CN109576604A - A kind of impact-resistant abrasion-proof material for laser manufacture - Google Patents

A kind of impact-resistant abrasion-proof material for laser manufacture Download PDF

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Publication number
CN109576604A
CN109576604A CN201910088499.9A CN201910088499A CN109576604A CN 109576604 A CN109576604 A CN 109576604A CN 201910088499 A CN201910088499 A CN 201910088499A CN 109576604 A CN109576604 A CN 109576604A
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laser
impact
alloy
resistant
resistant abrasion
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CN201910088499.9A
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CN109576604B (en
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王敏
陈海涛
董思远
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Shenyang Continental Laser Engineering Technology Co Ltd
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Shenyang Continental Laser Engineering Technology Co Ltd
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/56Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.7% by weight of carbon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/005Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/44Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/46Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/48Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/54Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00Coating starting from inorganic powder
    • C23C24/08Coating starting from inorganic powder by application of heat or pressure and heat
    • C23C24/10Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
    • C23C24/103Coating with metallic material, i.e. metals or metal alloys, optionally comprising hard particles, e.g. oxides, carbides or nitrides
    • C23C24/106Coating with metal alloys or metal elements only

Abstract

The present invention provides a kind of impact-resistant abrasion-proof material for laser manufacture, it is grouped as by following mass percent group: C:2.9-3.8%, Cr:15-23%, Si:1.00-1.30%, Ni:0.2-0.95%, Mn:0.9-1.5%, W:2-5.5%, V:14-21%, B:0.8-1.8%, Nb:5.50-10%, Y:0.8-2.3%, surplus are Fe and inevitable impurity.The laser melting coating for the impact-resistant abrasion-proof that the present invention provides iron(-)base powder has shock resistance, corrosion-resistant, anti abrasive performance, can be used for the laser manufacture of the large-scale and middle-size and small-size component of the complex working conditions such as Large Crusher.The composite wear part prepared using laser meets complex working condition to the needs of workpiece working surface comprehensive mechanical property, while the common material of low cost can be used in matrix, and the matrix after use also carries out secondary recycling using laser manufacture;The present invention can not only provide the utilization rate of component overall material, while can improve and service life reduction maintenance and repair time is intended for single use, and increase resource utilization, reduce manpower loss.

Description

A kind of impact-resistant abrasion-proof material for laser manufacture
Technical field
The invention belongs to laser melting and coating technique field, in particular to a kind of laser manufactures impact-resistant abrasion-proof alloy powder.
Background technique
Laser fabrication technology history is not long, but is developed so far from its birth, in aerospace field, garage There is a large amount of engineer application in the fields such as industry, metallurgy, petrochemical industry, electric power large rotor, but do not have the powder specifically for laser manufacture End.The technical advantage of laser manufacture is the laser using high energy beam, utilizes powder quickly to be formed in matrix surface complete with matrix Different alloy-layers, while having a certain amount of basic material and being diluted in alloy-layer, i.e., alloy composition of layer is designed to powder Divide and generates deviation, and existing a large amount of powder design does not all consider the diluting effect of matrix.
Now with the rapid growth of industrial products steel, coal, cement output, raw material, the broken of finished product, grinding work Consume a large amount of wear-resistant material.Largely the operating condition of the jaw tup of component such as crushers, ball grinding machine lining board, abrading-ball etc. is all Impact and abrasion compound action, and shock resistance decline can be directly resulted in by improving wearability, seriously affect workpiece uses the longevity Life, this is implacable contradiction under impact wear operating condition, while using traditional preparation method prepare impact-resistant abrasion-proof layer when There is the net distributions of the segregation of tissue and hard phase, can all deteriorate shock resistance.Laser manufacture quickly solidification, tissue are thin The small uniformly granular distribution of hard phase simultaneously, so that the alloy-layer of laser manufacture has better Impact wear resistance.
Summary of the invention
According to above content, the invention mainly includes researching and developing, a kind of shock resistance meeting impact wear duty requirements is resistance to Alloy material is ground, it can be full in carbon steel, low-alloy steel, high-alloy steel matrix surface manufacture cladding layer by laser melting and coating technique Abrasion resistance properties demand of foot under the conditions of impact.
A kind of impact-resistant abrasion-proof material for laser manufacture, is grouped as by following mass percent group: C:2.9-3.8%, Cr:15-23%, Si:1.00-1.30%, Ni:0.2-0.95%, Mn:0.9-1.5%, W:2-5.5%: V:14-21%, B:0.8- 1.8%, Nb:5.50-10%, Y:0.8-2.3%, surplus are Fe and inevitable impurity.
The characteristics of this alloy powder, is to fully consider that matrix prepares alloy-layer to laser using ferrous alloy as matrix The influence of energy breaks through the proportion rule of traditional alloy design, using the ability of the superpower capture carbon of niobium and vanadium, inside alloy-layer Form a large amount of abrasion-resistive hard particle;The chromium of certain content can be in free state in alloy-layer simultaneously, have alloy-layer Tissue has a certain amount of retained austenite while good corrosion resisting property, can meet rushing with corrosive medium fluid simultaneously It hits and washes away.
A large amount of experiment has been carried out in the research process of the powder, has carried out multiple groups reality for impact-resistant abrasion-proof performance demand The content proportion for having first verified that carbon and vanadium is tested, discovery obtains alloy-layer when carrying out material composition design using vanadium/carbon ≈ 3 Hardness less than HRC50, and after being heat-treated, hardness is further decreased, find that there are bases through composition detection and design ingredient comparison The dilution of body and the scaling loss of carbon cause laser to prepare the deviations of alloy-layer and powdered ingredients.It is found into multiple groups experimental verification is crossed The ratio excellent of vanadium carbon of the invention, this become the impact-resistant abrasion-proof material design basis, on this basis into The perfect experiment of powder property of having gone.The collective effect of niobium and vanadium can further refine crystal grain and reduce grain size, promote crystal grain Refinement while refined the sizes of abrasion resistant particles, this has very big raising, while the carbide of niobium to shock resistance It can be distributed in crystal boundary, certain pinning effect is woven with to group, the intensity of alloy-layer parent phase can be improved, ensure that alloy-layer is provided simultaneously with Good wearability and impact resistance.Design of material will combine vanadium/carbon, vanadium/niobium and niobium/carbon ratio in the invention, warp Test data is verified as vanadium: niobium: carbon ≈ 10:5:2.So the design of niobium element content is also the pass that the design of material needs to optimize Key factor, content of niobium are less than 5.5%, and unobvious to the thinning effect of crystal grain, content of niobium is greater than 10%, and the carbide of niobium has obviously Clustering phenomena destroy laser cladding layer shock resistance, while extra niobium can with iron formed unstable compound it is further The shock resistance of deteriorated tissue, so to be designed as 5.5-10% best for the content of niobium.It is good that the addition of chromium allows alloy-layer to have Corrosion resistance, while residual chromium is remarkably improved the content of wearability and retained austenite to the solution strengthening of matrix, it is preferably full The demand of foot impact operating condition.Ferrous alloy is generally difficult to take into account wearability and obdurability, increases carbon content to increase wearability When with alloy content, the toughness that will lead to the agglomeration deterioration alloy of alloy carbide causes shock resistance to decline.This hair The bright collective effect using vanadium niobium and optimize its ratio, so that the ferrous alloy of laser manufacture obtains of a large amount of Dispersed precipitates Grain does not deteriorate toughness, so that ferrous alloy has simultaneously because the good collocation of vanadium niobium carbon ensure that particle dispersion distributional pattern Good Impact wear resistance.
What the present invention provided has the significant performance suitable for laser manufacture with impact-resistant abrasion-proof material, has in guarantee Laser manufacture alloy-layer of good performance is obtained in the diluted situation of matrix, and metal powder is allowed to play it under laser melting and coating process Optimal Impact wear resistance.
What the present invention provided has impact-resistant abrasion-proof laser melting coating iron(-)base powder, uses in actual operation 6kw optical fiber laser or 4kw solid state laser, carbon steel, low-alloy steel, high-alloy steel surface laser cladding technological parameter It is: power: 2800-4000W, circle spot diameter: 3.2-6mm, scanning speed: 800-1500mm/min, overlapping rate: 45-65%, Powder feed rate: 22-42g/min.But the material is after laser prepares preheating and laser melting coating before needing to have laser melting coating Heat treatment can be used surface induction and heat the hot standby heat treatment carried out after preheating and cladding, and preheating temperature is 200 DEG C of a surface left side The right side, heat treatment temperature is 480-620 DEG C after laser melting coating.
The beneficial effects of the present invention are.
The laser melting coating for the impact-resistant abrasion-proof that the present invention provides has shock resistance, corrosion-resistant, wear-resisting with iron(-)base powder The performance of damage can be used for the laser manufacture of the large-scale and middle-size and small-size component of the complex working conditions such as Large Crusher.It is prepared using laser Composite wear part, it can be achieved that the design concept that will be use the best steel to make the knife's edge, it is comprehensive to workpiece working surface to meet complex working condition The needs of mechanical property are closed, while the common material of low cost can be used in matrix, and the matrix after use is also using laser Manufacture carries out secondary recycling.The invention can not only provide the utilization rate of component especially large component overall material, simultaneously It greatly improves and service life reduction maintenance and repair time is intended for single use, increase resource utilization, reduce manpower loss.
Detailed description of the invention
Fig. 1 is the impact-resistant abrasion-proof materials microstructure state diagram for laser manufacture that embodiment 1 is prepared.
Fig. 2 is the impact-resistant abrasion-proof materials microstructure state diagram for laser manufacture that embodiment 2 is prepared.
Specific embodiment
Embodiment 1.
With 6KW optical fiber laser, R & D design anti-attrition heat resistanceheat resistant iron(-)base powder, material composition matches as follows: by weight Percentages, include C:3.0%, Cr:19%, Si:1.00%, Ni:0.55%, Mn:1.3%, W:2.4%: V:16.2%, B:1.0%, Nb:8%, Y:0.9%, surplus are Fe and inevitable impurity, carry out laser manufacture to ball grinding machine lining board.Trial-production sample is determined first Block basic material is 35CrMo, and sample block size 100mm × 100mm × 20mm first clears up specimen surface, with using acetone Cleaning is carried out to degrease;Impact-resistant abrasion-proof alloy powder is carried out to the drying and processing of 200 DEG C of heat preservation 1.5h.It is heated using surface Equipment carries out induction to workpiece surface and quickly heats up to 200 DEG C and laser equipment Synchronous Heating, and laser melting coating condition is adopted after having With melting and coating process parameter: power 3800W, hot spot circular diameter 3.4mm, scanning speed 1100mm/min, overlapping rate 50% are synchronized and are sent Powder 36g/min carries out laser melting coating.The impact-resistant abrasion-proof alloy-layer that 1.4mm thickness is obtained after laser melting coating, since alloy-layer contains A large amount of alloying component obtains a large amount of hard particles after laser melting coating with good wearability, simultaneously because chromium content ratio Higher, the comparision contents of retained austenite are big, and residual stress is also relatively high, need to be heat-treated after carrying out cladding, heat treatment temperature It is 495 DEG C.The structural state of the alloy-layer of acquisition is as shown in Fig. 1.
The laser cladding layer of acquisition is detected, hardness is HRC63.3~65.2, and uniformity of hardness is good, is fluctuated small. The cladding layer carries out its dry friction coefficient of friction-wear test 0.40, and weightlessness is the 18% of Cr12MoV on year-on-year basis, and wearability obtains To greatly improving.Carry out nonstandard non-notch impact test to cladding layer, compared with Cr12MoV, impact flexibility and its 7% is reduced compared to toughness, significantly lower but wearability does not occur and is significantly increased for toughness.
Embodiment 2.
With 4KW solid state laser, the anti-attrition heat resistanceheat resistant Co-based alloy powder of R & D design, material composition matches as follows: by weight Amount percentages, C:3.4%, Cr:17%, Si:1.20%, Ni:0.8%, Mn:0.95%, W:3.5%: V:19%, B:1.3%, Nb: 8.20%, Y:0.9%, surplus are Fe and inevitable impurity.Determine that trial-production sample block basic material is 45 steel, sample block size first 100mm × 100mm × 20mm, first clears up specimen surface, is degreased with cleaning is carried out with acetone;Shock resistance is resistance to Grind the drying and processing that alloy powder carries out 200 DEG C of heat preservation 1.5h.Workpiece surface incude quickly using surface heating equipment 230 DEG C and laser equipment Synchronous Heating are heated to, laser melting coating condition uses melting and coating process parameter: power 4000W, light after having Spot circular diameter 4.0mm, scanning speed 1000mm/min, overlapping rate 55%, synchronous powder feeding system 42g/min carry out laser melting coating.Laser is molten The impact-resistant abrasion-proof alloy-layer that 1.6mm thickness is obtained after covering obtains after laser melting coating since alloy-layer contains a large amount of alloying component A large amount of hard particles have good wearability, simultaneously because chromium content is relatively high, the comparision contents of retained austenite are big, residual Residue stress is also relatively high, needs to be heat-treated after carrying out cladding, and heat treatment temperature is 510 DEG C.It is fast that heat treatment can eliminate laser preparation The stress generated during rapid hardening is solid, while can promote metastable state tissue to stable structural transformation, improve the shock resistance of tissue The structural state of performance, the alloy-layer of acquisition is as shown in Fig. 2.
The laser cladding layer of acquisition is detected, hardness is HRC63.3~65.2, and uniformity of hardness is good, is fluctuated small. The cladding layer carries out its dry friction coefficient of friction-wear test 0.40, and weightlessness is the 6% of Cr12MoV on year-on-year basis, and wearability reaches It greatly improves.
The laser cladding layer of acquisition is detected, hardness is HRC65.4~66.6, and uniformity of hardness is good, is fluctuated small. The cladding layer carries out its dry friction coefficient of friction-wear test 0.45, and weightlessness is the 11% of Cr12MoV on year-on-year basis, and wearability obtains To greatly improving.Carry out nonstandard non-notch impact test to cladding layer, compared with Cr12MoV, impact flexibility and its 9.2% is reduced compared to toughness, significantly lower but wearability does not occur and is significantly increased for toughness.

Claims (3)

1. a kind of impact-resistant abrasion-proof material for laser manufacture, which is characterized in that be grouped as by following mass percent group: C: 2.9-3.8%, Cr:15-23%, Si:1.00-1.30%, Ni:0.2-0.95%, Mn:0.9-1.5%, W:2-5.5%: V:14-21%, B:0.8-1.8%, Nb:5.50-10%, Y:0.8-2.3%, surplus are Fe and inevitable impurity.
2. a kind of impact-resistant abrasion-proof material for laser manufacture, which is characterized in that be grouped as by following mass percent group: C: 3.0%, Cr:19%, Si:1.00%, Ni:0.55%, Mn:1.3%, W:2.4%: V:16.2%, B:1.0%, Nb:8%, Y:0.9%, it is remaining Amount is Fe and inevitable impurity.
3. a kind of impact-resistant abrasion-proof material for laser manufacture, which is characterized in that be grouped as by following mass percent group: C: 3.4%, Cr:17%, Si:1.20%, Ni:0.8%, Mn:0.95%, W:3.5%: V:19%, B:1.3%, Nb:8.20%, Y:0.9%, it is remaining Amount is Fe and inevitable impurity.
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113564586A (en) * 2021-08-18 2021-10-29 沈阳大陆激光工程技术有限公司 Wear-resistant material for compositely manufacturing rolling mill centering guide plate in laser cladding mode and preparation method
CN114653952A (en) * 2020-12-23 2022-06-24 鑫精合激光科技发展(北京)有限公司 Hook manufacturing method
CN115233220A (en) * 2022-08-04 2022-10-25 沈阳大陆激光先进制造技术创新有限公司 Wear-resistant material for laser cladding carbon and boron common reinforcement

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080253919A1 (en) * 2005-04-29 2008-10-16 Koppern Entwicklungs Gmbh & Co. Kg Powder-Metallurgically Produced, Wear-Resistant Material
CN103194685A (en) * 2013-04-02 2013-07-10 安泰科技股份有限公司 Ceramimetallurgical high-wear-resistance high-toughness cold work die steel and preparation method thereof
US20140076260A1 (en) * 2012-09-15 2014-03-20 L. E. Jones Company Corrosion and wear resistant iron based alloy useful for internal combustion engine valve seat inserts and method of making and use thereof
CN104357748A (en) * 2014-10-31 2015-02-18 广东电网有限责任公司电力科学研究院 Iron-based nanocrystalline composite coating for protecting boiler tail heating surface and laser-cladding forming process of iron-based nanocrystalline composite coating

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080253919A1 (en) * 2005-04-29 2008-10-16 Koppern Entwicklungs Gmbh & Co. Kg Powder-Metallurgically Produced, Wear-Resistant Material
US20140076260A1 (en) * 2012-09-15 2014-03-20 L. E. Jones Company Corrosion and wear resistant iron based alloy useful for internal combustion engine valve seat inserts and method of making and use thereof
CN103194685A (en) * 2013-04-02 2013-07-10 安泰科技股份有限公司 Ceramimetallurgical high-wear-resistance high-toughness cold work die steel and preparation method thereof
CN104357748A (en) * 2014-10-31 2015-02-18 广东电网有限责任公司电力科学研究院 Iron-based nanocrystalline composite coating for protecting boiler tail heating surface and laser-cladding forming process of iron-based nanocrystalline composite coating

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114653952A (en) * 2020-12-23 2022-06-24 鑫精合激光科技发展(北京)有限公司 Hook manufacturing method
CN113564586A (en) * 2021-08-18 2021-10-29 沈阳大陆激光工程技术有限公司 Wear-resistant material for compositely manufacturing rolling mill centering guide plate in laser cladding mode and preparation method
CN115233220A (en) * 2022-08-04 2022-10-25 沈阳大陆激光先进制造技术创新有限公司 Wear-resistant material for laser cladding carbon and boron common reinforcement

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