CN205328317U - Splitting machine - Google Patents

Splitting machine Download PDF

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Publication number
CN205328317U
CN205328317U CN201520976312.6U CN201520976312U CN205328317U CN 205328317 U CN205328317 U CN 205328317U CN 201520976312 U CN201520976312 U CN 201520976312U CN 205328317 U CN205328317 U CN 205328317U
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CN
China
Prior art keywords
idler roller
fuselage
raw material
strainer
cutting machine
Prior art date
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 - Fee Related
Application number
CN201520976312.6U
Other languages
Chinese (zh)
Inventor
李诗云
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JINJIANG CHAOJUN MACHINERY CO., LTD.
Original Assignee
李诗云
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 李诗云 filed Critical 李诗云
Priority to CN201520976312.6U priority Critical patent/CN205328317U/en
Application granted granted Critical
Publication of CN205328317U publication Critical patent/CN205328317U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a splitting machine, include the fuselage and establish splitting machine structure, the winding mechanism on the fuselage respectively and be located the straining device between splitting machine structure and the winding mechanism, straining device includes first tensioning roller, second tensioning roller, two supporting shoes and two thrustors, and two relative position departments at the fuselage are established in the supporting shoe correspondence, are equipped with the installation department on every supporting shoe, the thrustor respectively with the both ends fixed connection of first tensioning roller, slide and establish in two installation departments in the both ends of first tensioning roller, second tensioning roller rotates through the bearing axial that establish on the fuselage and one side of installation department is kept away from at first tensioning roller to adjacent setting, and first tensioning roller is just mutually perpendicular with raw materials stroke direction respectively with the setting of second tensioning roller level. The utility model discloses utilize straining device suitably to adjust the raw materials surface tension after cutting, guarantee that the raw materials is at the suitable tension of the in -process of advancing and can not take place the skew or be out of shape for raw materials after the rolling is neat pleasing to the eye, adequate quality.

Description

A kind of cutting machine
Technical field
This utility model relates to the Scissoring device technical field of textile material, particularly relates to a kind of cutting machine。
Background technology
The work in-processes such as non-woven fabrics, PVC, leather need to cut according to follow-up workshop section and customer requirement, cutting machine is by the capital equipment cut, the raw material of significantly roomy diameter is cut through fixed width, arranged, rewinding is the machine of inside and outside uniformly suitable finished product volume again, main task is view picture raw material to cut into some fabric widths meeting user specification and excises burr, control the coil diameter of finished product volume, so as to meet specification of dispatching from the factory。But, existing cutting machine work efficiency is not high, easily occurs shrinking the out-of-flatness phenomenon that narrows due to overtension particularly in rewinding。
Utility model content
Technical problem to be solved in the utility model is to provide a kind of cutting machine, adjustable raw material surface tension in conductive process, it is ensured that after rewinding, raw material is smooth attractive in appearance, indeformable, corrugationless。
In order to solve above-mentioned technical problem, this utility model be the technical scheme is that
A kind of cutting machine, including fuselage and be separately positioned on the cutting mechanism on fuselage and rolling-up mechanism, described rolling-up mechanism is located at the front along raw material stroke directions of cutting mechanism;Also include the strainer being located on fuselage and between cutting mechanism and rolling-up mechanism。
Preferably, the rear along raw material stroke directions of described cutting mechanism is provided with for guiding raw material to the rear material guide mechanism of cutting mechanism, and the two ends of described rear material guide mechanism are respectively fixedly connected with fuselage。
Preferably, being provided with for guiding raw material to the front material guide mechanism of strainer between described cutting mechanism and strainer, the two ends of described front material guide mechanism are respectively fixedly connected with fuselage。
Preferably, described rolling-up mechanism includes the first winding portion and the second winding portion, and described first winding portion is arranged on strainer front one branch along raw material stroke directions, and described second winding portion is arranged on the strainer another branch in front along raw material stroke directions。
Preferably, described first winding portion and the second winding portion include winding inflatable shaft, magnetic powder cluth, spragging gear and travelling gear respectively, described spragging gear and magnetic powder cluth are in transmission connection, described travelling gear and spragging gear are in transmission connection, and described winding inflatable shaft is assemblied on fuselage by the fixing bearing connected and one end of described winding inflatable shaft is fixed with travelling gear and is connected。
Preferably, described fuselage is provided with two closing devices, each closing device includes opening-closing plate, folding cylinder and folding piston rod, one end that described folding piston rod stretches out folding cylinder is articulated with the middle part of opening-closing plate, one end of described opening-closing plate horizontally rotates and is arranged on fuselage, and the other end is provided with the socket part matched with the winding inflatable shaft other end。
Preferably, described strainer includes the first idler roller, the second idler roller, two bracers and two thrustors, a bracer described in two is laterally correspondingly arranged at two relative position of fuselage, each described bracer is provided with installation portion, two described thrustors are fixed with the two ends of the first idler roller respectively and are connected, and the two ends of described first idler roller are slidably arranged in two installation portions;Described second idler roller is arranged on fuselage by bearing axial rotation and is disposed adjacent in the side in the first remotely mounted portion of idler roller, and described first idler roller and the second idler roller are all horizontally disposed with and perpendicular with raw material stroke directions respectively。
Preferably, described first idler roller and the second idler roller are positioned at same level。
Preferably, described thrustor is pushing tow cylinder and ejector piston bar, and described ejector piston bar one end is inserted in pushing tow cylinder, and the other end connects the first idler roller。
The beneficial effects of the utility model: owing to being provided with strainer between cutting mechanism and rolling-up mechanism, utilize strainer that the stock chart surface tension after cutting suitably is adjusted, ensure the raw material suitable tension force in traveling process without there is skew or deformation, make the raw material neat appearance after rolling, best in quality。
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model。
Fig. 2 is this utility model strainer structural representation。
Fig. 3 is the use view one of this utility model closing device。
Fig. 4 is the use view two of this utility model closing device。
Fig. 5 is this utility model unreeling structure structural representation。
Description of reference numerals:
10, fuselage;11, connecting cross beam;12, protective cover;20, unreeling structure;21, frame is unreeled;22, air-expanding shaft is unreeled;23, magnetic powder brake;30, rear material guide mechanism;40, cutting mechanism;50, front material guide mechanism;60, strainer;61, the first idler roller;62, the second idler roller;63, bracer is propped up;64, thrustor;630, installation portion;70, rolling-up mechanism;71, the first winding portion;72, the second winding portion;80, closing device;81, opening-closing plate;82, folding cylinder;83, folding piston rod;90, airduct。
Detailed description of the invention
Below in conjunction with accompanying drawing, this utility model is described in detail。
As Figure 1-5, the present embodiment provides a kind of cutting machine, including fuselage 10 and be separately positioned on the cutting mechanism 40 on fuselage 10 and rolling-up mechanism 70, described rolling-up mechanism 70 is located at the front along raw material stroke directions of cutting mechanism 40, also includes the strainer 60 being located on fuselage 10 and between cutting mechanism 40 and rolling-up mechanism 70。For ease of steady guide and the suitable tension force ensureing suitable guide process Raw volume, the rear along raw material stroke directions of described cutting mechanism 40 is provided with for guiding raw material to the rear material guide mechanism 30 of cutting mechanism 40, it is provided with for guiding raw material to the front material guide mechanism 50 of strainer 60 between described cutting mechanism 40 and strainer 60, the two ends of described rear material guide mechanism 30 are respectively fixedly connected with fuselage 10, and the two ends of described front material guide mechanism 50 are respectively fixedly connected with fuselage 10。
In the present embodiment, described fuselage 10 includes two opposite pedestals and the connecting cross beam 11 of two described pedestals of level connection joint, and described cutting mechanism 40, rolling-up mechanism 70, strainer 60, front material guide mechanism 50 and rear material guide mechanism 30 are arranged between two described pedestals。Additionally, as shown in Figure 5 also can set an independent unreeling structure 20 outside the present embodiment fuselage 10 again, described unreeling structure 20 includes unreeling frame 21, unreel air-expanding shaft 22, magnetic powder brake 23, the described air-expanding shaft 22 that unreels is for placing stock roll, its two ends are assemblied in respectively through the bearing arrangement of fixing connection and unreel in frame 21, and described in unreel one end of air-expanding shaft 22 and be in transmission connection by gear and magnetic powder brake 23, realize adjusting by magnetic powder brake 23 and unreel the air-expanding shaft 22 Tensity size adjustment to stock roll, stock roll is made to have suitable tension force without deforming or displacement etc.。
In the present embodiment, described front material guide mechanism 50 can be made up of one or more leading material roller, and each described leading material roller is arranged on fuselage 10 by bearing axial rotation, and each leading material roller is all horizontally disposed with and perpendicular with the stroke directions of raw material。Similarly, described rear material guide mechanism 30 also can be made up of one or more rear guide roller, and each described rear guide roller is arranged on fuselage 10 by bearing axial rotation, and each rear guide roller is all horizontally disposed with and perpendicular with the stroke directions of raw material。Described cutting mechanism 40 include axial rotation be arranged on fuselage 10 cut rotating shaft and multiple slip cap is located at the cutter assembly cutting in rotating shaft。For ease of cutting accurate positioning, wherein having a described front material guide mechanism 50 to be positioned in same level with one of them described rear material guide mechanism 30, described cutting mechanism 40 is positioned at the top of this horizontal plane。
In the present embodiment, described rolling-up mechanism 70 includes the first winding portion 71 and the second winding portion 72, described first winding portion 71 is arranged on the strainer 60 front one branch along raw material stroke directions, described second winding portion 72 is arranged on the strainer 60 another branch in front along raw material stroke directions, so that raw material draws forward toward two different directions after strainer 60, being easy to separately, the adjacent feed after cutting is wound by the first winding portion 71 and the second winding portion 72 respectively。
As a kind of preferred implementation: described first winding portion 71 and the second winding portion 72 include winding inflatable shaft respectively, magnetic powder cluth, spragging gear and travelling gear, described spragging gear and magnetic powder cluth are in transmission connection, described travelling gear and spragging gear are in transmission connection, described winding inflatable shaft is assemblied on fuselage 10 by the fixing bearing connected and one end of described winding inflatable shaft is fixed with travelling gear and is connected, by the magnetic powder cluth adjustable winding inflatable shaft Tensity size to raw material, ensure that raw material has suitable tension force without deforming or displacement etc.。For ease of fixed disassembly air-expanding shaft with take off the volume of the finished product after rewinding, described fuselage 10 is provided with two closing devices 80, each closing device 80 includes opening-closing plate 81, folding cylinder 82 and folding piston rod 83, one end that described folding piston rod 83 stretches out folding cylinder 82 is articulated with the middle part of opening-closing plate 81, one end of described opening-closing plate 81 horizontally rotates and is arranged on fuselage 10, the other end is provided with the socket part matched with the winding inflatable shaft other end, and operationally the other end of each air-expanding shaft is connected with opening-closing plate 81 socket part of corresponding position respectively。
In the present embodiment, described strainer 60 includes first idler roller the 61, second idler roller 62, two bracer 63 and two thrustors 64, a bracer 63 described in two is laterally correspondingly arranged at two relative position of fuselage 10, each described bracer 63 is provided with installation portion 630, two described thrustors 64 are fixed with the two ends of the first idler roller 61 respectively and are connected, and the two ends of described first idler roller 61 are slidably arranged in two installation portions 630;Described second idler roller 62 is arranged on fuselage 10 and is disposed adjacent the side in the first remotely mounted portion 630 of idler roller 61 by travelling gear and bearing axial rotation, and described first idler roller 61 and the second idler roller 62 are all horizontally disposed with and perpendicular with raw material stroke directions respectively, preferably described first idler roller 61 and the second idler roller 62 are positioned at same level, described thrustor 64 can be pushing tow cylinder and ejector piston bar, described ejector piston bar one end is inserted in pushing tow cylinder, and the other end connects the first idler roller 61。
The stroke of the raw material of the present embodiment is: material guide mechanism 50 strainer 60 rolling-up mechanism 70 before material guide mechanism 30 cutting mechanism 40 after unreeling structure 20。Wherein, raw material penetrates from the gap between the first idler roller 61 and the second idler roller 62 after cutting after the guiding function of front material guide mechanism 50, the gap width between the first idler roller 61 and the second idler roller 62 is adjusted to adapt to the characteristic of different material by the piston rod expanding-contracting action of thrustor 64, thus ensureing the raw material enough tension force in traveling process without there is skew or deformation, make the raw material neat appearance after rolling, best in quality。
On the basis of technique scheme, the present embodiment cutting machine also can farther include blower fan and airduct 90, described airduct 90 is connected with blower fan, and airduct 90 can be improved by the connecting cross beam 11 between two base bottom and obtain, namely connecting cross beam 11 be set to hollow pipe and at an upper portion thereof interval offer the air outlet of opening upwards, utilize the foreign bodies such as the cloth bits on the upwards distinguished and admirable removing raw material of blower fan and airduct 90 blowout, soft flocks, dust, it is ensured that cut the material quality of rear rewinding。
Separately, for safety operation, the present embodiment also can rotate in cutting mechanism 40 side and arrange protective cover 12, can be L-shaped to the cross sectional shape of protective cover 12, operationally cover above cutting mechanism 40, rotatably abut up on connecting cross beam 11 when needing the position adjusting cutter assembly。
This utility model is not limited to above-mentioned preferred forms, and anyone should learn the structure change made under enlightenment of the present utility model, and every have same or like technical scheme with this utility model, each falls within protection domain of the present utility model。

Claims (9)

1. a cutting machine, including fuselage (10) and be separately positioned on the cutting mechanism (40) on fuselage (10) and rolling-up mechanism (70), described rolling-up mechanism (70) is located at the front along raw material stroke directions of cutting mechanism (40), it is characterized in that, also include being located at the strainer (60) that fuselage (10) is upper and is positioned between cutting mechanism (40) and rolling-up mechanism (70), described strainer (60) includes the first idler roller (61), second idler roller (62) and two thrustors (64), two described thrustors (64) are fixed with the two ends of the first idler roller (61) respectively and are connected, described second idler roller (62) is arranged on fuselage (10) by bearing axial rotation and above and is disposed adjacent with the first idler roller (61), the first idler roller (61) is promoted to adjust the first idler roller (61) and the gap of the second idler roller (62) closer or far from the second idler roller (62) by thrustor (64), and described first idler roller (61) and the second idler roller (62) are all horizontally disposed with and perpendicular with raw material stroke directions respectively。
2. cutting machine according to claim 1, it is characterized in that, the rear along raw material stroke directions of described cutting mechanism (40) is provided with for guiding raw material to the rear material guide mechanism (30) of cutting mechanism (40), and the two ends of described rear material guide mechanism (30) are respectively fixedly connected with fuselage (10)。
3. cutting machine according to claim 1, it is characterized in that, being provided with between described cutting mechanism (40) and strainer (60) for guiding raw material to the front material guide mechanism (50) of strainer (60), the two ends of described front material guide mechanism (50) are respectively fixedly connected with fuselage (10)。
4. cutting machine according to claim 1, it is characterized in that, described rolling-up mechanism (70) includes the first winding portion (71) and the second winding portion (72), described first winding portion (71) is arranged on the strainer (60) front one branch along raw material stroke directions, and described second winding portion (72) is arranged on the strainer (60) the another branch in front along raw material stroke directions。
5. cutting machine according to claim 4, it is characterized in that, described first winding portion (71) and the second winding portion (72) include winding inflatable shaft, magnetic powder cluth, spragging gear and travelling gear respectively, described spragging gear and magnetic powder cluth are in transmission connection, described travelling gear and spragging gear are in transmission connection, and described winding inflatable shaft is assemblied on fuselage by the fixing bearing connected and one end of described winding inflatable shaft is fixed with travelling gear and is connected。
6. cutting machine according to claim 5, it is characterized in that, described fuselage (10) is provided with two closing devices (80), each closing device (80) includes opening-closing plate (81), folding cylinder (82) and folding piston rod (83), one end that described folding piston rod (83) stretches out folding cylinder (82) is articulated with the middle part of opening-closing plate (81), one end of described opening-closing plate (81) horizontally rotates and is arranged on fuselage (10), and the other end is provided with the socket part matched with the winding inflatable shaft other end。
7. the cutting machine according to any one of claim 1 to 6, it is characterized in that, described strainer (60) also includes two bracers (63), a bracer (63) described in two is laterally correspondingly arranged at two relative position of fuselage (10), each described bracer (63) is provided with installation portion (630), the two ends of described first idler roller (61) are slidably arranged in two installation portions (630), and described second idler roller (62) is disposed adjacent the side in the first idler roller (61) remotely mounted portion (630)。
8. cutting machine according to claim 7, it is characterised in that described first idler roller (61) and the second idler roller (62) are positioned at same level。
9. cutting machine according to claim 7, it is characterised in that described thrustor (64) is pushing tow cylinder and ejector piston bar, described ejector piston bar one end is inserted in pushing tow cylinder, and the other end connects the first idler roller (61)。
CN201520976312.6U 2015-12-01 2015-12-01 Splitting machine Expired - Fee Related CN205328317U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520976312.6U CN205328317U (en) 2015-12-01 2015-12-01 Splitting machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520976312.6U CN205328317U (en) 2015-12-01 2015-12-01 Splitting machine

Publications (1)

Publication Number Publication Date
CN205328317U true CN205328317U (en) 2016-06-22

Family

ID=56214671

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520976312.6U Expired - Fee Related CN205328317U (en) 2015-12-01 2015-12-01 Splitting machine

Country Status (1)

Country Link
CN (1) CN205328317U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106829614A (en) * 2017-03-28 2017-06-13 东莞市曼罗兰精密机械有限公司 A kind of multilayer mantle laminating automatic cutting equipment
CN112466746A (en) * 2020-04-29 2021-03-09 山东芯源微电子有限公司 Membrane diffusion source forming machine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106829614A (en) * 2017-03-28 2017-06-13 东莞市曼罗兰精密机械有限公司 A kind of multilayer mantle laminating automatic cutting equipment
CN112466746A (en) * 2020-04-29 2021-03-09 山东芯源微电子有限公司 Membrane diffusion source forming machine
CN112466746B (en) * 2020-04-29 2022-04-15 山东芯源微电子有限公司 Membrane diffusion source forming machine

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20170825

Address after: 362212, Quanzhou, Fujian province Jinjiang city pond town shop pool Village North 345

Patentee after: JINJIANG CHAOJUN MACHINERY CO., LTD.

Address before: 362200, Quanzhou, Fujian province Jinjiang city pond town shop pool Village North 221

Patentee before: Li Shiyun

CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160622

Termination date: 20201201