located at the pedestal that moves up and down guide plate and the eccentric shaft that is connected these both sides, connection fuselage both sides of fuselage outer surface, two ends, bottom are moved up and down the guide plate two side wall panels by pull bar connection moulding middle envelope shaped support in the biserial, support is divided into lower and upper cross-member, slotted hole is opened at the entablature middle part, symmetry is screwed into the mobile handwheel of two row envelopes film seats, and this handwheel lower end is mounted with the middle envelope cooling-part that middle envelope heater block, an end that an end connects heating power supply are connected with cooling fluid from the A-P order.
A upper glue roller clutch cylinder is respectively established at traction rubber roll two ends, and traction rubber roll one end is with synchronously by transmission and is linked to each other with traction electric machine.
The blowing swing arm comprises suspension bracket, is connected in the swing arm tube of suspension bracket lower end, and the suspension bracket upper end is connected to the fuselage two side wall panels by its cross bar, and cross bar is connected in the fuselage two side wall panels by bearing.
Cutter device comprises the cutter support and is located at the cutter of top in this support.
The cutter support is the spike of stapling together, and two pin are fixed in the fuselage two side wall panels respectively.
With respect to prior art, the beneficial effects of the utility model are:
1, efficient energy-saving, native system with the single-row biserial (it is raw material that Bag Making Machine adopts duplex volume film) that changes into, utilizes the energy close with single printed volume can process two bags simultaneously machinery at every turn, raises the efficiency in the time of effective energy savings.
2, full-automation, the hardware components matching computer system of device realizes whole-course automation control.
Description of drawings
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is the structural representation of envelope preformed for the first time parts, cutter device in the biserial of the present utility model.
Fig. 3 seals profiled part in envelope preformed for the second time parts, the biserial in the biserial of the present utility model.
The specific embodiment
The utility model will be further described below in conjunction with the drawings and specific embodiments.
As shown in Figure 1, a kind of biserial formation system that is used for the flexible package bag, it is made up of profiled part, traction element, blowing swing arm 3, cutter device 18.Profiled part is made up of envelope profiled part in envelope preformed for the second time parts, the biserial in envelope preformed for the first time parts, the biserial in the biserial.Traction element by traction rubber roll 16, comprised film roller A9 and crossed the two-part film roller 17 of crossing of film roller B11 and form.Blowing swing arm 3 is installed on the traction element below, and a side is connected to displacement sensor.The native system parts by the order that is connected in fuselage 10 two side wall panels from A-P from bottom to top are: seal the parts of preformed for the first time 38, traction rubber roll 16, blowing swing arm 3 in the biserial, cross film roller A9, cutter device 18, cross to seal in the parts of preformed for the second time, the biserial in film roller B11, the biserial and seal profiled part.
In the biserial envelope for the first time preformed parts 38 by the pedestal 39 that is installed in fuselage 10 both sides, moulding support component, two ends by bolt be installed in pedestal 39 seven rubber rolls 40, be installed in three couples preformed for the first time spoon that pedestal 39 bilateral symmetry distribute 41, the three pairs of moulding of preformed for the first time awl pinch rollers 53, are formed forming roll 54 and are formed.The moulding support component by the bottom by bolt be installed on fuselage 10 vertical preformed first time support 60, be installed to the L shaped suspension holdfast 62 of this cantilever tip, be installed to the moulding supporting steel plate 61 of suspension holdfast bottom by bolt by bolt and securing member.For the first time preformed spoon 41 by horizontal type moulding spoon spoon body 56, securing member 57, be tightened in the fastening adjustment handle 59 of securing member one side.The awl of preformed moulding for the first time pinch roller 53 is made up of curved lever 55 and both securing members 43 of vertical support bar 42, horizontal type, the fastening adjustment handle 44 that is tightened in securing member one side.Format roll 54 is made up of format roll roll shaft 46, the securing member 45 of horizontal type and the fastening adjustment handle 58 that is tightened in securing member one side.Coating materials is sent to envelope preformed for the first time parts in this biserial through pay-off, under the school shape of format roll 54 and moulding supporting steel plate 61, impel coating materials that moulding supporting steel plate 61 is surrounded the formation tubular, this moment, the coating materials cross section formed " C " word shape that is rotated counterclockwise 90 degree.
Envelope preformed for the second time parts are made up of the pedestal 64 that is installed in fuselage 10 both sides, the support component of preformed for the second time 65, the pinch roller of preformed for the second time 74, the depression bar of preformed for the second time 72, the pedestal of preformed for the second time 68 in the biserial.For the second time preformed support component 65 is made up of by the L shaped suspension holdfast 70 that bolt and securing member are installed to this support the bottom is installed on fuselage 10 by bolt vertical preformed second time support 69, be set up in parallel two.Horizontal edge is mounted with strip shaped steel plate 81 under the support, for the second time preformed pedestal 68 is made up of the parts of two spikes of stapling together, its foot is secured to pedestal 64 by bolt, securing member 73 is housed on the pedestal, securing member is tightened by adjusting screw(rod) 71, and the securing member lower end is connected with two pairs of preformed second time depression bars that are set up in parallel 72, two groups of preformed second time pinch rollers 74 that are set up in parallel.Coating materials is split into biserial after the processing of machine front member, under the effect of format roll and shaped steel plate 81, the biserial coating materials is rolled into tubular respectively, after preformed second time pinch roller 74, the depression bar of preformed for the second time 72 are pressed, and basic forming.
The envelope profiled part connects envelope shaped support 76 that moulding move up and down guide plate 116 two side wall panels with the eccentric shaft 117 that is connected this two side wall panels, the pedestal 75 that connects fuselage 10 both sides, two ends, bottom by pull bar by the guide plate 116 that moves up and down that two side wall panels is arranged in fuselage 10 outer surfaces in the biserial, support is divided into lower and upper cross-member, slotted hole 77 is opened at the entablature middle part, symmetry is screwed into the mobile handwheel 78 of two row envelopes film seats, and this handwheel lower end is mounted with the middle envelope cooling-part 80 that middle envelope heater block 79, an end that an end connects heating power supply are connected with cooling fluid from the A-P order.Coating materials is pulled so far along shaped steel plate 81, envelope heater block 79 heat seals in being subjected to, envelope cooling-part 80 cooling and shapings in the warp again.
A upper glue roller clutch cylinder 63 is respectively established at traction rubber roll 16 two ends, and traction rubber roll 16 1 ends are with synchronously by transmission and are linked to each other with traction electric machine 32.This traction rubber roll 16 is responsible for the traction coating materials, processes for corresponding component.
3 pairs of coating materials of blowing swing arm play the effect of gravitation control, and it is made up of suspension bracket 4, the swing arm tube 5 that is connected in the suspension bracket lower end, and suspension bracket 4 upper ends are connected to fuselage 10 two side wall panels by its cross bar 6, and cross bar 6 is connected in fuselage 10 two side wall panels by bearing.
Cutter device is made up of 18 cutter supports 7 and the cutter 8 of being located in this support the top, and cutter support 7 is the spike of stapling together, and two pin are fixed in fuselage 10 two side wall panels respectively.This cutter is used for coating materials is divided into biserial.
Coating materials at traction drive of rubber roll and rubber roll 40, cross under 17 transmissions of film roller, in biserial, seal the preliminary integer of preformed parts for the first time earlier, be divided into biserial through cutter 8 again, then envelope preformed for the second time parts carry out integer to the biserial coating materials again in biserial, by envelope profiled part in the biserial edge sealing bar in the film bag is carried out cooling and shaping after the heat seal then, so far finish the biserial moulding of coating materials.
Claims (8)
1, a kind of biserial formation system that is used for the flexible package bag is characterized in that comprising profiled part, traction element, blowing swing arm (3), cutter device (18); Profiled part comprises in the biserial in envelope preformed for the first time parts, the biserial and seals profiled part in envelope preformed for the second time parts, the biserial, traction element comprises traction rubber roll (16), comprised film roller A (9) and crosses the two-part film roller (17) of crossing of film roller B (11), the traction element below is located in blowing swing arm (3), and a side is connected with displacement sensor; The native system parts by the order that is connected in fuselage (10) two side wall panels from A-P from bottom to top are: seal preformed parts (38), traction rubber roll (16), blowing swing arm (3) for the first time in the biserial, cross film roller A (9), cutter device (18), cross to seal in film roller B (11), the biserial in the parts of preformed for the second time, the biserial and seal profiled part.
2, the biserial formation system that is used for the flexible package bag according to claim 1, it is characterized in that in the biserial envelope for the first time preformed parts (38) comprise the pedestal (39) that connects fuselage (10) both sides, moulding support component, two ends by bolt be connected in pedestal (39) some rubber rolls (40), preformed spoon (41), the three pairs of moulding of the preformed for the first time awl pinch rollers (53), are formed forming roll (54) for the first time to be connected in three couple that pedestal (39) bilateral symmetry distributes; The moulding support component comprises that the bottom is connected in the vertical preformed first time support (60) of fuselage (10) by bolt, be connected to the L shaped suspension holdfast (62) of this support by bolt and securing member, be connected to the moulding supporting steel plate (61) of suspension holdfast bottom by bolt, preformed spoon (41) comprises horizontal type moulding spoon spoon body (56) for the first time, securing member (57), be tightened in the fastening adjustment handle (59) of securing member one side, the moulding awl pinch roller of preformed for the first time (53) comprises vertical support bar (42), the curved lever of horizontal type (55) and both securing members (43), be tightened in the fastening adjustment handle (44) of securing member one side, format roll (54) comprises the format roll roll shaft (46) of horizontal type, securing member (45) and be tightened in the fastening adjustment handle (58) of securing member one side.
3, the biserial formation system that is used for the flexible package bag according to claim 1, it is characterized in that envelope preformed for the second time parts comprise the pedestal (64) that connects fuselage (10) both sides in the biserial, preformed support component (65) for the second time, preformed pinch roller (74) for the second time, preformed depression bar (72) for the second time, preformed pedestal (68) for the second time, preformed support component (65) comprises that the bottom is connected in the vertical preformed second time support (69) of fuselage (10) by bolt for the second time, two L shaped suspension holdfasts (70) that are connected to this support by bolt and securing member that are set up in parallel, horizontal edge is mounted with strip shaped steel plate (81) under the support, preformed pedestal (68) comprises the parts composition of two spikes of stapling together for the second time, its foot is secured to pedestal (64) by bolt, be connected with securing member (73) on the pedestal, securing member is tightened by adjusting screw(rod) (71), and the securing member lower end is connected with two pairs of preformed second time depression bars (72) that are set up in parallel, two groups of preformed second time pinch rollers (74) that are set up in parallel.
4, the biserial formation system that is used for the flexible package bag according to claim 1, what it is characterized in that in the biserial that the envelope profiled part comprises that two side wall panels is located at fuselage (10) outer surface moves up and down guide plate (116) and the eccentric shaft that is connected these both sides (117), the pedestal (75) that connects fuselage (10) both sides, the two ends, bottom connect the middle envelope shaped support (76) that moulding moves up and down guide plate (116) two side wall panels by pull bar, support is divided into lower and upper cross-member, slotted hole (77) is opened at the entablature middle part, symmetry is screwed into the two row envelope mobile handwheels of film seat (78), and this handwheel lower end is mounted with the middle envelope heater block (79) that an end connects heating power supply from the A-P order, one end is connected with the middle envelope cooling-part (80) of cooling fluid.
5, the biserial formation system that is used for the flexible package bag according to claim 1 is characterized in that drawing rubber roll (16) two ends and respectively establishes a upper glue roller clutch cylinder (63), and traction rubber roll (16) one ends are with synchronously by transmission and are linked to each other with traction electric machine (32).
6, the biserial formation system that is used for the flexible package bag according to claim 1, it is characterized in that blowing swing arm (3) comprises suspension bracket (4), is connected in the swing arm tube (5) of suspension bracket lower end, suspension bracket (4) upper end is connected to fuselage (10) two side wall panels by its cross bar (6), and cross bar (6) is connected in fuselage (10) two side wall panels by bearing.
7, the biserial formation system that is used for the flexible package bag according to claim 1 is characterized in that cutter device comprises (18) cutter support (7) and is located in this support the cutter (8) of top.
8, the biserial formation system that is used for the flexible package bag according to claim 1 is characterized in that cutter support (7) is the spike of stapling together, and two pin are fixed in fuselage (10) two side wall panels respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201575814U CN201415510Y (en) | 2009-05-26 | 2009-05-26 | Double rank forming system for making flexible package bags |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201575814U CN201415510Y (en) | 2009-05-26 | 2009-05-26 | Double rank forming system for making flexible package bags |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201415510Y true CN201415510Y (en) | 2010-03-03 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009201575814U Expired - Fee Related CN201415510Y (en) | 2009-05-26 | 2009-05-26 | Double rank forming system for making flexible package bags |
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| Country | Link |
|---|---|
| CN (1) | CN201415510Y (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102529159A (en) * | 2012-02-17 | 2012-07-04 | 江阴市汇通包装机械有限公司 | Middle sealing bag making machine |
| CN104108200A (en) * | 2014-06-18 | 2014-10-22 | 中山市新宏业自动化工业有限公司 | Double-outlet automatic nozzle welding bag making machine and bag making process using same |
| CN105522755A (en) * | 2015-07-03 | 2016-04-27 | 无锡市铁民印刷机械有限公司 | Double-output middle sealing full-automatic bag-making apparatus and bag-making method thereof |
-
2009
- 2009-05-26 CN CN2009201575814U patent/CN201415510Y/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102529159A (en) * | 2012-02-17 | 2012-07-04 | 江阴市汇通包装机械有限公司 | Middle sealing bag making machine |
| CN104108200A (en) * | 2014-06-18 | 2014-10-22 | 中山市新宏业自动化工业有限公司 | Double-outlet automatic nozzle welding bag making machine and bag making process using same |
| CN105522755A (en) * | 2015-07-03 | 2016-04-27 | 无锡市铁民印刷机械有限公司 | Double-output middle sealing full-automatic bag-making apparatus and bag-making method thereof |
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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: 20100303 Termination date: 20160526 |