CN102218567A - Improved-alloy compound cutting disc blade - Google Patents

Improved-alloy compound cutting disc blade Download PDF

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Publication number
CN102218567A
CN102218567A CN201110142188XA CN201110142188A CN102218567A CN 102218567 A CN102218567 A CN 102218567A CN 201110142188X A CN201110142188X A CN 201110142188XA CN 201110142188 A CN201110142188 A CN 201110142188A CN 102218567 A CN102218567 A CN 102218567A
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CN
China
Prior art keywords
disc
alloy
performances
improved
substrate
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Pending
Application number
CN201110142188XA
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Chinese (zh)
Inventor
綦洛阳
李文喜
刘雄杰
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.)
XIANGFAN BOYA FINE WORKMANSHIP MACHINE CO Ltd
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XIANGFAN BOYA FINE WORKMANSHIP MACHINE 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.)
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Publication date
Application filed by XIANGFAN BOYA FINE WORKMANSHIP MACHINE CO Ltd filed Critical XIANGFAN BOYA FINE WORKMANSHIP MACHINE CO Ltd
Priority to CN201110142188XA priority Critical patent/CN102218567A/en
Publication of CN102218567A publication Critical patent/CN102218567A/en
Pending legal-status Critical Current

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Abstract

The invention discloses an improved-alloy compound disc cutting blade, which is applied to the shearing machining of various sheet materials in the metallurgy industry. An embedded composite material is embedded on a substrate to server as a cutting edge, the composite material is hard alloy, and the substrate is of a split structure. For a cutting edge part, a scrapped import disc cutting blade can be utilized and is subjected to secondary grinding to machine a new cutting edge; and an inner substrate of a split structure is compounded with a selected cheap steel material by using a special compounding technology, and then a disc cutting blade with excellent performances is remanufactured. Under the condition that the performances of a cutting disc are guaranteed, scrapped import or domestic high-quality blades are taken as raw materials, failure forms and the working state of the cutting disc are comprehensively considered, characteristics such as high hardness and good wear resistance of import alloy steel are fully utilized, and the secondary grinding and machining are carried out on an inner compound split substrate; thus the performances of precious alloy are brought into full play, the comprehensive performances of the blade are improved, and the cost can be effectively reduced simultaneously; in addition, the improved-alloy compound disc cutting blade has the advantages of good performances, low cost, easiness for machining, high yield and the like.

Description

Modified form alloy complex disc blade
Technical field
The present invention relates to the processing of metallurgy industry sheet material and use circle shear, is a kind of composite blade that is used on the cut edge circle shear specifically.
Background technology
In the modern steel industry, cut edge circle shear is widely used in iron and steel, the production of non-ferrous metal processing strip, as cold-rolling mill, side cut rewinding unit, crop shears, stretch-bending straightening unit etc.Its purposes has two kinds, and a kind of is to be used for the metal plate and belt production process to cut away strip both sides raw edges, in order to later process production; Another kind is to be cut into the desired width of final products.And cutting disc is the critical component that it realizes function, the manufacturing of cylinder blade mostly adopts the monoblock raw material to process (selection is variant) both at home and abroad at present, and homemade cylinder blade performance is exactly the difference of material property not as the key factor of import blade, secondly is Technology for Heating Processing.Therefore the raw material of selecting for use are one of effective ways that improve the circle shear performance.But select the import alloy material for use, product cost will increase thereupon.Now also have the cylinder blade of small part specific use to adopt carbide alloy or other material edge cover technology, but its difficulty of processing is big, the cost height, yield rate is low, and scope is restricted.
Summary of the invention
For overcoming the deficiencies in the prior art, goal of the invention of the present invention is to provide a kind of modified form alloy complex disc blade, and is compound by special technique, and to improve the cutting disc combination property, realization reduces cost, aim of saving.
For achieving the above object, technical program of the present invention lies in: stud with composite bed on the matrix as cutting edge, composite bed is a carbide alloy, and matrix is a split-type structural.
The cutting edge position utilizes written-off import cylinder blade, through the secondary reconditioning, and the cutting edge that processing makes new advances; Inner base adopts split-type structural, designs two sloping platform rank at inner ring, by with the cooperating of alloy part, can bear larger axis to power; Select cheap steel for use, compound through special complex technique, to change a social system out the cylinder blade of excellent performance.
The present invention compared with prior art, under the situation that guarantees the cutting disc performance, by being raw material to written-off import or homemade high-quality blade, take all factors into consideration the failure mode and the duty thereof of cutting disc, make full use of import steel alloy hardness height, characteristics that wearability is good, by secondary reconditioning, processing, inner compound split type matrix, perform to the performance of valuable alloy ultimate attainment, when realizing promoting the combination property of blade, can effectively reduce cost, have that performance is good, cost is low, easy processing, yield rate advantages of higher.
Description of drawings
Fig. 1 is a structure diagram of the present invention;
Fig. 2 is reconditioning of the present invention, improvement pre-structure figure.
The specific embodiment
As shown in Figure 1, the present invention changes a social system composite bed 1 earlier: mill oblique angle, two ends, middle mill groove, reconditioning cutting edge again, again according to changing a social system specification processing matrix 3: require the chamfering grinding two ends outside, the middle groove of processing; Composite bed 1 passes through adhesive linkage 2 strong bond together with complex matrix 3, and after compound the finishing, whole reconditioning is to reach dimensions and high service precision.The import high duty alloy material that composite bed 1 of the present invention is an excellent performance also can be other Hardmetal materials.
Thick, fine finishining of the present invention needs a plurality of processes, with maximum assurance precision, and after each machined, all will carry out The heat treatment of oil oven timeliness, to eliminate the internal stress that machined produces.
As shown in Figure 1, be blade figure before written-off reconditioning, the improvement.

Claims (3)

1. a modified form alloy complex disc blade is characterized in that: stud with composite bed (1) on the matrix (3) as cutting edge.
2. modified form alloy complex disc blade according to claim 1 is characterized in that: composite bed (1) is a carbide alloy.
3. modified form alloy complex disc blade according to claim 1 is characterized in that: matrix (3) is a split-type structural.
CN201110142188XA 2011-05-30 2011-05-30 Improved-alloy compound cutting disc blade Pending CN102218567A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201110142188XA CN102218567A (en) 2011-05-30 2011-05-30 Improved-alloy compound cutting disc blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201110142188XA CN102218567A (en) 2011-05-30 2011-05-30 Improved-alloy compound cutting disc blade

Publications (1)

Publication Number Publication Date
CN102218567A true CN102218567A (en) 2011-10-19

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CN201110142188XA Pending CN102218567A (en) 2011-05-30 2011-05-30 Improved-alloy compound cutting disc blade

Country Status (1)

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CN (1) CN102218567A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102658605A (en) * 2012-05-02 2012-09-12 厦门钨业股份有限公司 Manufacturing method of super-hard material high-wear-resistance precision support frame/block
CN104942879A (en) * 2015-07-08 2015-09-30 安徽华天机械股份有限公司 Flat and round cutter and manufacturing method thereof
CN108161382A (en) * 2018-03-15 2018-06-15 江苏亿斯赛尔自动化科技有限公司 Cutting disc welds firing technique
RU2752719C1 (en) * 2020-12-21 2021-07-30 Федеральное государственное бюджетное образовательное учреждение высшего образования "Тверской государственный технический университет" Method for manufacturing disc knife

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0123770A2 (en) * 1982-10-15 1984-11-07 Vereinigte Edelstahlwerke Aktiengesellschaft (Vew) Method of making cutters for hot shears
CN2198060Y (en) * 1994-01-28 1995-05-24 武汉钢铁(集团)公司 Disk shear edge
CN2372084Y (en) * 1999-01-22 2000-04-05 秦皇岛开发区宏维表面工程技术研究所 Shear blade
CN2608203Y (en) * 2003-04-28 2004-03-31 武汉华欣精密机械有限责任公司 High precision hard alloy composite disk knife
CN201592287U (en) * 2009-10-11 2010-09-29 襄樊市博亚机械有限公司 Compound alloy disc knife
CN202199837U (en) * 2011-05-30 2012-04-25 襄阳博亚精工机器有限公司 Improved composite alloy disc knife

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0123770A2 (en) * 1982-10-15 1984-11-07 Vereinigte Edelstahlwerke Aktiengesellschaft (Vew) Method of making cutters for hot shears
CN2198060Y (en) * 1994-01-28 1995-05-24 武汉钢铁(集团)公司 Disk shear edge
CN2372084Y (en) * 1999-01-22 2000-04-05 秦皇岛开发区宏维表面工程技术研究所 Shear blade
CN2608203Y (en) * 2003-04-28 2004-03-31 武汉华欣精密机械有限责任公司 High precision hard alloy composite disk knife
CN201592287U (en) * 2009-10-11 2010-09-29 襄樊市博亚机械有限公司 Compound alloy disc knife
CN202199837U (en) * 2011-05-30 2012-04-25 襄阳博亚精工机器有限公司 Improved composite alloy disc knife

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102658605A (en) * 2012-05-02 2012-09-12 厦门钨业股份有限公司 Manufacturing method of super-hard material high-wear-resistance precision support frame/block
CN102658605B (en) * 2012-05-02 2015-05-20 厦门钨业股份有限公司 Manufacturing method of super-hard material high-wear-resistance precision support frame/block
CN104942879A (en) * 2015-07-08 2015-09-30 安徽华天机械股份有限公司 Flat and round cutter and manufacturing method thereof
CN108161382A (en) * 2018-03-15 2018-06-15 江苏亿斯赛尔自动化科技有限公司 Cutting disc welds firing technique
RU2752719C1 (en) * 2020-12-21 2021-07-30 Федеральное государственное бюджетное образовательное учреждение высшего образования "Тверской государственный технический университет" Method for manufacturing disc knife

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Address after: Thirteen, 441003, Torch Hotel,, 15 Spring Garden Road, Hubei, Xiangfan, Xiangyang

Applicant after: Xiangyang Boya Precision Machinery Co., Ltd.

Address before: Thirteen, 441003, Torch Hotel,, 15 Spring Garden Road, Hubei, Xiangfan, Xiangyang

Applicant before: Xiangfan Boya fine Workmanship Machine Co., Ltd.

COR Change of bibliographic data

Free format text: CORRECT: APPLICANT; FROM: XIANGFAN BOYA FINE WORKMANSHIP MACHINE CO., LTD. TO: XIANGYANG BOYA PRECISION INDUSTRIAL MACHINERY CO., LTD.

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Application publication date: 20111019