CN208019522U - Flying shear blade and its installation fixed structure - Google Patents

Flying shear blade and its installation fixed structure Download PDF

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Publication number
CN208019522U
CN208019522U CN201721655992.7U CN201721655992U CN208019522U CN 208019522 U CN208019522 U CN 208019522U CN 201721655992 U CN201721655992 U CN 201721655992U CN 208019522 U CN208019522 U CN 208019522U
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CN
China
Prior art keywords
blade
flying shear
cutting edge
cutter head
upper cutter
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
CN201721655992.7U
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Chinese (zh)
Inventor
朱德友
王清贵
周刚
陈刚
梁勇
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.)
Panzhihua Gangcheng Group Co Ltd
Original Assignee
Panzhihua Gangcheng Group 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 Panzhihua Gangcheng Group Co Ltd filed Critical Panzhihua Gangcheng Group Co Ltd
Priority to CN201721655992.7U priority Critical patent/CN208019522U/en
Application granted granted Critical
Publication of CN208019522U publication Critical patent/CN208019522U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of flying shear blade and its installation fixed structures, are related to metallurgy rolling technical field.Flying shear blade solves the problems, such as that reinforcing bar is easy to cause in shear reinforcement to be deformed, the technical solution adopted is that:Flying shear blade, bolt hole is arranged in blade body, and the sharpness of 30 ° of the blade basil, cutting edge 2.5~3.0mm of thickness, cutting edge increases;Arc clip is set on cutting edge, changes stress form when material cutting, reduction material is shear-deformable in shearing, improves the straightness of material.Flying shear blade installs fixed structure, including upper cutter head, lower tool apron and flying shear blade, the basil of blade on upper cutter head is towards on front side of the upper cutter head direction of motion, the installation directions of two blades on the contrary, by change cutting edge when shear material above and below blade stress form, the deformation of reduction material end to end;The cutting edge center of two blades is located on front side of upper cutter head center line, eliminates the adverse effect to shearing material because of the excessive cutting edge in flying shear backlash, ensures lumber recovery.

Description

Flying shear blade and its installation fixed structure
Technical field
The utility model is related to metallurgy rolling technical field, specifically a kind of steel rolling flying shear blade and its installation fixed knot Structure.
Background technology
Flying shear is mainly used for middle-size and small-size mill, is set to after mm finishing mill unit, before cold bed entrance, is normally rolling When, the rolled piece that finish rolling milling train is shut out is cut into the cut lengths for adapting to cold bed length.Multiple length spiral is sheared by flying shear In production process, due to there are rolling mill speed with flying shear speeds match is not quite identical, there are gap, blades to steel for flying shear gear The factors such as impact force and back the rollgang abrasion of muscle, the multiple length spiral after shearing, there are the bendings end to end of shearing Phenomenon causes multiple length spiral lumber recovery too low.
In the above problem, the structure of blade and the mounting structure of blade be cause spiral lumber recovery low reason it One.The existing blade basil is big, and cutting edge thickness is big, is straight snips mouth, and cutting force is insufficient when shearing, is easy to cause in shear reinforcement Reinforcing bar deforms, and reduces the straightness of reinforcing bar.
Existing blade mounting means is to be fixedly mounted on the gasket of 5mm and blade on tool apron ontology with two bolts, Side coil fixes blade, its blade is made to be integrally connected with tool apron ontology.The cutting edge center of upper bottom knife is located at tool apron center line On, appearance meeting flying shear backlash is excessive after long-term production, this can cause the cutting edge of blade to cause harmful effect to shearing material, drop Low lumber recovery.
Utility model content
The utility model provides a kind of flying shear blade first, and the basil for solving existing flying shear blade is big, and cutting edge thickness is big, It is easy to cause reinforcing bar deformation when shear reinforcement, reduces the straightness problem of reinforcing bar.
Technical solution is used by the utility model solves above-mentioned technical problem:Flying shear blade, including blade body, knife Bolt hole is set on piece ontology, and the basil of blade is 30 °, and the thickness of cutting edge is 2.5~3.0mm, and arc clip is arranged on cutting edge.
It is further:The radius of the arc clip is 95.2mm, action 5mm.
Specifically, the bolt hole is two.
The utility model also provides a kind of flying shear blade installation fixed structure, solves existing flying shear blade installation fixed structure The problem of it is excessive to occur flying shear backlash after long-term production, reduces lumber recovery.
Technical solution is used by the utility model solves above-mentioned technical problem:Flying shear blade installs fixed structure, packet Upper cutter head, lower tool apron are included, and is respectively arranged in two blades up and down of upper cutter head and lower tool apron, the sword of the blade on upper cutter head Towards the front side of the upper cutter head direction of motion, the installation fixed-direction of two blades is opposite at angle;Two blades are above-mentioned side The cutting edge center of flying shear blade in case, two blades is located on front side of upper cutter head center line.
Specifically, the cutting edge center of two blades is located at 5mm on front side of upper cutter head center line.
It is further:In the lower groove of the upper cutter head, gasket is set on rear side of the traffic direction of blade, lower tool apron it is upper In groove, backing plate is set on front side of the traffic direction of blade.
Specifically, the thickness of the gasket is 10mm.
The utility model has the beneficial effects that:Since the basil of flying shear blade is small, cutting edge thickness is thin, increases the cutting edge of a knife or a sword of cutting edge Sharp degree reduces radial cutting force when shearing material, while arc clip being arranged on cutting edge, when changing material cutting by Power form, reduce material shearing when it is shear-deformable, improve the straightness of material.
The more existing mounting means of flying shear blade that flying shear blade installs fixed structure rotates 180 °, two blades of change Impact direction, to change cutting edge when shearing material on bottom knife blade stress form, reduce material deformation end to end.Two The cutting edge center of a blade is located on front side of upper cutter head center line, eliminates because flying shear backlash is excessive, cutting edge is to shearing material not Profit influences, and ensure that lumber recovery.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model flying shear blade.
Fig. 2 is the side view of Fig. 1.
Fig. 3 is the schematic diagram of the utility model flying shear blade installation fixed structure.
Parts, position and number in figure:Blade body 1, bolt hole 11, arc clip 12, upper cutter head 2, lower groove 21, Gasket 22, lower tool apron 3, upper groove 31, backing plate 32.
Specific implementation mode
The utility model is described in further detail below in conjunction with the accompanying drawings.
As depicted in figs. 1 and 2, two spiral shells are arranged in blade body 1 for the utility model flying shear blade, including blade body 1 Keyhole 11, bolt hole 11 are used to blade body 1 being mounted on tool apron.The basil of blade is 30 °, and the thickness of cutting edge is 2.5~3.0mm, setting arc clip 12 on cutting edge.The radius of arc clip 12 is 95.2mm, action 5mm.
60 ° of smallers of the basil of the relatively existing conventional blade of the basil of flying shear blade, cutting edge thickness is compared to existing conventional knife The thickness 5mm of piece is thinner, increases the sharpness of cutting edge, reduces radial cutting force when shearing material.Meanwhile it being set on cutting edge Arc clip 12 is set to change stress form when material cutting that is, by original straight snips mouth processing camber clip 12, reduce Material is shear-deformable in shearing, improves the straightness of material.
As shown in figure 3, the utility model flying shear blade installs fixed structure, including upper cutter head 2, lower tool apron 3, and respectively Two blades up and down of upper cutter head 2 and lower tool apron 3 are installed on by two high-strength bolts, two blades are in above-described embodiment Flying shear blade.The installation fixed-directions of two blades on the contrary, the basil of blade on upper cutter head 2 towards 2 side of moving of upper cutter head To front side, the rear side of the basil of the blade on lower tool apron 3 towards 3 direction of motion of lower tool apron.In shear history, 2 He of upper cutter head The rotation direction of lower tool apron 3 is as shown in the camber line arrow in Fig. 3.The more existing mounting means of blade rotates 180 °, changes two The Impact direction of blade, to change cutting edge when shearing material above and below blade stress form, reduce material deformation end to end.
In the lower groove 21 of upper cutter head 2, gasket 22 is set on rear side of the traffic direction of blade, in the upper groove 31 of lower tool apron 3, Backing plate 32 is set on front side of the traffic direction of blade.The cutting edge center of two blades is located at 5mm on front side of 2 center line of upper cutter head, eliminates Because flying shear backlash is excessive, cutting edge ensures lumber recovery to the adverse effect of shearing material.Flying shear blade installation fixed structure is not necessarily to Existing equipment is changed greatly, upgrading is easily modified.

Claims (6)

1. flying shear blade installs fixed structure, including upper cutter head (2), lower tool apron (3), and be respectively arranged in upper cutter head (2) and Two blades up and down of lower tool apron (3), it is characterised in that:The basil of blade on upper cutter head (2) is towards upper cutter head (2) movement side To front side, the installation fixed-direction of two blades is opposite;Two blades include blade body (1), in blade body (1) Bolt hole (11) is set, and the basil of blade is 30 °, and the thickness of cutting edge is 2.5~3.0mm, and arc clip (12) is arranged on cutting edge; The cutting edge center of two blades is located on front side of upper cutter head (2) center line.
2. flying shear blade as described in claim 1 installs fixed structure, it is characterised in that:The radius of the arc clip (12) For 95.2mm, action 5mm.
3. flying shear blade as described in claim 1 installs fixed structure, it is characterised in that:The bolt hole (11) is two.
4. flying shear blade as claimed in claim 1,2 or 3 installs fixed structure, it is characterised in that:In the cutting edge of two blades The heart is located at 5mm on front side of upper cutter head (2) center line.
5. flying shear blade as claimed in claim 1,2 or 3 installs fixed structure, it is characterised in that:Under the upper cutter head (2) In groove (21), the upper groove (31) of setting gasket (22) on rear side of the traffic direction of blade, lower tool apron (3) is interior, the operation of blade Setting backing plate (32) on front side of direction.
6. flying shear blade as claimed in claim 5 installs fixed structure, it is characterised in that:The thickness of the gasket (22) is 10mm。
CN201721655992.7U 2017-12-01 2017-12-01 Flying shear blade and its installation fixed structure Expired - Fee Related CN208019522U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721655992.7U CN208019522U (en) 2017-12-01 2017-12-01 Flying shear blade and its installation fixed structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721655992.7U CN208019522U (en) 2017-12-01 2017-12-01 Flying shear blade and its installation fixed structure

Publications (1)

Publication Number Publication Date
CN208019522U true CN208019522U (en) 2018-10-30

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ID=63898216

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721655992.7U Expired - Fee Related CN208019522U (en) 2017-12-01 2017-12-01 Flying shear blade and its installation fixed structure

Country Status (1)

Country Link
CN (1) CN208019522U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111215689A (en) * 2019-12-06 2020-06-02 中冶华天南京工程技术有限公司 Novel multi-length flying shear mechanism and bar shearing method thereof
CN115090954A (en) * 2022-07-26 2022-09-23 中钢设备有限公司 Cutter head device of flying shear with tightly-fixed cutting edge

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111215689A (en) * 2019-12-06 2020-06-02 中冶华天南京工程技术有限公司 Novel multi-length flying shear mechanism and bar shearing method thereof
CN115090954A (en) * 2022-07-26 2022-09-23 中钢设备有限公司 Cutter head device of flying shear with tightly-fixed cutting edge

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Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20181030

Termination date: 20191201

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