CN101062538A - Method for manufacturing mould and its structure - Google Patents

Method for manufacturing mould and its structure Download PDF

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Publication number
CN101062538A
CN101062538A CN 200610075945 CN200610075945A CN101062538A CN 101062538 A CN101062538 A CN 101062538A CN 200610075945 CN200610075945 CN 200610075945 CN 200610075945 A CN200610075945 A CN 200610075945A CN 101062538 A CN101062538 A CN 101062538A
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China
Prior art keywords
mould
thin plate
metal
cavity
thin
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CN 200610075945
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Chinese (zh)
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林承洋
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Individual
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Individual
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Priority to CN 200610075945 priority Critical patent/CN101062538A/en
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Abstract

The invention relates to a mold fabrication method by dividing at least one patterned notch on several thin plates, laminating machining on each cut plate, stacking them into the mold, with the notches formed into the mold cavity, cooling system and ejection system. It can greatly reduce the manufacturing cost and time of mold, getting rid of the extra size of the mold, shrinking it to achieve the goal of light mold.

Description

Mould manufacturing method and structure thereof
Technical field
The present invention relates to a kind of mould structure, particularly a kind of quick Fabrication, accuracy high and lamination type mould manufacturing method and structure thereof cheaply.
Background technology
For the strain arriving in low margin age, all trades and professions are all pursued the reduction of self cost, and effective and efficient manner reduces cost with a large amount of productions exactly for manufacturing industry, the mass-produced most important condition then must provide the mould that casts out this product, utilize filling mold forming mode to make in a large number, but product category must constantly be weeded out the old and bring forth the new now, and the cost of especially consumption electronic products, so mould manufacturing and efficient are the steps of can not ignore.
Mould is a kind of for the injection of melt molding liquid, special implement with moulding reservation shape, structure article, and common shaping dope for example: plastic solution, metallic solution etc., the shaping dope of high temperature is poured in the mould, make model fixed-type this mold cools down again, by ejection system model is ejected, the interior shaping dope of mould is essential to be heated through high temperature earlier so this model is owing to being poured in, so general mould all has cooling system in design again.
Existing mold must be through processing procedures such as borings in addition, therefore need consider the structural strength that each boring processing procedure can bear and the space of reservation at the material of mould and volume, no matter therefore traditional moulds all is one of factor of considering at volume or material, cause the volume of mould and weight to dwindle or to reduce; Moreover carry out cooling step behind the mould filling mould, and also must model be ejected after the cooling by ejection system, therefore mould also must have ejection system in design, add original mould inner mould cave again, so mould process during fabrication complexity very, and above-mentioned die cavity, cooling system and ejection system processing procedure are to use the bore mode gradation to carry out with technology now mostly, so also must expend a large amount of time and money
The present invention is directed to the problems referred to above, propose a kind of mould manufacturing method and structure thereof, can effectively overcome the shortcoming of prior art.
Summary of the invention
Main purpose of the present invention provides a kind of mould manufacturing method and structure thereof, utilizes the lamination mode simultaneously die cavity, cooling system and ejection system to be finished simultaneously, significantly reduces the cost of manufacture and the time of mould.
Another object of the present invention provides a kind of mould manufacturing method and structure thereof, establishes operation by folding under vacuum state, and the engaging force between the thin plate is significantly increased, and the space between the thin plate is eliminated.
Another purpose of the present invention provides a kind of mould manufacturing method and structure thereof, is different from the prior art structure, can exempt the unnecessary volume of mould itself, makes the volume-diminished of mould, and then makes mould reach the requirement of lighting.
A further object of the present invention provides a kind of mould manufacturing method and structure thereof, by lamination mode mfg. moulding die, owing to can cut accurately and folded establishing, can make Mold Making precision better.
According to the present invention, a kind of mould manufacturing method, a plurality of thin plates at first are provided, and make each thin plate cut at least one patterning opening, each thin plate after then will cutting carries out lamination processing, these thin plates are folded mutually established the formation mould, and these patterning openings form at least one cavity in the folded back of establishing.
And mould structure of the present invention is to be established by a plurality of sheet packs to form, and each thin plate is provided with at least one patterning opening, and when these sheet packs were established, each patterning opening was stacked and formed at least one cavity.
The present invention is owing to utilize the lamination mode simultaneously die cavity, cooling system and ejection system to be finished simultaneously, significantly reduce the cost of manufacture and the time of mould, and this lamination mode mfg. moulding die, owing to can cut accurately and folded establishing, can make Mold Making precision better, the present invention is different from the prior art structure in addition, can exempt the unnecessary volume of mould itself, make the volume-diminished of mould, and then make mould reach the requirement of lighting, and establish operation by under vacuum state, folding, and the engaging force between the thin plate is significantly increased, the space between the thin plate is eliminated.
Below the effect of setting forth purpose of the present invention, technology contents, characteristics and being reached is described in detail by the specific embodiment conjunction with figs..
Description of drawings
Fig. 1 is a schematic perspective view of the present invention.
Fig. 2 analyses and observe decomposing schematic representation for solid of the present invention.
Schematic perspective view when Fig. 3 establishes for thin slice of the present invention is folded.
Fig. 4 is the manufacturing flow chart of mould of the present invention.
The figure number explanation
10 mould structures, 12 thin plates
12a thin plate 12b thin plate
14 counterdies, 16 patrixes
18 pour into hole 20 die cavitys
22 passages, 24 through holes
26 patterning openings
The specific embodiment
Mould manufacturing method of the present invention is different from the existing machinery bore mode, no matter at time, precision and the cost of Mold Making improvement is significantly arranged all, below is just explained orally at mould structure and manufacture process.
At first introduce structure of the present invention, with reference to Figure 1 and Figure 2, this mould structure 10 is to be formed by a plurality of thin plate 12 folded establishing, the material of this thin plate 12 is a metal material, and thin plate 12 also can be heat-resisting material in addition, and this mould structure 10 comprises counterdie 14 and patrix 16, this counterdie 14 is provided with one and pours into hole 18, and between counterdie 14 and patrix 16, be provided with a die cavity 20, pour into hole 18 therewith die cavity 20 communicate, this pours into hole 18 and can pour into and flow in this die cavity 20 for the shaping dope of fusion; Be provided with cooling system and ejection system in addition in the mould structure 10 in addition, this cooling system is that form with a plurality of passages 22 presents at this embodiment, ejection system then is to present in the form that counterdie 14 is provided with four through holes 24 at this embodiment, this cooling system can make the shaping dope cooling that pours into form the model body, and ejection system then can eject the model body.
Please be simultaneously with reference to Fig. 2 and shown in Figure 3, because of mould structure 10 is to be formed by a plurality of thin plate 12 folded establishing, so each thin plate 12 is provided with a plurality of patterning openings 26, for example counterdie 14 structural thin plate 12a are provided with the through hole 24 and the die cavity 20 of ejection system of part among Fig. 3, the passage that pours into hole 18 and cooling system 22 that then has part at patrix 16 structural thin plate 12b, respectively with thin plate 12 folded patrix 16 and the counterdies 14 of being set as, the folded back patrix 16 of establishing can formation pour into hole 18, the passage 22 of cooling system and the depressed part of die cavity 20, counterdie 14 then can form the through hole 24 of ejection system, the passage 22 of cooling system and the protuberance of die cavity 20; Therefore the patterning opening 26 on each thin plate 12 can be selected from die cavity 20, pour into a wherein part of hole 18, cooling system and ejection system because of the folded position difference of establishing, establish when forming mould structure 10 when these thin plates 12 are folded, each patterning opening 26 is stacked and is formed a plurality of cavitys, and these cavitys just comprise the passage 22 that pours into hole 18, die cavity 20, cooling system and the through hole 24 of ejection system.
Then introduce the manufacture method of this mould, please refer to shown in Figure 4, at first carry out step S1, this step is by Computer Simulation, also the notion that is about to the designer is set up product model in computer, and on the model of being set up, set up out mould, and in mould, add cooling system, ejection system etc., then the model of being set up is carried out emulation section (slicing), produce embryo rapidly with the mode and the form of stacking layer by layer, Chang Yong computer software can be selected Autocad now, Solid-work or PRO-ENGINEER etc., therefore can learn the minimum area of each section by Computer Simulation, thickness and the position is set produces mould in folded mode of establishing.
Then carry out step S2 according to the data that computer calculated, this step S2 prepares a plurality of sheet metals, this thin plate can be formed by cutter cutting or laser cutting, then carry out step S3, this step is the one or more patterning openings of cutting on each thin plate, and this patterning number of openings, position and area all are that the data that calculate according to computer are cut; Then carry out lamination procedure of processing S4, this step must be carried out under vacuum state, this step is the thin slice that each cutting is finished to be folded establish, wherein can utilize adhesive agent between each thin slice, the metal welding, laser spot welding, modes such as electric resistance welding or ultrasonic joint are folded and are established, and each thin slice is finished the preliminary form of back formation mould folded establishing, and this step mode commonly used is a laser spot welding, laser spot welding is laser directly to be penetrated do accurate welding on the pad of sheet surface, therefore this welding only produces the heat of a little, so other partly can't be influenced; The metal welding then is at thin sheet surface the layer of metal layer to be set, and utilizes HTHP to make to form alloy between metal level and the thin plate and thin plate is engaged, and this metal level is a copper metal layer.
And each thin slice is behind storehouse, and the patterning opening storehouse on each thin slice forms a plurality of cavitys, and these cavitys comprise die cavity, cooling system passage, ejection system through hole and the hole that pours into of shaping dope input is provided; Carry out step S5 at last, this step is to carry out the surface treatment of thin portion at die surface, and this surface treatment is to utilize high temperature to make the trickle fusion of die surface, makes die surface present smooth effect, can finish mould structure 10 as shown in Figure 1.
The above is by embodiment characteristics of the present invention to be described, its objective is that person skilled can understand content of the present invention and implement according to this, rather than be used for limiting claim of the present invention, therefore other does not anyly break away from the identity property that spirit set forth in the present invention finishes and modifies or revise, and must be included in the claim scope of the present invention.

Claims (13)

1, a kind of mould manufacturing method is characterized in that, this method comprises the following steps:
A plurality of thin plates are provided;
Each this thin plate cuts at least one patterning opening; And
Each this thin plate after the cutting is carried out lamination processing, those thin plates are folded mutually established the formation mould, and those patterning openings form at least one cavity in the folded back of establishing.
2, mould manufacturing method according to claim 1 is characterized in that, this lamination processing is to carry out under vacuum state.
3, mould manufacturing method according to claim 1 is characterized in that, the material of this thin plate is selected from metal or heat-resisting material.
4, mould manufacturing method according to claim 1 is characterized in that, this patterning opening can be formed by cutter cutting or laser cutting.
5, mould manufacturing method according to claim 1 is characterized in that, those thin plates utilize adhesive agent, metal welding, laser spot welding, electric resistance welding or ultrasonic juncture to fold mutually and establish.
6, mould manufacturing method according to claim 5 is characterized in that, this metal welding is at this thin sheet surface the layer of metal layer to be set, and utilizes HTHP to make between this metal level and this thin plate and forms alloy, and this thin plate is engaged.
7, mould manufacturing method according to claim 1 is characterized in that, this cavity is to be selected from die cavity, to eject passage or cooling duct.
8, mould manufacturing method according to claim 1 is characterized in that, provides those thin plate steps to take a step forward and comprises a Computer Simulation step, is used for obtaining this patterning opening shape, area and the position that each this thin plate cuts.
9, a kind of mould structure is characterized in that, it is to be established by a plurality of sheet packs to form, and each this thin plate is provided with at least one patterning opening, and when those sheet packs were established, this patterning opening formed at least one cavity by stacking.
10, mould structure according to claim 9 is characterized in that, the material of this thin plate is selected from metal or heat-resisting material.
11, mould structure according to claim 9 is characterized in that, this patterning opening can be formed by cutter cutting or laser cutting.
12, mould structure according to claim 9 is characterized in that, those thin plates are to utilize modes such as adhesive agent, metal welding, laser spot welding, electric resistance welding or ultrasonic joint to fold mutually to establish.
13, mould structure according to claim 9 is characterized in that, this cavity is to be selected from die cavity, to eject passage or cooling duct.
CN 200610075945 2006-04-25 2006-04-25 Method for manufacturing mould and its structure Pending CN101062538A (en)

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Application Number Priority Date Filing Date Title
CN 200610075945 CN101062538A (en) 2006-04-25 2006-04-25 Method for manufacturing mould and its structure

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Application Number Priority Date Filing Date Title
CN 200610075945 CN101062538A (en) 2006-04-25 2006-04-25 Method for manufacturing mould and its structure

Publications (1)

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CN101062538A true CN101062538A (en) 2007-10-31

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103264269A (en) * 2013-06-13 2013-08-28 沈阳飞机工业(集团)有限公司 Processing method of long-narrow composite material molding part assembling mould
CN103659207A (en) * 2013-12-23 2014-03-26 上海爱知锻造有限公司 Technology for manufacturing edge trimming die of crankshaft forge piece
CN104989642A (en) * 2015-08-02 2015-10-21 衢州市易凡设计有限公司 Multilayer screw shaft
CN105945523A (en) * 2016-06-14 2016-09-21 沈阳飞机工业(集团)有限公司 Machining method for thermal drawing die with complex profiles
CN106175946A (en) * 2016-08-29 2016-12-07 北京缔佳医疗器械有限公司 The production method of a kind of dental appliance and device
CN108857300A (en) * 2018-07-24 2018-11-23 苏州普热斯勒先进成型技术有限公司 A kind of simple die and its manufacturing method
CN109228267A (en) * 2018-11-15 2019-01-18 陕西宏象房车科技发展有限公司 Thermoplastic plate reshaping device and forming method

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103264269A (en) * 2013-06-13 2013-08-28 沈阳飞机工业(集团)有限公司 Processing method of long-narrow composite material molding part assembling mould
CN103264269B (en) * 2013-06-13 2015-10-28 沈阳飞机工业(集团)有限公司 The processing method of long narrow class composite material forming part combination mould
CN103659207A (en) * 2013-12-23 2014-03-26 上海爱知锻造有限公司 Technology for manufacturing edge trimming die of crankshaft forge piece
CN104989642A (en) * 2015-08-02 2015-10-21 衢州市易凡设计有限公司 Multilayer screw shaft
CN105945523A (en) * 2016-06-14 2016-09-21 沈阳飞机工业(集团)有限公司 Machining method for thermal drawing die with complex profiles
CN105945523B (en) * 2016-06-14 2018-08-21 沈阳飞机工业(集团)有限公司 The hot-stretch mould processing method of complex profile
CN106175946A (en) * 2016-08-29 2016-12-07 北京缔佳医疗器械有限公司 The production method of a kind of dental appliance and device
CN108857300A (en) * 2018-07-24 2018-11-23 苏州普热斯勒先进成型技术有限公司 A kind of simple die and its manufacturing method
CN109228267A (en) * 2018-11-15 2019-01-18 陕西宏象房车科技发展有限公司 Thermoplastic plate reshaping device and forming method

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Open date: 20071031