CN103343339B - The laser repair method of Drawing Die - Google Patents

The laser repair method of Drawing Die Download PDF

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Publication number
CN103343339B
CN103343339B CN201310267077.0A CN201310267077A CN103343339B CN 103343339 B CN103343339 B CN 103343339B CN 201310267077 A CN201310267077 A CN 201310267077A CN 103343339 B CN103343339 B CN 103343339B
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overlay cladding
drawing die
laser
repair method
adopts
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CN103343339A (en
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唐全林
张智明
高云飞
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Suzhou Haiershi Information Technology Co ltd
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Suzhou Tangshi Machinery Manufacturing Co Ltd
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Abstract

The present invention relates to a kind of laser repair method of Drawing Die, the surface of Drawing Die to be repaired is processed, detects analysis, remove the fatigue layer of abrading section; Built-up welding is carried out to abrading section and forms the first overlay cladding, then at the first layer overlay cladding enterprising windrow weldering formation second overlay cladding, the thickness of described first overlay cladding is 2mm to 3mm, the thickness of described second overlay cladding is 2mm to 3mm, built-up welding adopts the mode of preset powder feeding, is that light source carries out lap connection scanning to mould with fast-transverse-flow CO2 laser.The laser repair method of Drawing Die of the present invention carries out laser melting coating to the surface of Drawing Die, and the size of its surface hardness and abrading section can be made to reach service requirements.

Description

The laser repair method of Drawing Die
Technical field
The present invention relates to a kind of laser cladding method, especially a kind of laser melting coating restorative procedure of die surface.
Background technology
Punching press is at room temperature, utilizes the press tool be arranged on pressing machine to apply pressure to material, makes it produce separation or viscous deformation, thus obtains a kind of pressure processing method of required part.Press tool is requisite tooling in punching production, is technological-intensive product.The quality of stamping parts, production efficiency and production cost etc., have direct relation with die design and manufacture.Press tool is divided into blanking die, piercing die, bending die, Drawing Die, flaring die etc. according to technological property, these press tools are are all inevitably worn and torn in the course of the work, but because each mould role is different, stressing conditions during punching press is different, and the degree of wear in working process and wearing character are also different.Carry out die surface reparation by common overlaying method, the shortcomings such as deflection is large, hardness is not enough, easy to crack can be brought.And different moulds should select more suitable renovation technique according to its characteristic, otherwise the mold use life-span cannot be protected, and can have a strong impact on mold use precision, cause produced quality product to decline.
Laser melting coating refers to and is made it to melt with matrix surface skim through laser irradiation by coated material cladding matrix surface placed by selecting with different adding material modes simultaneously, and it is extremely low to form extent of dilution after rapid solidification, the top coat of metallurgical binding is become with matrix, the remarkable processing method improving the wear-resisting, anti-corrosion, heat-resisting, anti-oxidant of substrate surface and electrical specification, thus reach the object of surface modification or reparation.With built-up welding, spraying, plating and gas phase sediment-filled phase ratio, laser melting coating has that extent of dilution is little, dense structure, coating and matrix is combined, be applicable to that cladding material is many, granularity and the feature such as content is large.How laser melting and coating technique being effectively applied to the reparation of Drawing Die, is the problem that those skilled in the art needs to solve.
Summary of the invention
The technical problem to be solved in the present invention is to provide a kind of surface to Drawing Die and carries out laser melting coating, makes the size of its surface hardness and abrading section reach the laser repair method of the Drawing Die of service requirements.
In order to solve the problems of the technologies described above, the invention provides a kind of laser repair method of Drawing Die, comprise following concrete steps:
The first step, the surface of Drawing Die to be repaired to be processed;
Second step, carry out detection analyze, determine abrading section and abrasion loss thereof;
The fatigue layer of the 3rd step, removal abrading section;
4th step, detection analytical results according to Drawing Die, programme to the die cavity of abrading section, formulates processing parameter;
5th step, built-up welding is carried out to abrading section form the first overlay cladding, then at the first layer overlay cladding enterprising windrow weldering formation second overlay cladding, the thickness of described first overlay cladding is 2mm to 3mm, the thickness of described second overlay cladding is 2mm to 3mm, in weld deposit process, constantly evenly knock mould alloy cladding layer, built-up welding adopts the mode of preset powder feeding, be that light source carries out lap connection scanning to mould with fast-transverse-flow CO2 laser, laser power is 1200W to 1400W, spot size is 12mm × 1.8mm, laser apparatus is 255mm to 265mm from the distance between Substrate, sweep velocity is 150mm/min to 180mm/min, amount of lap is 4.5mm, powder sending quantity is 8g/min to 11g/min, the component of the powdered alloy that the first overlay cladding adopts and weight percent content are C≤0.1%, Cr:15% to 19%, B:1.5% to 2.5%, Si:1% to 2%, Mo:0.8% to 1%, Mn:2% to 5%, all the other are Fe, the component of the powdered alloy that the second overlay cladding adopts and weight percent content are C≤0.1%, Cr:9% to 12%, B:1.5% to 2.5%, Si:1% to 2%, Mo:1.2% to 1.6%, Mn:5% to 7%, W:2% to 4%, V: 2% to 6%, TiO 2: 5% to 10%, all the other are Fe,
6th step, detection surface hardness and deflection, carry out mechanical workout, permeation flaw detection to the Drawing Die after repairing.
The mass percentage content of the Mn in the powdered alloy that above-mentioned second overlay cladding adopts is 5.6% to 6.6%.
The mass percentage content of the W in the powdered alloy that above-mentioned second overlay cladding adopts is 2.8% to 3.5%.
The mass percentage content of the V in the powdered alloy that above-mentioned second overlay cladding adopts is 4.2% to 5.8%.
TiO in the powdered alloy that above-mentioned second overlay cladding adopts 2mass percentage content be 6.3% to 8.7%.
The beneficial effect that the present invention brings is: the laser repair method of Drawing Die of the present invention is lower according to the wearing character of Drawing Die first built-up welding one deck hardness, wear resistance generally organizes the first overlay cladding that is comparatively fine and close, good uniformity, higher, good second overlay cladding of wear resistance of built-up welding one deck hardness on the first overlay cladding again, during the second overlay cladding built-up welding, the first overlay cladding does not still cool, and both all have selected suitable powdered alloy and carry out built-up welding, wettability between two overlay claddings is good, in conjunction with tightr.The content of the strict control C of the powdered alloy of the second overlay cladding, be conducive to the wettability improving cladding layer, prevent from cracking in cladding process and pore, add appropriate B, Si and make alloy form matrix based on austenite after solidification, utilize appropriate Cr, Mn, W, Mo, V, TiO 2carry out alloy strengthening to ferrous alloy, even if C content is lower, the hardness of cladding layer also can reach more than 55.5HRC, fully meets the hardness requirement that mould uses, and has very high wear resistance.Adopt the mode of preset powder feeding in addition, strictly control powder sending quantity, and laser power, sweep velocity, amount of lap etc. are optimized, such that the homogeneity of structure of cladding layer is good, thickness and hardness even.The method did not need to carry out preheating to mould before built-up welding, without the need to annealing to mould after built-up welding, effectively can control the distortion of mould, and heat can be avoided to concentrate generation thermal stresses by carrying out laser melting coating in an orderly manner everywhere, be conducive to reducing distortion further, improve hardness and the wear resistance of mould.
Embodiment
Embodiment 1
The concrete steps of the laser repair method of the Drawing Die of the present embodiment are as follows:
The first step, the surface of Drawing Die to be repaired to be processed, by removings such as the dust in Drawing Die, greasy dirt, corrosions.
Second step, carry out detection and analyze, original working conditions, hardness and the mechanical property parameters of record Drawing Die, detects the size at each position of Drawing Die, determines abrading section and abrasion loss thereof.
3rd step, remove the right angle of abrading section by polishing, remove the fatigue layer of abrading section, and clean.
4th step, detection analytical results according to Drawing Die, programme (numerical control machining simulation system that programming can use Mitsubishi) to the die cavity of abrading section, formulate processing parameter.
5th step, built-up welding is carried out to abrading section form the first overlay cladding, then at the first layer overlay cladding enterprising windrow weldering formation second overlay cladding, the thickness of described first overlay cladding is 3mm, the thickness of described second overlay cladding is 3mm, in weld deposit process, constantly evenly knock mould alloy cladding layer with mallet.Built-up welding adopts the mode of preset powder feeding, is that light source carries out lap connection scanning to mould with fast-transverse-flow CO2 laser.Laser power is 1400W, and spot size is 12mm × 1.8mm, and laser apparatus is 265mm from the distance between Substrate, and sweep velocity is 180mm/min, and amount of lap is 4.5mm, and powder sending quantity is 8g/min.The component of the powdered alloy that the first overlay cladding adopts and weight percent content are C:0.07%, Cr:15.4%, B:2.2%, Si:1.4%, Mo:0.8%, Mn:2.5%, and all the other are Fe.The component of the powdered alloy that the second overlay cladding adopts and weight percent content are C:0.08%, Cr:10.2%, B:2%, Si:1.5%, Mo:1.5%, Mn:6.5%, V: 4.5%, W:3.2%, TiO 2: 8.1%, all the other are Fe.
6th step, detection surface hardness and deflection, carry out mechanical workout, permeation flaw detection to the Drawing Die after repairing.
Mean value through the surface hardness of the Drawing Die of the laser repair method reparation of the Drawing Die of the present embodiment reaches 57.2HRC, and the hardness Schwellenwert in all check points is 55.7HRC.
Embodiment 2
The rest part of the laser repair method of the Drawing Die of the present embodiment is identical with embodiment 1, difference is: laser power is 1200W, spot size is 12mm × 1.8mm, laser apparatus is 255mm from the distance between Substrate, sweep velocity is 170mm/min, amount of lap is 4.5mm, and powder sending quantity is 10g/min.The component of the powdered alloy that the first overlay cladding adopts and weight percent content are C:0.09%, Cr:17.5%, B:1.7%, Si:1.1%, Mo:0.9%, Mn:3.4%, and all the other are Fe.The component of the powdered alloy that the second overlay cladding adopts and weight percent content are C:0.06%, Cr:11.6%, B:1.8%, Si:1.2%, Mo:1.3%, Mn:5.8%, V:5.3%, W:3.4%, TiO 2: 7.6%, all the other are Fe.
Mean value through the surface hardness of the Drawing Die of the laser repair method reparation of the Drawing Die of the present embodiment reaches 57.3HRC, and the hardness Schwellenwert in all check points is 55.6HRC.
Embodiment 3
The rest part of the laser repair method of the Drawing Die of the present embodiment is identical with embodiment 1, difference is: laser power is 1300W, spot size is 12mm × 1.8mm, laser apparatus is 260mm from the distance between Substrate, sweep velocity is 180mm/min, amount of lap is 4.5mm, and powder sending quantity is 8g/min.The component of the powdered alloy that the first overlay cladding adopts and weight percent content are C:0.05%, Cr:16.5%, B:2%, Si:1.3%, Mo:0.8%, Mn:3.6%, and all the other are Fe.The component of the powdered alloy that the second overlay cladding adopts and weight percent content are C:0.09%, Cr:7.6%, B:2.2%, Si:1.8%, Mo:1.5%, Mn:5.9%, V: 4.8%, W:2.9%, TiO 2: 6.7%, all the other are Fe.
Mean value through the surface hardness of the Drawing Die of the laser repair method reparation of the Drawing Die of the present embodiment reaches 57.4 HRC, and the hardness Schwellenwert in all check points is 55.7HRC.
Obviously, above-described embodiment is only for example of the present invention is clearly described, and is not the restriction to embodiments of the present invention.For those of ordinary skill in the field, can also make other changes in different forms on the basis of the above description.Here exhaustive without the need to also giving all embodiments.And these belong to spirit institute's apparent change of extending out of the present invention or change and are still among protection scope of the present invention.

Claims (5)

1. a laser repair method for Drawing Die, comprises following concrete steps:
The first step, the surface of Drawing Die to be repaired to be processed;
Second step, carry out detection analyze, determine abrading section and abrasion loss thereof;
The fatigue layer of the 3rd step, removal abrading section;
4th step, detection analytical results according to Drawing Die, programme to the die cavity of abrading section, formulates processing parameter;
5th step, built-up welding is carried out to abrading section form the first overlay cladding, then at the first layer overlay cladding enterprising windrow weldering formation second overlay cladding, the thickness of described first overlay cladding is 2mm to 3mm, the thickness of described second overlay cladding is 2mm to 3mm, in weld deposit process, constantly evenly knock mould alloy cladding layer, built-up welding adopts the mode of preset powder feeding, be that light source carries out lap connection scanning to mould with fast-transverse-flow CO2 laser, laser power is 1200W to 1400W, spot size is 12mm × 1.8mm, laser apparatus is 255mm to 265mm from the distance between Substrate, sweep velocity is 150mm/min to 180mm/min, amount of lap is 4.5mm, powder sending quantity is 8g/min to 11g/min, the component of the powdered alloy that the first overlay cladding adopts and weight percent content are C≤0.1%, Cr:15% to 19%, B:1.5% to 2.5%, Si:1% to 2%, Mo:0.8% to 1%, Mn:2% to 5%, all the other are Fe, the component of the powdered alloy that the second overlay cladding adopts and weight percent content are C≤0.1%, Cr:9% to 12%, B:1.5% to 2.5%, Si:1% to 2%, Mo:1.2% to 1.6%, Mn:5% to 7%, W:2% to 4%, V: 2% to 6%, TiO 2: 5% to 10%, all the other are Fe,
6th step, detection surface hardness and deflection, carry out mechanical workout, permeation flaw detection to the Drawing Die after repairing.
2. the laser repair method of Drawing Die according to claim 1, is characterized in that: the mass percentage content of the Mn in the powdered alloy that the second overlay cladding adopts is 5.6% to 6.6%.
3. the laser repair method of Drawing Die according to claim 1, is characterized in that: the mass percentage content of the W in the powdered alloy that the second overlay cladding adopts is 2.8% to 3.5%.
4. the laser repair method of Drawing Die according to claim 1, is characterized in that: the mass percentage content of the V in the powdered alloy that the second overlay cladding adopts is 4.2% to 5.8%.
5. the laser repair method of Drawing Die according to claim 1, is characterized in that: the TiO in the powdered alloy that the second overlay cladding adopts 2mass percentage content be 6.3% to 8.7%.
CN201310267077.0A 2013-06-29 2013-06-29 The laser repair method of Drawing Die Expired - Fee Related CN103343339B (en)

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CN106350813A (en) * 2016-09-06 2017-01-25 张家港清研再制造产业研究院有限公司 Repair method of drawing die of back cover of roller washing machine
CN109487262B (en) * 2018-09-04 2020-12-04 中国科学院近代物理研究所 FeNi-based laser cladding doped tungsten carbide/chromium carbide composite reinforced high-temperature-resistant wear-resistant coating and preparation method thereof

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CN101974750B (en) * 2010-07-06 2011-09-07 山东能源机械集团大族再制造有限公司 Laser strengthening process for tapered surface of pick body
CN102021568B (en) * 2010-07-06 2011-11-23 山东能源机械集团大族再制造有限公司 Method for laser hardening gear part
CN102002707A (en) * 2010-11-25 2011-04-06 秦皇岛洪川实业有限公司 Laser repairing method of damaged finishing roller
CN102677048A (en) * 2012-05-27 2012-09-19 丹阳市宏图机械制造有限公司 Laser repairing technology for high-speed motor rotor
CN103572283B (en) * 2012-07-18 2015-09-23 重庆广播电视大学 The laser reinforcing process of perforating head
CN103668179B (en) * 2012-07-18 2016-01-27 深圳市华宇顺塑胶有限公司 Without the need to the laser repairing process of the vehicle mould of preheating
CN102828181A (en) * 2012-09-20 2012-12-19 丹阳宏图激光科技有限公司 Laser cladding repair process for cross shafts
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