CN101648227A - Multi-location cold extruding forming method of sleeve barrel - Google Patents
Multi-location cold extruding forming method of sleeve barrel Download PDFInfo
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- CN101648227A CN101648227A CN200910102040A CN200910102040A CN101648227A CN 101648227 A CN101648227 A CN 101648227A CN 200910102040 A CN200910102040 A CN 200910102040A CN 200910102040 A CN200910102040 A CN 200910102040A CN 101648227 A CN101648227 A CN 101648227A
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- cold extrusion
- sleeve
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- 238000000034 method Methods 0.000 title claims abstract description 12
- 239000000463 material Substances 0.000 claims abstract description 78
- 238000007493 shaping process Methods 0.000 claims abstract description 12
- 238000000641 cold extrusion Methods 0.000 claims description 88
- 238000011282 treatment Methods 0.000 claims description 13
- 238000003825 pressing Methods 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 8
- 239000002699 waste material Substances 0.000 abstract description 5
- 238000007688 edging Methods 0.000 abstract 1
- 238000004080 punching Methods 0.000 abstract 1
- 239000002184 metal Substances 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002994 raw material Substances 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000007769 metal material Substances 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 238000007514 turning Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
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Abstract
The invention provides a multi-location cold extruding forming method of a sleeve barrel, comprising the following step: fracturing materials to form a cold extruding material part, and also comprising the following cold extruding processing steps after material fracturing: shaping and edging both ends of the material part; digging guide holes on both ends of the material part; digging a hexagonalhole of the sleeve barrel on the basis of the guide holes, and prolonging the length of the material part; digging a square hole of the sleeve barrel on the basis of the guide holes, forming a guidehole section on the bottom of the square hole and prolonging the material part; digging a transverse inner groove of the sleeve barrel positioned in the hexagonal hole on the hole wall of the hexagonal hole; digging a middle circular hole and a guide hole on the bottom of the hexagonal hole; and punching the material part positioned between the square hole and the middle circular hole to be communicated to form a small circular hole of the sleeve barrel. The invention enables the sleeve barrel to be manufactured by the cold extruding method, has quick speed, high precision and production efficiency, few waste material and even no waste material, thereby greatly saving the original materials and reducing the production cost; and in addition, the cold extruding enhances the mechanical property of products and ensures the quality of the products, thus the products have more advantages on a utilization function.
Description
Technical field
The present invention relates to the manufacturing technology field of extruded sleeve.
Background technology
Sleeve is a kind of instrument commonly used, and its profile is a cylinder, and sleeve has central through hole, and central through hole comprises the hexagonal hole section that is in a side and the cubic hole section of opposite side, between cubic hole section and the hexagonal hole section middle circular hole portion is arranged, and horizontal septal fossula is arranged in the hexagonal hole.At present, make sleeve and generally adopt turning, operation is various, and especially the difficulty of processing in horizontal septal fossula in the hexagonal hole and cubic hole is big, efficient is low, and hole wall is more crude, and product quality can't guarantee.And sleeve has the bigger characteristics of central through hole, therefore, with traditional manufacturing process can cause cut the material weight greater than moulding after product weight, waste of raw materials is very big, cost is higher.
Summary of the invention
Technical problem to be solved by this invention provides a kind of multistation cold extrusion forming method of sleeve, can save raw material, reduces production costs, and improves the quality of products.For this reason, the present invention is by the following technical solutions: it comprises that fracture forms the step of cold extrusion materials and parts, behind fracture, is provided with following cold extrusion and handles:
A. to the shaping bundle limit, two ends of materials and parts,
B. pilot hole is dug at the two ends of materials and parts, wherein, the aperture that need are dug the pilot hole that the end in hole, sleeve four directions dug is the spigot surface shape and greater than the aperture in hole, sleeve four directions,
The end face that C. materials and parts need be dug hexagonal hole faces the place ahead, on the basis of pilot hole, and the length of digging the hexagonal hole of sleeve and prolonging materials and parts,
The end face that D. materials and parts need be dug cubic hole faces the place ahead, digs the cubic hole of sleeve on the basis of pilot hole, forms the pilot hole section at the bottom of the hole, and prolongs materials and parts,
E. the hole wall of described hexagonal hole is dug sleeve and is in horizontal septal fossula in the hexagonal hole,
F. at the bottom of the hole of hexagonal hole, dig Zhong Yuan hole and pilot hole,
G. dash the materials and parts between logical cubic hole and the Zhong Yuan hole, form the small sircle hole of sleeve;
A is handled in described cold extrusion and the cold extrusion treatments B is combined as 1 cold extrusion station or is no more than 4 cold extrusion stations;
Described cold extrusion is handled C and is carried out after the cold extrusion treatments B, or, when the cold extrusion treatments B is divided into a plurality of station, can be in last station of cold extrusion treatments B and carries out;
Cold extrusion processing F and cold extrusion processing E, cold extrusion processing C or cold extrusion processing D are in same station or carry out in a station separately;
E is handled in cold extrusion and cold extrusion processing D carries out with station or be in after the cold extrusion processing D and before the cold extrusion processing G carrying out.
A is handled in cold extrusion can be divided into 1 road or 2 roads, promptly finishes the task that A is handled in cold extrusion by the cold extrusion of one and 2 station, for example, and the 1st first end face of station shaping, second end face of the 2nd station shaping; The cold extrusion treatments B also can be divided into 1 road or 2 roads, promptly finishes the task of cold extrusion treatments B by the cold extrusion of one and 2 station, and for example, the 1st station digs pilot hole to first end face, and the 2nd station digs pilot hole to second end face; The combination that A and cold extrusion treatments B are handled in cold extrusion can be a design station number of handling A and cold extrusion treatments B itself according to cold extrusion, carry out permutation and combination and the processing of the cold extrusion of 4 stations more than being formed up to, such as, after the combination, the 1st first end face of station shaping, the 2nd station digs locating hole to last end face, and to back one end face shaping, the 3rd station digs locating hole to back one end face, in this case, cold extrusion is handled C and be may be incorporated in the 3rd station, and this is that very reasonably station can be realized the progressively cold-extrusion shaping to materials and parts in proper order, improve the cold extrusion quality, different cold extrusions are handled can be combined in on the station, too much to avoid station, influence cost.
Certainly, cold extrusion is handled A and the also available station of cold extrusion treatments B or two stations and is finished, and carries out on the station of cold extrusion processing C after them.
Cold extrusion is handled E and is preferably carried out at same station with cold extrusion processing D, and its purpose also is to make them can organic assembling, thereby neither influences the cold extrusion quality, can reduce cold extrusion station number as far as possible again.
Cold extrusion is a kind of plastic working technique, and it makes metal volume make plastic transfer under the prerequisite of not destroying metalline, reaches few cutting, does not have cutting and make metal forming.Form a large amount of metal debris when so just having avoided machining, save iron and steel and various metal material in a large number.
The design and the procedure arrangement that carry out station at target product are one of cold-stamped emphasis, the present invention is by rationally delineating the station operation, make sleeve can adopt the manufacturing of cold-stamped method, speed is fast, the precision height, the production efficiency height, can not adopt or adopt turning boring seldom, cut material weight product weight after the moulding no better than, less waste material even do not have waste material, save material greatly, reduce production costs.And cold extrusion makes metal material produce plastic deformation, and the metal inside tissue is changed, and the pulling force aspect more is added with raising, has improved mechanical performance of products, has guaranteed product quality, makes product have more advantage on function of use.
Description of drawings
Fig. 1 is the cold extrusion station schematic diagram of embodiment provided by the present invention.
Fig. 2 is the A-A cutaway view of Fig. 1.
Fig. 3 is the B-B cutaway view of Fig. 1.
The specific embodiment
With reference to accompanying drawing 1,2,3.The present invention includes the step of fracture formation cold extrusion materials and parts, raw materials used is the steel profile of circle for the cross section.Behind fracture, it carries out cold extrusion in proper order by following station, in drawing and description specifically describe, for materials and parts, the upper surface is front end face, the lower surface is rear end face, and the upper end of materials and parts is described materials and parts front end or head, and the lower end of materials and parts is described materials and parts rear end or afterbody, downward direction can be understood as direction backward, direction upwards can be understood as direction forward, unless specialize, is circular hole otherwise the hole of being dug is circle cross-section:
(1). the cold extrusion materials and parts, to the shaping bundle limit, rear end of materials and parts, make its periphery 11 smooth mellow and full, and form certain gradient or radian, mould is located with materials and parts when helping down the step cold extrusion, makes raising cold extrusion quality and reduces the mould loss;
(2). with materials and parts Rotate 180 degree, the cold extrusion materials and parts are to shaping bundle limit, rear end, the front end pressing of postrotational materials and parts; End periphery 12 is smooth mellow and full after making materials and parts, and forms certain gradient or radian, to help down step mould and materials and parts location during cold extrusion, makes raising cold extrusion quality and reduces the mould loss;
(3). again with materials and parts Rotate 180 degree, the cold extrusion materials and parts flatten and dig pilot hole 13 to the front end of postrotational materials and parts, and mould is located with materials and parts when helping down the step cold extrusion, and raising cold extrusion quality also reduces the mould loss;
(4). the cold extrusion materials and parts, from the front end of materials and parts backward, on the basis of pilot hole 13, dig the hexagonal hole 5 of sleeve and the length that prolongs materials and parts, rear end face at materials and parts digs pilot hole 15, the aperture of pilot hole 15 is the spigot surface shape and greater than the aperture in hole 4, sleeve four directions, like this, in follow-up cold extrusion process, mould and materials and parts location in the time of not only can utilizing pilot hole to help to go on foot cold extrusion down, improve the cold extrusion quality and reduce the mould loss, the bore portions of pilot hole can be directly as the spigot surface 1 around the cubic hole of sleeve after the cubic hole of sleeve is shaped simultaneously;
(5). with materials and parts Rotate 180 degree, the cold extrusion materials and parts to postrotational materials and parts, dig cubic hole 4 backward from front end on the basis of pilot hole, form pilot hole section 17 at the bottom of the hole, and prolong materials and parts; Utilize back mold and dig sleeve and be in the horizontal septal fossula 2 in the hexagonal hole and at the bottom of the hole of hexagonal hole, dig Zhong Yuan hole 3 and pilot hole 18 towards excellent hole wall to hexagonal hole;
(6). with materials and parts Rotate 180 degree, dash the materials and parts between logical cubic hole 4 and the Zhong Yuan hole 3, form the small sircle hole 4 in the sleeve central through hole, make described sleeve, the front hole section of its central through hole is that hexagonal hole 5, rear orifice section are cubic hole 6, and described middle circular hole 3 and small sircle hole 4 are arranged between hexagonal hole and the cubic hole.
In Fig. 1, begin to the right side from left side figure, represent the materials and parts shape behind station 1, station 2, station 3, station 4, station 5, station 6 respectively.
Claims (3)
1. the multistation cold extrusion forming method of a sleeve is characterized in that it comprises that fracture forms the step of cold extrusion materials and parts, behind fracture, is provided with following cold extrusion processing:
A. to the shaping bundle limit, two ends of materials and parts,
B. pilot hole is dug at the two ends of materials and parts, wherein, the aperture that need are dug the pilot hole that the end in hole, sleeve four directions dug is the spigot surface shape and greater than the aperture in hole, sleeve four directions,
The end face that C. materials and parts need be dug hexagonal hole faces the place ahead, on the basis of pilot hole, and the length of digging the hexagonal hole of sleeve and prolonging materials and parts,
The end face that D. materials and parts need be dug cubic hole faces the place ahead, digs the cubic hole of sleeve on the basis of pilot hole, forms the pilot hole section at the bottom of the hole, and prolongs materials and parts,
E. the hole wall of described hexagonal hole is dug sleeve and is in horizontal septal fossula in the hexagonal hole,
F. at the bottom of the hole of hexagonal hole, dig Zhong Yuan hole and pilot hole,
G. dash the materials and parts between logical cubic hole and the Zhong Yuan hole, form the small sircle hole section of sleeve;
A is handled in described cold extrusion and the cold extrusion treatments B is combined as 1 cold extrusion station or is no more than 4 cold extrusion stations;
Described cold extrusion is handled C and is carried out after the cold extrusion treatments B, or, when the cold extrusion treatments B is divided into a plurality of station, can be in last station of cold extrusion treatments B and carries out;
Cold extrusion processing F and cold extrusion processing E, cold extrusion processing C or cold extrusion processing D are in same station or carry out in a station separately;
E is handled in cold extrusion and cold extrusion processing D carries out with station or be in after the cold extrusion processing D and before the cold extrusion processing G carrying out.
2. the multistation cold extrusion forming method of a kind of sleeve as claimed in claim 1 is characterized in that it carries out cold extrusion in proper order by following station:
(1). the cold extrusion materials and parts, to the shaping bundle limit, rear end of materials and parts;
(2). with materials and parts Rotate 180 degree, the cold extrusion materials and parts are to shaping bundle limit, rear end, the front end pressing of postrotational materials and parts;
(3). again with materials and parts Rotate 180 degree, the cold extrusion materials and parts flatten and dig pilot hole to the front end of postrotational materials and parts;
(4). the cold extrusion materials and parts, from the front end of materials and parts backward, on the basis of pilot hole, the length of digging the hexagonal hole of sleeve and prolonging materials and parts is dug pilot hole at the rear end face of materials and parts, and the aperture of pilot hole is the spigot surface shape and greater than the aperture in hole, sleeve four directions;
(5). with materials and parts Rotate 180 degree, the cold extrusion materials and parts to postrotational materials and parts, dig the cubic hole of sleeve backward from front end on the basis of pilot hole, form the pilot hole section at the bottom of the hole, and prolong materials and parts; Utilizing back mold to reach towards the hole wall of rod to hexagonal hole digs the horizontal septal fossula in the sleeve hexagonal hole and dig Zhong Yuan hole and pilot hole at the bottom of the hole of hexagonal hole;
(6). dash the materials and parts between logical cubic hole and the Zhong Yuan hole, form the small sircle hole of sleeve, make described sleeve.
3. the multistation cold extrusion forming method of a kind of sleeve as claimed in claim 2 is characterized in that in station (6), earlier with materials and parts Rotate 180 degree, dashes the materials and parts between logical cubic counterbore and the Zhong Yuan hole again.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009101020406A CN101648227B (en) | 2009-08-27 | 2009-08-27 | Multi-location cold extruding forming method of sleeve barrel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009101020406A CN101648227B (en) | 2009-08-27 | 2009-08-27 | Multi-location cold extruding forming method of sleeve barrel |
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| Publication Number | Publication Date |
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| CN101648227A true CN101648227A (en) | 2010-02-17 |
| CN101648227B CN101648227B (en) | 2012-05-09 |
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| CN2009101020406A Active CN101648227B (en) | 2009-08-27 | 2009-08-27 | Multi-location cold extruding forming method of sleeve barrel |
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Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN102172656A (en) * | 2010-12-10 | 2011-09-07 | 深圳航空标准件有限公司 | Resonance rod cold heading manufacturing method |
| CN102205488A (en) * | 2010-03-31 | 2011-10-05 | 中国商用飞机有限责任公司 | Method for processing hole in split-sleeve cold extrusion manner |
| CN102581052A (en) * | 2012-02-13 | 2012-07-18 | 浙江拓进五金工具有限公司 | Multi-position cold extrusion molding method for universal sockets |
| CN103143580A (en) * | 2013-03-12 | 2013-06-12 | 宁波安拓实业有限公司 | Manufacturing process of conical sleeve |
| CN103785699A (en) * | 2012-10-30 | 2014-05-14 | 加特可株式会社 | Method for forming hollowing portion of shaft portion |
| CN106112402A (en) * | 2016-07-29 | 2016-11-16 | 余姚市婉珍五金厂 | A kind of sleeve cold extrusion processing technics |
| CN108838622A (en) * | 2018-06-25 | 2018-11-20 | 常州市胜彪标准件模具有限公司 | A kind of cold extruding processing method of anti-rotary seat |
| CN110116186A (en) * | 2019-05-08 | 2019-08-13 | 宁波安拓实业有限公司 | The manufacturing method of Automobile Service square hole cross recess sleeve blank |
| CN112475206A (en) * | 2020-11-11 | 2021-03-12 | 金华市忠信五金工具有限公司 | Forming method of hexagonal screwdriver bit sleeve |
| CN112475205A (en) * | 2020-11-11 | 2021-03-12 | 金华市忠信五金工具有限公司 | Method for forming plum-blossom-shaped batch head sleeve |
| CN113458787A (en) * | 2020-03-31 | 2021-10-01 | 邱晨 | Manufacturing method and manufacturing device of screw cap |
Family Cites Families (4)
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| CN100453251C (en) * | 2006-04-20 | 2009-01-21 | 高盟企业股份有限公司 | Method for manufacturing sleeve |
| CN1850423A (en) * | 2006-04-24 | 2006-10-25 | 安徽宁国中鼎金属制品有限公司 | Automobile bushing multi-station cold-upsetting shaping method |
| CN100579710C (en) * | 2006-10-31 | 2010-01-13 | 宁波安拓实业有限公司 | Method for producing angle pin casing tube |
| CN201267837Y (en) * | 2008-09-27 | 2009-07-08 | 北京新光凯乐汽车冷成型件有限责任公司 | Anchoring clamping piece blank multi-station cold extrusion mold |
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2009
- 2009-08-27 CN CN2009101020406A patent/CN101648227B/en active Active
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102205488A (en) * | 2010-03-31 | 2011-10-05 | 中国商用飞机有限责任公司 | Method for processing hole in split-sleeve cold extrusion manner |
| CN102172656A (en) * | 2010-12-10 | 2011-09-07 | 深圳航空标准件有限公司 | Resonance rod cold heading manufacturing method |
| CN102172656B (en) * | 2010-12-10 | 2013-05-08 | 深圳航空标准件有限公司 | Resonance rod cold heading manufacturing method |
| CN102581052A (en) * | 2012-02-13 | 2012-07-18 | 浙江拓进五金工具有限公司 | Multi-position cold extrusion molding method for universal sockets |
| CN103785699B (en) * | 2012-10-30 | 2017-02-22 | 加特可株式会社 | Method for forming hollowing portion of shaft portion |
| CN103785699A (en) * | 2012-10-30 | 2014-05-14 | 加特可株式会社 | Method for forming hollowing portion of shaft portion |
| CN103143580B (en) * | 2013-03-12 | 2015-05-20 | 宁波安拓实业有限公司 | Manufacturing process of conical sleeve |
| CN103143580A (en) * | 2013-03-12 | 2013-06-12 | 宁波安拓实业有限公司 | Manufacturing process of conical sleeve |
| CN106112402A (en) * | 2016-07-29 | 2016-11-16 | 余姚市婉珍五金厂 | A kind of sleeve cold extrusion processing technics |
| CN108838622A (en) * | 2018-06-25 | 2018-11-20 | 常州市胜彪标准件模具有限公司 | A kind of cold extruding processing method of anti-rotary seat |
| CN110116186A (en) * | 2019-05-08 | 2019-08-13 | 宁波安拓实业有限公司 | The manufacturing method of Automobile Service square hole cross recess sleeve blank |
| CN110116186B (en) * | 2019-05-08 | 2021-03-30 | 宁波安拓实业有限公司 | Method for manufacturing square hole cross groove sleeve blank for automobile repair |
| CN113458787A (en) * | 2020-03-31 | 2021-10-01 | 邱晨 | Manufacturing method and manufacturing device of screw cap |
| CN112475206A (en) * | 2020-11-11 | 2021-03-12 | 金华市忠信五金工具有限公司 | Forming method of hexagonal screwdriver bit sleeve |
| CN112475205A (en) * | 2020-11-11 | 2021-03-12 | 金华市忠信五金工具有限公司 | Method for forming plum-blossom-shaped batch head sleeve |
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| Publication number | Publication date |
|---|---|
| CN101648227B (en) | 2012-05-09 |
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Denomination of invention: A multi position cold extrusion method for sleeve Effective date of registration: 20220704 Granted publication date: 20120509 Pledgee: Industrial and Commercial Bank of China Limited Shangyu sub branch Pledgor: ZHEJIANG TUOJIN HARDWARE TOOL Co.,Ltd. Registration number: Y2022330001236 |
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Date of cancellation: 20231220 Granted publication date: 20120509 Pledgee: Industrial and Commercial Bank of China Limited Shangyu sub branch Pledgor: ZHEJIANG TUOJIN HARDWARE TOOL Co.,Ltd. Registration number: Y2022330001236 |
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