CN104874619A - Spiral loop apparatus for steel belts - Google Patents

Spiral loop apparatus for steel belts Download PDF

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Publication number
CN104874619A
CN104874619A CN201510231336.3A CN201510231336A CN104874619A CN 104874619 A CN104874619 A CN 104874619A CN 201510231336 A CN201510231336 A CN 201510231336A CN 104874619 A CN104874619 A CN 104874619A
Authority
CN
China
Prior art keywords
steel band
rotating shaft
disk
shaft group
fuselage
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.)
Pending
Application number
CN201510231336.3A
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Chinese (zh)
Inventor
姚冬泉
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.)
Wuxi Chinese Workers' Thin Plate Co Ltd
Original Assignee
Wuxi Chinese Workers' Thin Plate Co Ltd
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 Wuxi Chinese Workers' Thin Plate Co Ltd filed Critical Wuxi Chinese Workers' Thin Plate Co Ltd
Priority to CN201510231336.3A priority Critical patent/CN104874619A/en
Publication of CN104874619A publication Critical patent/CN104874619A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a spiral loop apparatus for steel belts. The apparatus body is a disc, the periphery of the disc apparatus body is provided with an outer rotating shaft set, an inner rotating shaft set is disposed in the disc apparatus body, a turning roll is disposed in the center of the disc apparatus body, and the turning roll is arranged in the center of the inner rotating shaft set. The disc apparatus body is provided with a material collecting device, the material collecting device is arranged between the outer rotating shaft set and the inner rotating shaft set. The disc apparatus body is connected with a steel belt, the steel belt is fed into the inner rotating shaft set and sent out from the turning roll through rotation of the outer rotating shaft set, and the material collecting device is used for tightening the steel belt conveyed into the inner rotating shaft set through the outer rotating shaft set. By adopting the above mode, the spiral loop apparatus for the steel belts can reduce friction and bump on the steel belts during transportation, so the damage to equipment can be reduced, and the spiral loop apparatus is simple in structure, safe and reliable.

Description

Steel band spiral loop device
Technical field
The present invention relates to steel band manufacture field, particularly relate to a kind of steel band spiral loop device.
Background technology
When utilizing band steel as some workpiece of Raw material processing, needing a certain amount of band steel to be wrapped on kink, temporarily storing and use for process equipment.Steel band in spiral loop is made up of two groups of hurricane bands, and the taking the lead of the magnetic tape trailer of inner ring and outer ring is connected, and turns to contrary.The hurricane band of outer ring is along with constantly feeding inwards, and external diameter increases gradually, just needs rewinding inwards.Existing spiral loop formula, by feeding motor High Rotation Speed, just can be taken in after constantly impacting, very large to the damage of equipment like this.
Summary of the invention
The technical problem that the present invention mainly solves is to provide a kind of steel band spiral loop device, and the friction produced when can reduce rewinding and shock, reduce the damage to equipment, and structure is simple, safe and reliable.
For solving the problems of the technologies described above, the technical scheme that the present invention adopts is: provide a kind of steel band spiral loop device, fuselage disk, the excircle of described fuselage disk is provided with outer shaft group, the inside of described fuselage disk is provided with interior rotating shaft group, the central part of described fuselage disk is provided with slewing rollers, described slewing rollers are positioned at the central part of rotating shaft group, on described fuselage disk, also erection has material collecting device, described material collecting device is between outer shaft group and interior rotating shaft group, described fuselage disk is connected with steel band, steel band is rotated by outer shaft group to be sent into interior rotating shaft group and sends from slewing rollers, described material collecting device is for tightening up the steel band of rotating shaft group in outer shaft group driving-belt.
In a preferred embodiment of the present invention, described material collecting device comprises driving head, and described driving head is connected with the axis of guide, the described axis of guide is connected with turning center axle, and described turning center axle is provided with deflecting roller.
In a preferred embodiment of the present invention, be arranged on above fuselage disk by connecting rod bottom described material collecting device, upper end hang on crossbeam, and described connecting rod is I shape.
In a preferred embodiment of the present invention, described outer shaft group comprises multiple outer shaft, and described outer shaft is uniform intervals distribution inside the excircle of fuselage disk, and described steel band is around in inside outer shaft group.
In a preferred embodiment of the present invention, described interior rotating shaft group comprises multiple interior rotating shaft, and described interior rotating shaft is around the center of circle uniform intervals distribution of fuselage disk, and described steel band is around in the outside of interior rotating shaft group.
In a preferred embodiment of the present invention, described fuselage disk is provided with steel band entrance and steel band outlet, described steel band enters fuselage disk from steel band entrance, sends from steel band outlet.
The invention has the beneficial effects as follows: steel band spiral loop device of the present invention, the friction produced when can reduce rewinding and shock, reduce the damage to equipment, and structure is simple, safe and reliable.
Accompanying drawing explanation
In order to be illustrated more clearly in the technical scheme in the embodiment of the present invention, below the accompanying drawing used required in describing embodiment is briefly described, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings, wherein:
Fig. 1 is the structural representation of steel band spiral loop device one of the present invention preferred embodiment;
Fig. 2 is the partial structurtes schematic diagram of the steel band spiral loop device shown in Fig. 1;
In accompanying drawing, the mark of each parts is as follows: 1, fuselage disk, and 2, outer shaft group, 3, interior rotating shaft group, 4, slewing rollers, 5, material collecting device, 6, steel band, 7, connecting rod, 8, outer shaft, 9, interior rotating shaft, 51, driving head, 52, the axis of guide, 53, turning center axle, 54, deflecting roller.
Detailed description of the invention
Be clearly and completely described to the technical scheme in the embodiment of the present invention below, obviously, described embodiment is only a part of embodiment of the present invention, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making other embodiments all obtained under creative work prerequisite, belong to the scope of protection of the invention.
Refer to Fig. 1, a kind of steel band spiral loop device, comprise: fuselage disk 1, the excircle of described fuselage disk 1 is provided with outer shaft group 2, the inside of described fuselage disk 1 is provided with interior rotating shaft group 3, the central part of described fuselage disk 1 is provided with slewing rollers 4, described slewing rollers 4 are positioned at the central part of rotating shaft group 3, on described fuselage disk 1, also erection has material collecting device 5, described material collecting device 5 is between outer shaft group 2 and interior rotating shaft group 3, described fuselage disk 1 is connected with steel band 6, steel band 6 is rotated by outer shaft group 2 to be sent into interior rotating shaft group 3 and sends from slewing rollers 4, described material collecting device 5 is for tightening up the steel band of rotating shaft group 3 in outer shaft group 2 driving-belt.
In addition, described material collecting device 5 comprises driving head 51, and described driving head 51 is connected with the axis of guide 52, and the described axis of guide 52 is connected with turning center axle 53, and described turning center axle 53 is provided with deflecting roller 54.
In addition, be arranged on above fuselage disk 1 by connecting rod 7 bottom described material collecting device 5, upper end hang on crossbeam, and described connecting rod 7 is in I shape.
In addition, described outer shaft group 2 comprises multiple outer shaft 8, and described outer shaft 8 is uniform intervals distribution inside the excircle of fuselage disk 1, and described steel band 6 is around in inside outer shaft group.
In addition, described interior rotating shaft group 3 comprises multiple interior rotating shaft 9, and described interior rotating shaft 9 is around the center of circle uniform intervals distribution of fuselage disk 1, and described steel band 6 is around in the outside of interior rotating shaft group 3.
In addition, described fuselage disk 1 is provided with steel band entrance and steel band outlet, described steel band 6 enters fuselage disk from steel band entrance, extracts out (the passive pull-out of strength on the front of band steel) from steel band outlet.
Steel band spiral loop device specific works principle of the present invention is as follows: steel band 6 enters from steel band entrance, by inside outer shaft group 2 around in round, then interior rotating shaft group 3 is being delivered to, round is coiled into outside interior rotating shaft group 3, steel band 6 is last to be sent along slewing rollers 4 from the outlet of the steel band of fuselage disk 1, in feeding process, steel band 6 is sent constantly into, steel band in outer shaft group 2 is on the increase, external diameter increases gradually, be about to be full of in outer shaft group 2 is stop feeding, during etc. needs rewinding, declined by the driving head 51 of material collecting device 1, deflecting roller 54 is driven to decline, when the steel band 6 in interior rotating shaft 3 is constantly extracted out from outlet, steel band 6 driving wheel 54 that can rotate drives steel band 6 to rotate, make to tighten up around steel band 6 inner ring in outer shaft group 2, be convenient to rewinding.When not needing rewinding, driving head 51 drives deflecting roller 56 to rise.
Be different from prior art, steel band spiral loop device of the present invention, the friction produced when can reduce rewinding and shock, reduce the damage to equipment, and structure is simple, safe and reliable
The foregoing is only embodiments of the invention; not thereby the scope of the claims of the present invention is limited; every utilize description of the present invention to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical field, be all in like manner included in scope of patent protection of the present invention.

Claims (6)

1. a steel band spiral loop device, it is characterized in that, comprise: fuselage disk, the excircle of described fuselage disk is provided with outer shaft group, the inside of described fuselage disk is provided with interior rotating shaft group, the central part of described fuselage disk is provided with slewing rollers, described slewing rollers are positioned at the central part of rotating shaft group, on described fuselage disk, also erection has material collecting device, described material collecting device is between outer shaft group and interior rotating shaft group, described fuselage disk is connected with steel band, steel band is rotated by outer shaft group to be sent into interior rotating shaft group and sends from slewing rollers, described material collecting device is for tightening up the steel band of rotating shaft group in outer shaft group driving-belt.
2. steel band spiral loop device according to claim 1, it is characterized in that, described material collecting device comprises driving head, and described driving head is connected with the axis of guide, the described axis of guide is connected with turning center axle, described turning center axle is provided with deflecting roller.
3. steel band spiral loop device according to claim 1, is characterized in that, be arranged on above fuselage disk by connecting rod bottom described material collecting device, upper end hang on crossbeam, and described connecting rod is I shape.
4. steel band spiral loop device according to claim 1, is characterized in that, described outer shaft group comprises multiple outer shaft, and described outer shaft is uniform intervals distribution inside the excircle of fuselage disk, and described steel band is around in inside outer shaft group.
5. steel band spiral loop device according to claim 1, is characterized in that, described interior rotating shaft group comprises multiple interior rotating shaft, and described interior rotating shaft is around the center of circle uniform intervals distribution of fuselage disk, and described steel band is around in the outside of interior rotating shaft group.
6. steel band spiral loop device according to claim 1, is characterized in that, described fuselage disk is provided with steel band entrance and steel band outlet, described steel band enters fuselage disk from steel band entrance, sends from steel band outlet.
CN201510231336.3A 2015-05-08 2015-05-08 Spiral loop apparatus for steel belts Pending CN104874619A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510231336.3A CN104874619A (en) 2015-05-08 2015-05-08 Spiral loop apparatus for steel belts

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510231336.3A CN104874619A (en) 2015-05-08 2015-05-08 Spiral loop apparatus for steel belts

Publications (1)

Publication Number Publication Date
CN104874619A true CN104874619A (en) 2015-09-02

Family

ID=53942444

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510231336.3A Pending CN104874619A (en) 2015-05-08 2015-05-08 Spiral loop apparatus for steel belts

Country Status (1)

Country Link
CN (1) CN104874619A (en)

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EXSB Decision made by sipo to initiate substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20150902